US3459504A - Formation of carbide compounds by vapor deposition on graphite bodies - Google Patents
Formation of carbide compounds by vapor deposition on graphite bodies Download PDFInfo
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- US3459504A US3459504A US588578A US3459504DA US3459504A US 3459504 A US3459504 A US 3459504A US 588578 A US588578 A US 588578A US 3459504D A US3459504D A US 3459504DA US 3459504 A US3459504 A US 3459504A
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title description 35
- 229910002804 graphite Inorganic materials 0.000 title description 33
- 239000010439 graphite Substances 0.000 title description 33
- 150000001875 compounds Chemical class 0.000 title description 17
- 230000015572 biosynthetic process Effects 0.000 title description 6
- 238000007740 vapor deposition Methods 0.000 title description 3
- 229910052710 silicon Inorganic materials 0.000 description 38
- 239000010703 silicon Substances 0.000 description 38
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 33
- 238000000151 deposition Methods 0.000 description 19
- 230000008021 deposition Effects 0.000 description 18
- 229910052739 hydrogen Inorganic materials 0.000 description 17
- 239000001257 hydrogen Substances 0.000 description 17
- 238000000034 method Methods 0.000 description 17
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 14
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 13
- 229910010271 silicon carbide Inorganic materials 0.000 description 13
- VXEGSRKPIUDPQT-UHFFFAOYSA-N 4-[4-(4-methoxyphenyl)piperazin-1-yl]aniline Chemical compound C1=CC(OC)=CC=C1N1CCN(C=2C=CC(N)=CC=2)CC1 VXEGSRKPIUDPQT-UHFFFAOYSA-N 0.000 description 11
- 239000005049 silicon tetrachloride Substances 0.000 description 11
- 239000007789 gas Substances 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 8
- 239000000203 mixture Substances 0.000 description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 5
- 239000000460 chlorine Substances 0.000 description 5
- 229910052804 chromium Inorganic materials 0.000 description 5
- 239000011651 chromium Substances 0.000 description 5
- BUMGIEFFCMBQDG-UHFFFAOYSA-N dichlorosilicon Chemical compound Cl[Si]Cl BUMGIEFFCMBQDG-UHFFFAOYSA-N 0.000 description 5
- 230000003028 elevating effect Effects 0.000 description 5
- 150000004820 halides Chemical class 0.000 description 5
- -1 silicon halide Chemical class 0.000 description 5
- 229910052719 titanium Inorganic materials 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- 229910052720 vanadium Inorganic materials 0.000 description 5
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 5
- 229910052726 zirconium Inorganic materials 0.000 description 5
- 238000001764 infiltration Methods 0.000 description 4
- 230000008595 infiltration Effects 0.000 description 4
- 239000004744 fabric Substances 0.000 description 3
- 239000008246 gaseous mixture Substances 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 2
- 229910052801 chlorine Inorganic materials 0.000 description 2
- KBDJQNUZLNUGDS-UHFFFAOYSA-N dibromosilicon Chemical compound Br[Si]Br KBDJQNUZLNUGDS-UHFFFAOYSA-N 0.000 description 2
- MROCJMGDEKINLD-UHFFFAOYSA-N dichlorosilane Chemical compound Cl[SiH2]Cl MROCJMGDEKINLD-UHFFFAOYSA-N 0.000 description 2
- 229910052736 halogen Inorganic materials 0.000 description 2
- 150000002367 halogens Chemical group 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- AIFMYMZGQVTROK-UHFFFAOYSA-N silicon tetrabromide Chemical compound Br[Si](Br)(Br)Br AIFMYMZGQVTROK-UHFFFAOYSA-N 0.000 description 2
- ZDHXKXAHOVTTAH-UHFFFAOYSA-N trichlorosilane Chemical compound Cl[SiH](Cl)Cl ZDHXKXAHOVTTAH-UHFFFAOYSA-N 0.000 description 2
- 239000005052 trichlorosilane Substances 0.000 description 2
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 241000244423 Pteris cretica Species 0.000 description 1
- GDTBXPJZTBHREO-UHFFFAOYSA-N bromine Substances BrBr GDTBXPJZTBHREO-UHFFFAOYSA-N 0.000 description 1
- 229910052794 bromium Inorganic materials 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- SLLGVCUQYRMELA-UHFFFAOYSA-N chlorosilicon Chemical compound Cl[Si] SLLGVCUQYRMELA-UHFFFAOYSA-N 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- VJIYRPVGAZXYBD-UHFFFAOYSA-N dibromosilane Chemical compound Br[SiH2]Br VJIYRPVGAZXYBD-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 125000005843 halogen group Chemical group 0.000 description 1
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 1
- 229910000039 hydrogen halide Inorganic materials 0.000 description 1
- 239000012433 hydrogen halide Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 108090000623 proteins and genes Proteins 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 150000003377 silicon compounds Chemical class 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- ABTOQLMXBSRXSM-UHFFFAOYSA-N silicon tetrafluoride Chemical class F[Si](F)(F)F ABTOQLMXBSRXSM-UHFFFAOYSA-N 0.000 description 1
- CFTHARXEQHJSEH-UHFFFAOYSA-N silicon tetraiodide Chemical class I[Si](I)(I)I CFTHARXEQHJSEH-UHFFFAOYSA-N 0.000 description 1
- XUGSDIOYQBRKGF-UHFFFAOYSA-N silicon;hydrochloride Chemical compound [Si].Cl XUGSDIOYQBRKGF-UHFFFAOYSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- IBOKZQNMFSHYNQ-UHFFFAOYSA-N tribromosilane Chemical compound Br[SiH](Br)Br IBOKZQNMFSHYNQ-UHFFFAOYSA-N 0.000 description 1
- 238000001947 vapour-phase growth Methods 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B32/00—Carbon; Compounds thereof
- C01B32/90—Carbides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/50—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
- C04B41/5053—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials non-oxide ceramics
- C04B41/5057—Carbides
- C04B41/5059—Silicon carbide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
- C04B41/87—Ceramics
-
- 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
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
Definitions
- FIG. 2 RONALD C. BRACKEN RALPH F. STROUP GENE F. WAKEFIELD ATTORNEY GAS INLET FIG. 2
- This invention relates to a process for the formation of carbide compounds, and more particularly, but not by way of limitation, to the formation of such carbide compounds by deposition and infiltration of an element onto and into a graphite body with which it is to be reacted.
- carbide compounds such as silicon carbide which has a Mohs scale hardness of 9, has made them useful where wear resistant properties have been desired.
- Conventional methods for preparing carbide compounds, and in particular silicon carbide leave rather crudely formed bodies. When a silicon carbide body having relatively precise dimensions is needed, a crudely formed silicon carbide body must be machined to desired tolerance. Due to the hardness of compounds, machining is very time consuming and expensive.
- the present invention is particularly adapted to the forming of carbide compounds from a pre-shaped and machined body, the shaping and machining of which may be done relatively simply and cheaply.
- Such a use of the method of this invention is but illustrative, and other uses are contemplated.
- the invention may be generally described as a method including the steps of heating a graphite body to a temperature between 900 C. and 1300 C. and passing over the body, while maintained between 900 C. and 1300 C., a gaseous deposition mixture of YH X and hydrogen for sufficient time to form a layer of Y on said body, and elevating the temperature of said body to a temperature greater than 1430 C. and less than 1900 C. for permitting the Y layer to penetrate and react with the body, where:
- Y is selected from the group consisting of silicon, chromium, titanium, zirconium and vanadium, and
- X is a halogen
- FIGURE 1 is a schematic diagram of suitable apparatus for carrying out the invention
- FIGURE 2 is an enlarged diagrammatic illustration of the reactor of FIGURE 1;
- FIGURE 3 is a partial cutaway view in elevation of alternative apparatus for heating and suspending a body.
- FIGURE 1 hydrogen (H is introduced through adjustable valve 3 into a deoxygenizing purifier 4. From purifier 4, the hydrogen passes through volumetric measuring flow meter 5. From flow meter 5, the hydrogen discharges into and proximates the bottom of saturator 6. The upper portion of saturator 6 communicates through conduit 7 with the bottom of reactor 8. The top of reactor 8 communicates through conduit 9, to which a pressure gauge 10 is connected, with a manostat 11 which exhausts to the atmosphere.
- reactor 8 may comprise a gas tight chamber 12, within which are supported electrodes 13 and 14 externally connected to an alternating current power source 15. Between electrodes 13 and 14 is supported a body 16, about which a gas entering chamber 12 through conduit 7 and exiting chamber 12 through conduit 9 will circulate.
- the equipment may be constructed of quartz, a mild steel or the like which is unreactive in the presence of the halides mentioned above and hydrogen.
- Example 1 The equipment illustrated in FIGURES l and 2 was utilized. A graphite bar having a density of 1.6 gms./cm. was suspended between electrodes 13 and 14. The graphite body was thick, 1" wide and 5" long. The body was raised to about 1000 C. by impressing a 15 volt potential across electrodes 13 and 14, at which voltage the specimen drew 300 amperes of 60 cycles/ sec. current. About 7.5 liters/min. of hydrogen was bubbled through saturator 6 which was filled with silicon tetrachloride.
- Manostat 11 was set to maintain the pressure in reactor 8 at atmospheric.
- gas flow through chamber 12 was terminated.
- the temperature of the graphite body was then raised to about 1430 C. and maintained at this temperature for 10 minutes during which the silicon layer melted, infiltrated the graphite body and reacted therewith to form silicon carbide.
- deposition of the silicon layer on the graphite body is preferably done between about 900 C. and 1300 C., and the mole ratio of hydrogen to silicon tetrachloride is maintained within the range over which deposition of silicon will occur.
- the desired mole ratio of hydrogen to silicon tetrachloride for a given temperature-pressure system can easily be determined by use of published silicon-hydrogen-chloride equilibrium data, familiar to those skilled in the art. One such set of data may be found in Lever, The Equilibrium Behavior of the Silicon-Hydrogen-Chlorine System, p. 460, IBM Journal (September 1964).
- silicon tetrachloride is a preferred source of silicon
- the deposition of silicon can be effected by use of a silicon halide which term is used to include silicon-hydrogen-halide compounds.
- silicon fluorides which term is used to include silicon-hydrogen-fiuorine compounds
- silicon iodides which term is used to include silicon-hydrogen-iodine compounds
- the preferred silicon halides include trichlorosilane (SiHCl dichlorosilane (SiH C1 silicon dichloride (SiCl silicon tetrabromide (siBr tribromosilane (SiH Br), dibromosilane (SiH Br and silicon dibromide.
- Silicon dibromide and silicon dichloride only exist at higher temperatures and may be used to obtain faster deposition of silicon than obtainable with the other mentioned silicon bromides and chlorides (which terms are used to include silicon-hydrogen-bromine and silicon-hydrogen-chlorine compounds, respectively).
- Example 2 For faster deposition, the equipment described above may be employed, but a bed of silicon heated to about 800 C. is interposed between the saturator 6 and reactor 8. The gaseous mixture of silicon tetrachloride and hydrogen is passed through the bed and due to the unbalanced equilibrium of the system, silicon is etched from the bed forming a gaseous stream containing hydrogen and silicon dichloride. Upon introduction of the gas stream into the higher temperature zone of the reactor, approximately 1200 C., the equilibrium will again be imbalanced causing deposition of silicon on the graphite body. The exit gases, being depleted in silicon, may be recycled over the silicon bed and replenished in silicon. Thus enriched, the gas mixture can be used as feed gas. This procedure serves to lessen the net consumption of hydrogen and halide. After deposition of silicon for approximately 25 minutes, the gas flow may be terminated and the temperature raised to approximately 1430 C. for 10 minutes to permit infiltration of the silicon and reaction between the silicon and graphite.
- Infiltration and reaction between the silicon and graphite is preferably carried out at a temperature between l430 C. and 1850 C.
- the time required to deposit a desired layer of silicon on a given graphite body will vary with the dimensions of the body, the temperature of the deposition and the amount of hydrogen and silicon halide being circulated through the reactor, all of which will be appreciated by those skilled in the art. Also, the time at which the body, after deposition, is maintained at the elevated temperature will depend upon the dimensions of the body and the degree of infiltration desired.
- a relatively soft graphite body premachined to a desired shape, may be converted to a silicon carbide body having the desired shape, thus eliminating the costly machining of a silicon carbide blank.
- a graphite body such as solid cylindrical shaped graphite body 16 may be supported at three points by a base 17 or the like and radiantly heated by a cylindrical slotted graphite heater 18.
- Heater 18 is connected by electrodes 1'9 and 20 across a suitable power source, not illustrated.
- the structure illustrated in FIGURE 3 would of course be supported in a reactor body, such as illustrated in FIG- URE 2, to permit circulation of a gaseous deposition mixture therearound and may be used in lieu of the resistance heating technique used in the FIGURE 2 reactor.
- Other heating techniques such as radio frequency inductive heat- 5 ing and radiative heating from other sources can also be employed.
- a graphite cloth may be formed into a desired shape such as a cone, cylinder, ring or the like and placed in a suitable reaction chamber. Silicon may be deposited thereon and reacted therewith to produce a relatively rigid silicon carbide body having much greater strength and hardness than bodies formed by bonding graphite yarns together with elemental carbon. With the flexibility permitted by graphite cloth and the like, an almost infinite number of silicon carbide bodies of differing shapes and physical characteristics could be formed by use of the present invention.
- X is a halogen
- the subscript b is an integer representing the number of halogen atoms needed to form the compound, and the subscript a is an integer designating the number of hydrogen atoms in the molecule;
- Y H X is silicon tetrachloride.
- YI-I,,X is trichlorosilane.
- YH X is dichlorosilane. 5.
- a method for forming silicon carbide comprising the steps of:
- a method for forming silicon carbide comprising the steps of:
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Description
Aug. 5, 1969 R. c. BRACKEN ET AL 3,459,504
FORMATION OF CARBIDE COMPOUNDS BY VAPOR DEPOSITION ON GRAPHITE BODIES Filed om. 21, 1966 G I PRESSURE GUAGE l 7 5 REACTOR I I .7- 6 EXHAUST H2 PURIFIER 3 SATURATOR MANOSTAT EXHAUST I l I a I6 H INVENTORS:
RONALD C. BRACKEN RALPH F. STROUP GENE F. WAKEFIELD ATTORNEY GAS INLET FIG. 2
United States Patent 3,459,504 FORMATION OF CARBIDE COMPOUNDS BY VAPOR DEPOSITION ON GRAPHITE BODIES Ronald C. Bracken, Richardson, Ralph F. Stroup, Dallas,
and Gene F. Wakefield, Richardson, Tex., assignors to Texas Instruments Incorporated, Dallas, Tex., a corporation of Delaware Continuation-impart of application Ser. No. 565,606,
July 15, 1966. This application Oct. 21, 1966, Ser.
Int. Cl. C01b 31/30 U.S. Cl. 23208 7 Claims ABSTRACT OF THE DISCLOSURE A process for forming carbide compounds by heating a graphite body to an elevated temperature, passing a decomposable gaseous mixture of hydrogen and a compound of the element to be deposited over the graphite body, and subsequently elevating the temperature of the graphite body in order to effect penetration and conversion of the deposited element to a carbide of that element.
This application is a continuation-in-part of application Ser. No. 565,606, filed July 15, 1966, now abandoned, for Formation of Silicon Compounds.
This invention relates to a process for the formation of carbide compounds, and more particularly, but not by way of limitation, to the formation of such carbide compounds by deposition and infiltration of an element onto and into a graphite body with which it is to be reacted.
The hardness of carbide compounds, such as silicon carbide which has a Mohs scale hardness of 9, has made them useful where wear resistant properties have been desired. Conventional methods for preparing carbide compounds, and in particular silicon carbide, leave rather crudely formed bodies. When a silicon carbide body having relatively precise dimensions is needed, a crudely formed silicon carbide body must be machined to desired tolerance. Due to the hardness of compounds, machining is very time consuming and expensive.
The present invention is particularly adapted to the forming of carbide compounds from a pre-shaped and machined body, the shaping and machining of which may be done relatively simply and cheaply. Such a use of the method of this invention is but illustrative, and other uses are contemplated.
The invention may be generally described as a method including the steps of heating a graphite body to a temperature between 900 C. and 1300 C. and passing over the body, while maintained between 900 C. and 1300 C., a gaseous deposition mixture of YH X and hydrogen for sufficient time to form a layer of Y on said body, and elevating the temperature of said body to a temperature greater than 1430 C. and less than 1900 C. for permitting the Y layer to penetrate and react with the body, where:
Y is selected from the group consisting of silicon, chromium, titanium, zirconium and vanadium, and
X is a halogen.
When Y is silicon, the integers a-l-b=4. These integers can assume any value between zero and four subject to the above condition. When Y is titanium, zirconium, chromium or vanadium, 12:0 and b assumes a value compatible with the valence of the metallic element in the compound.
To be more specific, reference is here made to the drawings, in which:
FIGURE 1 is a schematic diagram of suitable apparatus for carrying out the invention;
"ace
FIGURE 2 is an enlarged diagrammatic illustration of the reactor of FIGURE 1; and
FIGURE 3 is a partial cutaway view in elevation of alternative apparatus for heating and suspending a body.
In FIGURE 1, hydrogen (H is introduced through adjustable valve 3 into a deoxygenizing purifier 4. From purifier 4, the hydrogen passes through volumetric measuring flow meter 5. From flow meter 5, the hydrogen discharges into and proximates the bottom of saturator 6. The upper portion of saturator 6 communicates through conduit 7 with the bottom of reactor 8. The top of reactor 8 communicates through conduit 9, to which a pressure gauge 10 is connected, with a manostat 11 which exhausts to the atmosphere.
As illustrated in FIGURE 2, reactor 8 may comprise a gas tight chamber 12, within which are supported electrodes 13 and 14 externally connected to an alternating current power source 15. Between electrodes 13 and 14 is supported a body 16, about which a gas entering chamber 12 through conduit 7 and exiting chamber 12 through conduit 9 will circulate. The equipment may be constructed of quartz, a mild steel or the like which is unreactive in the presence of the halides mentioned above and hydrogen.
An understanding of the inventive method may be gained by consideration of the following examples.
Example 1 The equipment illustrated in FIGURES l and 2 was utilized. A graphite bar having a density of 1.6 gms./cm. was suspended between electrodes 13 and 14. The graphite body was thick, 1" wide and 5" long. The body was raised to about 1000 C. by impressing a 15 volt potential across electrodes 13 and 14, at which voltage the specimen drew 300 amperes of 60 cycles/ sec. current. About 7.5 liters/min. of hydrogen was bubbled through saturator 6 which was filled with silicon tetrachloride. The gaseous mixture of silicon tetrachloride and hydrogen, which contained about 59 mole percent silicon tetrachloride, was circulated through reactor 8 for 45 minutes to form alayer of silicon on the graphite body which was maintained at approximately 1000C. during the deposition. Manostat 11 was set to maintain the pressure in reactor 8 at atmospheric.
After the expiration of 30 minutes, gas flow through chamber 12 was terminated. The temperature of the graphite body was then raised to about 1430 C. and maintained at this temperature for 10 minutes during which the silicon layer melted, infiltrated the graphite body and reacted therewith to form silicon carbide.
It has been determined that deposition of the silicon layer on the graphite body is preferably done between about 900 C. and 1300 C., and the mole ratio of hydrogen to silicon tetrachloride is maintained within the range over which deposition of silicon will occur. The desired mole ratio of hydrogen to silicon tetrachloride for a given temperature-pressure system can easily be determined by use of published silicon-hydrogen-chloride equilibrium data, familiar to those skilled in the art. One such set of data may be found in Lever, The Equilibrium Behavior of the Silicon-Hydrogen-Chlorine System, p. 460, IBM Journal (September 1964).
While silicon tetrachloride is a preferred source of silicon, the deposition of silicon can be effected by use of a silicon halide which term is used to include silicon-hydrogen-halide compounds.
While silicon fluorides (which term is used to include silicon-hydrogen-fiuorine compounds) may be used, they are not preferred because of their low heat of reaction. Also, silicon iodides (which term is used to include silicon-hydrogen-iodine compounds) may be used, but are not preferred because of their low vapor pressure. Other than silicon tetrachloride, the preferred silicon halides include trichlorosilane (SiHCl dichlorosilane (SiH C1 silicon dichloride (SiCl silicon tetrabromide (siBr tribromosilane (SiH Br), dibromosilane (SiH Br and silicon dibromide. Silicon dibromide and silicon dichloride only exist at higher temperatures and may be used to obtain faster deposition of silicon than obtainable with the other mentioned silicon bromides and chlorides (which terms are used to include silicon-hydrogen-bromine and silicon-hydrogen-chlorine compounds, respectively).
Example 2 For faster deposition, the equipment described above may be employed, but a bed of silicon heated to about 800 C. is interposed between the saturator 6 and reactor 8. The gaseous mixture of silicon tetrachloride and hydrogen is passed through the bed and due to the unbalanced equilibrium of the system, silicon is etched from the bed forming a gaseous stream containing hydrogen and silicon dichloride. Upon introduction of the gas stream into the higher temperature zone of the reactor, approximately 1200 C., the equilibrium will again be imbalanced causing deposition of silicon on the graphite body. The exit gases, being depleted in silicon, may be recycled over the silicon bed and replenished in silicon. Thus enriched, the gas mixture can be used as feed gas. This procedure serves to lessen the net consumption of hydrogen and halide. After deposition of silicon for approximately 25 minutes, the gas flow may be terminated and the temperature raised to approximately 1430 C. for 10 minutes to permit infiltration of the silicon and reaction between the silicon and graphite.
Infiltration and reaction between the silicon and graphite is preferably carried out at a temperature between l430 C. and 1850 C.
The time required to deposit a desired layer of silicon on a given graphite body will vary with the dimensions of the body, the temperature of the deposition and the amount of hydrogen and silicon halide being circulated through the reactor, all of which will be appreciated by those skilled in the art. Also, the time at which the body, after deposition, is maintained at the elevated temperature will depend upon the dimensions of the body and the degree of infiltration desired.
By use of the above described method, a relatively soft graphite body, premachined to a desired shape, may be converted to a silicon carbide body having the desired shape, thus eliminating the costly machining of a silicon carbide blank.
While deposition of silicon from a silicon halide is used in the above examples, there may be substituted a halide of chromium, titanium, zirconium and vanadium. The equilibrium data for these halides may be easily calculated by techniques such as those used by Lever, The Equilibrium Behavior of the Silicon-Hydrogen-Chlorine System, p. 460, IBM Journal (September 1964). The various halides may be generally identified by formula:
YH X
When Y is silicon, the integers a+b=4. These integers can assume any value between zero and four subject to the above condition. When Y is titanium, zirconium, chromium or vanadium, 11:0 and [2 assumes a value compatible with the valence of the metallic element in the compound.
Additionally, as indicated by FIGURE 3, a graphite body such as solid cylindrical shaped graphite body 16 may be supported at three points by a base 17 or the like and radiantly heated by a cylindrical slotted graphite heater 18. Heater 18 is connected by electrodes 1'9 and 20 across a suitable power source, not illustrated. The structure illustrated in FIGURE 3 would of course be supported in a reactor body, such as illustrated in FIG- URE 2, to permit circulation of a gaseous deposition mixture therearound and may be used in lieu of the resistance heating technique used in the FIGURE 2 reactor. Other heating techniques such as radio frequency inductive heat- 5 ing and radiative heating from other sources can also be employed.
While the invention has been described in connection with a rigid graphite body, it can be used as well to bond layers of a flexible graphite or carbon yarn, cloth or rope. for example, a graphite cloth may be formed into a desired shape such as a cone, cylinder, ring or the like and placed in a suitable reaction chamber. Silicon may be deposited thereon and reacted therewith to produce a relatively rigid silicon carbide body having much greater strength and hardness than bodies formed by bonding graphite yarns together with elemental carbon. With the flexibility permitted by graphite cloth and the like, an almost infinite number of silicon carbide bodies of differing shapes and physical characteristics could be formed by use of the present invention.
While rather specific terms have been used in describing the embodiment of the invention, they are not intended, nor should they be construed, as a limitation on the invention as defined by the claims.
What is claimed is: 1. A method for forming carbide compounds, com, prising the steps of:
heating a graphite body to a temperature between 900 C. and 1300 C.;
passing over said body, while said body is maintained between 900 C. and 1300 C., a gaseous deposition mixture of H and YH X for sufiicient time to form a layer of Y on said body, wherein Y is an element selected from the class consisting of silicon, chromium, titanium, zirconium, and vanadium;
X is a halogen;
the subscript b is an integer representing the number of halogen atoms needed to form the compound, and the subscript a is an integer designating the number of hydrogen atoms in the molecule; and
elevating the temperature of said body to a temperature greater than 1430 C. and less than 1850 C. for permitting said Y layer to penetrate and react with said body, to form a carbide of said element. 2. The method of claim 1, wherein: Y H X is silicon tetrachloride. 3. The method of claim 1, wherein: YI-I,,X is trichlorosilane. 4. The method of claim 1, wherein: YH X is dichlorosilane. 5. A method for forming silicon carbide, comprising the steps of:
heating a graphite body to a temperature of about passing over said body, while said body is maintained at about 1000 C., a gaseous deposition mixture of a silicon halide and hydrogen for sufficient time to form a layer of silicon on said body; and
elevating the temperature of said body to a tempera- 60 ture of about 1430 C. for permitting said silicon layer to penetrate and react with said body to form silicon carbide on the surfaces of and within said body. 6. A method for forming silicon carbide, comprising the steps of:
passing into a heated bed of silicon a gaseous etching mixture of a silicon tetrachloride and hydrogen for forming silicon dichloride which is Capable of silicon deposition at temperatures between 900 C. and 1300 C.;
passing said silicon dichloride over a graphite body maintained between 900 C. and 1300 C. for depositing a layer of silicon on said graphite body; and
elevating the temperature of said graphite body after deposition of said layer of silicon to a temperature greater than 1430 C. and less than 1850 C. for permitting said silicon layer to penetrate and react with said graphite body to form silicon carbide on the surface of and within said body.
7. The method of claim 6, wherein the temperature of said silicon bed is about 800 C. and the mole fraction percentage of silicon tetrachloride in said silicon tetrachloride-hydrogen stream is between 5 and 9.
References Cited UNITED 6 FOREIGN PATENTS 397,372 8/1933 Great Britain. 636,472 2/ 1962 Canada.
5 OTHER REFERENCES Campbell et al.: The Vapor-Phase Deposition of Refractory Materials, Transactions of the Electrochemical Society, vol. 96, November 1949, pp. 325 and 326.
10 OSCAR R. VERTIZ, Primary Examiner G. T. OZAKI, Assistant Examiner US. Cl. X.R.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US58857866A | 1966-10-21 | 1966-10-21 |
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| Publication Number | Publication Date |
|---|---|
| US3459504A true US3459504A (en) | 1969-08-05 |
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| Application Number | Title | Priority Date | Filing Date |
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| US588578A Expired - Lifetime US3459504A (en) | 1966-10-21 | 1966-10-21 | Formation of carbide compounds by vapor deposition on graphite bodies |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3804664A (en) * | 1970-09-24 | 1974-04-16 | Japan Atomic Energy Res Inst | Process for chemical vapor deposition of zirconium carbide |
| US3925577A (en) * | 1972-11-24 | 1975-12-09 | Westinghouse Electric Corp | Silicon carbide coated graphite members and process for producing the same |
| US3927181A (en) * | 1972-07-06 | 1975-12-16 | Toyota Motor Co Ltd | Process for preparing hollow balls of silicon carbide and product formed thereby |
| US3969131A (en) * | 1972-07-24 | 1976-07-13 | Westinghouse Electric Corporation | Coated graphite members and process for producing the same |
| US4029844A (en) * | 1973-04-24 | 1977-06-14 | Atlantic Research Corporation | Rocket nozzle comprising pyrolytic graphite-silicon carbide inserts |
| US4131697A (en) * | 1973-06-15 | 1978-12-26 | Association Pour La Recherches Et Le Developpement Des Methodes Et Processus Industriels | Method of coating carbon filaments with silicon carbide |
| US4253863A (en) * | 1977-06-07 | 1981-03-03 | International Telephone And Telegraph Corporation | Apparatus for mass producing fiber optic preforms and optic fibers |
| US4265843A (en) * | 1978-12-04 | 1981-05-05 | Kernforschungsanlage Julich Gesellschaft Mit Berschrankter Haftung | Method of producing shaped silicon-carbide bodies |
| US4276072A (en) * | 1977-06-07 | 1981-06-30 | International Telephone And Telegraph Corporation | Optical fiber fabrication |
| US4424193A (en) | 1979-07-09 | 1984-01-03 | Toshiba Ceramics Co., Ltd. | Constituent members of a semiconductor element-manufacturing apparatus and a reaction furnace for making said constituent members |
| US4668583A (en) * | 1984-04-13 | 1987-05-26 | Hi-Shear Corporation | Refractory coating |
| US4921725A (en) * | 1986-12-04 | 1990-05-01 | Centre National De La Recherche Scientifique (Cnrs) | Process for coating carbon fibers with a carbide |
| US20070073075A1 (en) * | 2005-09-29 | 2007-03-29 | Wacker Chemie Ag | Process and apparatus for the hydrogenation of chlorosilanes |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1018502A (en) * | 1905-07-06 | 1912-02-27 | Gen Electric | Incandescent bodies for electric lamps. |
| GB397372A (en) * | 1932-01-29 | 1933-08-24 | Philips Nv | Improvements in the winning of highly refractory carbides |
| CA636472A (en) * | 1962-02-13 | Enk Eduard | Process for the production of shaped bodies of silicon carbide | |
| US3205042A (en) * | 1961-10-17 | 1965-09-07 | Du Pont | Fluidized process for producing carbides |
| US3253886A (en) * | 1961-05-09 | 1966-05-31 | Union Carbide Corp | Process for producing ultrafine powders of refractory materials |
| US3269802A (en) * | 1962-12-10 | 1966-08-30 | Horizons Inc | Preparation of carbide structures |
| US3346678A (en) * | 1963-09-30 | 1967-10-10 | Harold A Ohlgren | Process for preparing carbon articles |
-
1966
- 1966-10-21 US US588578A patent/US3459504A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA636472A (en) * | 1962-02-13 | Enk Eduard | Process for the production of shaped bodies of silicon carbide | |
| US1018502A (en) * | 1905-07-06 | 1912-02-27 | Gen Electric | Incandescent bodies for electric lamps. |
| GB397372A (en) * | 1932-01-29 | 1933-08-24 | Philips Nv | Improvements in the winning of highly refractory carbides |
| US3253886A (en) * | 1961-05-09 | 1966-05-31 | Union Carbide Corp | Process for producing ultrafine powders of refractory materials |
| US3205042A (en) * | 1961-10-17 | 1965-09-07 | Du Pont | Fluidized process for producing carbides |
| US3269802A (en) * | 1962-12-10 | 1966-08-30 | Horizons Inc | Preparation of carbide structures |
| US3346678A (en) * | 1963-09-30 | 1967-10-10 | Harold A Ohlgren | Process for preparing carbon articles |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3804664A (en) * | 1970-09-24 | 1974-04-16 | Japan Atomic Energy Res Inst | Process for chemical vapor deposition of zirconium carbide |
| US3927181A (en) * | 1972-07-06 | 1975-12-16 | Toyota Motor Co Ltd | Process for preparing hollow balls of silicon carbide and product formed thereby |
| US3969131A (en) * | 1972-07-24 | 1976-07-13 | Westinghouse Electric Corporation | Coated graphite members and process for producing the same |
| US3925577A (en) * | 1972-11-24 | 1975-12-09 | Westinghouse Electric Corp | Silicon carbide coated graphite members and process for producing the same |
| US4029844A (en) * | 1973-04-24 | 1977-06-14 | Atlantic Research Corporation | Rocket nozzle comprising pyrolytic graphite-silicon carbide inserts |
| US4131697A (en) * | 1973-06-15 | 1978-12-26 | Association Pour La Recherches Et Le Developpement Des Methodes Et Processus Industriels | Method of coating carbon filaments with silicon carbide |
| US4276072A (en) * | 1977-06-07 | 1981-06-30 | International Telephone And Telegraph Corporation | Optical fiber fabrication |
| US4253863A (en) * | 1977-06-07 | 1981-03-03 | International Telephone And Telegraph Corporation | Apparatus for mass producing fiber optic preforms and optic fibers |
| US4265843A (en) * | 1978-12-04 | 1981-05-05 | Kernforschungsanlage Julich Gesellschaft Mit Berschrankter Haftung | Method of producing shaped silicon-carbide bodies |
| US4424193A (en) | 1979-07-09 | 1984-01-03 | Toshiba Ceramics Co., Ltd. | Constituent members of a semiconductor element-manufacturing apparatus and a reaction furnace for making said constituent members |
| US4624735A (en) * | 1979-07-09 | 1986-11-25 | Toshiba Ceramics Co., Ltd. | Constituent members of a semiconductor element-manufacturing apparatus and a reaction furnace for making said constituent members |
| US4668583A (en) * | 1984-04-13 | 1987-05-26 | Hi-Shear Corporation | Refractory coating |
| US4921725A (en) * | 1986-12-04 | 1990-05-01 | Centre National De La Recherche Scientifique (Cnrs) | Process for coating carbon fibers with a carbide |
| US20070073075A1 (en) * | 2005-09-29 | 2007-03-29 | Wacker Chemie Ag | Process and apparatus for the hydrogenation of chlorosilanes |
| JP2007091587A (en) * | 2005-09-29 | 2007-04-12 | Wacker Chemie Ag | Method and apparatus for hydrogenating chlorosilane |
| US7442824B2 (en) | 2005-09-29 | 2008-10-28 | Wacker Chemie Ag | Process and apparatus for the hydrogenation of chlorosilanes |
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