US3634143A - Preparation of iii{14 v alloys for infrared detectors - Google Patents
Preparation of iii{14 v alloys for infrared detectors Download PDFInfo
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- US3634143A US3634143A US823150A US3634143DA US3634143A US 3634143 A US3634143 A US 3634143A US 823150 A US823150 A US 823150A US 3634143D A US3634143D A US 3634143DA US 3634143 A US3634143 A US 3634143A
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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
- C30B23/00—Single-crystal growth by condensing evaporated or sublimed materials
- C30B23/02—Epitaxial-layer growth
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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
- C30B29/00—Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
- C30B29/10—Inorganic compounds or compositions
- C30B29/40—AIIIBV compounds wherein A is B, Al, Ga, In or Tl and B is N, P, As, Sb or Bi
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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
- H01L21/02—Manufacture or treatment of semiconductor devices or of parts thereof
- H01L21/02104—Forming layers
- H01L21/02365—Forming inorganic semiconducting materials on a substrate
- H01L21/02367—Substrates
- H01L21/0237—Materials
- H01L21/02387—Group 13/15 materials
- H01L21/02395—Arsenides
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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
- H01L21/02—Manufacture or treatment of semiconductor devices or of parts thereof
- H01L21/02104—Forming layers
- H01L21/02365—Forming inorganic semiconducting materials on a substrate
- H01L21/02367—Substrates
- H01L21/0237—Materials
- H01L21/02387—Group 13/15 materials
- H01L21/02398—Antimonides
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- H—ELECTRICITY
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- 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
- H01L21/02—Manufacture or treatment of semiconductor devices or of parts thereof
- H01L21/02104—Forming layers
- H01L21/02365—Forming inorganic semiconducting materials on a substrate
- H01L21/02518—Deposited layers
- H01L21/02521—Materials
- H01L21/02538—Group 13/15 materials
- H01L21/02546—Arsenides
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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
- H01L21/02—Manufacture or treatment of semiconductor devices or of parts thereof
- H01L21/02104—Forming layers
- H01L21/02365—Forming inorganic semiconducting materials on a substrate
- H01L21/02518—Deposited layers
- H01L21/02521—Materials
- H01L21/02538—Group 13/15 materials
- H01L21/02549—Antimonides
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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
- H01L21/02—Manufacture or treatment of semiconductor devices or of parts thereof
- H01L21/02104—Forming layers
- H01L21/02365—Forming inorganic semiconducting materials on a substrate
- H01L21/02612—Formation types
- H01L21/02617—Deposition types
- H01L21/02631—Physical deposition at reduced pressure, e.g. MBE, sputtering, evaporation
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- 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
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- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S420/00—Alloys or metallic compositions
- Y10S420/903—Semiconductive
Definitions
- ABSTRACT A single crystal lnAs-InSb alloy is prepared on a [ll-V substrate by flash evaporation of a mixture of granulated lnAs and InSb in a vacuum system, subsequent condensation and solidification of the vapor on the substrate and subsequent annealing. The flash evaporation and solidification is thus followed by suitable annealing of the deposited material for several weeks at a temperature close to but below the solidus temperature of the alloy. Prior to annealing, an oxide film may be formed on the deposited alloy to prevent loss of the more volatile constituents.
- the invention relates to the production of semiconductor materials, and more particularly relates to the production of single crystal III-V alloys for use in infrared detecting devices.
- group III-V compounds have been found to have properties which, for some applications, are superior to those of the group IV semiconductor materials. These compounds offer a wide range of energy gaps. lnAs and InSb have been found to offer energy gaps particularly suitable in the infrared region of the electromagnetic spectrum.
- Several methods are currently known for preparing homogeneous alloys of various IllV compounds. A few methods, such as chemical vapor deposition, have been used to form single crystal alloys of some of these materials. Little, however, is currently known about the formation of single crystal alloys of lnAs-InSb. Single crystals are of course necessary for use in electronic devices.
- a vapor is produced which diffuses toward a substrate held at a small distance from the evaporator.
- the substrate is maintained at temperature sufficiently low to condense all the constituents of the vapor including the most volatile ones.
- a film of the desired alloy condenses on the substrate and the film has approximately the same composition as the initial powder because the powder delivery rate is made sufficiently fast to negate the effect of some elements evaporating more rapidly than others as explained by Muller and Richards. Although a homogeneous alloy is deposited, it is not single crystal.
- Another object of the invention is to provide a method for fabricating single crystal allows of lnAs and lnSb which method can be performed in a commercially feasible short period of time.
- a method for preparing a single crystal III-V alloy on a suitable substrate comprising: (a) effecting the vaporization of the compounds which are the constituents of the III-V alloy to provide a vapor mixture; (b) depositing the III-V alloy on the substrate by condensation and solidification of the vapor mixture; and (c) annealing the deposited alloy until a suitably large area single crystal is formed.
- the method is more effective if a mixture of lnAs particles and InSb particles are impinged upon a heated surface which surface is heated above the melting point of the particles thereby vaporizing the particles and so that a homogenous alloy therefrom is deposited on a substrate which is maintained at a suitably low temperature for effecting condensation of the vapor.
- Annealing is preferably clone immediately below the solidus line.
- the flash evaporation apparatus used in this invention is contained within an enclosure which can be evacuated prior to its operation.
- a hopper is mounted within the enclosure for containing a powder mixture of the desired constituents.
- the hopper is initially filled with a finely powdered mixture of InSb and lnAs. This mixture has a proportional composition approximately the same as that desired in the ultimate single crystal to be formed.
- a boat preferably a tantalum boat, is mounted in the enclosure beneath the hopper so that the powder may be continuously fed from the hopper onto the boat.
- the boat is provided with means for heating it to a sufficient temperature.
- the boat temperature must be high enough to quickly evaporate the least volatile constituent of the mixed powder as the grains fall and impinge upon the boat.
- a temperature above l,500 C. would be desired.
- a vibrating or other feeder is provided to continuously feed the powdered mixture from the hopper to the boat at a desired feed rate.
- a substrate holder capable of being heated to a controlled temperature is positioned above the tantalum boat. I have positioned the heater l0 centimeters above the boat. A cleaned and etched III-V substrate is mounted to the substrate holder. During operation, the substrate will be maintained at a temperature sufficiently low to prevent revaporization or decomposition of the more volatile constituents. With the preferred constituents, the temperature of the substrate holder may be held preferably below 405 C.
- the preferred embodiment of my method begins by evacuating the enclosure preferably to a pressure below 10 Torr.
- the tantalum boat is heated to a temperature high enough to evaporate the least volatile constituents.
- the substrate is brought to its condensation temperature.
- the vibrating trough or other means is then energized to begin feeding a continuous stream from the hopper on to the tantalum boat. As the particles strike the boat, they are vaporized and the vapor diffuses through the enclosure.
- the substrate placed in the vapor stream issuing from the boat becomes immersed in the vapor and, because of its temperature, is a favorable site on which the vapor is condensed and solidified.
- the alloy deposited in this manner is homogeneous though not (except at a temperature within a very narrow range) a single crystal.
- the resultant film composition will be at least 56 mol percent indium antimonide and the balance indium arsenide for a substrate maintained at a temperature between 350 and 405 C. If the substrate is held at a range of temperature between 390 and 405 C. a single crystal may be formed even without annealing. I prefer to hold the substrate at a temperature between 398 and 400 C.
- the apparatus is cooled and a thin protective film is formed on the surface of the alloy to prevent loss of the more volatile constituents.
- a thin protective film which was 1,000 angstroms thick but small variations therein are of course possible. This film is desirable because of the annealing temperature used as explained below.
- the homogeneous polycrystalline alloy film is then preferably annealed at a temperature below, but preferably close to, the solidus temperature for the alloy deposited. Because annealing is done so close to the solidus temperature, the thin oxide film is needed to prevent loss of the more volatile constituent of the alloy. Good quality single crystals can be formed by annealing at such a temperature for a period of a few weeks rather than a few months. Of course, the exact anneal time and temperature will depend upon the constituents, the proportional composition, and the quality of the crystals desired.
- I may use mixtures of indium arsenide and indium antimonide over a fairly broad range of proportions.
- l may use 80 mol percent indium arsenide with the remainder indium antimonide, and I may vary the proportions of indium arsenide at any proportion between 80 mol percent to 40 mol percent, as for example to 70 mol percent, 60 mol percent, 50 mol percent, 46 mol percent, 44 mol percent, 42 mol percent and 40 mol percent, providing in each case indium antimonide for the balance ofthe mixture.
- 1 may provide a temperature of the tantalum boat at 1,000 C. but we prefer that the temperature be maintained at l,500 C. or above.
- the substrate may be held at a temperature of 300 to 405 C., securing crystalline material in certain cases without annealing.
- EXAMPLEI lnSb was ground into a powder and lnAs was ground into a powder and formed into a mixture having 44.0 mol percent lnSb and the balance lnAs. This mixture was continuously fed onto a tantalum boat above l,500 C. The substrate was held at 350 C. and a homogeneous alloy film was formed thereon. An oxide film 1,000 angstroms thick was formed on the surface and the substrate with its film was annealed at 555 C. for 3 weeks. Examination using Laue X-ray back reflection techniques indicated that the alloys were single crystal.
- EXAMPLEll lnSb was ground into a powder and lnAs was ground into a powder and formed into a mixture having a 60 mol percent lnSb content. This mixture was continuously fed onto a tantalum boat above l,500 C. The substrate was held at 350 C. and a homogeneous alloy film was formed thereon. An oxide film 1,000 angstroms thick was formed on the surface and the substrate with its film was annealed at 535C. for 4 weeks. Examination using Laue X-ray reflection techniques indicated that the alloy were single crystal.
- the method of the invention is performed by first effecting the vaporization of the intended constituents of the alloy in order to provide a vapor mixture of these constituents.
- a substrate immersed in this vapor provides a suitable site for the deposition of the lll-V alloy vapor by condensation and solidification.
- the deposited film is then preferably annealed below the solidus temperature until a suitably large area ofsingle crystal is formed.
- the preferred method for effecting the vaporization is to impinge particles of one of the constituent lll-V compounds upon a heated surface which is heated sufficiently high to cause practically instantaneous vaporization of the particles Simultaneously, particles of the other constituent lll-V compound are impinged on a surface heated hot enough to vaporize that compound.
- a single heated surface heated above the melting point of the least volatile constituent and to impinge the particles on the surface in the same proportion as that desired in the single crystal lll-V alloy.
- I 15 also desirable to form a thln protective film on the surface of the deposited alloy after depositing the alloy on the substrate but prior to annealing the alloy.
- oxides for this purpose and particularly silicon oxide.
- a method for preparing a single crystal Ill-V pseudobinary alloy on a substrate comprising in order:
- the substrate is maintained at a temperature below 400 C. during said depositing step, the vaporization is effected by impinging the particles ofthe constituent lll-V compounds on a heated surface maintained at a temperature above l,500 C. to effect vaporization thereof, and the annealing is effected by maintaining the deposited alloy at a temperature of approximately 555 C. for a period of approximately 3 weeks.
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Abstract
A single crystal InAs-InSb alloy is prepared on a III-V substrate by flash evaporation of a mixture of granulated InAs and InSb in a vacuum system, subsequent condensation and solidification of the vapor on the substrate and subsequent annealing. The flash evaporation and solidification is thus followed by suitable annealing of the deposited material for several weeks at a temperature close to but below the solidus temperature of the alloy. Prior to annealing, an oxide film may be formed on the deposited alloy to prevent loss of the more volatile constituents.
Description
United States Patent lnventor Leo C. Brennan Palo Alto, Calif.
Appl. No. 823,150
Filed May 8, 1969 Patented Jan. 11, 1972 Assignee Avco Corporation Cincinnati, Ohio PREPARATION OF Ill-V ALLOYS FOR INFRARED DETECTORS 9 Claims, No Drawings US. Cl l48/1.6, 75/ 1 34 T Int. Cl B0lj 17/30 Field of Search 148/15, 1.6; 75/134 T [56] References Cited UNITED STATES PATENTS 3,558,373 l/l97l Moody etal l48/l7l Primary Examiner-L. Dewayne Rutledge Assistant Examiner-E. L. Weise Attorneys-Charles M. Hogan, lrwin P. Garfinkle and Jerome R. Cox
ABSTRACT: A single crystal lnAs-InSb alloy is prepared on a [ll-V substrate by flash evaporation of a mixture of granulated lnAs and InSb in a vacuum system, subsequent condensation and solidification of the vapor on the substrate and subsequent annealing. The flash evaporation and solidification is thus followed by suitable annealing of the deposited material for several weeks at a temperature close to but below the solidus temperature of the alloy. Prior to annealing, an oxide film may be formed on the deposited alloy to prevent loss of the more volatile constituents.
PREPARATION OF III-V ALLOYS FOR INFRARED DETECTORS BACKGROUND The invention relates to the production of semiconductor materials, and more particularly relates to the production of single crystal III-V alloys for use in infrared detecting devices.
Various group III-V compounds have been found to have properties which, for some applications, are superior to those of the group IV semiconductor materials. These compounds offer a wide range of energy gaps. lnAs and InSb have been found to offer energy gaps particularly suitable in the infrared region of the electromagnetic spectrum. Several methods are currently known for preparing homogeneous alloys of various IllV compounds. A few methods, such as chemical vapor deposition, have been used to form single crystal alloys of some of these materials. Little, however, is currently known about the formation of single crystal alloys of lnAs-InSb. Single crystals are of course necessary for use in electronic devices.
The flash evaporation technique for depositing mixtures of the Ill-V compounds on a suitable substrate has been described in several technical papers. For example, E. K. Muller and J. L. Richards describe such a technique in an article entitled Miscibility of III-V Semiconductors Studied by Flash Evaporation which is found in the Apr. 1964 Journal of Applied Physics, Vol. 35, No. 4. The Muller and Richards technique, however, when used with the pseudobinary In- AslnSb system produces a homogenous solid alloy which is not single crystal. In their conventional flash evaporation process, a powder of fine grains is fed continuously onto a heated evaporator which is hot enough to vaporize all of the constituents. As each grain strikes the evaporator, a vapor is produced which diffuses toward a substrate held at a small distance from the evaporator. The substrate is maintained at temperature sufficiently low to condense all the constituents of the vapor including the most volatile ones. A film of the desired alloy condenses on the substrate and the film has approximately the same composition as the initial powder because the powder delivery rate is made sufficiently fast to negate the effect of some elements evaporating more rapidly than others as explained by Muller and Richards. Although a homogeneous alloy is deposited, it is not single crystal.
Various types of annealing processes have been performed in the semiconductor fabrication art. Finely ground powders have been very tightly compressed and annealed for periods extending anywhere from several weeks to several months. Such annealing, however, requires extensive periods of time thereby making conventional annealing substantially impractical and commercially undesirable for the manufacture of devices. Although the annealing of fine compressed powders of lnAs and lnSb has produced ingots with homogeneous regions, the ingots themselves were not homogeneous. Furthermore, such ingots were polycrystalline.
In an attempt to fabricate alloys of InAsInSb zone recrystallization, similar to zone refining, has been used but, while producing ingots with homogeneous regions, produces an overall polycrystalline ingot. Similarly, directional freezing has been used but it too produces polycrystalline ingots.
It is therefore an object of the invention to provide a method for fabricating single crystal alloys of two or more Ill-V compounds.
Another object of the invention is to provide a method for fabricating single crystal allows of lnAs and lnSb which method can be performed in a commercially feasible short period of time.
Further objects and features of the invention will be apparent from the following specification and claims.
SUMMARY OF THE INVENTION We have found that the foregoing and other objects may be attained by a method for preparing a single crystal III-V alloy on a suitable substrate, the method comprising: (a) effecting the vaporization of the compounds which are the constituents of the III-V alloy to provide a vapor mixture; (b) depositing the III-V alloy on the substrate by condensation and solidification of the vapor mixture; and (c) annealing the deposited alloy until a suitably large area single crystal is formed.
The method is more effective if a mixture of lnAs particles and InSb particles are impinged upon a heated surface which surface is heated above the melting point of the particles thereby vaporizing the particles and so that a homogenous alloy therefrom is deposited on a substrate which is maintained at a suitably low temperature for effecting condensation of the vapor. Annealing is preferably clone immediately below the solidus line.
DETAILED DESCRIPTION The flash evaporation apparatus used in this invention is contained within an enclosure which can be evacuated prior to its operation. A hopper is mounted within the enclosure for containing a powder mixture of the desired constituents. In the preferred embodiment, the hopper is initially filled with a finely powdered mixture of InSb and lnAs. This mixture has a proportional composition approximately the same as that desired in the ultimate single crystal to be formed. A boat, preferably a tantalum boat, is mounted in the enclosure beneath the hopper so that the powder may be continuously fed from the hopper onto the boat. The boat is provided with means for heating it to a sufficient temperature. The boat temperature must be high enough to quickly evaporate the least volatile constituent of the mixed powder as the grains fall and impinge upon the boat. For the preferred lnAs-InSb powder, a temperature above l,500 C. would be desired. A vibrating or other feeder is provided to continuously feed the powdered mixture from the hopper to the boat at a desired feed rate.
A substrate holder capable of being heated to a controlled temperature is positioned above the tantalum boat. I have positioned the heater l0 centimeters above the boat. A cleaned and etched III-V substrate is mounted to the substrate holder. During operation, the substrate will be maintained at a temperature sufficiently low to prevent revaporization or decomposition of the more volatile constituents. With the preferred constituents, the temperature of the substrate holder may be held preferably below 405 C.
The preferred embodiment of my method begins by evacuating the enclosure preferably to a pressure below 10 Torr. The tantalum boat is heated to a temperature high enough to evaporate the least volatile constituents. The substrate is brought to its condensation temperature. The vibrating trough or other means is then energized to begin feeding a continuous stream from the hopper on to the tantalum boat. As the particles strike the boat, they are vaporized and the vapor diffuses through the enclosure. The substrate placed in the vapor stream issuing from the boat becomes immersed in the vapor and, because of its temperature, is a favorable site on which the vapor is condensed and solidified. The alloy deposited in this manner is homogeneous though not (except at a temperature within a very narrow range) a single crystal. For example, with a mixture of 60 mol percent indium antimonide and the balance indium arsenide, the resultant film composition will be at least 56 mol percent indium antimonide and the balance indium arsenide for a substrate maintained at a temperature between 350 and 405 C. If the substrate is held at a range of temperature between 390 and 405 C. a single crystal may be formed even without annealing. I prefer to hold the substrate at a temperature between 398 and 400 C.
Following the deposition of a sufficiently thick film of the homogeneous alloy, the apparatus is cooled and a thin protective film is formed on the surface of the alloy to prevent loss of the more volatile constituents. I used an oxide film which was 1,000 angstroms thick but small variations therein are of course possible. This film is desirable because of the annealing temperature used as explained below.
The homogeneous polycrystalline alloy film is then preferably annealed at a temperature below, but preferably close to, the solidus temperature for the alloy deposited. Because annealing is done so close to the solidus temperature, the thin oxide film is needed to prevent loss of the more volatile constituent of the alloy. Good quality single crystals can be formed by annealing at such a temperature for a period of a few weeks rather than a few months. Of course, the exact anneal time and temperature will depend upon the constituents, the proportional composition, and the quality of the crystals desired.
It is obvious that a great variety of proportional compositions, temperatures, and constituents may be used in performing the process of my invention. I may use mixtures of indium arsenide and indium antimonide over a fairly broad range of proportions. l may use 80 mol percent indium arsenide with the remainder indium antimonide, and I may vary the proportions of indium arsenide at any proportion between 80 mol percent to 40 mol percent, as for example to 70 mol percent, 60 mol percent, 50 mol percent, 46 mol percent, 44 mol percent, 42 mol percent and 40 mol percent, providing in each case indium antimonide for the balance ofthe mixture.
1 may provide a temperature of the tantalum boat at 1,000 C. but we prefer that the temperature be maintained at l,500 C. or above.
The substrate may be held at a temperature of 300 to 405 C., securing crystalline material in certain cases without annealing. The following examples illustrate the process and the composition ofthe invention using particular materials, steps, and conditions. It is to be understood that these examples are furnished by way of illustration and are not intended to be by way of limitation.
EXAMPLEI lnSb was ground into a powder and lnAs was ground into a powder and formed into a mixture having 44.0 mol percent lnSb and the balance lnAs. This mixture was continuously fed onto a tantalum boat above l,500 C. The substrate was held at 350 C. and a homogeneous alloy film was formed thereon. An oxide film 1,000 angstroms thick was formed on the surface and the substrate with its film was annealed at 555 C. for 3 weeks. Examination using Laue X-ray back reflection techniques indicated that the alloys were single crystal.
EXAMPLEll lnSb was ground into a powder and lnAs was ground into a powder and formed into a mixture having a 60 mol percent lnSb content. This mixture was continuously fed onto a tantalum boat above l,500 C. The substrate was held at 350 C. and a homogeneous alloy film was formed thereon. An oxide film 1,000 angstroms thick was formed on the surface and the substrate with its film was annealed at 535C. for 4 weeks. Examination using Laue X-ray reflection techniques indicated that the alloy were single crystal.
Thus, in general, the method of the invention is performed by first effecting the vaporization of the intended constituents of the alloy in order to provide a vapor mixture of these constituents. A substrate immersed in this vapor provides a suitable site for the deposition of the lll-V alloy vapor by condensation and solidification. The deposited film is then preferably annealed below the solidus temperature until a suitably large area ofsingle crystal is formed.
The preferred method for effecting the vaporization is to impinge particles of one of the constituent lll-V compounds upon a heated surface which is heated sufficiently high to cause practically instantaneous vaporization of the particles Simultaneously, particles of the other constituent lll-V compound are impinged on a surface heated hot enough to vaporize that compound. I have found it preferable to use a single heated surface, heated above the melting point of the least volatile constituent and to impinge the particles on the surface in the same proportion as that desired in the single crystal lll-V alloy. I
I 15 also desirable to form a thln protective film on the surface of the deposited alloy after depositing the alloy on the substrate but prior to annealing the alloy. We have used oxides for this purpose and particularly silicon oxide.
It is to be understood that while the specific examples given describe preferred embodiments of my invention, they are for the purposes ofillustration only, that the method of the invention is not limited to the precise details and conditions disclosed, and that various changes may be made therein without departing from the spirit of the invention which is defined by the following claims.
I claim:
1. A method for preparing a single crystal Ill-V pseudobinary alloy on a substrate, the method comprising in order:
a. effecting the vaporization of the compounds which are the intended constituents of said alloy to provide a vapor mixture;
b. depositing a IllV alloy on the substrate by condensation and solidification of said vapor mixture on the substrate; and
c. annealing the deposited alloy until a suitably large area single crystal is formed.
2. A method according to claim 1, wherein said vaporization is effected by:
a. impinging particles ofa constituent lll-V compound on a heated surface to vaporize them, the surface being heated to a temperature above the melting point of the particles impinged thereon; and
b. simultaneously impinging particles ofanother constituent lIl-V compound on a heated surface to vaporize them, the surface being heated to a temperature above the melting point of the particles impinging thereon.
3. A method according to claim 2, wherein the particles are impinged on the same surface in proportions approximating the proportions desired in said single crystal Ill-V alloy.
4. A method according to claim 3, wherein said constituents comprise lnSb and lnAs, the substrate is maintained at a temperature below 405 C. during said depositing step, and said heated surface is maintained at a temperature above I ,500 C. during said vaporization.
5. A method according to claim 4, wherein the constituents are 44 mole percent lnSb and the balance lnAs, the annealing period is approximately 3 weeks, and the annealing temperature is approximately 555 C.
6. A method according to claim 1, wherein after said depositing, but prior to said annealing, a film is formed on the surface ofthe deposited alloy.
7. A method according to claim 6, wherein the film is a silicon oxide film.
8. A method according to claim 7, wherein the constituents are 44 mol percent lnSb and the balance lnAs, the substrate is maintained at a temperature below 400 C. during said depositing step, the vaporization is effected by impinging the particles ofthe constituent lll-V compounds on a heated surface maintained at a temperature above l,500 C. to effect vaporization thereof, and the annealing is effected by maintaining the deposited alloy at a temperature of approximately 555 C. for a period of approximately 3 weeks.
9. A method according to claim 7, wherein the constituents are 60 mol percent indium antimonide and the balance indium arsenide.
P0405) UNITED STATES PATENT GFFICE CERTIFICATE F CECTFON Patent No. hated January 11 2 1972 Inventoflg'; Leo Brennan I It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Column 1, line 30 should read H. produces a. homogengous solid alloy.
Column 2, lines 9-10 should-read 8 0.50 that a. homogeneous alloy therefrom ison;
Column 2, lines 4-6-47 should read 0.. ho e pressure below 10' "Form .H;
Column 2, line 5-1- should read muvapor diffuses throughguig the enclosure. o
Column 3, line 55 should read ...the alloyg were single crystal.
000; I column 3, lines YB-68 should read ..;.vaporization of the particles, Simultaneously, H
Signed and sealed this 1st day of August1972..
(SEAL) Attest:
EDWARD M. FLETQHERJR. ROBERT GOTTSCHALK Att6S'Cl1'lgOfflC6I I Commissioner of Patents
Claims (8)
- 2. A method according to claim 1, wherein said vaporization is effected by: a. impinging particles of a constituent III-V compound on a heated surface to vaporize them, the surface being heated to a temperature above the melting point of the particles impinged thereon; and b. simultaneously impinging particles of another constituent III-V compound on a heated surface to vaporize them, the surface being heated to a temperature above the melting point of the particles impinging thereon.
- 3. A method according to claim 2, wherein the particles are impinged on the same surface in proportions approximating the proportions desired in said single crystal III-V alloy.
- 4. A method according to claim 3, wherein said constituents comprise InSb and InAs, the substrate is maintained at a temperature below 405* C. during said depositing step, and said heated surface is maintained at a temperature above 1,500* C. during said vaporization.
- 5. A method according to claim 4, wherein the constituents are 44 mole percent InSb and the balance InAs, the annealing period is approximately 3 weeks, and the annealing temperature is approximately 555* C.
- 6. A method according to claim 1, wherein after said depositing, but prior to said annealing, a film is formed on the surface of the deposited alloy.
- 7. A method according to claim 6, wherein the film is a silicon oxide film.
- 8. A method according to claim 7, wherein the constituents are 44 mol percent InSb and the balance InAs, the substrate is maintained at a temperature below 400* C. during said depositing step, the vaporization is effected by impinging the particles of the constituent III-V compounds on a heated surface maintained at a temperature above 1,500* C. to effect vaporization thereof, and the annealing is effected by maintaining the deposited alloy at a temperature of approximately 555* C. for a period of approximately 3 weeks.
- 9. A method according to claim 7, wherein the constituents are 60 mol percent indium antimonide and the balance indium arsenide.
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US82315069A | 1969-05-08 | 1969-05-08 |
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US3634143A true US3634143A (en) | 1972-01-11 |
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US823150A Expired - Lifetime US3634143A (en) | 1969-05-08 | 1969-05-08 | Preparation of iii{14 v alloys for infrared detectors |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2414367A1 (en) * | 1978-01-16 | 1979-08-10 | Western Electric Co | MOLECULAR BEAM EPITAXY PROCESS WITH PRE-MIX |
US4433343A (en) * | 1981-12-22 | 1984-02-21 | Levine Michael A | Extrinsic infrared detector with dopant site charge-neutralization |
US4468415A (en) * | 1981-03-30 | 1984-08-28 | Asahi Kasei Kogyo Kabushiki Kaisha | Indium-antimony complex crystal semiconductor and process for production thereof |
US4539178A (en) * | 1981-03-30 | 1985-09-03 | Asahi Kasei Kogyo Kabushiki Kaisha | Indium-antimony complex crystal semiconductor and process for production thereof |
US5190613A (en) * | 1988-10-02 | 1993-03-02 | Canon Kabushiki Kaisha | Method for forming crystals |
US5363799A (en) * | 1987-08-08 | 1994-11-15 | Canon Kabushiki Kaisha | Method for growth of crystal |
US20070062333A1 (en) * | 2005-09-20 | 2007-03-22 | Junichi Saito | Method and apparatus for producing metallic ultrafine particles |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3558373A (en) * | 1968-06-05 | 1971-01-26 | Avco Corp | Infrared detecting materials,methods of preparing them,and intermediates |
-
1969
- 1969-05-08 US US823150A patent/US3634143A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3558373A (en) * | 1968-06-05 | 1971-01-26 | Avco Corp | Infrared detecting materials,methods of preparing them,and intermediates |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2414367A1 (en) * | 1978-01-16 | 1979-08-10 | Western Electric Co | MOLECULAR BEAM EPITAXY PROCESS WITH PRE-MIX |
US4468415A (en) * | 1981-03-30 | 1984-08-28 | Asahi Kasei Kogyo Kabushiki Kaisha | Indium-antimony complex crystal semiconductor and process for production thereof |
US4539178A (en) * | 1981-03-30 | 1985-09-03 | Asahi Kasei Kogyo Kabushiki Kaisha | Indium-antimony complex crystal semiconductor and process for production thereof |
US4433343A (en) * | 1981-12-22 | 1984-02-21 | Levine Michael A | Extrinsic infrared detector with dopant site charge-neutralization |
US5363799A (en) * | 1987-08-08 | 1994-11-15 | Canon Kabushiki Kaisha | Method for growth of crystal |
US5190613A (en) * | 1988-10-02 | 1993-03-02 | Canon Kabushiki Kaisha | Method for forming crystals |
US20070062333A1 (en) * | 2005-09-20 | 2007-03-22 | Junichi Saito | Method and apparatus for producing metallic ultrafine particles |
US20090008842A1 (en) * | 2005-09-20 | 2009-01-08 | Junichi Saito | Method and apparatus for producing metallic ultrafine particles |
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