US2155651A - Manufacture of aluminum alloys - Google Patents
Manufacture of aluminum alloys Download PDFInfo
- Publication number
- US2155651A US2155651A US148662A US14866237A US2155651A US 2155651 A US2155651 A US 2155651A US 148662 A US148662 A US 148662A US 14866237 A US14866237 A US 14866237A US 2155651 A US2155651 A US 2155651A
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- Prior art keywords
- aluminum
- alloy
- alloys
- powders
- silicon
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- Expired - Lifetime
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- 229910000838 Al alloy Inorganic materials 0.000 title description 13
- 238000004519 manufacturing process Methods 0.000 title description 5
- 229910045601 alloy Inorganic materials 0.000 description 27
- 239000000956 alloy Substances 0.000 description 27
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 26
- 229910052782 aluminium Inorganic materials 0.000 description 25
- 239000000843 powder Substances 0.000 description 22
- 238000010438 heat treatment Methods 0.000 description 17
- 239000012298 atmosphere Substances 0.000 description 14
- 229910052751 metal Inorganic materials 0.000 description 14
- 239000002184 metal Substances 0.000 description 14
- 230000001427 coherent effect Effects 0.000 description 13
- 239000002245 particle Substances 0.000 description 12
- 239000000203 mixture Substances 0.000 description 10
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 9
- 230000006835 compression Effects 0.000 description 9
- 238000007906 compression Methods 0.000 description 9
- 229910052710 silicon Inorganic materials 0.000 description 9
- 239000010703 silicon Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 238000000034 method Methods 0.000 description 8
- 239000000047 product Substances 0.000 description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 239000004615 ingredient Substances 0.000 description 6
- 230000001590 oxidative effect Effects 0.000 description 6
- 238000010791 quenching Methods 0.000 description 6
- 230000000171 quenching effect Effects 0.000 description 6
- 230000000754 repressing effect Effects 0.000 description 6
- 239000000126 substance Substances 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 4
- 229910052749 magnesium Inorganic materials 0.000 description 4
- 239000011777 magnesium Substances 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 238000003825 pressing Methods 0.000 description 4
- DSSYKIVIOFKYAU-XCBNKYQSSA-N (R)-camphor Chemical compound C1C[C@@]2(C)C(=O)C[C@@H]1C2(C)C DSSYKIVIOFKYAU-XCBNKYQSSA-N 0.000 description 3
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 3
- 241000723346 Cinnamomum camphora Species 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 3
- -1 aluminum compound Chemical class 0.000 description 3
- 229910052791 calcium Inorganic materials 0.000 description 3
- 239000011575 calcium Substances 0.000 description 3
- 229960000846 camphor Drugs 0.000 description 3
- 229930008380 camphor Natural products 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 229910000861 Mg alloy Inorganic materials 0.000 description 2
- 229910000676 Si alloy Inorganic materials 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 229910002065 alloy metal Inorganic materials 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 238000004512 die casting Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 229910000967 As alloy Inorganic materials 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 241000237858 Gastropoda Species 0.000 description 1
- 238000003483 aging Methods 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000007596 consolidation process Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000002274 desiccant Substances 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0408—Light metal alloys
- C22C1/0416—Aluminium-based alloys
Definitions
- This invention relates to aluminum alloys and is concerned principally with the production of such alloys from finely divided metal powders containing a relatively large proportion of aluminum and a relatively small proportion of one or more metals that are alloyable withaluminum.
- the invention aims to produce improved alumiill num alloy metal objects in a dense form or with controlled porosity.
- Aluminum oxidizes very readily, particularly when it is finely divided. Particles of aluminum or aluminum alloys do not bond together when subjected to ordinary sintering operations, even when they have been compressed together under high pressures. I attribute this to the presence of a thin film of aluminum omde or other aluminum compound upon the surface. of the metal particles which prevents the particles from sticking together.
- powders of aluminum or aluminum alloy may be bound together by compressing them into a coherent mass, heating the coherent mass in a desiccated non-oxidizing atmosphere and maintaining the coherent .mass in said atmosphere for a relatively long period of time at a temperature below the melting point of aluminum but at which dlfiusion of aluminum occurs between the particles.
- a reducing atmosphere is preferable, but oddly enough, any non-oxidizing atmosphere is suitable provided that it is substantially desiccated.
- the resulting alloy mass may be tempered or agehardened provided that the mass is quenched from an elevated temperature prior to the tempering or age-hardening operation.
- the aluminum alloys which result from the practice of my invention may be produced in any desired density ranging from slightly above the density of the unconsolidated powders to the density of wrought aluminum alloys.
- a porous aluminum alloy may be produced in the process of my invention by employing a pressure such that the resulting coherent mass contains voids or by including in the mixture of finely divided metals volatile substances such as camphor or a volatile salt. If such a volatile substance is .employed,
- the powders employed should be very finely divided. Preferably, they should pass through 325 mesh, although the presence of some minus 200 mesh material may be tolerated. Moreover, they should be employed in a fresh condition with a minimum of oxidation productions on their-surfaces.
- the aluminum and the alloy ingredients such as magnesium, copper, nickel, manganese, silicon, iron, chromium and zinc may be employed as powders of the elements or as alloy powders.
- an alloy metal object there may be added to the master alloy suchv proportions of magnesium or other metals in finely divided form as may be required for the particular product. In all cases the powders employed must be thoroughly mixed prior to compression.
- the powdered mixture formed as described above is subjected to compression employing pressures of from 5 to 100 tons per square inch. No binding material is necessary, although the presence of camphor or a volatile salt or the like is desirable when an alloy of controlled porosity is required.
- the slugs'or other consolidated pieces which are formed in the compression operation are subjected to heat treatment.
- the treatment temperature should be approximately two-thirds of the weighted average of the melting points of the elements present in the mass.
- the heat treatment should take place at temperatures ranging from 450 to 650 C., and should endurev from 30 minutes to 24 hours.
- the heating must be carried out in a non-oxidizing atmos phere from which substantially all water has been removed. Thus the heating may be conducted in a vacuum or in a desiccated atmosphere of hydrogen, city gas, natural gas, carbon monoxide or carbon dioxide.
- the resulting alloy should be subjected to quenching in order to render it amenable to hardening by subsequent heating or aging.
- This quenching may take place immediately after heat treatment, in which case the hot alloy is removed from the furnace and plunged directly into a quenching bath, (preferably of water at about 20 C.) or the heat treated object may be allowed to cool down slowly, to-atmospheric temperatures or thereabouts and later reheated and quenched. In this latter procedure the heat treated alloys should not be allowed to cool at a rate greater than 600 C. per hour.
- the cooling should take place in the non-oxidizing atmosphere.
- the cooled object should be reheated to a temperature ranging from 450 C. to 550 C.
- the quenched alloys formed from aluminum powders as hereinbefore described may be tempered and hardened by heating them to and maintaining them at a temperature ranging from 100 to 200 C. for a time ranging from 15 minutes to 24 hours. They may also ,be age-hardened (precipitation hardening) at room temperature by retaining them at this temperature for a period ranging from one hour to thirty .days.
- the heat treated alloy should be subjected to a second pressing or repressing operation either before or after quenching.
- Aluminum and silicon powders in a relatively clean condition and advantageously of sufficient fineness to pass 200 to 325 mesh screens are thoroughly mixed. If a porous alloy is desired non-metallic volatile ingredients such as camphor may also be added and thoroughly incor porated. of the mixture should be as finely divided as the metallic powders.
- the aluminum may constitute from '70 to 97% by weight of the metallic constituents of the mixture and the silicon from 3 to 30% by weight.
- the aluminum should constitute from to by weight of the mixture, the balance being made up of silicon.
- the powders after thorough mixing are placed in a mold and subjected to compression un icr a piston or the like. As indicated hereinbefore the powders subjected to compression should be in a relatively cold condition.
- the pressure employed will vary depending upon the desired den sity of the final product. If a very porous strucrate not to exceed 600 0. per hour.
- the pressure may well be as low as five tons per square inch(or even less provided that a coherent mass is formed).
- the pressure employed may be as high as tons per square inch.
- a pressure of 45 to 65 tons per square inch is generally satisfactory.
- the object produced in the compression operation is relatively fragile but sufficiently coherent to stand considerable handling and to hold together during the heating operation.
- the heating operation is designed to bind the particles of metalpowder securely together by diffusion welding or alloying.
- a closed furnace is employed. Reducing or inert atmosphere is maintained within the furnace by passing a current of hydrogen gas or the like through it.
- the hydrogen or other gas supplied to the furnace should first be passed over a desiccating agent such as metallic calcium. It is desirable to maintain a boat of metallic calcium within the furnace during the sintering operation as a further safeguard against the presence of moisture.
- the temperature of treatment should be in the neighborhood of 500 C. This temperature is high enough to permit diffusion Welding without melting either the silicon -or the aluminum and is also high enough to expel any volatile material which has been included in the mass for purposes of developing porosity. The volatile matter escapes as vapors and in escaping forms minute channels through the product.
- the coherent mass is held at the elevated temperature for about 8 hours. Thereafter, it is either quenched immediately in water or permitted to cool down to room temperature at a In case the alloy is allowed to cool, it is then heated up to from 450 to 550 0., held at this temperature for from one-half to two hours in a non-oxidizing atmosphere, and then quenched in water at room temperature.
- a silicon aluminum or other aluminum alloy produced as described hereinbefore is satisfactory for many uses without further treatment.
- the repressing operation may increase the strength of the product but its principal function is to increase its density.
- the repressing operation should be carried out in substantially the same manner as the original pressing operation. If the original pressing operation has been conducted with the metal powder in suitable dies, the same dies or dies of virtually the same size and shape may be employed in the repressing operation. In general the pressures employed in the repressing operation range from 45 to 65 tons per square inch.
- the kind and proportion of the metal alloying ingredients employed with the aluminum vary Weight, with silicon making up the balance.
- Aluminum silicon-copper-nickel magnesium alloys should correspond to the following composition:
- a process for producing a porous mass of aluminum alloy comprising compressing into a. coherent mass a mixture of a solid substance that is volatile at a relatively low temperature and finely-divided metal powders containing a relatively large proportion of aluminum and a relatively small proportion of a metal alloyable with aluminum and heating said coherent mass for a considerable perlodof time at a temperature below the melting point of aluminum but at which diffusion of aluminum occurs between the metal powder particles while said particles remain in a substantially solid condition, said temperature being above the volatilizing temperature of the volatile substance and said heating taking place in a desiccated non-oxidiz- K ing atmosphere, whereby the metal powder particles become welded together and the volatile substance is expelled to produce a porous mass.
- a process for producing aluminum alloys which comprises compressing into a coherent mass finely-divided metal powders containing a relatively large proportion of aluminum powder particles having relatively small amounts of oxidation products on the surface thereof and a relatively small proportion of a metallic alloying ingredient, and heating said coherent mass for a considerable period of time at a temperature at which the metal powder particles remain in a solid condition but at which diifusion of aluminum occurs between the metal powder particles, said heating taking place in the presence of metallic calcium in an atmosphere that is desiccated and inert with respect to metallic aluminum.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Description
Patented as, less MANUFACE F AL cries M ALLOYS Qlaus Guenter Goetzel, New York, N. Y.,"assignor to Hardy Metallurgical Corporation, a corporation oi Delaware No Erawing.
Application June 17, 1937,
Serial No. 148,662
2 Claims.
This invention relates to aluminum alloys and is concerned principally with the production of such alloys from finely divided metal powders containing a relatively large proportion of aluminum and a relatively small proportion of one or more metals that are alloyable withaluminum.
' The invention aims to produce improved alumiill num alloy metal objects in a dense form or with controlled porosity.
Aluminum oxidizes very readily, particularly when it is finely divided. Particles of aluminum or aluminum alloys do not bond together when subjected to ordinary sintering operations, even when they have been compressed together under high pressures. I attribute this to the presence of a thin film of aluminum omde or other aluminum compound upon the surface. of the metal particles which prevents the particles from sticking together. However, as a result of my investigations I have discovered that powders of aluminum or aluminum alloy may be bound together by compressing them into a coherent mass, heating the coherent mass in a desiccated non-oxidizing atmosphere and maintaining the coherent .mass in said atmosphere for a relatively long period of time at a temperature below the melting point of aluminum but at which dlfiusion of aluminum occurs between the particles. Thus by diffusion welding the particles become bound together, despite the presence of relatively small amounts of oxidation products on the surface of the powder particles. A reducing atmosphere is preferable, but oddly enough, any non-oxidizing atmosphere is suitable provided that it is substantially desiccated.
If copper, nickel, manganese, silicon, iron, chromium, zinc or other metal which alloys with aluminum is included with the finely divided aluminum that is subjected to the compression and heat treatment operation described above, the resulting alloy mass may be tempered or agehardened provided that the mass is quenched from an elevated temperature prior to the tempering or age-hardening operation.
The aluminum alloys which result from the practice of my invention may be produced in any desired density ranging from slightly above the density of the unconsolidated powders to the density of wrought aluminum alloys. A porous aluminum alloy may be produced in the process of my invention by employing a pressure such that the resulting coherent mass contains voids or by including in the mixture of finely divided metals volatile substances such as camphor or a volatile salt. If such a volatile substance is .employed,
high pressures may be used and a dense mass formed. Thereafter, the volatile material is driven off during the heating operation so that the desired porous structure results.
The powders employed should be very finely divided. Preferably, they should pass through 325 mesh, although the presence of some minus 200 mesh material may be tolerated. Moreover, they should be employed in a fresh condition with a minimum of oxidation productions on their-surfaces. The aluminum and the alloy ingredients such as magnesium, copper, nickel, manganese, silicon, iron, chromium and zinc may be employed as powders of the elements or as alloy powders. Thus I have found it convenient to form a master alloy of aluminum arid silicon in powdered form by atomizing the molten alloy in an atmosphere of hydrogen or city gas.
In forming an alloy metal object, there may be added to the master alloy suchv proportions of magnesium or other metals in finely divided form as may be required for the particular product. In all cases the powders employed must be thoroughly mixed prior to compression. The
1 powders should be retained in' a dry condition during and prior to compression in order to avoid the formation of excessive amounts of oxidation products.
The powdered mixture formed as described above is subjected to compression employing pressures of from 5 to 100 tons per square inch. No binding material is necessary, although the presence of camphor or a volatile salt or the like is desirable when an alloy of controlled porosity is required.
Better results are obtained when the powders are compressed into a coherent mass in a relatively cold condition. Compression of hot powders into a coherent mass is not recommended.
The slugs'or other consolidated pieces which are formed in the compression operation are subjected to heat treatment. The treatment temperature should be approximately two-thirds of the weighted average of the melting points of the elements present in the mass. Generally, the heat treatment should take place at temperatures ranging from 450 to 650 C., and should endurev from 30 minutes to 24 hours. The heating must be carried out in a non-oxidizing atmos phere from which substantially all water has been removed. Thus the heating may be conducted in a vacuum or in a desiccated atmosphere of hydrogen, city gas, natural gas, carbon monoxide or carbon dioxide.
After heat treatment the resulting alloy should be subjected to quenching in order to render it amenable to hardening by subsequent heating or aging. This quenching may take place immediately after heat treatment, in which case the hot alloy is removed from the furnace and plunged directly into a quenching bath, (preferably of water at about 20 C.) or the heat treated object may be allowed to cool down slowly, to-atmospheric temperatures or thereabouts and later reheated and quenched. In this latter procedure the heat treated alloys should not be allowed to cool at a rate greater than 600 C. per hour. The cooling should take place in the non-oxidizing atmosphere. The cooled object should be reheated to a temperature ranging from 450 C. to 550 C. and held at this temperature for onehalf to two hours in a non-oxidizing atmosphere prior to quenching (preferably in water at about The quenched alloys formed from aluminum powders as hereinbefore described may be tempered and hardened by heating them to and maintaining them at a temperature ranging from 100 to 200 C. for a time ranging from 15 minutes to 24 hours. They may also ,be age-hardened (precipitation hardening) at room temperature by retaining them at this temperature for a period ranging from one hour to thirty .days.
If it is desired to produce a very dense or hard aluminum alloy the heat treated alloy should be subjected to a second pressing or repressing operation either before or after quenching.
Aluminum alloys prepared in the manner described briefiy above possess physical properties considerably superior to those of corresponding alloys prepared by heretofore customary methods, for example, casting. Moreover, my invention possesses an advantage in that it permits the manufacture of alloys of any desired degree of porosity and also permits the production of alloys of uniform porosity. A further advantage resides in the fact that alloys may be prepared in accordance with the invention with proportions of ingredients that would not be possible or practical in cast alloys. Fourthly, porous alloys may be prepared according to my invention which possess a hardness and ,malleability corresponding to dense cast alloys.
My invention will be more thoroughly understood in the light of the following detailed description of the preparation of an aluminum silicon alloy according to the process of my invention.
Aluminum and silicon powders in a relatively clean condition and advantageously of sufficient fineness to pass 200 to 325 mesh screens are thoroughly mixed. If a porous alloy is desired non-metallic volatile ingredients such as camphor may also be added and thoroughly incor porated. of the mixture should be as finely divided as the metallic powders.
The aluminum may constitute from '70 to 97% by weight of the metallic constituents of the mixture and the silicon from 3 to 30% by weight. Preferably, the aluminum should constitute from to by weight of the mixture, the balance being made up of silicon.
The powders after thorough mixing are placed in a mold and subjected to compression un icr a piston or the like. As indicated hereinbefore the powders subjected to compression should be in a relatively cold condition. The pressure employed will vary depending upon the desired den sity of the final product. If a very porous strucrate not to exceed 600 0. per hour.
volatile non-metallic ingredients ture is desired the pressure may well be as low as five tons per square inch(or even less provided that a coherent mass is formed). When very dense objects are desired, the pressure employed may be as high as tons per square inch. For objects having a density comparable with the density of cast or forged aluminum alloys, a pressure of 45 to 65 tons per square inch is generally satisfactory.
The object produced in the compression operation is relatively fragile but sufficiently coherent to stand considerable handling and to hold together during the heating operation.
The heating operation is designed to bind the particles of metalpowder securely together by diffusion welding or alloying. A closed furnace is employed. Reducing or inert atmosphere is maintained within the furnace by passing a current of hydrogen gas or the like through it. In order to assure that the atmosphere within the furnace is completely desiccated the hydrogen or other gas supplied to the furnace should first be passed over a desiccating agent such as metallic calcium. It is desirable to maintain a boat of metallic calcium within the furnace during the sintering operation as a further safeguard against the presence of moisture.
In the case of the aluminum silicon alloy described hereinbefore, the temperature of treatment should be in the neighborhood of 500 C. This temperature is high enough to permit diffusion Welding without melting either the silicon -or the aluminum and is also high enough to expel any volatile material which has been included in the mass for purposes of developing porosity. The volatile matter escapes as vapors and in escaping forms minute channels through the product.
In the event that an absorptive porous structure is desired, it is better to form a porous alloy by including volatile material in the primary mixture, as contrasted with employing no volatile material and relying upon a low pressure of consolidation to give the required porosity. This is because the volatile material in escaping assures the presence of channels to the outside surface of the alloy object, whereas the other method may result in blind pores which cannot absorb.
The coherent mass is held at the elevated temperature for about 8 hours. Thereafter, it is either quenched immediately in water or permitted to cool down to room temperature at a In case the alloy is allowed to cool, it is then heated up to from 450 to 550 0., held at this temperature for from one-half to two hours in a non-oxidizing atmosphere, and then quenched in water at room temperature.
A silicon aluminum or other aluminum alloy produced as described hereinbefore is satisfactory for many uses without further treatment. However, it may be desirable to increase its strength by a second pressing or repressing operation which may occur either before or after quenching and with the material in a substantially cold condition. The repressing operation may increase the strength of the product but its principal function is to increase its density. The repressing operation should be carried out in substantially the same manner as the original pressing operation. If the original pressing operation has been conducted with the metal powder in suitable dies, the same dies or dies of virtually the same size and shape may be employed in the repressing operation. In general the pressures employed in the repressing operation range from 45 to 65 tons per square inch.
The kind and proportion of the metal alloying ingredients employed with the aluminum vary Weight, with silicon making up the balance.
When aluminum-silicon-copper-magnesium alloys are desired the following are satisfactory composition ranges:
Per cent Aluminum 83 to 96 Silicon 3 to 10 Copper 1 to 5 Magnesium 0.1 to 2 Aluminum silicon-copper-nickel magnesium alloys should correspond to the following composition:
Per cent Aluminum 61 to 94 Silicon 5 to 25 Copper 0.5 to 5 Nickel 0.5 to 5 Magnesium .1 to 4 'only by forging, by die-casting operations or by complicated machining processes. The method bf the invention achieves substantially the simplicity and high output rate of die-casting opera tions while permitting the use of alloy compositions that cannot be die-cast and hence have been fabricated heretofore largely by complex machining operations. Alloy products prepared in accordance with the invention are especially suited for use wherever a; combination of strength, lightness and accuracy of configuration is important.
I claim:
1. In a process for producing a porous mass of aluminum alloy, the improvement which comprises compressing into a. coherent mass a mixture of a solid substance that is volatile at a relatively low temperature and finely-divided metal powders containing a relatively large proportion of aluminum and a relatively small proportion of a metal alloyable with aluminum and heating said coherent mass for a considerable perlodof time at a temperature below the melting point of aluminum but at which diffusion of aluminum occurs between the metal powder particles while said particles remain in a substantially solid condition, said temperature being above the volatilizing temperature of the volatile substance and said heating taking place in a desiccated non-oxidiz- K ing atmosphere, whereby the metal powder particles become welded together and the volatile substance is expelled to produce a porous mass.
2. A process for producing aluminum alloys which comprises compressing into a coherent mass finely-divided metal powders containing a relatively large proportion of aluminum powder particles having relatively small amounts of oxidation products on the surface thereof and a relatively small proportion of a metallic alloying ingredient, and heating said coherent mass for a considerable period of time at a temperature at which the metal powder particles remain in a solid condition but at which diifusion of aluminum occurs between the metal powder particles, said heating taking place in the presence of metallic calcium in an atmosphere that is desiccated and inert with respect to metallic aluminum.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US148662A US2155651A (en) | 1937-06-17 | 1937-06-17 | Manufacture of aluminum alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US148662A US2155651A (en) | 1937-06-17 | 1937-06-17 | Manufacture of aluminum alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2155651A true US2155651A (en) | 1939-04-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US148662A Expired - Lifetime US2155651A (en) | 1937-06-17 | 1937-06-17 | Manufacture of aluminum alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2155651A (en) |
Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2673310A (en) * | 1949-09-07 | 1954-03-23 | Deutsche Edelstahlwerke Ag | Permanent magnet |
| US2796660A (en) * | 1946-07-17 | 1957-06-25 | Aluminium Ind Ag | Method for the production of light metal articles |
| US2987816A (en) * | 1956-12-10 | 1961-06-13 | Robert A Noland | Bonding aluminum metals |
| US3073294A (en) * | 1959-07-02 | 1963-01-15 | Eaton Mfg Co | Aluminum valve |
| US3152893A (en) * | 1962-02-23 | 1964-10-13 | Alloys Res & Mfg Corp | Process for preventing oxidation of hot worked parts |
| US3210166A (en) * | 1959-03-24 | 1965-10-05 | Minnesota Mining & Mfg | Cast porous metal |
| US3232754A (en) * | 1961-11-07 | 1966-02-01 | Alloys Res & Mfg Corp | Porous metallic bodies and fabrication methods therefor |
| US3250838A (en) * | 1964-08-04 | 1966-05-10 | Alloys Res & Mfg Corp | Techniques for compacting aluminum powder mixtures |
| US3273833A (en) * | 1965-01-21 | 1966-09-20 | Dow Chemical Co | Airfoil structure |
| US3297435A (en) * | 1963-03-22 | 1967-01-10 | Int Nickel Co | Production of heat-treatable aluminum casting alloy |
| US3301671A (en) * | 1964-03-03 | 1967-01-31 | Alloys Res & Mfg Corp | Aluminous sintered parts and techniques for fabricating same |
| US3331684A (en) * | 1965-01-26 | 1967-07-18 | Alloys Res & Mfg Corp | Method of forming porous aluminum strip |
| US3392015A (en) * | 1965-08-24 | 1968-07-09 | Int Nickel Co | Aluminum-base alloy for use at elevated temperatures |
| US3712589A (en) * | 1971-06-24 | 1973-01-23 | Olin Corp | Porous or foamed metal energy absorption device |
| US3860420A (en) * | 1970-12-21 | 1975-01-14 | Air Reduction | Method of making welding rods by sintering in the presence of a liquid phase |
| US3901691A (en) * | 1972-01-20 | 1975-08-26 | Ethyl Corp | Aluminum-silicon alloy |
| US3996047A (en) * | 1974-03-07 | 1976-12-07 | Airco, Inc. | Method and mold for producing round rods by powder metallurgy |
| US4038738A (en) * | 1975-01-10 | 1977-08-02 | Uddeholms Aktiebolag | Method and means for the production of bar stock from metal powder |
| US4045857A (en) * | 1973-11-08 | 1977-09-06 | Agency Of Industrial Science & Technology | Method for manufacture of aluminum sheet and sintered high-density aluminum laminate by direct powder rolling process |
| US4099314A (en) * | 1976-03-10 | 1978-07-11 | Societe De Vente De L'aluminium Pechiney | Method of producing hollow bodies in aluminum-silicon alloys by powder-extrusion |
| US4224267A (en) * | 1978-03-28 | 1980-09-23 | Westinghouse Electric Corp. | Wire, rod, stick, and the like, with or without fluxing agent for welding applications |
| US5023051A (en) * | 1989-12-04 | 1991-06-11 | Leggett & Platt Incorporated | Hypoeutectic aluminum silicon magnesium nickel and phosphorus alloy |
| US5304343A (en) * | 1989-12-29 | 1994-04-19 | Showa Denko K.K. | Aluminum-alloy powder, sintered aluminum-alloy, and method for producing the sintered aluminum-alloy |
| US20050036899A1 (en) * | 2002-01-29 | 2005-02-17 | Rene Lindenau | Method for producing sintered components from a sinterable material |
-
1937
- 1937-06-17 US US148662A patent/US2155651A/en not_active Expired - Lifetime
Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2796660A (en) * | 1946-07-17 | 1957-06-25 | Aluminium Ind Ag | Method for the production of light metal articles |
| US2673310A (en) * | 1949-09-07 | 1954-03-23 | Deutsche Edelstahlwerke Ag | Permanent magnet |
| US2987816A (en) * | 1956-12-10 | 1961-06-13 | Robert A Noland | Bonding aluminum metals |
| US3210166A (en) * | 1959-03-24 | 1965-10-05 | Minnesota Mining & Mfg | Cast porous metal |
| US3073294A (en) * | 1959-07-02 | 1963-01-15 | Eaton Mfg Co | Aluminum valve |
| US3232754A (en) * | 1961-11-07 | 1966-02-01 | Alloys Res & Mfg Corp | Porous metallic bodies and fabrication methods therefor |
| US3152893A (en) * | 1962-02-23 | 1964-10-13 | Alloys Res & Mfg Corp | Process for preventing oxidation of hot worked parts |
| US3297435A (en) * | 1963-03-22 | 1967-01-10 | Int Nickel Co | Production of heat-treatable aluminum casting alloy |
| US3301671A (en) * | 1964-03-03 | 1967-01-31 | Alloys Res & Mfg Corp | Aluminous sintered parts and techniques for fabricating same |
| US3250838A (en) * | 1964-08-04 | 1966-05-10 | Alloys Res & Mfg Corp | Techniques for compacting aluminum powder mixtures |
| US3273833A (en) * | 1965-01-21 | 1966-09-20 | Dow Chemical Co | Airfoil structure |
| US3331684A (en) * | 1965-01-26 | 1967-07-18 | Alloys Res & Mfg Corp | Method of forming porous aluminum strip |
| US3392015A (en) * | 1965-08-24 | 1968-07-09 | Int Nickel Co | Aluminum-base alloy for use at elevated temperatures |
| US3860420A (en) * | 1970-12-21 | 1975-01-14 | Air Reduction | Method of making welding rods by sintering in the presence of a liquid phase |
| US3712589A (en) * | 1971-06-24 | 1973-01-23 | Olin Corp | Porous or foamed metal energy absorption device |
| US3901691A (en) * | 1972-01-20 | 1975-08-26 | Ethyl Corp | Aluminum-silicon alloy |
| US4045857A (en) * | 1973-11-08 | 1977-09-06 | Agency Of Industrial Science & Technology | Method for manufacture of aluminum sheet and sintered high-density aluminum laminate by direct powder rolling process |
| US3996047A (en) * | 1974-03-07 | 1976-12-07 | Airco, Inc. | Method and mold for producing round rods by powder metallurgy |
| US4038738A (en) * | 1975-01-10 | 1977-08-02 | Uddeholms Aktiebolag | Method and means for the production of bar stock from metal powder |
| US4099314A (en) * | 1976-03-10 | 1978-07-11 | Societe De Vente De L'aluminium Pechiney | Method of producing hollow bodies in aluminum-silicon alloys by powder-extrusion |
| US4224267A (en) * | 1978-03-28 | 1980-09-23 | Westinghouse Electric Corp. | Wire, rod, stick, and the like, with or without fluxing agent for welding applications |
| US5023051A (en) * | 1989-12-04 | 1991-06-11 | Leggett & Platt Incorporated | Hypoeutectic aluminum silicon magnesium nickel and phosphorus alloy |
| US5304343A (en) * | 1989-12-29 | 1994-04-19 | Showa Denko K.K. | Aluminum-alloy powder, sintered aluminum-alloy, and method for producing the sintered aluminum-alloy |
| US20050036899A1 (en) * | 2002-01-29 | 2005-02-17 | Rene Lindenau | Method for producing sintered components from a sinterable material |
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