US20030118798A1 - Copper interconnection and the method for fabricating the same - Google Patents
Copper interconnection and the method for fabricating the same Download PDFInfo
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- US20030118798A1 US20030118798A1 US10/329,219 US32921902A US2003118798A1 US 20030118798 A1 US20030118798 A1 US 20030118798A1 US 32921902 A US32921902 A US 32921902A US 2003118798 A1 US2003118798 A1 US 2003118798A1
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- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
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Definitions
- the present invention relates to a copper interconnection structure and its fabrication method and, more particularly, to a copper interconnection structure of a increasing Cu interconnection lifetime, and its fabrication method.
- FIGS. 1A to 1 D are sectional views of a copper interconnection illustrating a conventional copper interconnection fabrication process.
- the conventional copper interconnection structure is provided with a barrier metal (Ta) layer 12 made of mainly high melting point metal such as Ta on an insulating layer 11 , a thin seed Cu layer 14 fabricated by sputtering a Cu interconnection layer 16 a fabricated using a method such as electro plating to thickly deposit Cu, and an SiN layer 17 fabricated by using sputtering to deposit SiN or the like.
- a barrier metal (Ta) layer 12 made of mainly high melting point metal such as Ta on an insulating layer 11
- a thin seed Cu layer 14 fabricated by sputtering a Cu interconnection layer 16 a fabricated using a method such as electro plating to thickly deposit Cu
- SiN layer 17 fabricated by using sputtering to deposit SiN or the like.
- a Cu interconnection groove 10 is fabricated on the insulating layer 11 , then the barrier metal (Ta) layer 12 mainly made of high melting point metal such as Ta is fabricated thin by sputtering and, further as shown in FIG. 1B, seed Cu is thinly sputtered to fabricate the seed Cu layer 14 .
- Cu is thickly deposited by a method such as electro-plating to fabricate the Cu layer 16 . This is subjected to heat treatment at about 400° C. for 10 min. to several hours according to an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. Subsequently, as shown in FIG.
- the layer is made flat by the chemical mechanical polishing (CMP) method or the like to fabricate an interconnection 16 a .
- CMP chemical mechanical polishing
- a surface of the interconnection 16 a is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 1D, an insulating film, such as SiN or the like, is deposited by sputtering to fabricate the SiN layer 17 .
- Objects of the present invention are to provide a copper interconnection structure which eliminates the foregoing drawbacks of the conventional art, and solves the technical problems to increase an interconnection lifetime, and its fabrication method.
- a constitution of a copper interconnection structure of the present invention is characterized in that in the vicinity of an interface between Cu and barrier metal or between Cu and a cap layer, in order to selectively reduce holes existed in an interface between Cu or a Cu alloy layer and a barrier metal layer, hole reduction impurities added to Cu form a solid solution, the hole reduction impurities are precipitated, amorphous Cu is provided or a compound with Cu is formed, whereby holes in the vicinity of the interface are reduced, contribution of interface diffusion to Cu EM is reduced, a lifetime is increased, and simultaneously adhesiveness and resistance to stress migration are increased.
- a constitution of a copper interconnection fabrication method of the present invention is characterized in that after sputtering of barrier metal on an interconnection groove, in order to reduce holes existed in an interface between Cu or a Cu alloy layer and a barrier metal layer, hole reduction impurities added to Cu are ion-implanted in the barrier metal, heat treatment is executed, seed Cu is sputtered, and then Cu which makes an interconnection is deposited thereon, the hole reduction impurities form a solid solution in the vicinity of the interface between Cu and the barrier metal, the hole reduction impurities are precipitated, and amorphous Cu is provided or a compound with Cu is formed.
- a constitution of another copper interconnection fabrication method of the present invention is characterized in that Cu or a Cu alloy is embedded in an interconnection groove fabricated in an interconnection surface, an interconnection is fabricated by using the CMP method or the like, then impurities are ion-implanted in order to reduce holes existed in an interface between Cu or a Cu alloy layer and a barrier metal layer, heat treatment is executed, a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer, and then a cap layer is fabricated by sputtering to make Cu amorphous in the vicinity of an interface with the cap layer.
- the impurities in place of ion-implantation of the hole reduction impurities added to the Cu executed to selectively reduce the holes existed in the interface between the Cu or the Cu alloy layer and the barrier metal layer, and the heat treatment, the impurities can be diffused from thin layer by heat treatment in place of ion-implantation, and then diffused by heat.
- the step of executing the treatment such as cleaning and/or plasma irradiation on the surface of the interconnection to remove the Cu natural oxide layer can be executed after the fabrication of the interconnection, and then the hole reduction impurities can be ion-implanted.
- the step of executing the treatment such as cleaning and/or plasma irradiation on the surface of the interconnection to remove the Cu natural oxide layer can be executed after the fabrication of the interconnection, and then the hole reduction impurities can be deposited by a very thin layer, and the hole reduction impurities can be one of Nb, Ta, Si, Ru and V.
- FIGS. 1A to 1 D are sectional views of a copper interconnection illustrating a conventional copper interconnection fabrication process.
- FIGS. 2A to 2 E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a first embodiment of the present invention.
- FIGS. 3A to 3 E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a second embodiment of the present invention.
- FIGS. 4A to 4 E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a third embodiment of the present invention.
- FIGS. 5A to 5 F are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a fourth embodiment of the present invention.
- FIGS. 6A to 6 F are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a fifth embodiment of the present invention.
- FIGS. 7A to 7 E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a sixth embodiment of the present invention.
- FIGS. 8A to 8 E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a seventh embodiment of the present invention.
- FIGS. 9A to 9 E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to an eight embodiment of the present invention.
- FIGS. 2A to 2 E are sectional views showing a process of a fabrication method according to a first embodiment of the present invention.
- a barrier metal (Ta) layer 12 mainly made of high melting point metal such as Ta is fabricated thereon by sputtering.
- impurities 13 a such as Nb are injected by injection energy of 2 keV to 5 keV, and a dose amount of 1.0E14 cm ⁇ 2 , and subjected to annealing at about 900° C. for several min. Accordingly, the impurity Nb becomes a solid solution on the surface to fabricate an impurity part (Nb) 15 .
- seed Cu is thinly sputtered to fabricate a seed Cu layer 14 , and Cu is thickly deposited subsequently by a method such as electro-plating to fabricate a Cu layer 16 .
- the Cu layer 16 is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove.
- CMP method or the like the layer is made flat to fabricate an interconnection 16 a as shown in FIG. 2D.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 2E, SiN or the like is sputtered to fabricate an insulating layer 17 .
- an interconnection structure can be obtained, where an impurity Si in place of the impurity Nb 13 is precipitated in the vicinity of the interface between the seed Cu layer 14 and the Ta barrier metal layer 12 of the interconnection layer.
- a barrier metal (Ta) layer 12 is fabricated by sputtering as shown in FIG. 2A.
- impurities such as Si are injected by injection energy of 5 keV to 10 keV, and a dose amount of 2.0E14 cm ⁇ 2 to 5.0E14 cm ⁇ 2 , and subjected to annealing at about 850° C. for several min. Accordingly, the impurity Si is precipitated on a very surface of Ta to fabricate an impurity (Si) part 15 a.
- the process thereafter is similar to the fabrication process of the interconnection structure where the impurity Nb 13 becomes a solid solution in the vicinity of the interface between the seed Cu layer 14 and the Ta barrier metal layer 12 of the interconnection layer, that is, the steps from FIGS. 2C to 2 E are sequentially executed.
- the interconnection groove 10 is fabricated on the insulating layer 11 .
- the interconnection groove 10 can be fabricated on a semiconductor layer, another interconnection layer and/or a combination thereof.
- FIGS. 3A to 3 E are sectional views showing a process of a fabrication method according to a second embodiment of the present invention.
- a barrier metal (Ta) layer 12 mainly made of high melting point metal such as Ta, and a seed Cu layer 14 made of seed Cu are fabricated thin by sputtering.
- impurities 13 a such as Ta are injected by injection energy of 5.0 keV, and a dose amount of 1.0E15 cm ⁇ 2 , and subjected to annealing at about 900° C.
- Cu becomes amorphous in the vicinity of an interface between the seed Cu and the barrier Ta to from an amorphous Cu layer 14 a .
- Cu is thickly deposited by a method such as electro-plating to fabricate a Cu layer 16 .
- the Cu layer 16 is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the interconnection groove.
- an interconnection 16 a is fabricated as shown in FIG. 3D.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 3E, SiN or the like is sputtered to fabricate an insulating layer 17 .
- an interconnection structure is obtained, where there is an amorphous Cu layer 14 a in an interface between the seed Cu layer 14 and the Ta layer 12 .
- FIGS. 4A to 4 E are sectional views showing a process of a fabrication method according to a third embodiment of the present invention.
- a barrier metal layer 12 mainly made of high melting point metal such as Ta, and a seed Cu layer 14 made of seed Cu are fabricated thin by sputtering.
- a solid phase Si layer 18 containing impurities such as Si is fabricated by several nm, and subjected to annealing at about 900° C.
- Cu—Si compound layer 18 a in an interface between the seed Cu layer 14 and the Ta layer 12 .
- Cu is thickly deposited by a method such as electro-plating to fabricate a Cu layer 16 .
- the Cu layer 16 is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove 10 .
- an interconnection 18 a is fabricated as shown in FIG. 4D.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 4E, SiN or the like is deposited by sputtering to fabricate an insulating layer 17 .
- SiN or the like is deposited by sputtering to fabricate an insulating layer 17 .
- an interconnection structure is obtained, where there is a Cu—Si compound layer. 18 a in an interface between the seed Cu layer 14 and the barrier metal Ta layer 12 .
- FIGS. 5A to 5 F are sectional views showing a process of a fabrication method according to a fourth embodiment of the present invention.
- a barrier metal layer 12 mainly made of high melting point metal such as Ta, and a seed Cu layer 14 made of seed Cu are fabricated thin by sputtering.
- Cu is thickly deposited by a method such as electro-plating to fabricate a Cu layer 16 .
- This layer is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove.
- an interconnection 16 a is fabricated as shown in FIG. 5B.
- a CuOx natural oxide film 20 is shown on the Cu layer 16 .
- impurities 21 such as V are injected by injection energy of 2 keV to 5 keV, and a dose amount of 1.0E14 cm ⁇ 2 , and subjected to annealing at about 900° C. for several min.
- the impurity V becomes a solid solution in the vicinity of an interface CuOx 20 and the interconnection Cu of the surface.
- FIG. 5C impurities 21 such as V are injected by injection energy of 2 keV to 5 keV, and a dose amount of 1.0E14 cm ⁇ 2 , and subjected to annealing at about 900° C. for several min.
- the impurity V becomes a solid solution in the vicinity of an interface CuOx 20 and the interconnection Cu of the surface.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove the Cu natural oxide layer 20 and, then, as shown in FIG. 5F, SiN or the like is deposited by sputtering.
- an interconnection structure is obtained, where an impurity V layer 21 a becomes a solid solution in an interface between a cap SiN 17 and the Cu layer 16 .
- FIGS. 6A to 6 F are sectional views showing a process of a fabrication method according to a fifth embodiment of the present invention.
- a barrier metal layer 12 mainly made of high melting point metal such as Ta, and a seed Cu layer 14 are fabricated thin by sputtering.
- Cu is thickly deposited by a method such as electro-plating to fabricate a Cu layer 16 .
- This layer is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove.
- a CuOx natural oxide film 20 is shown on the Cu layer 16 .
- CMP method or the like is used to fabricate an interconnection, and a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove the Cu natural oxide layer 20 as shown in FIG. 6C.
- impurities such as Si are injected by injection energy of 5 keV to 10 keV, and a dose amount of 1.0E15 cm ⁇ 2 , and subjected to annealing at about 900° C. for several min.
- An amorphous Cu layer is fabricated in the vicinity of the surface of the Cu layer.
- SiN or the like is deposited by sputtering.
- an interconnection structure is obtained, where there is an amorphous Cu layer 23 in an interface between a cap SiN 17 .and the Cu layer 16 .
- FIGS. 7A to 7 E are sectional views showing a fabrication process of a copper interconnection according to a sixth embodiment of the present invention.
- a barrier metal layer 12 mainly made of high melting point metal such as Ta is sputtered.
- impurities such as Nb 13 are injected by injection energy of 2 keV to 5 keV, and a dose amount of 1.0E14 cm ⁇ 2 , and subjected to annealing at about 350° C. for several min.
- the impurity Nb becomes a solid solution on a very surface of the Ta layer 12 .
- a seed Cu layer 14 is thinly sputtered, and then a Cu layer 16 is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 250 to 350° C. for 5 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove.
- an interconnection 16 a is fabricated as shown in FIG. 7C.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an SiC layer 17 or the like is fabricated by sputtering.
- an interconnection structure is obtained, where an impurity Nb 15 becomes a solid solution in an interface between the seed Cu layer 14 and the Ta layer 12 , and this interconnection is set as a lower layer interconnection.
- a via hole 71 is fabricated by a normal etching method, and treated such as ashing and/or cleaning.
- a via hole 71 as in the case of the interconnection groove, sputtering of a barrier metal layer 12 a of Ta or the like, injection of impurities 15 a such as Nb and annealing, and sputtering of a seed Cu layer 14 b , and electro-plating and annealing of a Cu layer 16 a are executed.
- CMP is executed to fabricate a via hole constituted of the barrier metal layer 12 a of Ta or the like, the seed Cu layer 14 b , the impurities 15 a such as Nb, and the Cu layer 16 .
- FIG. 7D an interlayer insulating film 11 a is fabricated, and an upper layer interconnection is fabricated by a method similar to that of the lower layer interconnection and, accordingly as shown in FIG. 7E, a multilayer interconnection of a single damascene structure is fabricated.
- the embodiment shows the structure where the impurity becomes a solid solution in the interface between the seed Cu layer and the Ta layer in all of the lower layer interconnection, the via hole, and the upper layer interconnection.
- a structure can also be fabricated, where the invention is applied to one of the lower layer interconnection, the via hole and the upper layer interconnection.
- the number of interconnection layers is not limited to two, and the invention can be applied to a case of much more layers.
- the embodiment shows the case of the via hole made of Cu. However, other materials such as W may be used.
- FIG. 8A to 8 E are sectional views showing a copper interconnection fabrication process according to a seventh embodiment of the present invention.
- a barrier metal layer 12 mainly made of high melting point metal such as Ta, and a seed Cu layer 14 are thinly sputtered.
- impurities such as Ta are injected by injection energy of 5 keV, and a dose amount of 1.0E15 cm ⁇ 2 , and subjected to annealing at about 400° C. for several min.
- Cu in the vicinity of an interface between the seed layer Cu 14 and the Ta barrier metal layer 12 become amorphous.
- a Cu layer 16 a is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 380° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. Subsequently, by using CMP method or the like, an interconnection is fabricated.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an SiC layer 17 or the like is fabricated by sputtering.
- an interconnection structure is obtained, where there is an amorphous Cu layer 14 a in the interface between the seed Cu layer and the Ta layer, and this interconnection is set as a lower layer interconnection.
- a low dielectric constant film 11 a as an interlayer insulating film of a via hole part 81 , and an SiCN layer 17 a or the like are fabricated.
- a low dielectric constant film as an interlayer insulating film of an upper layer interconnection, and an SiO 2 film 11 b are fabricated.
- an anti-reflection compound (ARC) film, a photoresist and an etching mask are fabricated and, by using gas containing fluorocarbon or the like, the via hole 81 is opened by etching.
- FIG. 8D After treatment such as (wet) cleaning of the opening, a film prevented from a reflection, a photoresist, and an etching mask are deposited to fabricate an upper layer interconnection groove 82 . As shown in FIG. 8D, after treatment such as (wet) cleaning of the opening, a film prevented from a reflection, a photoresist, and an etching mask are deposited to fabricate an upper layer interconnection groove 82 . As shown in FIG.
- a Cu layer 16 d is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 350° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove.
- an interconnection is fabricated.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an SiN layer 17 or the like is fabricated by sputtering.
- a laminated structure can be fabricated, where there is an amorphous Cu layer 14 f in an interface between the seed Cu layer and the Ta layer, and this interconnection is set as a lower layer interconnection.
- the embodiment shows the structure where the amorphous Cu layer 14 f is present in the interface between the seed Cu layer and the Ta layer in both of the lower layer interconnection/the via hole and the upper layer interconnection.
- a structure can also be fabricated, where the invention is applied to one of the lower layer interconnection/the via hole and the upper layer interconnection.
- the number of interconnection layers is not limited to two, and the invention can be applied to a case of much more layers.
- FIGS. 9A to 9 E are sectional views showing a copper interconnection fabrication process according to an eighth embodiment of the present invention.
- a barrier metal layer 12 mainly made of high melting point metal such as Ta, and a seed Cu layer 14 are thinly sputtered.
- a solid phase containing impurities such as Si ( 18 ) are deposited, and subjected to annealing at about 400° C. for several min., to fabricate a Cu—Si compound 18 a in an interface between the seed layer Cu 14 and the Ta barrier metal layer 12 as shown in FIG. 9B.
- a Cu layer 16 a is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 350 to 400° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove.
- an interconnection is fabricated.
- a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an SiN layer 17 or the like is fabricated by sputtering.
- an interconnection structure is obtained, where there is a Cu—Si compound 18 a in the interface between the seed Cu layer and the Ta layer, and this interconnection is set as a lower layer interconnection.
- a low dielectric constant film 11 c as an interlayer insulating film of a via hole part, and an SiCN layer 17 d or the like are fabricated.
- a low dielectric constant film as an interlayer insulating film of an upper layer interconnection, and an SiO 2 film 11 d are fabricated.
- a reflection prevention film, a photoresist and an etching mask are fabricated and, by using gas containing fluorocarbon or the like, an upper layer interconnection groove 91 is opened by etching.
- a reflection prevention film for via hole opening, a photoresist, and an etching mask are fabricated, and etched to fabricate a via hole 92 .
- a barrier metal layer 12 d mainly made of high melting point metal such as Ta, and a seed Cu layer 14 g are executed, impurities such as Ta 12 d are injected (injection energy of 5 keV, and a dose amount of 1.0E15 cm ⁇ 2 ), and subjected to annealing, and Cu 18 b , 18 c in the vicinity of an interface between the seed Cu layer and the Ta barrier layer becomes amorphous.
- a Cu layer 16 e is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 380° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. Subsequently, by using CMP method or the like, an interconnection is fabricated. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an SiN layer 17 f or the like is fabricated by sputtering. Thus, an interconnection structure can be fabricated, where there is a seed Cu layer 14 g in an interface between the seed Cu layer and the Ta layer, and this interconnection is set as an upper layer interconnection.
- the embodiment shows the interconnection structure where the amorphous Cu layer is present in the interface between the seed Cu layer and the Ta layer in the lower layer interconnection, and the Cu—Si compound is present, in the interface between the seed Cu layer and the Ta layer in the via hole and the upper layer interconnection.
- application can be made to various combinations, e.g., a case where structures are similar between the lower layer interconnection/the via hole and the upper layer interconnection, a case where in one of the structures, one of the copper interconnection fabrication methods of the first to fifth embodiments of the invention is employed, and other cases.
- the number of interconnection layers is not limited to two, and the invention can be applied to a case of much more layers.
- impurities to be added to Cu many are possible.
- Nb or Ta which fully fabricates a solid solution with Cu is suitable.
- a Cu—Nb compound is continuously present in an interface between Cu and Nb to greatly reduce holes.
- this example is also advantageous in that there no resistance increases by impurities.
- V belonging to the same group as Nb may also be suitable.
- a Cu—Si compound has been considered to contribute to an EM improvement.
- a method of implanting Si ions by good controllability, or the like is also preferable.
- Ru which causes an oxide to exhibit good conductivity is also preferable from the standpoint of removing CuOx from the interface and maintaining conductivity as RuOx.
- ion implantation conditions of impurities may be conditions for making the vicinity of a very surface of Cu amorphous.
- An advantage accompanying the amorphous vicinity of the Cu interface is an improvement in physical properties such as adhesiveness and mechanical strength made by elimination of stress imbalance or local concentration to a passivation film such as a cap layer caused by a difference in growth rate according to criystal orientation during Cu crystal growth which occurs even at a room temperature.
- the Cu amorphous treatment executed before the above-described CuSix treatment provides many effects such as uniform generation of CuSix.
- the present invention is effective in that when an interconnection width is narrower than an average Cu grain size, and a grain boundary becomes a bamboo structure, a bamboo effect for increasing a lifetime appears, and thus a lifetime is increased by about two digits compared with the Al interconnection.
- a reason is that if there are impurities deposited in a gap in the vicinity of the interface between Cu and barrier metal (or cap), or if there is amorphous Cu in the interface between Cu and barrier metal (or cap), the number of holes, many being present in the interface between normal different materials, is reduced, and thus interface diffusion occurring through the holes can be suppressed. Accordingly, as Cu diffusion path by the EM, interface contribution is reduced, whereby a main Cu diffusion mechanism becomes lattice diffusion.
- the impurities are not only precipitated in the interface, but may fabricate a compound in the interface.
- a compound in the interface For example, it is known that Ta, Nb or the like fully fabricates a solid solution with Cu. Presence of such a compound may reduce holes in the interface to increase an EM lifetime.
- silicide treatment of the Cu surface increases an EM lifetime, and its combination with the present invention can expectedly increase the lifetime more.
- Use in the multilayer interconnection provides large resistance to stress migration caused by heat treatment executed for fabrication of each layer.
- selection of a material of a melting point higher than that of Cu for a via hole enables fabrication of an interconnection structure of high interconnection reliability.
- via adhesiveness can be enhanced, contribution can be made to a reduction in an initial failure rate, and Cu aggregation in the via which is one of failure modes can be suppressed.
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Abstract
A copper interconnection where holes in the vicinity of an interface are reduced to lower contribution of interface diffusion to Cu the EM, increase a lifetime, and simultaneously increase adhesiveness and resistance to stress migration is constituted in a manner that impurities 15 form a solid solution in the vicinity of an interface between a Cu layer 16 and a barrier metal layer 12, the impurities are precipitated, and an amorphous Cu layer 14 is fabricated, or a compound with Cu is fabricated. The copper interconnection is also constituted in a manner that impurities 15 form a solid solution in the vicinity of an interface between the Cu layer 16 and a cap layer 19, the impurities 15 are precipitated, and an amorphous Cu layer 14 is fabricated, or a compound with Cu is fabricated.
Description
- 1. Field of the Invention
- The present invention relates to a copper interconnection structure and its fabrication method and, more particularly, to a copper interconnection structure of a increasing Cu interconnection lifetime, and its fabrication method.
- 2. Description of the Prior Art
- It is well known that in recent years efforts have been made to achieve high performance and functionality of a semiconductor integrated circuit used for an information electronic equipment such as a cell phone. Such a semiconductor integrated circuit has many circuit elements, for example transistors. It is also a well-known fact that such a semiconductor integrated circuit is fabricated by using a high-precision semiconductor fabrication process. Further, in the high-precision semiconductor fabrication process, an interconnection structure of an increased interconnection lifetime, especially a copper interconnection structure attracts attention.
- FIGS. 1A to 1D are sectional views of a copper interconnection illustrating a conventional copper interconnection fabrication process. Referring to FIGS. 1A to 1D, the conventional copper interconnection structure is provided with a barrier metal (Ta)
layer 12 made of mainly high melting point metal such as Ta on aninsulating layer 11, a thinseed Cu layer 14 fabricated by sputtering aCu interconnection layer 16 a fabricated using a method such as electro plating to thickly deposit Cu, and anSiN layer 17 fabricated by using sputtering to deposit SiN or the like. - Next, a conventional copper interconnection fabrication method will be described by referring to the sectional views of FIGS. 1A to 1D again.
- First, according to the conventional copper interconnection fabrication process, as shown in FIG. 1A, a
Cu interconnection groove 10 is fabricated on theinsulating layer 11, then the barrier metal (Ta)layer 12 mainly made of high melting point metal such as Ta is fabricated thin by sputtering and, further as shown in FIG. 1B, seed Cu is thinly sputtered to fabricate theseed Cu layer 14. Subsequently, Cu is thickly deposited by a method such as electro-plating to fabricate theCu layer 16. This is subjected to heat treatment at about 400° C. for 10 min. to several hours according to an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. Subsequently, as shown in FIG. 1C, the layer is made flat by the chemical mechanical polishing (CMP) method or the like to fabricate aninterconnection 16 a. A surface of theinterconnection 16 a is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 1D, an insulating film, such as SiN or the like, is deposited by sputtering to fabricate theSiN layer 17. - As an example of an electromigration (EM) suppression in an Al interconnection, there is an example of adding a small amount of impurities such as Cu to Al as described in Japanese Patent Application Laid-Open No. Hei 08 (1996)-107110 (paragraphs 0015 to 0020, FIG. 1).
- Such impurities are added because as described in “Al—Ti and Al—Ti—Si thin alloy films”, Albertus G. Dirks, Tien Tien, and Janet M. Towner, pp. 2010, “Journal of Applied Physics”, vol. 59-6 (1968), impurities are precipitated on a grain boundary to lower a hole density, whereby contribution of grain boundary diffusion is reduced. In the Cu interconnection, an EM main diffusion path is considered to be an interface between Cu and other materials. Accordingly, interface holes must be selectively removed.
- However, in such a copper interconnection fabrication method, there are problems that an EM resistance of the copper interconnection is low, and particularly, in a case of the copper interconnection width is narrow, the copper interconnection has shorter lifetime than the Al interconnection. A reason is that in the case of the Al interconnection, if an interconnection width is smaller than an average Al grain size, and a gain boundary becomes a bamboo structure, Al lattice diffusion becomes a main diffusion mechanism. This lattice diffusion is much slower than either grain boundary or interface diffusion. Thus, in the case of the narrow interconnection where grain boundary diffusion is dominant which achieves a bamboo grain boundary structure, an EM lifetime is longer than a wide interconnection.
- On the other hand, in the case of the Cu interconnection, even if an interconnection width is smaller than an average Cu grain size, and a grain boundary becomes a bamboo structure, not Cu lattice diffusion but interface diffusion becomes a main diffusion mechanism. Thus, an increase in the EM lifetime observed in the case of the thin Al interconnection is not seen in the case of the Cu interconnection. As a result, in the case of an interconnection width is small, the Cu interconnection has shorter lifetime than the Al interconnection.
- Objects of the present invention are to provide a copper interconnection structure which eliminates the foregoing drawbacks of the conventional art, and solves the technical problems to increase an interconnection lifetime, and its fabrication method.
- A constitution of a copper interconnection structure of the present invention is characterized in that in the vicinity of an interface between Cu and barrier metal or between Cu and a cap layer, in order to selectively reduce holes existed in an interface between Cu or a Cu alloy layer and a barrier metal layer, hole reduction impurities added to Cu form a solid solution, the hole reduction impurities are precipitated, amorphous Cu is provided or a compound with Cu is formed, whereby holes in the vicinity of the interface are reduced, contribution of interface diffusion to Cu EM is reduced, a lifetime is increased, and simultaneously adhesiveness and resistance to stress migration are increased.
- A constitution of a copper interconnection fabrication method of the present invention is characterized in that after sputtering of barrier metal on an interconnection groove, in order to reduce holes existed in an interface between Cu or a Cu alloy layer and a barrier metal layer, hole reduction impurities added to Cu are ion-implanted in the barrier metal, heat treatment is executed, seed Cu is sputtered, and then Cu which makes an interconnection is deposited thereon, the hole reduction impurities form a solid solution in the vicinity of the interface between Cu and the barrier metal, the hole reduction impurities are precipitated, and amorphous Cu is provided or a compound with Cu is formed.
- Further, a constitution of another copper interconnection fabrication method of the present invention is characterized in that Cu or a Cu alloy is embedded in an interconnection groove fabricated in an interconnection surface, an interconnection is fabricated by using the CMP method or the like, then impurities are ion-implanted in order to reduce holes existed in an interface between Cu or a Cu alloy layer and a barrier metal layer, heat treatment is executed, a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer, and then a cap layer is fabricated by sputtering to make Cu amorphous in the vicinity of an interface with the cap layer.
- Furthermore, according to the present invention, in place of ion-implantation of the hole reduction impurities added to the Cu executed to selectively reduce the holes existed in the interface between the Cu or the Cu alloy layer and the barrier metal layer, and the heat treatment, the impurities can be diffused from thin layer by heat treatment in place of ion-implantation, and then diffused by heat. The step of executing the treatment such as cleaning and/or plasma irradiation on the surface of the interconnection to remove the Cu natural oxide layer can be executed after the fabrication of the interconnection, and then the hole reduction impurities can be ion-implanted. Further, the step of executing the treatment such as cleaning and/or plasma irradiation on the surface of the interconnection to remove the Cu natural oxide layer can be executed after the fabrication of the interconnection, and then the hole reduction impurities can be deposited by a very thin layer, and the hole reduction impurities can be one of Nb, Ta, Si, Ru and V.
- FIGS. 1A to 1D are sectional views of a copper interconnection illustrating a conventional copper interconnection fabrication process.
- FIGS. 2A to 2E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a first embodiment of the present invention.
- FIGS. 3A to 3E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a second embodiment of the present invention.
- FIGS. 4A to 4E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a third embodiment of the present invention.
- FIGS. 5A to 5F are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a fourth embodiment of the present invention.
- FIGS. 6A to 6F are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a fifth embodiment of the present invention.
- FIGS. 7A to 7E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a sixth embodiment of the present invention.
- FIGS. 8A to 8E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to a seventh embodiment of the present invention.
- FIGS. 9A to 9E are sectional views of a copper interconnection illustrating a copper interconnection fabrication process according to an eight embodiment of the present invention.
- Next, detailed description will be made of a copper interconnection structure and its fabrication method according to several embodiments of the present invention with reference to the accompanying drawings.
- FIGS. 2A to 2E are sectional views showing a process of a fabrication method according to a first embodiment of the present invention. First, in the fabrication method of the first embodiment of the invention, as shown in FIG. 2A, after a
Cu interconnection groove 10 is fabricated on an insulatinglayer 11, a barrier metal (Ta)layer 12 mainly made of high melting point metal such as Ta is fabricated thereon by sputtering. Subsequently, as shown in FIG. 2B,impurities 13 a such as Nb are injected by injection energy of 2 keV to 5 keV, and a dose amount of 1.0E14 cm−2, and subjected to annealing at about 900° C. for several min. Accordingly, the impurity Nb becomes a solid solution on the surface to fabricate an impurity part (Nb) 15. - Then, as shown in FIG. 2C, seed Cu is thinly sputtered to fabricate a
seed Cu layer 14, and Cu is thickly deposited subsequently by a method such as electro-plating to fabricate aCu layer 16. TheCu layer 16 is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. Subsequently, by using CMP method or the like, the layer is made flat to fabricate aninterconnection 16 a as shown in FIG. 2D. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 2E, SiN or the like is sputtered to fabricate an insulatinglayer 17. - Thus, an interconnection structure is obtained, where the
impurity Nb 13 becomes a solid solution in the vicinity of an interface between theseed Cu layer 14 and the Tabarrier metal layer 12 of the interconnection layer. - On the other hand, an interconnection structure can be obtained, where an impurity Si in place of the
impurity Nb 13 is precipitated in the vicinity of the interface between theseed Cu layer 14 and the Tabarrier metal layer 12 of the interconnection layer. First, as in the case of the fabrication process of the interconnection structure where theimpurity Nb 13 becomes a solid solution in the vicinity of the interface between theseed Cu layer 14 and the Tabarrier metal layer 12 of the interconnection layer, a barrier metal (Ta)layer 12 is fabricated by sputtering as shown in FIG. 2A. - Subsequently, as shown in FIG. 2B, impurities such as Si are injected by injection energy of 5 keV to 10 keV, and a dose amount of 2.0E14 cm −2 to 5.0E14 cm−2, and subjected to annealing at about 850° C. for several min. Accordingly, the impurity Si is precipitated on a very surface of Ta to fabricate an impurity (Si)
part 15 a. - The process thereafter is similar to the fabrication process of the interconnection structure where the
impurity Nb 13 becomes a solid solution in the vicinity of the interface between theseed Cu layer 14 and the Tabarrier metal layer 12 of the interconnection layer, that is, the steps from FIGS. 2C to 2E are sequentially executed. - The embodiment has been described by way of example where the
interconnection groove 10 is fabricated on the insulatinglayer 11. Apparently, however, theinterconnection groove 10 can be fabricated on a semiconductor layer, another interconnection layer and/or a combination thereof. - FIGS. 3A to 3E are sectional views showing a process of a fabrication method according to a second embodiment of the present invention. First, in the fabrication method of the second embodiment of the invention, as shown in FIG. 3A, after a
Cu interconnection groove 10 is fabricated on an insulatinglayer 11, a barrier metal (Ta)layer 12 mainly made of high melting point metal such as Ta, and aseed Cu layer 14 made of seed Cu are fabricated thin by sputtering. Subsequently, as shown in FIG. 3B,impurities 13 a such as Ta are injected by injection energy of 5.0 keV, and a dose amount of 1.0E15 cm−2, and subjected to annealing at about 900° C. for several min. Accordingly, Cu becomes amorphous in the vicinity of an interface between the seed Cu and the barrier Ta to from anamorphous Cu layer 14 a. Subsequently, as shown in FIG. 3C, Cu is thickly deposited by a method such as electro-plating to fabricate aCu layer 16. TheCu layer 16 is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the interconnection groove. - Subsequently, by using CMP method or the like, an
interconnection 16 a is fabricated as shown in FIG. 3D. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 3E, SiN or the like is sputtered to fabricate an insulatinglayer 17. Thus, an interconnection structure is obtained, where there is anamorphous Cu layer 14 a in an interface between theseed Cu layer 14 and theTa layer 12. - FIGS. 4A to 4E are sectional views showing a process of a fabrication method according to a third embodiment of the present invention. First, in the fabrication method of the third embodiment of the invention, as shown in FIG. 4A, after a
Cu interconnection groove 10 is fabricated on an insulatinglayer 11, abarrier metal layer 12 mainly made of high melting point metal such as Ta, and aseed Cu layer 14 made of seed Cu are fabricated thin by sputtering. Subsequently, as shown in FIG. 4B, a solidphase Si layer 18 containing impurities such as Si is fabricated by several nm, and subjected to annealing at about 900° C. for several min., to fabricate a Cu—Si compound layer 18 a in an interface between theseed Cu layer 14 and theTa layer 12. As shown in FIG. 4C, Cu is thickly deposited by a method such as electro-plating to fabricate aCu layer 16. TheCu layer 16 is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill thegroove 10. - Subsequently, by using CMP method or the like, an
interconnection 18 a is fabricated as shown in FIG. 4D. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, as shown in FIG. 4E, SiN or the like is deposited by sputtering to fabricate an insulatinglayer 17. Thus, an interconnection structure is obtained, where there is a Cu—Si compound layer. 18 a in an interface between theseed Cu layer 14 and the barriermetal Ta layer 12. - FIGS. 5A to 5F are sectional views showing a process of a fabrication method according to a fourth embodiment of the present invention. First, in the fabrication method of the fourth embodiment of the invention, as shown in FIG. 5A, after a
Cu interconnection groove 10 is fabricated on an insulatinglayer 11, abarrier metal layer 12 mainly made of high melting point metal such as Ta, and aseed Cu layer 14 made of seed Cu are fabricated thin by sputtering. Subsequently, Cu is thickly deposited by a method such as electro-plating to fabricate aCu layer 16. This layer is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. - Subsequently, by using CMP method or the like, an
interconnection 16 a is fabricated as shown in FIG. 5B. In the drawing, a CuOxnatural oxide film 20 is shown on theCu layer 16. Here, as shown in FIG. 5C,impurities 21 such as V are injected by injection energy of 2 keV to 5 keV, and a dose amount of 1.0E14 cm−2, and subjected to annealing at about 900° C. for several min. The impurity V becomes a solid solution in the vicinity of aninterface CuOx 20 and the interconnection Cu of the surface. As shown in FIG. 5E, a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove the Cunatural oxide layer 20 and, then, as shown in FIG. 5F, SiN or the like is deposited by sputtering. Thus, an interconnection structure is obtained, where animpurity V layer 21 a becomes a solid solution in an interface between acap SiN 17 and theCu layer 16. - FIGS. 6A to 6F are sectional views showing a process of a fabrication method according to a fifth embodiment of the present invention. First, in the fabrication method of the fifth embodiment of the invention, as shown in FIG. 6A, after a
Cu interconnection groove 10 is fabricated on an insulatinglayer 11, abarrier metal layer 12 mainly made of high melting point metal such as Ta, and aseed Cu layer 14 are fabricated thin by sputtering. Subsequently, Cu is thickly deposited by a method such as electro-plating to fabricate aCu layer 16. This layer is subjected to heat treatment at about 400° C. for about 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. In the drawing, a CuOxnatural oxide film 20 is shown on theCu layer 16. - Subsequently, as shown in FIG. 6B, CMP method or the like is used to fabricate an interconnection, and a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove the Cu
natural oxide layer 20 as shown in FIG. 6C. As shown in FIG. 6D, impurities such as Si are injected by injection energy of 5 keV to 10 keV, and a dose amount of 1.0E15 cm−2, and subjected to annealing at about 900° C. for several min. An amorphous Cu layer is fabricated in the vicinity of the surface of the Cu layer. Subsequently, SiN or the like is deposited by sputtering. Thus, an interconnection structure is obtained, where there is anamorphous Cu layer 23 in an interface between a cap SiN 17.and theCu layer 16. - Next, description will be made of single and dual damascene structures, and a fabrication method thereof when the present invention is applied to the single damascene structure having a multilayer interconnection including at least one of such interconnections, for example the above-described interconnection structure of each layer, or the dual damascene structure having the above-described interconnection structure over two layers, for example a via hole and its upper layer interconnection.
- First, the case where the invention is applied to the single damascene structure is described. FIGS. 7A to 7E are sectional views showing a fabrication process of a copper interconnection according to a sixth embodiment of the present invention.
- According to the fabrication method of the multiplayer interconnection of the sixth embodiment of the invention where the copper interconnection fabrication method of the embodiment is applied to the single damascene structure, as shown in FIG. 7A, after a
Cu interconnection groove 10 is fabricated, abarrier metal layer 12 mainly made of high melting point metal such as Ta is sputtered. Subsequently, impurities such asNb 13 are injected by injection energy of 2 keV to 5 keV, and a dose amount of 1.0E14 cm−2, and subjected to annealing at about 350° C. for several min. - As shown in FIG. 7B, the impurity Nb becomes a solid solution on a very surface of the
Ta layer 12. Aseed Cu layer 14 is thinly sputtered, and then aCu layer 16 is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 250 to 350° C. for 5 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. - Subsequently, by using CMP method or the like, an
interconnection 16 a is fabricated as shown in FIG. 7C. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, anSiC layer 17 or the like is fabricated by sputtering. Thus, an interconnection structure is obtained, where animpurity Nb 15 becomes a solid solution in an interface between theseed Cu layer 14 and theTa layer 12, and this interconnection is set as a lower layer interconnection. - Then, a low dielectric
constant film 11 a as an interlayer insulating film, and anSiCN layer 17 a are fabricated thin. A viahole 71 is fabricated by a normal etching method, and treated such as ashing and/or cleaning. For this viahole 71, as in the case of the interconnection groove, sputtering of abarrier metal layer 12 a of Ta or the like, injection ofimpurities 15 a such as Nb and annealing, and sputtering of aseed Cu layer 14 b, and electro-plating and annealing of aCu layer 16 a are executed. - Subsequently, CMP is executed to fabricate a via hole constituted of the
barrier metal layer 12 a of Ta or the like, theseed Cu layer 14 b, theimpurities 15 a such as Nb, and theCu layer 16. Then, as shown in FIG. 7D, aninterlayer insulating film 11 a is fabricated, and an upper layer interconnection is fabricated by a method similar to that of the lower layer interconnection and, accordingly as shown in FIG. 7E, a multilayer interconnection of a single damascene structure is fabricated. - The embodiment shows the structure where the impurity becomes a solid solution in the interface between the seed Cu layer and the Ta layer in all of the lower layer interconnection, the via hole, and the upper layer interconnection. However, a structure can also be fabricated, where the invention is applied to one of the lower layer interconnection, the via hole and the upper layer interconnection. Moreover, the number of interconnection layers is not limited to two, and the invention can be applied to a case of much more layers. The embodiment shows the case of the via hole made of Cu. However, other materials such as W may be used.
- Next, description is made of a case of applying the copper interconnection fabrication method of the embodiment of the invention to a via first structure in a dual damascene structure. FIG. 8A to 8E are sectional views showing a copper interconnection fabrication process according to a seventh embodiment of the present invention.
- According to the fabrication method of the multiplayer interconnection of the seventh embodiment of the invention where the copper interconnection fabrication method of the embodiment is applied to a via first structure in a dual damascene structure, as shown in FIG. 8A, after a Cu interconnection groove, is fabricated, a
barrier metal layer 12 mainly made of high melting point metal such as Ta, and aseed Cu layer 14 are thinly sputtered. Subsequently, impurities such as Ta are injected by injection energy of 5 keV, and a dose amount of 1.0E15 cm−2, and subjected to annealing at about 400° C. for several min. As shown in FIG. 8B, Cu in the vicinity of an interface between theseed layer Cu 14 and the Tabarrier metal layer 12 become amorphous. - Subsequently, a
Cu layer 16 a is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 380° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. Subsequently, by using CMP method or the like, an interconnection is fabricated. - Further, as shown in FIG. 8C, a surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an
SiC layer 17 or the like is fabricated by sputtering. Thus, an interconnection structure is obtained, where there is anamorphous Cu layer 14 a in the interface between the seed Cu layer and the Ta layer, and this interconnection is set as a lower layer interconnection. - Further, a low dielectric
constant film 11 a as an interlayer insulating film of a viahole part 81, and anSiCN layer 17 a or the like are fabricated. Subsequently, a low dielectric constant film as an interlayer insulating film of an upper layer interconnection, and an SiO2 film 11 b are fabricated. Then, an anti-reflection compound (ARC) film, a photoresist and an etching mask are fabricated and, by using gas containing fluorocarbon or the like, the viahole 81 is opened by etching. - Then, as shown in FIG. 8D, after treatment such as (wet) cleaning of the opening, a film prevented from a reflection, a photoresist, and an etching mask are deposited to fabricate an upper layer interconnection groove 82. As shown in FIG. 8E, after normal treatment such as wet cleaning and/or cleaning, as in the case of the lower layer interconnection, sputtering of a
barrier metal layer 12 c mainly made of high melting point metal such as Ta, and aseed Cu layer 14d are executed, impurities such as Ta 13 c are injected by injection energy of 5 keV, and a dose amount of 1.0E15 cm−2, and subjected to annealing, and Cu in the vicinity of an interface between the seed Cu layer and the Ta barrier layer becomes amorphous. - Subsequently, a
Cu layer 16 d is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 350° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. - Subsequently, by using CMP method or the like, an interconnection is fabricated. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an
SiN layer 17 or the like is fabricated by sputtering. Thus, a laminated structure can be fabricated, where there is an amorphous Cu layer 14 f in an interface between the seed Cu layer and the Ta layer, and this interconnection is set as a lower layer interconnection. - The embodiment shows the structure where the amorphous Cu layer 14 f is present in the interface between the seed Cu layer and the Ta layer in both of the lower layer interconnection/the via hole and the upper layer interconnection. However, a structure can also be fabricated, where the invention is applied to one of the lower layer interconnection/the via hole and the upper layer interconnection. Moreover, the number of interconnection layers is not limited to two, and the invention can be applied to a case of much more layers.
- Next, as a dual damascene fabrication method, in addition to the method for opening the via hole shown in the copper interconnection fabrication method of the seventh embodiment of the invention, and then fabricating the interconnection groove for the upper layer interconnection (via first), an example of a method for first fabricating an interconnection groove, and then a via hole (trench first) will be described as a copper interconnection fabrication method of an eight embodiment of the present invention.
- That is, description is made of a case where the invention is applied to a trench first structure in a dual damascene structure. FIGS. 9A to 9E are sectional views showing a copper interconnection fabrication process according to an eighth embodiment of the present invention.
- According to the fabrication method of the multiplayer interconnection of the eighth embodiment of the invention where the copper interconnection fabrication method of the embodiment is applied to a via first structure in a dual damascene structure, as shown in FIG. 9A, after a Cu interconnection groove is fabricated, a
barrier metal layer 12 mainly made of high melting point metal such as Ta, and aseed Cu layer 14 are thinly sputtered. - Subsequently, a solid phase containing impurities such as Si ( 18) are deposited, and subjected to annealing at about 400° C. for several min., to fabricate a Cu—
Si compound 18 a in an interface between theseed layer Cu 14 and the Tabarrier metal layer 12 as shown in FIG. 9B. Subsequently, aCu layer 16 a is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 350 to 400° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. - Subsequently, as shown in FIG. 9C, by using CMP method or the like, an interconnection is fabricated. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an
SiN layer 17 or the like is fabricated by sputtering. Thus, an interconnection structure is obtained, where there is a Cu—Si compound 18 a in the interface between the seed Cu layer and the Ta layer, and this interconnection is set as a lower layer interconnection. - A low dielectric
constant film 11 c as an interlayer insulating film of a via hole part, and anSiCN layer 17 d or the like are fabricated. Subsequently, a low dielectric constant film as an interlayer insulating film of an upper layer interconnection, and an SiO2 film 11 d are fabricated. Then, a reflection prevention film, a photoresist and an etching mask are fabricated and, by using gas containing fluorocarbon or the like, an upperlayer interconnection groove 91 is opened by etching. - Then, as shown in FIG. 9D, after removal of the etching mask, a reflection prevention film for via hole opening, a photoresist, and an etching mask are fabricated, and etched to fabricate a via
hole 92. - After normal treatment such as wet cleaning and/or cleaning, as in the case of the lower layer interconnection, sputtering of a
barrier metal layer 12 d mainly made of high melting point metal such as Ta, and aseed Cu layer 14 g are executed, impurities such asTa 12 d are injected (injection energy of 5 keV, and a dose amount of 1.0E15 cm−2), and subjected to annealing, andCu 18 b, 18 c in the vicinity of an interface between the seed Cu layer and the Ta barrier layer becomes amorphous. - Subsequently, as shown in FIG. 9E, a
Cu layer 16 e is fabricated thick by a method such as electro-plating. This layer is subjected to heat treatment at about 380° C. for 10 min. to several hours in accordance with an interconnection thickness and/or an interconnection width to grow Cu grains, and uniformly fill the groove. Subsequently, by using CMP method or the like, an interconnection is fabricated. A surface of the interconnection is treated such as cleaning and/or plasma irradiation to remove a Cu natural oxide layer and, then, an SiN layer 17 f or the like is fabricated by sputtering. Thus, an interconnection structure can be fabricated, where there is aseed Cu layer 14 g in an interface between the seed Cu layer and the Ta layer, and this interconnection is set as an upper layer interconnection. - The embodiment shows the interconnection structure where the amorphous Cu layer is present in the interface between the seed Cu layer and the Ta layer in the lower layer interconnection, and the Cu—Si compound is present, in the interface between the seed Cu layer and the Ta layer in the via hole and the upper layer interconnection. However, application can be made to various combinations, e.g., a case where structures are similar between the lower layer interconnection/the via hole and the upper layer interconnection, a case where in one of the structures, one of the copper interconnection fabrication methods of the first to fifth embodiments of the invention is employed, and other cases. Moreover, the number of interconnection layers is not limited to two, and the invention can be applied to a case of much more layers.
- In the diffusion mechanism of the EM, there are lattice diffusion, grain boundary diffusion, interface diffusion, and the like depending on a main diffusion path. It is known that the diffusion is carried out via holes in many cases. In such a case, hole generation occurs at a first stage, holes are exchanged (accordingly material movement) at a second stage, and it is said that substantially equal amounts of activation energy are needed for both. Thus, in both grain boundary diffusion and interface diffusion executed through a grain boundary or an interface where there are many holes, activation energy is lower than lattice diffusion becase of lack of hole-generation activation energy to make diffusion faster.
- For an EM suppression in the Al interconnection, as described in Patent Document 1, there is an example of adding a small amount of impurities such as Cu to Al. This is employed because as described in Nonpatent Document 1, impurities are deposited in an Al grain boundary to lower a hole density, whereby contribution of grain boundary diffusion is reduced. In the Cu interconnection, an dominant EM diffusion path is considered to be an interface with other materials. Thus, interface holes may be selectively removed.
- As impurities to be added to Cu, many are possible. In addition to those deposited in the interface, as,an example, Nb or Ta which fully fabricates a solid solution with Cu is suitable. For example, in the Cu and Nb system, a Cu—Nb compound is continuously present in an interface between Cu and Nb to greatly reduce holes. Compared with the case where impurities are deposited, this example is also advantageous in that there no resistance increases by impurities. V belonging to the same group as Nb may also be suitable.
- Recently, a Cu—Si compound has been considered to contribute to an EM improvement. Thus, a method of implanting Si ions by good controllability, or the like is also preferable. In addition, Ru which causes an oxide to exhibit good conductivity is also preferable from the standpoint of removing CuOx from the interface and maintaining conductivity as RuOx.
- Further, from the standpoint of making an interface structure continuous, it may be effective to make Cu amorphous to remove holes. Accordingly, ion implantation conditions of impurities may be conditions for making the vicinity of a very surface of Cu amorphous. An advantage accompanying the amorphous vicinity of the Cu interface is an improvement in physical properties such as adhesiveness and mechanical strength made by elimination of stress imbalance or local concentration to a passivation film such as a cap layer caused by a difference in growth rate according to criystal orientation during Cu crystal growth which occurs even at a room temperature. Moreover, the Cu amorphous treatment executed before the above-described CuSix treatment provides many effects such as uniform generation of CuSix.
- As apparent from the foregoing, the present invention is effective in that when an interconnection width is narrower than an average Cu grain size, and a grain boundary becomes a bamboo structure, a bamboo effect for increasing a lifetime appears, and thus a lifetime is increased by about two digits compared with the Al interconnection.
- A reason is that if there are impurities deposited in a gap in the vicinity of the interface between Cu and barrier metal (or cap), or if there is amorphous Cu in the interface between Cu and barrier metal (or cap), the number of holes, many being present in the interface between normal different materials, is reduced, and thus interface diffusion occurring through the holes can be suppressed. Accordingly, as Cu diffusion path by the EM, interface contribution is reduced, whereby a main Cu diffusion mechanism becomes lattice diffusion.
- The impurities are not only precipitated in the interface, but may fabricate a compound in the interface. For example, it is known that Ta, Nb or the like fully fabricates a solid solution with Cu. Presence of such a compound may reduce holes in the interface to increase an EM lifetime. There is a report that silicide treatment of the Cu surface increases an EM lifetime, and its combination with the present invention can expectedly increase the lifetime more.
- Use in the multilayer interconnection provides large resistance to stress migration caused by heat treatment executed for fabrication of each layer. In the single damascene structure, selection of a material of a melting point higher than that of Cu for a via hole enables fabrication of an interconnection structure of high interconnection reliability. In the dual damascene structure, since via adhesiveness can be enhanced, contribution can be made to a reduction in an initial failure rate, and Cu aggregation in the via which is one of failure modes can be suppressed.
Claims (125)
1. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer; and
hole reduction impurities added to said Cu precipitated in a first interface in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
2. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer; and
hole reduction impurities added to said Cu to fabricate a solid solution with said Cu in a first interface in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
3. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer; and
a hole reduction amorphous layer present in a first interface, in which said Cu is made amorphous, in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
4. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer; and
a hole reduction compound layer present in a first interface, in which a compound with said Cu is fabricated, in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
5. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer;
an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer; and
hole reduction impurities added to said Cu precipitated in a second interface in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
6. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer;
an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer; and
hole reduction impurities added to said Cu to fabricate a solid solution with said Cu in a second interface in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
7. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer;
an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer; and
a hole reduction amorphous layer present in a second interface, in which said Cu is made amorphous, in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
8. A copper interconnection comprising:
a barrier metal layer fabricated on an interconnection groove;
a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer;
an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer; and
a hole reduction compound layer present in a second interface, in which a compound with said Cu is fabricated, in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
9. The copper interconnection according to claim 1 , wherein said hole reduction impurities added to said Cu is one selected from Nb, Ta, Si, Ru, and V.
10. The copper interconnection according to claim 5 , wherein said hole reduction impurities added to said Cu is one selected from Nb, Ta, Si, Ru, and V.
11. A method for manufacturing a copper interconnection, comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a hole reduction impurity fabricating step(A) of ion-implanting hole reduction impurities in said barrier metal in order to reduce holes fabricated in a first interface between a Cu or Cu alloy layer for an interconnection and said barrier metal layer after said barrier metal sputtering step, and executing heat treatment;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said hole reduction impurity fabricating step(A);
a Cu depositing step of depositing Cu which makes an interconnection on said seed Cu after said seed Cu sputtering step; and,
thereby making said hole reduction impurities precipitate in said vicinity of said first interface.
12. The method for manufacturing a copper interconnection, according to claim 11 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said first interface.
13. The method for manufacturing a copper interconnection, according to claim 11 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, making said hole reduction impurities a Cu amorphous in said vicinity of said first interface.
14. The method for manufacturing a copper interconnection, according to claim 11 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a Cu compound with said Cu in said vicinity of said first interface.
15. A method for manufacturing a copper interconnection, comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a hole reduction impurity fabricating step(B) of depositing hole reduction impurities by a solid phase in order to reduce holes fabricated in a first interface between a Cu or Cu alloy layer for an interconnection and said barrier metal layer after said sputtering step, and diffusing said impurities by heat;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said hole reduction impurity fabricating step(B);
a Cu depositing step of depositing Cu which makes an interconnection on said seed Cu after said seed Cu sputtering step; and,
thereby making said hole reduction impurities precipitate in said vicinity of said first interface.
16. The method for manufacturing a copper interconnection, according to claim 15 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said first interface.
17. The method for manufacturing a copper interconnection, according to claim 15 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a Cu compound with said Cu in said vicinity of said first interface.
18. A method for manufacturing a copper interconnection, comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said barrier metal sputtering step;
a hole reduction impurity fabricating step(A) of ion-implanting hole reduction impurities in said barrier metal in order to reduce holes fabricated in a first interface between a Cu or Cu alloy layer for an interconnection and said barrier metal layer after said seed Cu sputtering step, and executing heat treatment;
a Cu depositing step of depositing Cu which makes an interconnection on said seed Cu after said hole reduction impurity fabricating step(A); and,
thereby making said hole reduction impurities precipitate in said vicinity of said first interface.
19. The method for manufacturing a copper interconnection, according to claim 18 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said first interface.
20. The method for manufacturing a copper interconnection, according to claim 18 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, making said hole reduction impurities a Cu amorphous in said vicinity of said first interface.
21. The method for manufacturing a copper interconnection, according to claim 18 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a Cu compound with said Cu in said vicinity of said first interface.
22. A method for manufacturing a copper interconnection, comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said barrier metal sputtering step;
a Cu interconnection fabricating step of embedding a Cu or Cu alloy layer in said interconnection groove after said seed Cu sputtering step, and fabricating an interconnection by using CMP method;
a hole reduction impurity fabricating step(C) of ion-implanting hole reduction impurities in order to reduce holes fabricated in a second interface between said Cu or Cu alloy layer and an insulating cap layer fabricated on said Cu or Cu alloy layer to insulate and protect said Cu or Cu alloy layer after said Cu interconnection fabricating step, and executing heat treatment;
a natural oxide layer removing step of removing a natural oxide layer of said Cu by executing treatment such as cleaning and/or plasma irradiation on a surface of said interconnection after said second hole reduction impurity fabricating step;
an insulating cap layer sputtering deposition step of depositing said insulating cap layer by sputtering after said natural oxide layer removing step; and,
thereby making said hole reduction impurities precipitate in said vicinity of said second interface.
23. The method for manufacturing a copper interconnection, according to claim 22 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said second interface.
24. The method for manufacturing a copper interconnection, according to claim 22 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, making said hole reduction impurities a Cu amorphous in said vicinity of said second interface.
25. The method for manufacturing a copper interconnection, according to claim 22 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, fabricating a Cu compound with said Cu in said vicinity of said second interface.
26. A method for manufacturing a copper interconnection, comprising:
a barrier metal sputtering step of sputtering barrier metal ion an interconnection groove;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said barrier metal sputtering step;
a Cu interconnection fabricating step of embedding a Cu or Cu alloy layer in said interconnection groove after said seed Cu sputtering step, and fabricating an interconnection by using CMP method;
a hole reduction impurity fabricating step(D) of depositing hole reduction impurities by a solid phase in order to reduce holes fabricated in a second interface between said Cu or Cu alloy layer and an insulating cap layer fabricated on said Cu or Cu alloy layer to insulate and protect said Cu or Cu alloy layer after said Cu interconnection fabricating step, and executing heat treatment;
a natural oxide layer removing step of removing a natural oxide layer of said Cu by executing treatment such as cleaning and/or plasma irradiation on a surface of said interconnection after said second hole reduction impurity fabricating step;
an insulating cap layer sputtering deposition step of depositing said insulating cap layer by sputtering after said natural oxide layer removing step; and
thereby making said hole reduction impurities precipitate in said vicinity of said second interface.
27. The method for manufacturing a copper interconnection, according to claim 26 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, fabricating a Cu compound with said Cu in said vicinity of said second interface.
28. The method for manufacturing a copper interconnection, according to claim 26 , wherein in place of said hole reduction impurity depositing step, a Cu compound fabricating step of fabricating a compound with said Cu in said vicinity of said second interface is executed.
29. The method for manufacturing a copper interconnection, according to claim 22 , wherein said natural oxide layer removing step is executed after said Cu interconnection fabricating step, and then said hole reduction impurity fabricating step(C) is executed.
30. The method for manufacturing a copper interconnection, according to claim 26 , wherein said natural oxide layer removing step is executed after said Cu interconnection fabricating step, and then said hole reduction impurity fabricating step(D) is executed.
31. The method for manufacturing a copper interconnection, according to claim 11 , wherein said hole reduction impurities are one selected from Nb, Ta, Si, Ru, and V.
32. The method for manufacturing a copper interconnection, according to claim 15 , wherein said hole reduction impurities are one selected from Nb, Ta, Si, Ru, and V.
33. The method for manufacturing a copper interconnection, according to claim 18 , wherein said hole reduction impurities are one selected from Nb, Ta, Si, Ru, and V.
34. The method for manufacturing a copper interconnection, according to claim 22 , wherein said hole reduction impurities are one selected from Nb, Ta, Si, Ru, and V.
35. The method for manufacturing a copper interconnection, according to claim 26 , wherein said hole reduction impurities are one selected from Nb, Ta, Si, Ru, and V.
36. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in a group of interconnections of said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, and hole reduction impurities added to said Cu precipitated in a first interface in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
37. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in a group of interconnections of said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, and hole reduction impurities added to said Cu to fabricate a solid solution in a first interface in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
38. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in a group of interconnections of said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, and a Cu hole reduction amorphous layer present in a first interface in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
39. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in a group of interconnections of said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, and a hole reduction compound layer present in a first interface, in which a compound with said Cu is fabricated, in order to reduce holes fabricated in said first interface between said Cu or Cu alloy layer and said barrier metal layer.
40. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer, and hole reduction impurities added to said Cu precipitated in a second interface in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
41. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer, and hole reduction impurities added to said Cu to fabricate a solid solution in a second interface in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
42. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer, and a hole reduction amorphous layer present in a second interface, in which said Cu is made amorphous, in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
43. A copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, comprising:
at least one or more copper interconnections included in said lower interconnection layer, said upper interconnection layer or said via hole,
wherein said copper interconnection is provided with a barrier metal layer fabricated on an interconnection groove, a Cu or Cu alloy layer for an interconnection fabricated on said barrier metal layer, an insulating cap layer fabricated on said Cu or Cu alloy layer to protect and insulate said Cu or Cu alloy layer, and a hole reduction compound layer present in a second interface, in which a compound with said Cu is fabricated, in order to reduce holes fabricated in said second interface between said Cu or Cu alloy layer and said insulating cap layer.
44. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 36 , wherein said hole reduction impurities are one selected from Nb, Ta, Si, Ru, and V.
45. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 36 , wherein said multi-layer interconnection structure is a single damascene.
46. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 37 , wherein said multi-layer interconnection structure is a single damascene.
47. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 38 , wherein said multi-layer interconnection structure is a single damascene.
48. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 39 , wherein said multi-layer interconnection structure is a single damascene.
49. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 40 , wherein said multi-layer interconnection structure is a single damascene.
50. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 41 , wherein said multi-layer interconnection structure is a single damascene.
51. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 42 , wherein said multi-layer interconnection structure is a single damascene.
52. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 43 , wherein said multi-layer interconnection structure is a single damascene.
53. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 36 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
54. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 37 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
55. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 38 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
56. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 39 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
57. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 40 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
58. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 41 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
59. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 42 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
60. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 43 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in a via first process for fabricating an interconnection groove after opening of a via.
61. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 36 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
62. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 37 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
63. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 38 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
64. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 39 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
65. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 40 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
66. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 41 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
67. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 42 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
68. The copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 43 , wherein said dual damascene is fabricated in a trench first process for opening a via after fabrication of an interconnection groove.
69. A method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in a manufacturing process of said copper interconnection, said process comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a hole reduction impurity fabricating step(A) of ion-implanting hole reduction impurities in said barrier metal in order to reduce holes fabricated in a first interface between a Cu or , Cu alloy layer for an interconnection and said barrier metal layer after said barrier metal sputtering step, and executing heat treatment;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said hole reduction impurity fabricating step(A);
a Cu depositing step of depositing Cu which makes an interconnection on said seed Cu after said seed Cu sputtering step; and,
thereby making said hole reduction impurities precipitate in said vicinity of said first interface.
70. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 69 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said first interface.
71. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 69 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, making said hole reduction impurities a Cu amorphous in said vicinity of said first interface.
72. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper wire, according to claim 69 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a Cu compound with said Cu in said vicinity of said first interface.
73. A method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in a manufacturing process of said copper interconnection, said process comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a hole reduction impurity fabricating step(B) of depositing hole reduction impurities by a solid phase in order to reduce holes fabricated in a first interface between a Cu or Cu alloy layer for an interconnection and said barrier metal layer after said sputtering step, and diffusing said impurities by heat;
a hole reduction impurity fabricating step of implanting ions in said barrier metal to execute heat treatment;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said hole reduction impurity fabricating step(B);
a Cu depositing step of depositing Cu which makes an interconnection on said seed Cu after said seed Cu sputtering step; and
thereby making said hole reduction impurities precipitate in said vicinity of said first interface.
74. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 73 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said first interface.
75. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 73 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a Cu compound with said Cu in said vicinity of said first interface.
76. A method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on the lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in a manufacturing process of said copper interconnection, said process comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said barrier metal sputtering step;
a hole reduction impurity fabricating step(A) of ion-implanting hole reduction impurities in said barrier metal in order to reduce holes fabricated in a first interface between a Cu or Cu alloy layer for an interconnection and said barrier metal layer after said seed Cu sputtering step, and executing heat treatment;
a Cu depositing step of depositing Cu which makes an interconnection on said seed Cu after said hole reduction impurity fabricating step(A); and
thereby making said hole reduction impurities precipitate in said vicinity of said first interface.
77. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 76 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said first interface.
78. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 76 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, making said hole reduction impurities a Cu amorphous in said vicinity of said first interface.
79. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 76 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said first interface, fabricating a Cu compound with said Cu in said vicinity of said first interface.
80. A method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on the lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in a manufacturing process of said copper interconnection, said process comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said barrier metal sputtering step;
a Cu interconnection fabricating step of embedding a Cu or Cu alloy layer in said interconnection groove after said seed Cu sputtering step, and fabricating an interconnection by using CMP method;
a hole reduction impurity fabricating step(C) of ion-implanting hole reduction impurities in order to reduce holes fabricated in a second interface between said Cu or Cu alloy layer and an insulating cap layer fabricated on said Cu or Cu alloy layer to insulate and protect said Cu or Cu alloy layer after said Cu interconnection fabricating step, and executing heat treatment;
a natural oxide layer removing step of removing a natural oxide layer of said Cu by executing treatment such as cleaning and/or plasma irradiation on a surface of said interconnection after said second hole reduction impurity fabricating step;
an insulating cap layer sputtering deposition step of depositing said insulating cap layer by sputtering after said natural oxide layer removing step; and
thereby making said hole reduction impurities precipitate in said vicinity of said first interface.
81. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 80 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said second interface.
82. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 80 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, making said hole reduction impurities a Cu amorphous in said vicinity of said second interface.
83. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 80 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, fabricating a Cu compound with said Cu in said vicinity of said second interface.
84. A method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on the lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in a manufacturing process of said copper interconnection, said process comprising:
a barrier metal sputtering step of sputtering barrier metal on an interconnection groove;
a seed Cu sputtering step of sputtering seed Cu which becomes a seed after said barrier metal sputtering step;
a Cu interconnection fabricating step of embedding a Cu or Cu alloy layer in said interconnection groove after said seed Cu sputtering step, and fabricating an interconnection by using CMP method;
a hole reduction impurity fabricating step(D) of depositing hole reduction impurities by a solid phase in order to reduce holes fabricated in a second interface between said Cu or Cu alloy layer and an insulating cap layer fabricated on said Cu or Cu alloy layer to insulate and protect said Cu or Cu alloy layer after said Cu interconnection fabricating step, and executing heat treatment;
a natural oxide layer removing step of removing a natural oxide layer of said Cu by executing treatment such as cleaning and/or plasma irradiation on a surface of said interconnection after said second hole reduction impurity fabricating step;
an insulating cap layer sputtering deposition step of depositing said insulating cap layer by sputtering after said natural oxide layer removing step; and,
thereby making said hole reduction impurities precipitate in said vicinity of said second interface.
85. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 84 , wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, fabricating a solid solution of said hole reduction impurities with said Cu in said vicinity of said second interface.
86. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 84, wherein in place of making said hole reduction impurities precipitate in said vicinity of said second interface, fabricating a Cu compound with said Cu in said vicinity of said second interface.
87. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 80 , wherein said natural oxide layer removing step is executed after said Cu interconnection fabricating step, and then said second hole reduction impurity fabricating step is executed.
88. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 84, wherein said natural oxide layer removing step is executed after said Cu interconnection fabricating step, and then said third hole reduction impurity fabricating step is executed.
89. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, at least one or more of said lower interconnection layer, said upper interconnection layer, and said via hole being fabricated in said manufacturing process of said copper interconnection, according to claim 69 , wherein the hole reduction impurities are one selected from Nb, Ta, Si, Ru, and V.
90. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 69 , wherein said multi-layers interconnection structure is a single damascene.
91. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 70 , wherein said multi-layers interconnection structure is a single damascene.
92. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 71 , wherein said multi-layers interconnection structure is a single damascene.
93. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 72 , wherein said multi-layers interconnection structure is a single damascene.
94. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 73 , wherein said multi-layers interconnection structure is a single damascene.
95. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 74 , wherein said multi-layers interconnection structure is a single damascene.
96. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 75 , wherein said multi-layers interconnection structure is a single damascene.
97. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 76 , wherein said multi-layers interconnection structure is a single damascene.
98. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 77 , wherein said multi-layers interconnection structure is a single damascene.
99. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 78 , wherein said multi-layers interconnection structure is a single damascene.
100. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 79 , wherein said multi-layers interconnection structure is a single damascene.
101. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 80 , wherein said multi-layers interconnection structure is a single damascene.
102. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 81 , wherein said multi-layers interconnection structure is a single damascene.
103. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 82 , wherein said multi-layers interconnection structure is a single damascene.
104. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 83 , wherein said multi-layers interconnection structure is a single damascene.
105. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 84 , wherein said multi-layers interconnection structure is a single damascene.
106. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 85 , wherein said multi-layers interconnection structure is a single damascene.
107. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 86 , wherein said multi-layers interconnection structure is a single damascene.
108. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 69 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
109. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 70 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
110. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 71 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
111. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 72 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
112. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 73 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
113. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 74 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
114. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 75 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
115. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 76 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
116. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 77 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
117. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 78 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
118. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 79 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
119. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 80 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
120. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 81 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
121. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 82 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
122. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 83 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
123. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 84 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
124. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 85 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
125. The method for manufacturing a copper interconnection with multi-layers having a lower interconnection layer of one layer, an upper interconnection layer positioned on said lower interconnection layer to be different from said one layer, and a via hole for interconnecting said lower and upper wring layers, according to claim 86 , wherein said multi-layer interconnection structure is a dual damascene, and said dual damascene is fabricated in at least one of a via first process for fabricating said interconnection groove after opening of said via, a trench first process for opening said via after fabrication of said interconnection groove.
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| DE10339990B4 (en) * | 2003-08-29 | 2012-11-22 | Advanced Micro Devices, Inc. | A method of fabricating a metal line having increased resistance to electromigration along an interface of a dielectric barrier layer by implanting material into the metal line |
| US20080174018A1 (en) * | 2003-09-09 | 2008-07-24 | Matsushita Electric Industrial Co., Ltd. | Semiconductor device and method for fabricating the same |
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| US20090236744A1 (en) * | 2005-03-02 | 2009-09-24 | Takao Kinoshita | Semiconductor device and method of producing the same |
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| US20180308944A1 (en) * | 2014-03-13 | 2018-10-25 | Taiwan Semiconductor Manufacturing Company Limited | Semiconductor device and sidewall passivation and method of making |
| US10510854B2 (en) * | 2014-03-13 | 2019-12-17 | Taiwan Semiconductor Manufacturing Company Limited | Semiconductor device having gate body and inhibitor film between conductive prelayer over gate body and conductive layer over inhibitor film |
| CN105244310A (en) * | 2014-06-30 | 2016-01-13 | 中芯国际集成电路制造(上海)有限公司 | Formation method of interconnection structure |
| CN113053800A (en) * | 2020-03-30 | 2021-06-29 | 台湾积体电路制造股份有限公司 | Interconnection layer and method of manufacturing the same |
| CN114664732A (en) * | 2022-05-25 | 2022-06-24 | 合肥晶合集成电路股份有限公司 | A kind of semiconductor integrated device and its manufacturing method |
Also Published As
| Publication number | Publication date |
|---|---|
| US20050250328A1 (en) | 2005-11-10 |
| TW200301952A (en) | 2003-07-16 |
| US7315084B2 (en) | 2008-01-01 |
| TW571389B (en) | 2004-01-11 |
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