US3200009A - Method of producing hyperpure silicon - Google Patents
Method of producing hyperpure silicon Download PDFInfo
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- US3200009A US3200009A US165455A US16545562A US3200009A US 3200009 A US3200009 A US 3200009A US 165455 A US165455 A US 165455A US 16545562 A US16545562 A US 16545562A US 3200009 A US3200009 A US 3200009A
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- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
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- 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
- C01B32/914—Carbides of single elements
- C01B32/956—Silicon carbide
- C01B32/963—Preparation from compounds containing silicon
- C01B32/977—Preparation from organic compounds containing silicon
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- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B33/00—Silicon; Compounds thereof
- C01B33/02—Silicon
- C01B33/021—Preparation
- C01B33/027—Preparation by decomposition or reduction of gaseous or vaporised silicon compounds other than silica or silica-containing material
- C01B33/035—Preparation by decomposition or reduction of gaseous or vaporised silicon compounds other than silica or silica-containing material by decomposition or reduction of gaseous or vaporised silicon compounds in the presence of heated filaments of silicon, carbon or a refractory metal, e.g. tantalum or tungsten, or in the presence of heated silicon rods on which the formed silicon is deposited, a silicon rod being obtained, e.g. Siemens process
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B41/00—Obtaining germanium
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- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
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- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
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- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/46—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for heating the substrate
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- 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
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
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- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B25/00—Single-crystal growth by chemical reaction of reactive gases, e.g. chemical vapour-deposition growth
- C30B25/02—Epitaxial-layer growth
- C30B25/14—Feed and outlet means for the gases; Modifying the flow of the reactive gases
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L21/00—Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
Definitions
- the inlet for the gaseous reaction mixture in such devices is located on or in the base structure carrying the holders for the core rods.
- the gas inlet has a nozzle-shaped design so that the fresh gas mixture is caused to flow from the location of the core-rod holders along the core rods in the longitudinal direction of the rods.
- the semiconductor material has a uniform thickness over the entire length of the core rods during the processing period. This is of advantage particularly for a m'onocrystalline growth of the semiconductor material being precipitated, because such a monocrystalline rod can be sawed or cut, without further fabrication, into a multiplicity of discs or wafers all having the same size and thus being all suitable as monocrystalline base bodies for electronic semiconductor devices of a great variety of types.
- the economy of operation becomes appreciably impaired if the gas-entering speed becomes too small, and that the speed range within which the desired improvement is achieved is substantially between 100 and 200 m./sec. Maintaining the gas-entering speed below about 200 m./sec. has
- the additional advantage of preventing breakage of equipment for example of a quartz bell forming the upper portion of the hermetically sealed vessel structure, or lifting of the quartz bell from the mounting base constituting the bottom wall of the reaction chamber, in the event of a high-pressure gas build-up in the reaction space, caused by clouding or narrowing of the gas outlet.
- FIG. 1 shows schematically and partly in section an apparatus for the production of hyperpure silicon
- FIG. 2 shows separately an inlet nozzle for the gaseous reaction mixture which forms part of the apparatus according to FIG. 1.
- hydrogen to be employed as carrier and reaction gas
- a gas bottle 2 through a shut-off valve 3 and a plural-stage pressurereduction valve 4 from which the gas passes through a gas-flow meter 5 to an evaporator 6.
- a liquid semiconductor compound preferably silicochloroform SiHCl or silicon tetrachloride SiC1 is evaporated.
- the hydrogen becomes mixed with the evaporated silicon compound, such as silico-chloroform, and passes through a gas pipe 7 to a nozzle-type inlet device 8 and thence into the reaction space.
- the inlet nozzle 8 may have an inner diameter of about 2 mm.
- the rods for example and is designed to produce a turbulent How of gas along core rods 10 of hyperpure silicon.
- the rods for example, have a thickness of 3 mm. and a length of about 400 mm.
- the rods 10 are mounted in a reaction vessel comprising an hermetically sealed quartz cylinder or bell 11 whose inner diameter, for example, is approximately mm., and whose height, for example, is approximately 550 mm. It will be understood that the numerical values here given are properly correlated to one another, but may be modified in accordance with the requirements or desiderata of a particular method or apparatus.
- the bottom of the reaction chamber is closed by a metallic base plate 12, which is hollow and preferably cooled in its interior by a flowing or circulating coolant.
- the lower ends of the two rods 10 are inserted in respective bores of holders 14 consisting, for example of spectral carbon which in turn are fastened in cylindrical supports 15, inserted into the base plate 12, for example, by having a screw thread in engagement with threaded bores of the base plate 12.
- holders 14 consisting, for example of spectral carbon which in turn are fastened in cylindrical supports 15, inserted into the base plate 12, for example, by having a screw thread in engagement with threaded bores of the base plate 12.
- At least one of the cylindrical bodies 15 is insulated from the base plate 12 by an insulating sleeve 16.
- the cylindrical bodies 15 are connected to terminals 9 to be attached to a supply of electrical current for heating the core rods 10.
- the upper ends of the rods 10 are electrically interconnected by a bridge piece 13 which preferably consists of the same semiconductor material, namely silicon, as the core rods 10.
- the turbulent flow of gases issuing from the orifice of the nozzle 8 passes along the rods 10 toward the top of the reaction space where the gas flow becomes reversed.
- the spent residual gases leave the reaction vessel through an outlet pipe 17, which concentrically surrounds the nozzle 8.
- the nozzle 8 is so designed that the entire reaction gas mixture entering into the reaction vessel, for example in a quantity of about 2.5 m. /h., is whirled about in the reaction space so that a largest possible proportion of the gases enter into contact with the surface of the core rods 10. This promotes a uniform growth of semiconductor material on the carrier rods.
- the rods are heated electrically to the above-mentioned pyrolytic temperature, for example, in the neighborhood of 1000 to 1100 C.
- the speed at which the gaseous mixture enters through the nozzle into the reaction space is below 200 111/ sec. and is, for example, in the neighborhood of 150 m./ sec.
- the nozzle head 8a may have a threaded neck portion 8b screwed onto the top end of the inlet pipe 7.
- a bore 80 of the nozzle has a diameter of 5 to mm. but is constricted at the nozzle mouth 8d to a diameter of about 0.5 to 4 mm. over a length of about 2 to 5 mm.
- the method of the invention is applicable in the same manner for the produtcion of other semiconductor materials, for example germanium, silicon carbide SiC, indium antimonide InSb, or gallium arsenide GaAs, in which cases the same advantages, uniform product, and trouble-free operation are simultaneously secured.
- semiconductor materials for example germanium, silicon carbide SiC, indium antimonide InSb, or gallium arsenide GaAs, in which cases the same advantages, uniform product, and trouble-free operation are simultaneously secured.
- a process for producing a silicon body by reaction of a gaseous mixture of hydrogen and a gaseous compound of silicon in a reaction chamber comprising heating a silicon core body of approximately the same purity as the silicon to be precipitated to glowing temperature, the heated body effecting the reaction, introducing said gaseous mixture, at a velocity of at least 100 m./sec. and below 200 m./ sec. into the reaction chamber to produce a high degree of turbulence whereby the gas mixture flows longitudinally along said core body to etfect eflicient reaction into silicon and uniformly thicken said core body.
- a process for producing a silicon body by reaction of a gaseous mixture of hydrogen and a gaseous silicon compound selected from the group consisting of silicochloroform and silicon tetrachloride in a reaction chamber comprising heating a silicon core body of approximately the same purity as the silicon to be precipitated to glowing temperature, the heated body effecting the reaction, introducing said gaseous mixture, at a velocity of at least m./sec. and below 200 m./sec., into the reaction chamber to produce a high degree of turbulence whereby the gas mixture flows longitudinally along said core body to effect eificient reaction into silicon and uniformly thicken said core body.
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- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Silicon Compounds (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
- Chemical Vapour Deposition (AREA)
Description
1955 K. REUSCHEL ETAL 3,200,009
METHOD OF PRODUCING HYPERPURE SILICON Filed Jan. 10, 1962 United States Patent 3,200,009 METHOD OF PRODUCENG HYPERPURE SILICON Konrad Reuschel, Pretzfeld, and Arno Kersting, Lutzelsdorf, Germany, assignors to Siemens-Schuckertwerke Airtiengesellschaft, Berlin--Siemensstadt, Germany, a corporation of Germany Filed Jan. 10, 1962, Ser. No. 165,455 Claims priority, application Germany, Jan. 14, 1961, S 72,060 2 Claims. (Cl. 117201) Our invention relates to improvements in the production of hyperpure semiconductor material, particularly silicon, for electronic purposes. Application, Serial No. 90,291, filed February 20, 1961, and now Patent No. 3,099,534, a division of application, Serial No. 665,086, filed June 11, 1957, now Patent No. 3,011,877, and the parent application respectively claim methods and devices for preparing semiconductor material. According to these methods and devices, solid core rods of the same material are mounted on a common base and are electrically heated by passing current through the rods, while the rods are mounted in a sealed vessel traversed by reaction mixture comprising a gaseous compound of the semiconductor material to be precipitated and a gaseous reaction agent such as hydrogen. By means of electric current the rods are kept at a high temperature, for example between 900 and 1200 C. for silicon, at which the gaseous semiconductor compound becomes pyrolytically reduced and the resulting semiconductor material is precipitated upon the core rods, which gradually increase in thickness. The inlet for the gaseous reaction mixture in such devices is located on or in the base structure carrying the holders for the core rods. In a particular embodiment of the devices, the gas inlet has a nozzle-shaped design so that the fresh gas mixture is caused to flow from the location of the core-rod holders along the core rods in the longitudinal direction of the rods.
It is an object of our invention to improve the performance of such methods and devices toward an optimum rate of crystalline growth of the material being precipitated.
We have discovered, according to our invention, that this advantage is achieved if the speed of the reaction gas mixture entering into the pyrolytic reaction chamber of a sealed apparatus is maintained above 100 m./sec. (meters per second) but below 200 m./sec. at the mouth of the inlet nozzle. The significance of this rate of gas supply will be understood from the following.
For attaining large quantities of precipitated semiconductor material, it is generally desirable to keep the speed of the gaseous semiconductor compound entering into the reaction vessel as large as feasible, because the quantity of semiconductor material precipitating onto the cored rods is dependent, among other things, upon the throughput of gas.
We have found that by keeping the gas-entering speed below about 200 m./sec., the semiconductor material has a uniform thickness over the entire length of the core rods during the processing period. This is of advantage particularly for a m'onocrystalline growth of the semiconductor material being precipitated, because such a monocrystalline rod can be sawed or cut, without further fabrication, into a multiplicity of discs or wafers all having the same size and thus being all suitable as monocrystalline base bodies for electronic semiconductor devices of a great variety of types. However, we have found that the economy of operation becomes appreciably impaired if the gas-entering speed becomes too small, and that the speed range within which the desired improvement is achieved is substantially between 100 and 200 m./sec. Maintaining the gas-entering speed below about 200 m./sec. has
the additional advantage of preventing breakage of equipment, for example of a quartz bell forming the upper portion of the hermetically sealed vessel structure, or lifting of the quartz bell from the mounting base constituting the bottom wall of the reaction chamber, in the event of a high-pressure gas build-up in the reaction space, caused by clouding or narrowing of the gas outlet.
An embodiment of equipment by means of which the above-described can be performed in a simple manner is illustrated by way of example on the accompanying drawing in which:
FIG. 1 shows schematically and partly in section an apparatus for the production of hyperpure silicon; and
FIG. 2 shows separately an inlet nozzle for the gaseous reaction mixture which forms part of the apparatus according to FIG. 1.
In the illustrated apparatus, hydrogen, to be employed as carrier and reaction gas, is supplied from a gas bottle 2 through a shut-off valve 3 and a plural-stage pressurereduction valve 4 from which the gas passes through a gas-flow meter 5 to an evaporator 6. In the evaporator 6 a liquid semiconductor compound, preferably silicochloroform SiHCl or silicon tetrachloride SiC1 is evaporated. In the evaporator 6, therefore, the hydrogen becomes mixed with the evaporated silicon compound, such as silico-chloroform, and passes through a gas pipe 7 to a nozzle-type inlet device 8 and thence into the reaction space. The inlet nozzle 8 may have an inner diameter of about 2 mm. for example and is designed to produce a turbulent How of gas along core rods 10 of hyperpure silicon. The rods, for example, have a thickness of 3 mm. and a length of about 400 mm. The rods 10 are mounted in a reaction vessel comprising an hermetically sealed quartz cylinder or bell 11 whose inner diameter, for example, is approximately mm., and whose height, for example, is approximately 550 mm. It will be understood that the numerical values here given are properly correlated to one another, but may be modified in accordance with the requirements or desiderata of a particular method or apparatus. The bottom of the reaction chamber is closed by a metallic base plate 12, which is hollow and preferably cooled in its interior by a flowing or circulating coolant. The lower ends of the two rods 10 are inserted in respective bores of holders 14 consisting, for example of spectral carbon which in turn are fastened in cylindrical supports 15, inserted into the base plate 12, for example, by having a screw thread in engagement with threaded bores of the base plate 12. At least one of the cylindrical bodies 15 is insulated from the base plate 12 by an insulating sleeve 16. The cylindrical bodies 15 are connected to terminals 9 to be attached to a supply of electrical current for heating the core rods 10. The upper ends of the rods 10 are electrically interconnected by a bridge piece 13 which preferably consists of the same semiconductor material, namely silicon, as the core rods 10.
The turbulent flow of gases issuing from the orifice of the nozzle 8 passes along the rods 10 toward the top of the reaction space where the gas flow becomes reversed. The spent residual gases leave the reaction vessel through an outlet pipe 17, which concentrically surrounds the nozzle 8. The nozzle 8 is so designed that the entire reaction gas mixture entering into the reaction vessel, for example in a quantity of about 2.5 m. /h., is whirled about in the reaction space so that a largest possible proportion of the gases enter into contact with the surface of the core rods 10. This promotes a uniform growth of semiconductor material on the carrier rods. Then the rods are heated electrically to the above-mentioned pyrolytic temperature, for example, in the neighborhood of 1000 to 1100 C. As mentioned, the speed at which the gaseous mixture enters through the nozzle into the reaction space is below 200 111/ sec. and is, for example, in the neighborhood of 150 m./ sec.
As shown in FIG. 2, the nozzle head 8a may have a threaded neck portion 8b screwed onto the top end of the inlet pipe 7. A bore 80 of the nozzle has a diameter of 5 to mm. but is constricted at the nozzle mouth 8d to a diameter of about 0.5 to 4 mm. over a length of about 2 to 5 mm.
While reference is made in the foregoing description to the precipitation of silicon, the method of the invention is applicable in the same manner for the produtcion of other semiconductor materials, for example germanium, silicon carbide SiC, indium antimonide InSb, or gallium arsenide GaAs, in which cases the same advantages, uniform product, and trouble-free operation are simultaneously secured.
We claim:
1. A process for producing a silicon body by reaction of a gaseous mixture of hydrogen and a gaseous compound of silicon in a reaction chamber, comprising heating a silicon core body of approximately the same purity as the silicon to be precipitated to glowing temperature, the heated body effecting the reaction, introducing said gaseous mixture, at a velocity of at least 100 m./sec. and below 200 m./ sec. into the reaction chamber to produce a high degree of turbulence whereby the gas mixture flows longitudinally along said core body to etfect eflicient reaction into silicon and uniformly thicken said core body. 2. A process for producing a silicon body by reaction of a gaseous mixture of hydrogen and a gaseous silicon compound selected from the group consisting of silicochloroform and silicon tetrachloride in a reaction chamber, comprising heating a silicon core body of approximately the same purity as the silicon to be precipitated to glowing temperature, the heated body effecting the reaction, introducing said gaseous mixture, at a velocity of at least m./sec. and below 200 m./sec., into the reaction chamber to produce a high degree of turbulence whereby the gas mixture flows longitudinally along said core body to effect eificient reaction into silicon and uniformly thicken said core body.
References Cited by the Examiner UNITED STATES PATENTS RICHARD D. NEVIUS, Primary Examiner. M. A. BRINDISI, Examiner.
Claims (1)
1. A PROCESS FOR PRODUCING A SILICON BODY BY REACTION OF A GASEOUS MIXTURE OF HYDROGEN AND A GASEOUS COMPOUND OF SILICON IN A REACTION CHAMBER, COMPRISING HEATING A SILICON CORE BOYD OF APPROXIMATELY THE SAME PURITY AS THE SILICON TO BE PRECIPITATED TO GLOWING TEMPERATURE, THE HEATED BODY EFFECTING THE REACTION, INTRODUCING SAID GASEOUS MIXTURE, AT A VELOCITY OF AT LEAST 100 M./SEC. AND BELOW 200 M./SEC. INTO THE REACTION CHAMBER TO PRODUCE A HIGH DEGREE OF TURBULENCE WHEREBY THE GAS MIXTURE FLOWS LONGITUDINALLY ALONG SAID CORE BODY TO EFFECT EFFICIENT REACTION INTO SILICON AND UNIFORMLY THICKEN SAID CORE BODY.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DES49191A DE1061593B (en) | 1956-06-25 | 1956-06-25 | Device for obtaining the purest semiconductor material for electrotechnical purposes |
US665086A US3011877A (en) | 1956-06-25 | 1957-06-11 | Production of high-purity semiconductor materials for electrical purposes |
DES72060A DE1141852B (en) | 1956-06-25 | 1961-01-14 | Method for operating a device for extracting the purest semiconductor material, in particular silicon |
US90291A US3099534A (en) | 1956-06-25 | 1961-02-20 | Method for production of high-purity semiconductor materials for electrical purposes |
Publications (1)
Publication Number | Publication Date |
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US3200009A true US3200009A (en) | 1965-08-10 |
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Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
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US90291A Expired - Lifetime US3099534A (en) | 1956-06-25 | 1961-02-20 | Method for production of high-purity semiconductor materials for electrical purposes |
US165455A Expired - Lifetime US3200009A (en) | 1956-06-25 | 1962-01-10 | Method of producing hyperpure silicon |
US231878A Expired - Lifetime US3219788A (en) | 1956-06-25 | 1962-10-12 | Apparatus for the production of high-purity semiconductor materials |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
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US90291A Expired - Lifetime US3099534A (en) | 1956-06-25 | 1961-02-20 | Method for production of high-purity semiconductor materials for electrical purposes |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
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US231878A Expired - Lifetime US3219788A (en) | 1956-06-25 | 1962-10-12 | Apparatus for the production of high-purity semiconductor materials |
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US (3) | US3099534A (en) |
CH (2) | CH354308A (en) |
DE (2) | DE1061593B (en) |
FR (1) | FR1177821A (en) |
GB (2) | GB861135A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3941900A (en) * | 1973-03-28 | 1976-03-02 | Siemens Aktiengesellschaft | Method for producing highly pure silicon |
US4315968A (en) * | 1980-02-06 | 1982-02-16 | Avco Corporation | Silicon coated silicon carbide filaments and method |
US6284312B1 (en) | 1999-02-19 | 2001-09-04 | Gt Equipment Technologies Inc | Method and apparatus for chemical vapor deposition of polysilicon |
US6365225B1 (en) | 1999-02-19 | 2002-04-02 | G.T. Equipment Technologies, Inc. | Cold wall reactor and method for chemical vapor deposition of bulk polysilicon |
US20090127093A1 (en) * | 2005-05-25 | 2009-05-21 | Norbert Auner | Method for the production of silicon from silyl halides |
DE102009021825B3 (en) * | 2009-05-18 | 2010-08-05 | Kgt Graphit Technologie Gmbh | Pick-up cone for silicon seed rods |
US20110229638A1 (en) * | 2010-03-19 | 2011-09-22 | Gt Solar Incorporated | System and method for polycrystalline silicon deposition |
KR101811872B1 (en) | 2007-09-20 | 2017-12-22 | 미츠비시 마테리알 가부시키가이샤 | Reactor for polycrystalline silicon and polycrystalline silicon production method |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL123477C (en) * | 1958-05-16 | |||
DE1185150B (en) * | 1960-02-23 | 1965-01-14 | Siemens Ag | Process for the production of the purest semiconductor material, in particular silicon |
DE1243147B (en) * | 1960-02-25 | 1967-06-29 | Siemens Ag | Process for the production of the purest semiconductor material by chemical conversion from a gaseous compound of the same |
NL275555A (en) * | 1961-04-25 | |||
DE1138481C2 (en) * | 1961-06-09 | 1963-05-22 | Siemens Ag | Process for the production of semiconductor arrangements by single-crystal deposition of semiconductor material from the gas phase |
US3406044A (en) * | 1965-01-04 | 1968-10-15 | Monsanto Co | Resistance heating elements and method of conditioning the heating surfaces thereof |
US3416951A (en) * | 1965-07-28 | 1968-12-17 | Air Force Usa | Method for the pyrolytic deposition of silicon carbide |
US3463666A (en) * | 1965-08-27 | 1969-08-26 | Dow Corning | Monocrystalline beta silicon carbide on sapphire |
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US3941900A (en) * | 1973-03-28 | 1976-03-02 | Siemens Aktiengesellschaft | Method for producing highly pure silicon |
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KR101811872B1 (en) | 2007-09-20 | 2017-12-22 | 미츠비시 마테리알 가부시키가이샤 | Reactor for polycrystalline silicon and polycrystalline silicon production method |
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CN102428028A (en) * | 2009-05-18 | 2012-04-25 | Kgt石墨科技有限公司 | Support cone for silicon seed bars |
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Also Published As
Publication number | Publication date |
---|---|
DE1061593B (en) | 1959-07-16 |
US3099534A (en) | 1963-07-30 |
GB861135A (en) | 1961-02-15 |
US3219788A (en) | 1965-11-23 |
CH398248A (en) | 1965-08-31 |
FR1177821A (en) | 1959-04-29 |
GB956306A (en) | 1964-04-22 |
DE1141852B (en) | 1962-12-27 |
CH354308A (en) | 1961-05-15 |
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