US20190051768A1 - Method for graded anti-reflective coatings by physical vapor deposition - Google Patents
Method for graded anti-reflective coatings by physical vapor deposition Download PDFInfo
- Publication number
- US20190051768A1 US20190051768A1 US16/154,330 US201816154330A US2019051768A1 US 20190051768 A1 US20190051768 A1 US 20190051768A1 US 201816154330 A US201816154330 A US 201816154330A US 2019051768 A1 US2019051768 A1 US 2019051768A1
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- Prior art keywords
- graded
- refractive index
- reflective coating
- substrate
- gas
- Prior art date
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- 239000006117 anti-reflective coating Substances 0.000 title claims abstract description 87
- 238000000034 method Methods 0.000 title abstract description 64
- 238000005240 physical vapour deposition Methods 0.000 title description 8
- 239000000758 substrate Substances 0.000 claims abstract description 67
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 21
- 229910052710 silicon Inorganic materials 0.000 claims description 20
- 239000010703 silicon Substances 0.000 claims description 20
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 14
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 7
- 239000001301 oxygen Substances 0.000 claims description 7
- 229910052760 oxygen Inorganic materials 0.000 claims description 7
- 229910052757 nitrogen Inorganic materials 0.000 claims description 5
- 230000000295 complement effect Effects 0.000 claims description 3
- 150000004767 nitrides Chemical class 0.000 claims description 3
- 239000004065 semiconductor Substances 0.000 claims description 3
- 230000007704 transition Effects 0.000 claims 1
- 230000003247 decreasing effect Effects 0.000 abstract description 4
- 239000007789 gas Substances 0.000 description 34
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 20
- 229910001882 dioxygen Inorganic materials 0.000 description 20
- 239000000463 material Substances 0.000 description 16
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 12
- 229910001873 dinitrogen Inorganic materials 0.000 description 11
- 238000000151 deposition Methods 0.000 description 7
- 238000004544 sputter deposition Methods 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 6
- 230000008021 deposition Effects 0.000 description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 4
- 229910002092 carbon dioxide Inorganic materials 0.000 description 4
- 239000001569 carbon dioxide Substances 0.000 description 4
- 229910002091 carbon monoxide Inorganic materials 0.000 description 4
- 239000010408 film Substances 0.000 description 4
- 238000005086 pumping Methods 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- 229910052581 Si3N4 Inorganic materials 0.000 description 3
- 229910004286 SiNxOy Inorganic materials 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 3
- 238000005229 chemical vapour deposition Methods 0.000 description 3
- 230000003628 erosive effect Effects 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 238000000623 plasma-assisted chemical vapour deposition Methods 0.000 description 3
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 3
- MGWGWNFMUOTEHG-UHFFFAOYSA-N 4-(3,5-dimethylphenyl)-1,3-thiazol-2-amine Chemical compound CC1=CC(C)=CC(C=2N=C(N)SC=2)=C1 MGWGWNFMUOTEHG-UHFFFAOYSA-N 0.000 description 2
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 230000003667 anti-reflective effect Effects 0.000 description 2
- 229910052681 coesite Inorganic materials 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 229910052906 cristobalite Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000011737 fluorine Substances 0.000 description 2
- 229910052731 fluorine Inorganic materials 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- JCXJVPUVTGWSNB-UHFFFAOYSA-N nitrogen dioxide Inorganic materials O=[N]=O JCXJVPUVTGWSNB-UHFFFAOYSA-N 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 229910052682 stishovite Inorganic materials 0.000 description 2
- 239000013077 target material Substances 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052905 tridymite Inorganic materials 0.000 description 2
- 206010001513 AIDS related complex Diseases 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910004205 SiNX Inorganic materials 0.000 description 1
- 229910020286 SiOxNy Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 210000002945 adventitial reticular cell Anatomy 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 210000004027 cell Anatomy 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000003989 dielectric material Substances 0.000 description 1
- 210000002304 esc Anatomy 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000004313 glare Effects 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000010849 ion bombardment Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052754 neon Inorganic materials 0.000 description 1
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 238000004886 process control Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
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- H01L31/02161—
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/0021—Reactive sputtering or evaporation
- C23C14/0036—Reactive sputtering
- C23C14/0042—Controlling partial pressure or flow rate of reactive or inert gases with feedback of measurements
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/0021—Reactive sputtering or evaporation
- C23C14/0036—Reactive sputtering
- C23C14/0084—Producing gradient compositions
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0641—Nitrides
- C23C14/0652—Silicon nitride
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0676—Oxynitrides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/35—Sputtering by application of a magnetic field, e.g. magnetron sputtering
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B1/00—Optical elements characterised by the material of which they are made; Optical coatings for optical elements
- G02B1/10—Optical coatings produced by application to, or surface treatment of, optical elements
- G02B1/11—Anti-reflection coatings
- G02B1/113—Anti-reflection coatings using inorganic layer materials only
- G02B1/115—Multilayers
-
- H01L31/02168—
-
- H01L31/18—
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F71/00—Manufacture or treatment of devices covered by this subclass
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F77/00—Constructional details of devices covered by this subclass
- H10F77/30—Coatings
- H10F77/306—Coatings for devices having potential barriers
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F77/00—Constructional details of devices covered by this subclass
- H10F77/30—Coatings
- H10F77/306—Coatings for devices having potential barriers
- H10F77/311—Coatings for devices having potential barriers for photovoltaic cells
- H10F77/315—Coatings for devices having potential barriers for photovoltaic cells the coatings being antireflective or having enhancing optical properties
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
Definitions
- Embodiments of the invention generally relate to a method of forming an anti-reflective coating (ARC), and more particularly, for forming an ARC with a graded refractive index.
- ARC anti-reflective coating
- Thin film materials having a series of layers of metals and dielectrics of varying dielectric constants and refractive indices, such as a graded anti-reflective coating (ARC), are used to reduce glare or reflection.
- ARC graded anti-reflective coating
- Graded ARCs are often deposited by chemical vapor deposition (CVD) or plasma enhanced CVD (PECVD).
- CVD and PECVD pose a challenge because they require deposition at higher temperatures and incorporate large amounts of hydrogen, therefore resulting in impurities and low film quality.
- the present invention provides methods for forming an anti-reflective coating (ARC), and more particularly, for forming an ARC with a graded refractive index.
- ARC anti-reflective coating
- a method for forming a graded anti-reflective ARC in a physical vapor deposition processing chamber includes positioning a substrate on a substrate support below a target and flowing a first gas into the processing chamber to sputter the target to deposit a first portion of the graded ARC onto the substrate.
- the method also includes gradually flowing a second gas into the processing chamber to deposit a second portion of the graded ARC onto the substrate.
- the method further includes gradually flowing a third gas into the processing chamber while simultaneously gradually decreasing the flow of the second gas into the processing chamber to deposit a third portion of the graded ARC onto the substrate.
- the method also includes flowing the third gas into the processing chamber after stopping the flow of the second gas to form a fourth portion of the graded ARC.
- another method for forming a graded anti-reflective ARC in a physical vapor deposition processing chamber includes positioning a substrate on a substrate support below a silicon target and sputtering the silicon target to deposit a first portion of the graded ARC onto the substrate.
- the method also includes gradually flowing nitrogen gas into the processing chamber to deposit a second portion of the graded ARC onto the substrate.
- the method further includes gradually flowing oxygen gas into the processing chamber while simultaneously gradually decreasing the flow of the nitrogen gas into the processing chamber to deposit a third portion of the graded ARC onto the substrate.
- the method also includes flowing the oxygen gas into the processing chamber after stopping the flow of the nitrogen gas to form a fourth portion of the graded ARC onto the substrate.
- a film stack having a substrate having a graded ARC disposed thereon is provided.
- the graded ARC includes a first portion, a second portion disposed on the first portion, a third portion disposed on the second portion, and a fourth portion disposed on the third portion.
- the first portion has a first refractive index and the second portion has a second refractive index that is less than the first refractive index.
- the third portion has a third refractive index that is less than the second refractive index.
- the fourth portion has a fourth refractive index that is less than the third refractive index.
- FIG. 1 depicts a schematic cross-sectional view of a process chamber according to one embodiment of the invention.
- FIG. 2 depicts a cross sectional view of a filmstack having an anti-reflective coating (ARC) according to one embodiment of the invention.
- ARC anti-reflective coating
- FIG. 3 depicts a process flow diagram for forming an ARC according to one embodiment of the invention.
- FIG. 1 illustrates an exemplary physical vapor deposition (PVD) process chamber 100 (e.g., a sputter process chamber) suitable for sputter depositing materials according to one embodiment of the invention.
- PVD physical vapor deposition
- One example of the process chamber 100 that may be adapted to benefit from the invention is a PVD process chamber, available from Applied Materials, Inc., located in Santa Clara, Calif. It is contemplated that other sputter process chambers, including those from other manufactures, may be adapted to practice the present invention.
- the process chamber 100 includes a chamber body 108 having a processing volume 118 defined therein.
- the chamber body 108 has sidewalls 110 and a bottom 146 .
- the dimensions of the chamber body 108 and related components of the process chamber 100 are not limited and are generally proportionally larger than the size of a substrate 190 to be processed. Any suitable substrate size may be processed. Examples of suitable substrate sizes include substrates with a 200 mm diameter or 300 mm diameter.
- a chamber lid assembly 104 is mounted on the top of the chamber body 108 .
- the chamber body 108 may be fabricated from aluminum or other suitable materials.
- a substrate access port 130 is formed through the sidewall 110 of the chamber body 108 , facilitating the transfer of the substrate 190 into and out of the process chamber 100 .
- the access port 130 may be coupled to a transfer chamber and/or other chambers of a substrate processing system.
- a gas source 128 is coupled to the chamber body 108 to supply process gases into the processing volume 118 .
- process gases may include inert gases, non-reactive gases, and reactive gases if necessary.
- process gases examples include, but not limited to, argon gas (Ar), helium (He), neon gas (Ne), nitrogen gas (N 2 ), fluorine gas (F 2 ), oxygen gas (O 2 ), hydrogen gas (H2), H 2 O in vapor form, methane (CH4), carbon monoxide (CO), methane (CH 4 ), and/or carbon dioxide (CO 2 ), among others.
- a mass flow controllers (MFC) is coupled to the gas source 128 to finely and precisely control of the flow of gases.
- a pumping port 150 is formed through the bottom 146 of the chamber body 108 .
- a pumping device 152 is coupled to the processing volume 118 to evacuate and control the pressure therein.
- a pumping system and chamber cooling design enables high base vacuum (about 1 ⁇ 10 ⁇ 8 Torr or less) and low rate-of-rise (about 1,000 mTorr/min) at temperatures suited to thermal budget needs, e.g., about ⁇ 25 degrees Celsius to about 500 degrees Celsius.
- the pumping system is designed to provide precise control of process pressure which is a critical parameter for refractive index (RI) control and tuning.
- RI refractive index
- the lid assembly 104 generally includes a target 120 and a ground shield assembly 126 coupled thereto.
- the target 120 provides a material source that can be sputtered and deposited onto the surface of the substrate 190 during a PVD process.
- the target 120 serves as the cathode of the plasma circuit during DC sputtering.
- the target 120 or target plate may be fabricated from a material utilized for a deposition layer, or elements of the deposition layer to be formed in the process chamber 100 .
- a high voltage power supply such as a power source 132 , is connected to the target 120 to facilitate sputtering materials from the target 120 .
- the target 120 may be fabricated from a material containing silicon (Si), titanium (Ti), tantalum (Ta), hafnium (Hf), tungsten (W), cobalt (Co), nickel (Ni), copper (Cu), aluminum (Al), alloys thereof, or combinations thereof and the like.
- the target may be fabricated from silicon.
- the target 120 generally includes a peripheral portion 124 and a central portion 116 .
- the peripheral portion 124 is disposed over the sidewalls 110 of the chamber.
- the central portion 116 of the target 120 may have a curvature surface slightly extending towards the surface of the substrate 190 disposed on a substrate support 138 .
- the spacing between the target 120 and the substrate support 138 is maintained between about 50 mm to about 350 mm, for example, about 55 mm. It is contemplated that the dimension, shape, materials, configuration and diameter of the target 120 may be varied for specific process or substrate requirements.
- the target 120 may further include a backing plate having a central portion bonded and/or fabricated by a material desired to be sputtered onto the substrate surface.
- the target 120 may also include adjacent tiles or segmented materials that together form the target 120 .
- the lid assembly 104 may further comprise a full face erosion magnetron cathode 102 mounted above the target 120 which enhances efficient sputtering materials from the target 120 during processing.
- the full face erosion magnetron cathode 102 allows easy and fast process control and tailored film properties while ensuring consistent target erosion and uniform deposition of films, such as SiO x N y , across the wafer for a variety of values of x and y ranging from 0% to 100%.
- Examples of the magnetron assembly include a linear magnetron, a serpentine magnetron, a spiral magnetron, a double-digitated magnetron, a rectangularized spiral magnetron, among others.
- the ground shield assembly 126 of the lid assembly 104 includes a ground frame 106 and a ground shield 112 .
- the ground shield assembly 126 may also include other chamber shield member, target shield member, dark space shield, and dark space shield frame.
- the ground shield 112 is coupled to the peripheral portion 124 by the ground frame 106 defining an upper processing region 154 below the central portion of the target 120 in the processing volume 118 .
- the ground frame 106 electrically insulates the ground shield 112 from the target 120 while providing a ground path to the chamber body 108 of the process chamber 100 through the sidewalls 110 .
- the ground shield 112 constrains plasma generated during processing within the upper processing region 154 and dislodges target source material from the confined central portion 116 of the target 120 , thereby allowing the dislodged target source to be mainly deposited on the substrate surface rather than chamber sidewalls 110 .
- the ground shield 112 may be formed by one or more work-piece fragments and/or a number of these pieces bonding by processes known in the art, such as welding, gluing, high pressure compression, etc.
- a shaft 140 extending through the bottom 146 of the chamber body 108 couples to a lift mechanism 144 .
- the lift mechanism 144 is configured to move the substrate support 138 between a lower transfer position and an upper processing position.
- Bellows 142 circumscribe the shaft 140 and are coupled to the substrate support 138 to provide a flexible seal there between, thereby maintaining vacuum integrity of the chamber processing volume 118 .
- the substrate support 138 provides an electro-static chuck (ESC) 180 .
- the ESC 180 uses the attraction of opposite charges to hold both insulating and conducting substrates 190 for PVD processes and is powered by a DC power supply 181 .
- the ESC 180 comprises an electrode embedded within a dielectric body.
- the DC power supply 181 may provide a DC chucking voltage of about 200 volts to about 2000 volts to the electrode.
- the DC power supply 181 may also include a system controller for controlling the operation of the electrode by directing a DC current to the electrode for chucking and de-chucking the substrate 190 .
- the ESC 180 performs in the temperature range required by the thermal budget of the device integration requirements formed by the substrate 190 .
- a plasma is commonly formed from an inert gas, such as argon, before a reactive gas is introduced into the process chamber 100 .
- An antenna 176 such as one or more inductor coils, may be provided adjacent the process chamber 100 .
- An antenna power supply 175 may power the antenna 176 to inductively couple energy, such as RF energy, to the process gas to form plasma in a process zone in the process chamber 100 .
- process electrodes comprising a cathode below the substrate 190 and an anode above the substrate 190 may be used to couple RF power to generate plasma.
- the operation of the power source 175 may be controlled by a controller that also controls the operation of other components in the process chamber 100 .
- a shadow frame 122 is disposed on the periphery region of the substrate support 138 and is configured to confine deposition of source material sputtered from the target 120 to a desired portion of the substrate 190 surface.
- a chamber shield 136 may be disposed on the inner wall of the chamber body 108 and have a lip 156 extending inward to the processing volume 118 configured to support the shadow frame 122 disposed around the substrate support 138 . As the substrate support 138 is raised to the upper position for processing, an outer edge of the substrate 114 disposed on the substrate support 138 is engaged by the shadow frame 122 and the shadow frame 122 is lifted up and spaced away from the chamber shield 136 .
- the shadow frame 122 is set back on the chamber shield 136 .
- Lift pins (not shown) are selectively moved through the substrate support 138 to list the substrate 190 above the substrate support 138 to facilitate access to the substrate 190 by a transfer robot or other suitable transfer mechanism.
- a controller 148 is coupled to the process chamber 100 .
- the controller 148 includes a central processing unit (CPU) 160 , a memory 158 , and support circuits 162 .
- the controller 148 is utilized to control the process sequence, regulating the gas flows from the gas source 128 into the process chamber 100 and controlling ion bombardment of the target 120 .
- the CPU 160 may be of any form of a general purpose computer processor that can be used in an industrial setting.
- the software routines can be stored in the memory 158 , such as random access memory, read only memory, floppy or hard disk drive, or other form of digital storage.
- the support circuits 162 are conventionally coupled to the CPU 160 and may comprise cache, clock circuits, input/output subsystems, power supplies, and the like.
- the software routines when executed by the CPU 160 , transform the CPU into a specific purpose computer (controller) 148 that controls the process chamber 100 such that the processes are performed in accordance with the present invention.
- the software routines may also be stored and/or executed by a second controller (not shown) that is located remotely from the process chamber 100 .
- material is sputtered from the target 120 and deposited on the surface of the substrate 190 .
- the target 120 and the substrate support 138 are biased relative to each other by the power source 132 to maintain a plasma formed from the process gases supplied by the gas source 128 .
- the ions from the plasma are accelerated toward and strike the target 120 , causing target material to be dislodged from the target 120 .
- the dislodged target material and reactive process gases together form a layer on the substrate 190 with desired compositions.
- RF, DC or fast switching pulsed DC power supplies or combinations thereof provide tunable target bias for precise control of sputtering composition and deposition rates.
- FIG. 2 depicts a cross sectional view of a filmstack 200 having a graded ARC 204 according to one embodiment of the invention.
- FIG. 3 depicts a process flow diagram for forming the graded ARC 204 .
- a method 300 for forming the graded ARC 204 begins at block 302 by positioning the substrate 190 on the substrate support 138 and below the target 120 .
- the substrate 190 has one or more layers formed thereon, e.g., a silicon substrate having a photodiode 202
- the substrate support 138 includes an HTESC 180 .
- the substrate 202 is set about 55 mm away from the target 120 , and the target 120 is fabricated from silicon.
- the process chamber 100 pressure may be set to a low pressure, e.g., less than about 100 mTorr, or about 10 mTorr at room temperature.
- the DC power supply 181 is pulsed to provide less than about 20 kW, for example about 6 kW, at a frequency of about 100 kHz and a duty cycle of about 97%.
- one or more sputtering gasses from the gas source 128 are flowed into the process chamber 100 to sputter the silicon target 120 to form a first portion 206 of the graded ARC 204 having silicon onto the substrate 202 .
- the sputtering gas is argon gas flowed at about 30 sccm.
- one or more reactive gasses from the gas source 128 are flowed into the process chamber 100 to react with the silicon target 120 .
- the reactive gas is selected from a group comprising nitrogen gas (N 2 ), nitrogen dioxide (NO 2 ), fluorine gas (F 2 ), oxygen gas (O 2 ), hydrogen gas (H2), H 2 O in vapor form, methane (CH4), carbon monoxide (CO), methane (CH 4 ), and carbon dioxide (CO 2 ).
- nitrogen gas is gradually introduced into the process chamber 100 to form nitrogen plasma.
- the nitrogen gas is gradually introduced until it reaches about 100 sccm to form a second portion 208 of the graded ARC 204 having silicon nitride (SiN x wherein x is between about 0% to about 100%).
- SiN x silicon nitride
- the change in the composition of the graded ARC 204 from silicon in the first portion 206 to silicon nitride in the second portion 208 is gradual, i.e., no distinct layers in each portion of the graded ARC 204 .
- one or more reactive gasses from the gas source 128 is again flowed into the process chamber 100 to react with the silicon target 120 .
- oxygen gas is gradually introduced into the process chamber 100 to form oxygen plasma, while the flow of nitrogen gas is gradually decreased in the process chamber 100 .
- the oxygen gas is gradually introduced until it reaches to about 50 sccm to about 100 sccm, for example about 50 sccm or about 100 sccm, to form a third portion 210 of the graded ARC 204 having SiN x O y , wherein x and y are between about 0% to about 100%.
- the change in the composition of the graded ARC 204 from silicon nitride in the second portion 208 to SiN x O y in the third portion 210 is gradual, i.e., no distinct layers in each portion of the graded ARC 204 .
- the nitrogen gas is gradually reduced to 0 sccm to form a fourth portion 212 of the graded ARC 204 having silicon oxide SiO 2 .
- the oxygen gas continues to flow after the flow of nitrogen gas stops.
- the gradual flow changes in nitrogen gas and oxygen gas prevents the plasma from being extinguished in the process chamber 100 .
- the change in the composition of the graded ARC 204 from SiN x O y in the third portion 210 to SiO 2 in the fourth portion 212 is gradual, i.e., no distinct layers in each portion of the graded ARC 204 .
- an optional buffer laying having oxide or nitride may be deposited over the graded ARC 204 to form a filmstack 202 configured for a complementary metal-oxide-semiconductor (CMOS) image sensor device.
- CMOS complementary metal-oxide-semiconductor
- the refractive index of the graded ARC 204 (at about 633 nm) can be tuned from over about 2.0 to about 1.47.
- the refractive index of the ARC 204 is tuned to about 1.47.
- the graded ARC 204 has a refractive index between about 2.0 and about 2.5, for example, about 2.0 or about 2.1; (ii) at about 25 sccm of oxygen gas, the graded ARC 204 has a refractive index of between about 1.5 and about 2.0, for example about 1.75; (iii) at about 50 sccm of oxygen gas, the graded ARC 204 has a refractive index of between about 1.0 and about 1.5, for example about 1.47; (iv) at about 75 sccm of oxygen gas, the graded ARC 204 has a refractive index of between about 1.0 and about 1.5, for example about 1.48 or about 1.49; and (v) at about 100 sccm of oxygen gas, the graded ARC 204 has a refractive index of between about 1.0 and about 1.5, for example about 1.47.
- the graded ARC 204 has a low compressive stress level, i.e., the stress of the graded ARC 204 is tunable with different levels of oxygen gas.
- the graded ARC 204 has a stress level of ⁇ 599 MPa;
- the graded ARC 204 has a stress level of ⁇ 276 MPa;
- the graded ARC 204 has a stress level of ⁇ 144 MPa;
- the graded ARC 204 has a stress level of ⁇ 157 MPa;
- the graded ARC 204 has a stress level of ⁇ 119 MPa. Therefore, the graded ARC 204 provides
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Abstract
A method for forming an anti-reflective coating (ARC) includes positioning a substrate below a target and flowing a first gas to deposit a first portion of the graded ARC onto the substrate. The method includes gradually flowing a second gas to deposit a second portion of the graded ARC, and gradually flowing a third gas while simultaneously gradually decreasing the flow of the second gas to deposit a third portion of the graded ARC. The method also includes flowing the third gas after stopping the flow of the second gas to form a fourth portion of the graded ARC. In another embodiment a film stack having a substrate having a graded ARC disposed thereon is provided. The graded ARC includes a first portion, a second portion disposed on the first portion, a third portion disposed on the second portion, and a fourth portion disposed on the third portion.
Description
- This application is a divisional of U.S. patent application Ser. No. 14/531,549, filed Nov. 3, 2014, which claims benefit of U.S. Provisional Application Ser. No. 61/887,147, filed Nov. 13, 2013 (Attorney Docket No. APPM/20741USL01) and U.S. Provisional Application Ser. No. 61/904,437, filed Nov. 14, 2013 (Attorney Docket No. APPM/20741USL02), all of which are incorporated by reference in their entireties.
- Embodiments of the invention generally relate to a method of forming an anti-reflective coating (ARC), and more particularly, for forming an ARC with a graded refractive index.
- Many of the materials used in manufacturing solar cells, for example silicon, have high refractive indices and result in loss of incident sunlight by reflection. Thin film materials having a series of layers of metals and dielectrics of varying dielectric constants and refractive indices, such as a graded anti-reflective coating (ARC), are used to reduce glare or reflection.
- Graded ARCs are often deposited by chemical vapor deposition (CVD) or plasma enhanced CVD (PECVD). However, CVD and PECVD pose a challenge because they require deposition at higher temperatures and incorporate large amounts of hydrogen, therefore resulting in impurities and low film quality.
- Therefore, there is a need for an improved method of forming an ARC with a graded refractive index.
- The present invention provides methods for forming an anti-reflective coating (ARC), and more particularly, for forming an ARC with a graded refractive index.
- In one embodiment a method for forming a graded anti-reflective ARC in a physical vapor deposition processing chamber is provided. The method includes positioning a substrate on a substrate support below a target and flowing a first gas into the processing chamber to sputter the target to deposit a first portion of the graded ARC onto the substrate. The method also includes gradually flowing a second gas into the processing chamber to deposit a second portion of the graded ARC onto the substrate. The method further includes gradually flowing a third gas into the processing chamber while simultaneously gradually decreasing the flow of the second gas into the processing chamber to deposit a third portion of the graded ARC onto the substrate. The method also includes flowing the third gas into the processing chamber after stopping the flow of the second gas to form a fourth portion of the graded ARC.
- In another embodiment another method for forming a graded anti-reflective ARC in a physical vapor deposition processing chamber is provided. The method includes positioning a substrate on a substrate support below a silicon target and sputtering the silicon target to deposit a first portion of the graded ARC onto the substrate. The method also includes gradually flowing nitrogen gas into the processing chamber to deposit a second portion of the graded ARC onto the substrate. The method further includes gradually flowing oxygen gas into the processing chamber while simultaneously gradually decreasing the flow of the nitrogen gas into the processing chamber to deposit a third portion of the graded ARC onto the substrate. The method also includes flowing the oxygen gas into the processing chamber after stopping the flow of the nitrogen gas to form a fourth portion of the graded ARC onto the substrate.
- In yet another embodiment a film stack having a substrate having a graded ARC disposed thereon is provided. The graded ARC includes a first portion, a second portion disposed on the first portion, a third portion disposed on the second portion, and a fourth portion disposed on the third portion. The first portion has a first refractive index and the second portion has a second refractive index that is less than the first refractive index. The third portion has a third refractive index that is less than the second refractive index. The fourth portion has a fourth refractive index that is less than the third refractive index.
- So that the manner in which the above recited features of the present invention are attained and can be understood in detail, a more particular description of the invention, briefly summarized above, may be had by reference to the embodiments thereof which are illustrated in the appended drawings.
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FIG. 1 depicts a schematic cross-sectional view of a process chamber according to one embodiment of the invention. -
FIG. 2 depicts a cross sectional view of a filmstack having an anti-reflective coating (ARC) according to one embodiment of the invention. -
FIG. 3 depicts a process flow diagram for forming an ARC according to one embodiment of the invention. - To facilitate understanding, identical reference numerals have been used, where possible, to designate identical elements that are common to the figures. It is contemplated that elements and features of one embodiment may be beneficially incorporated in other embodiments without further recitation.
- It is to be noted, however, that the appended drawings illustrate only exemplary embodiments of this invention and are therefore not to be considered limiting of its scope, for the invention may admit to other equally effective embodiments.
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FIG. 1 illustrates an exemplary physical vapor deposition (PVD) process chamber 100 (e.g., a sputter process chamber) suitable for sputter depositing materials according to one embodiment of the invention. One example of theprocess chamber 100 that may be adapted to benefit from the invention is a PVD process chamber, available from Applied Materials, Inc., located in Santa Clara, Calif. It is contemplated that other sputter process chambers, including those from other manufactures, may be adapted to practice the present invention. - The
process chamber 100 includes achamber body 108 having aprocessing volume 118 defined therein. Thechamber body 108 hassidewalls 110 and abottom 146. The dimensions of thechamber body 108 and related components of theprocess chamber 100 are not limited and are generally proportionally larger than the size of asubstrate 190 to be processed. Any suitable substrate size may be processed. Examples of suitable substrate sizes include substrates with a 200 mm diameter or 300 mm diameter. - A
chamber lid assembly 104 is mounted on the top of thechamber body 108. Thechamber body 108 may be fabricated from aluminum or other suitable materials. Asubstrate access port 130 is formed through thesidewall 110 of thechamber body 108, facilitating the transfer of thesubstrate 190 into and out of theprocess chamber 100. Theaccess port 130 may be coupled to a transfer chamber and/or other chambers of a substrate processing system. - A
gas source 128 is coupled to thechamber body 108 to supply process gases into theprocessing volume 118. In one embodiment, process gases may include inert gases, non-reactive gases, and reactive gases if necessary. - Examples of process gases that may be provided by the
gas source 128 include, but not limited to, argon gas (Ar), helium (He), neon gas (Ne), nitrogen gas (N2), fluorine gas (F2), oxygen gas (O2), hydrogen gas (H2), H2O in vapor form, methane (CH4), carbon monoxide (CO), methane (CH4), and/or carbon dioxide (CO2), among others. In one embodiment, a mass flow controllers (MFC) is coupled to thegas source 128 to finely and precisely control of the flow of gases. - A
pumping port 150 is formed through thebottom 146 of thechamber body 108. Apumping device 152 is coupled to theprocessing volume 118 to evacuate and control the pressure therein. A pumping system and chamber cooling design enables high base vacuum (about 1×10−8 Torr or less) and low rate-of-rise (about 1,000 mTorr/min) at temperatures suited to thermal budget needs, e.g., about −25 degrees Celsius to about 500 degrees Celsius. The pumping system is designed to provide precise control of process pressure which is a critical parameter for refractive index (RI) control and tuning. - The
lid assembly 104 generally includes atarget 120 and aground shield assembly 126 coupled thereto. Thetarget 120 provides a material source that can be sputtered and deposited onto the surface of thesubstrate 190 during a PVD process. Thetarget 120 serves as the cathode of the plasma circuit during DC sputtering. - The
target 120 or target plate may be fabricated from a material utilized for a deposition layer, or elements of the deposition layer to be formed in theprocess chamber 100. A high voltage power supply, such as apower source 132, is connected to thetarget 120 to facilitate sputtering materials from thetarget 120. - In one embodiment, the
target 120 may be fabricated from a material containing silicon (Si), titanium (Ti), tantalum (Ta), hafnium (Hf), tungsten (W), cobalt (Co), nickel (Ni), copper (Cu), aluminum (Al), alloys thereof, or combinations thereof and the like. In one embodiment depicted herein, the target may be fabricated from silicon. - The
target 120 generally includes aperipheral portion 124 and acentral portion 116. Theperipheral portion 124 is disposed over thesidewalls 110 of the chamber. Thecentral portion 116 of thetarget 120 may have a curvature surface slightly extending towards the surface of thesubstrate 190 disposed on asubstrate support 138. The spacing between thetarget 120 and thesubstrate support 138 is maintained between about 50 mm to about 350 mm, for example, about 55 mm. It is contemplated that the dimension, shape, materials, configuration and diameter of thetarget 120 may be varied for specific process or substrate requirements. In one embodiment, thetarget 120 may further include a backing plate having a central portion bonded and/or fabricated by a material desired to be sputtered onto the substrate surface. Thetarget 120 may also include adjacent tiles or segmented materials that together form thetarget 120. - The
lid assembly 104 may further comprise a full faceerosion magnetron cathode 102 mounted above thetarget 120 which enhances efficient sputtering materials from thetarget 120 during processing. The full faceerosion magnetron cathode 102 allows easy and fast process control and tailored film properties while ensuring consistent target erosion and uniform deposition of films, such as SiOxNy, across the wafer for a variety of values of x and y ranging from 0% to 100%. Examples of the magnetron assembly include a linear magnetron, a serpentine magnetron, a spiral magnetron, a double-digitated magnetron, a rectangularized spiral magnetron, among others. - The
ground shield assembly 126 of thelid assembly 104 includes aground frame 106 and aground shield 112. Theground shield assembly 126 may also include other chamber shield member, target shield member, dark space shield, and dark space shield frame. Theground shield 112 is coupled to theperipheral portion 124 by theground frame 106 defining anupper processing region 154 below the central portion of thetarget 120 in theprocessing volume 118. Theground frame 106 electrically insulates theground shield 112 from thetarget 120 while providing a ground path to thechamber body 108 of theprocess chamber 100 through thesidewalls 110. Theground shield 112 constrains plasma generated during processing within theupper processing region 154 and dislodges target source material from the confinedcentral portion 116 of thetarget 120, thereby allowing the dislodged target source to be mainly deposited on the substrate surface rather thanchamber sidewalls 110. In one embodiment, theground shield 112 may be formed by one or more work-piece fragments and/or a number of these pieces bonding by processes known in the art, such as welding, gluing, high pressure compression, etc. - A
shaft 140 extending through thebottom 146 of thechamber body 108 couples to alift mechanism 144. Thelift mechanism 144 is configured to move thesubstrate support 138 between a lower transfer position and an upper processing position.Bellows 142 circumscribe theshaft 140 and are coupled to thesubstrate support 138 to provide a flexible seal there between, thereby maintaining vacuum integrity of thechamber processing volume 118. - The
substrate support 138 provides an electro-static chuck (ESC) 180. TheESC 180 uses the attraction of opposite charges to hold both insulating and conductingsubstrates 190 for PVD processes and is powered by aDC power supply 181. TheESC 180 comprises an electrode embedded within a dielectric body. TheDC power supply 181 may provide a DC chucking voltage of about 200 volts to about 2000 volts to the electrode. TheDC power supply 181 may also include a system controller for controlling the operation of the electrode by directing a DC current to the electrode for chucking and de-chucking thesubstrate 190. - The
ESC 180 performs in the temperature range required by the thermal budget of the device integration requirements formed by thesubstrate 190. For example, the temperature range for: (i) a detachable ESC 180 (DTESC) is about minus 25 degrees Celsius to about 100 degrees; (ii) a mid-temperature ESC 180 (MTESC) is about 100 degrees Celsius to about 200 degrees Celsius; (iii) a high temperature or high temperature biasable or high temperature high uniformity ESC 180 (HTESC or HTBESC or HTHUESC) is about 200 degrees Celsius to about 500 degrees Celsius, to ensure fast and uniform heating of thesubstrate 190. Additionally, any of the ESCs may be used without being heated, i.e., at room temperature. - After the process gas is introduced into the
process chamber 100, the gas is energized to form plasma. A plasma is commonly formed from an inert gas, such as argon, before a reactive gas is introduced into theprocess chamber 100. Anantenna 176, such as one or more inductor coils, may be provided adjacent theprocess chamber 100. Anantenna power supply 175 may power theantenna 176 to inductively couple energy, such as RF energy, to the process gas to form plasma in a process zone in theprocess chamber 100. Alternatively, or in addition, process electrodes comprising a cathode below thesubstrate 190 and an anode above thesubstrate 190 may be used to couple RF power to generate plasma. The operation of thepower source 175 may be controlled by a controller that also controls the operation of other components in theprocess chamber 100. - A
shadow frame 122 is disposed on the periphery region of thesubstrate support 138 and is configured to confine deposition of source material sputtered from thetarget 120 to a desired portion of thesubstrate 190 surface. Achamber shield 136 may be disposed on the inner wall of thechamber body 108 and have alip 156 extending inward to theprocessing volume 118 configured to support theshadow frame 122 disposed around thesubstrate support 138. As thesubstrate support 138 is raised to the upper position for processing, an outer edge of the substrate 114 disposed on thesubstrate support 138 is engaged by theshadow frame 122 and theshadow frame 122 is lifted up and spaced away from thechamber shield 136. When thesubstrate support 138 is lowered to the transfer position adjacent to the substratetransfer access port 130, theshadow frame 122 is set back on thechamber shield 136. Lift pins (not shown) are selectively moved through thesubstrate support 138 to list thesubstrate 190 above thesubstrate support 138 to facilitate access to thesubstrate 190 by a transfer robot or other suitable transfer mechanism. - A
controller 148 is coupled to theprocess chamber 100. Thecontroller 148 includes a central processing unit (CPU) 160, amemory 158, and supportcircuits 162. Thecontroller 148 is utilized to control the process sequence, regulating the gas flows from thegas source 128 into theprocess chamber 100 and controlling ion bombardment of thetarget 120. TheCPU 160 may be of any form of a general purpose computer processor that can be used in an industrial setting. The software routines can be stored in thememory 158, such as random access memory, read only memory, floppy or hard disk drive, or other form of digital storage. Thesupport circuits 162 are conventionally coupled to theCPU 160 and may comprise cache, clock circuits, input/output subsystems, power supplies, and the like. The software routines, when executed by theCPU 160, transform the CPU into a specific purpose computer (controller) 148 that controls theprocess chamber 100 such that the processes are performed in accordance with the present invention. The software routines may also be stored and/or executed by a second controller (not shown) that is located remotely from theprocess chamber 100. - During processing, material is sputtered from the
target 120 and deposited on the surface of thesubstrate 190. Thetarget 120 and thesubstrate support 138 are biased relative to each other by thepower source 132 to maintain a plasma formed from the process gases supplied by thegas source 128. The ions from the plasma are accelerated toward and strike thetarget 120, causing target material to be dislodged from thetarget 120. The dislodged target material and reactive process gases together form a layer on thesubstrate 190 with desired compositions. RF, DC or fast switching pulsed DC power supplies or combinations thereof provide tunable target bias for precise control of sputtering composition and deposition rates. -
FIG. 2 depicts a cross sectional view of afilmstack 200 having a gradedARC 204 according to one embodiment of the invention.FIG. 3 depicts a process flow diagram for forming the gradedARC 204. Referring toFIGS. 1-3 , amethod 300 for forming the gradedARC 204 begins atblock 302 by positioning thesubstrate 190 on thesubstrate support 138 and below thetarget 120. In one embodiment, thesubstrate 190 has one or more layers formed thereon, e.g., a silicon substrate having aphotodiode 202, and thesubstrate support 138 includes anHTESC 180. Thesubstrate 202 is set about 55 mm away from thetarget 120, and thetarget 120 is fabricated from silicon. In one embodiment, theprocess chamber 100 pressure may be set to a low pressure, e.g., less than about 100 mTorr, or about 10 mTorr at room temperature. In one embodiment, theDC power supply 181 is pulsed to provide less than about 20 kW, for example about 6 kW, at a frequency of about 100 kHz and a duty cycle of about 97%. - At
block 304, one or more sputtering gasses from thegas source 128 are flowed into theprocess chamber 100 to sputter thesilicon target 120 to form afirst portion 206 of the gradedARC 204 having silicon onto thesubstrate 202. In one embodiment, the sputtering gas is argon gas flowed at about 30 sccm. - At
block 306, one or more reactive gasses from thegas source 128 are flowed into theprocess chamber 100 to react with thesilicon target 120. In one embodiment, the reactive gas is selected from a group comprising nitrogen gas (N2), nitrogen dioxide (NO2), fluorine gas (F2), oxygen gas (O2), hydrogen gas (H2), H2O in vapor form, methane (CH4), carbon monoxide (CO), methane (CH4), and carbon dioxide (CO2). For example, in one embodiment, nitrogen gas is gradually introduced into theprocess chamber 100 to form nitrogen plasma. The nitrogen gas is gradually introduced until it reaches about 100 sccm to form asecond portion 208 of the gradedARC 204 having silicon nitride (SiNx wherein x is between about 0% to about 100%). As noted by the phantom lines inFIG. 2 , the change in the composition of the gradedARC 204 from silicon in thefirst portion 206 to silicon nitride in thesecond portion 208 is gradual, i.e., no distinct layers in each portion of the gradedARC 204. - At
block 308, one or more reactive gasses from thegas source 128 is again flowed into theprocess chamber 100 to react with thesilicon target 120. In one embodiment, oxygen gas is gradually introduced into theprocess chamber 100 to form oxygen plasma, while the flow of nitrogen gas is gradually decreased in theprocess chamber 100. The oxygen gas is gradually introduced until it reaches to about 50 sccm to about 100 sccm, for example about 50 sccm or about 100 sccm, to form athird portion 210 of the gradedARC 204 having SiNxOy, wherein x and y are between about 0% to about 100%. As discussed above, the change in the composition of the gradedARC 204 from silicon nitride in thesecond portion 208 to SiNxOy in thethird portion 210 is gradual, i.e., no distinct layers in each portion of the gradedARC 204. - At
block 310, while the flow of oxygen gas is gradually increasing, the nitrogen gas is gradually reduced to 0 sccm to form afourth portion 212 of the gradedARC 204 having silicon oxide SiO2. The oxygen gas continues to flow after the flow of nitrogen gas stops. Beneficially, the gradual flow changes in nitrogen gas and oxygen gas prevents the plasma from being extinguished in theprocess chamber 100. As discussed above, the change in the composition of the gradedARC 204 from SiNxOy in thethird portion 210 to SiO2 in thefourth portion 212 is gradual, i.e., no distinct layers in each portion of the gradedARC 204. In one embodiment, an optional buffer laying having oxide or nitride may be deposited over the gradedARC 204 to form afilmstack 202 configured for a complementary metal-oxide-semiconductor (CMOS) image sensor device. - Advantageously, as the graded
ARC 204 has no distinct layers in each 206, 208, 210 and 212 of the gradedportion ARC 204, the refractive index of the graded ARC 204 (at about 633 nm) can be tuned from over about 2.0 to about 1.47. In one embodiment, as the flow of the oxygen reaches about 50 sccm, the refractive index of theARC 204 is tuned to about 1.47. For example, in one embodiment: (i) at about 0 sccm of oxygen gas, the gradedARC 204 has a refractive index between about 2.0 and about 2.5, for example, about 2.0 or about 2.1; (ii) at about 25 sccm of oxygen gas, the gradedARC 204 has a refractive index of between about 1.5 and about 2.0, for example about 1.75; (iii) at about 50 sccm of oxygen gas, the gradedARC 204 has a refractive index of between about 1.0 and about 1.5, for example about 1.47; (iv) at about 75 sccm of oxygen gas, the gradedARC 204 has a refractive index of between about 1.0 and about 1.5, for example about 1.48 or about 1.49; and (v) at about 100 sccm of oxygen gas, the gradedARC 204 has a refractive index of between about 1.0 and about 1.5, for example about 1.47. - Additionally, as the flow of the oxygen increases to about 100 sccm the graded
ARC 204 has a low compressive stress level, i.e., the stress of the gradedARC 204 is tunable with different levels of oxygen gas. For example, in one embodiment: (i) at about 0 sccm of oxygen gas, the gradedARC 204 has a stress level of −599 MPa; (ii) at about 25 sccm of oxygen gas, the gradedARC 204 has a stress level of −276 MPa; (iii) at about 50 sccm of oxygen gas, the gradedARC 204 has a stress level of −144 MPa; (iv) at about 75 sccm of oxygen gas, the gradedARC 204 has a stress level of −157 MPa; and (v) at about 100 sccm of oxygen gas, the gradedARC 204 has a stress level of −119 MPa. Therefore, the gradedARC 204 provides an ARC that gradually controls the refractive index of thefilmstack 202 without having to control the thickness of the gradedARC 204, and has low stress levels. - While the foregoing is directed to embodiments of the present invention, other and further embodiments of the invention may be devised without departing from the basic scope thereof, and the scope thereof is determined by the claims that follow.
Claims (14)
1. A filmstack comprising:
a substrate having a graded anti-reflective coating disposed thereon, wherein the graded anti-reflective coating comprises:
a first portion having first refractive index;
a second portion disposed on the first portion, the second portion having a second refractive index less than the first refractive index;
a third portion disposed on the second portion, the third portion having a third refractive index less than the second refractive index; and
a fourth portion disposed on the third portion, the fourth portion having a fourth refractive index less than third refractive index.
2. The filmstack of claim 1 , wherein the first portion comprises silicon, the second portion comprises silicon and nitrogen, the third portion comprises silicon, nitrogen and oxygen, and the fourth portion comprises silicon and oxygen.
3. The filmstack of claim 2 , wherein the graded anti-reflective coating has a graded refractive index ranging from about 1.46 to about 2.00.
4. The filmstack claim 1 , wherein the substrate includes a photodiode disposed thereon.
5. The filmstack of claim 1 , wherein the substrate includes a buffer layer comprising oxide or nitride disposed over the graded anti-reflective coating.
6. The film stack of claim 2 , wherein the filmstack is configured for use in a complementary metal-oxide-semiconductor image sensor device.
7. A graded anti-reflective coating comprising:
a substrate;
a first portion of the graded anti-reflective coating disposed on the substrate, the first portion having a first refractive index;
a second portion of the graded anti-reflective coating disposed on the first portion, the second portion having a second refractive index that is less than the first refractive index;
a third portion of the graded anti-reflective coating disposed on the second portion, the third portion having a third refractive index that is less than the second refractive index; and
a fourth portion of the graded anti-reflective coating disposed on the third portion, the fourth portion having a fourth refractive index that is less than the third refractive index,
wherein the anti-reflective coating has a tuned stress level.
8. The graded anti-reflective coating of claim 7 , wherein the stress level is tuned to between −v119 MPa and −599 MPa.
9. The graded anti-reflective coating of claim 7 , wherein there are no distinct transitions of refractive index between the first portion and the fourth portion of the graded anti-reflective coating.
10. The graded anti-reflective coating of claim 7 , wherein the first portion comprises silicon, the second portion comprises silicon and nitrogen, the third portion comprises silicon, nitrogen and oxygen, and the fourth portion comprises silicon and oxygen.
11. The graded anti-reflective coating of claim 10 , wherein the graded anti-reflective coating has a graded refractive index ranging from about 1.46 to about 2.00.
12. The graded anti-reflective coating of claim 7 , wherein the substrate includes a photodiode disposed thereon.
13. The graded anti-reflective coating of claim 7 , wherein the substrate includes a buffer layer comprising oxide or nitride disposed over the graded anti-reflective coating.
14. The graded anti-reflective coating of claim 10 , wherein the graded anti-reflective coating is configured for use in a complementary metal-oxide-semiconductor image sensor device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16/154,330 US20190051768A1 (en) | 2013-11-13 | 2018-10-08 | Method for graded anti-reflective coatings by physical vapor deposition |
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| Application Number | Priority Date | Filing Date | Title |
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| US201361887147P | 2013-11-13 | 2013-11-13 | |
| US201361904437P | 2013-11-14 | 2013-11-14 | |
| US14/531,549 US10096725B2 (en) | 2013-11-13 | 2014-11-03 | Method for graded anti-reflective coatings by physical vapor deposition |
| US16/154,330 US20190051768A1 (en) | 2013-11-13 | 2018-10-08 | Method for graded anti-reflective coatings by physical vapor deposition |
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| Application Number | Title | Priority Date | Filing Date |
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| US14/531,549 Division US10096725B2 (en) | 2013-11-13 | 2014-11-03 | Method for graded anti-reflective coatings by physical vapor deposition |
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| US20190051768A1 true US20190051768A1 (en) | 2019-02-14 |
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| US14/531,549 Expired - Fee Related US10096725B2 (en) | 2013-11-13 | 2014-11-03 | Method for graded anti-reflective coatings by physical vapor deposition |
| US16/154,330 Abandoned US20190051768A1 (en) | 2013-11-13 | 2018-10-08 | Method for graded anti-reflective coatings by physical vapor deposition |
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| US14/531,549 Expired - Fee Related US10096725B2 (en) | 2013-11-13 | 2014-11-03 | Method for graded anti-reflective coatings by physical vapor deposition |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| TWI639719B (en) * | 2016-11-21 | 2018-11-01 | 行政院原子能委員會核能研究所 | A direct current magnetron arc coating device and method thereof |
| US11520082B2 (en) | 2017-08-31 | 2022-12-06 | Corning Incorporated | Hybrid gradient-interference hardcoatings |
| US11630243B2 (en) | 2017-08-31 | 2023-04-18 | Corning Incorporated | Hybrid gradient-interference hardcoatings |
| WO2019162041A1 (en) * | 2018-02-26 | 2019-08-29 | Evatec Ag | Stabilizing stress in a layer with respect to thermal loading |
| CN110104957A (en) * | 2019-04-17 | 2019-08-09 | 信利光电股份有限公司 | A kind of anti-reflective film of wide bandwidth and preparation method thereof |
| CN116845115A (en) | 2021-09-06 | 2023-10-03 | 上海晶科绿能企业管理有限公司 | Solar cells and photovoltaic modules |
| JP2024056426A (en) * | 2022-10-11 | 2024-04-23 | 東京エレクトロン株式会社 | Mounting table and substrate processing apparatus |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| DE3726731A1 (en) * | 1987-08-11 | 1989-02-23 | Hartec Ges Fuer Hartstoffe Und | METHOD FOR APPLYING COATS TO OBJECTS BY MEANS OF MAGNETIC FIELD SUPPORTED CATHODE SPRAYING IN A VACUUM |
| US5234748A (en) * | 1991-06-19 | 1993-08-10 | Ford Motor Company | Anti-reflective transparent coating with gradient zone |
| US5651865A (en) * | 1994-06-17 | 1997-07-29 | Eni | Preferential sputtering of insulators from conductive targets |
| US6495251B1 (en) * | 1997-06-20 | 2002-12-17 | Ppg Industries Ohio, Inc. | Silicon oxynitride protective coatings |
| US8815059B2 (en) * | 2010-08-31 | 2014-08-26 | Guardian Industries Corp. | System and/or method for heat treating conductive coatings using wavelength-tuned infrared radiation |
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2014
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| US10096725B2 (en) | 2018-10-09 |
| US20150132551A1 (en) | 2015-05-14 |
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