US3152893A - Process for preventing oxidation of hot worked parts - Google Patents

Process for preventing oxidation of hot worked parts Download PDF

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US3152893A
US3152893A US175235A US17523562A US3152893A US 3152893 A US3152893 A US 3152893A US 175235 A US175235 A US 175235A US 17523562 A US17523562 A US 17523562A US 3152893 A US3152893 A US 3152893A
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compact
hot working
hot
impregnant
oxidation
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Storchheim Samuel
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Alloys Research and Manufacturing Corp
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F3/26Impregnating
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/68Temporary coatings or embedding materials applied before or during heat treatment
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/008Using a protective surface layer

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  • This invention relates generally to the hot working of metals and more particularly to an improved method for inhibiting the oxidation of metal parts being hot worked.
  • the parts In fabricating metal parts by powder metallurgy techniques, the parts normally possess some degree of porosity during certain phases of the operation, as for example, after cold compaction. Because the pores may be partially interconnecting, even the innermost regions of the powder fabricated part can be penetrated by contaminants such as oxygen and nitrogen. By reason of this fact and because a porous metal compact presents a greater amount of exposed surface area to the heating atmosphere, the extent of contamination arising in porous metals may be severe as compared to that occurring in cast wrought materials exposed to an oxidizing atmosphere.
  • the extent of oxidation is also affected by the nature of the furnace used.
  • the main'constituents of combustion gases are 00,, nitrogen, water vapor and CO or 0
  • the relative amounts depend upon the degree of mixing and the quantities of fuel introduced into the burners.
  • the scaling or oxidizing gases in a furnace atmosphere are CO water vapor and 0 while the reducing constitucuts are CO and H and unburned hydrocarbons from the fuel.
  • the scaling action of the atmosphere at any temperature and for any time of contact depends upon the relative proportions of these gases in the atmosphere.
  • the atmosphere is normally air which in the case of steel, for example, forms a heavy free scale at all temperatures above 1200 F., the amount of scale increasing with temperature.
  • the metals being processed may consist of powder or particulate-fabricated or cast-wrought materials in the form of discontinuous billets, ingots or continuous slabs.
  • the technique in' accordance with the invention acts to generate a protective gaseous blanket about the part being worked and thereby permit the operations to be conducted in air.
  • the first step 10 in the process involves compaction of oxidation-sensitive metal powder or'finely divided particles above powder size to form a compact.
  • 'Such particles may be formed in the conventional way by atomization of molten metal by the use of air, steam or an inert gas, or by centrifugal spinning, shooting, graining or machining.
  • the compacts may be prepared in various ways, as by cold pressing, hot pressing or by sintering.
  • cold pressing the powders are placed in a die and then subjected to pressure at room temperature, this resulting in partial consolidation and conversion into handleable compacts having up to 98% of the density of the cast-wrought metal.
  • Cold pressing may be eifected by such methods as forging, rolling or explosive compacting.
  • hot pressing hot powders are placed in a'die or suitable containerand subjected to pressure. This technique has the advantage of requiring less pressure than cold compaction to produce a useable compact.
  • the powder may be heatedwithin the die, this being more feasible where the powders are highly sensitive to oxidae tion.
  • comp-acting dies may be avoided'by sintering loose powders for a period oftime and at a temperature appropriate to the metal, to produce a sinter cake through inter-particle bonding, the sinter cake being equivalent to a handleable compact.
  • the powder compacts are impregnated with a hydrocarbon liquid or solid having the prop- I erty of evolving protective vapors during pre-heating.
  • protective vapors are generated either through thermal decomposition of the impregnant or by its combinaiton.
  • carbon dioxide carbon 2 monoxide hydrogen, finely divided carbon particles or mixtures thereof.
  • useful low cost impregnants for this purpose are petroleum oils, both distillates and residuums, petroleum waxes and greases, and such hydrocarbon compounds as camphor, coal tars, pitches and various distillates.
  • impregnant must be such as to have a suitable boiling range relative to the temperature used for preheating the metal compact, and that it contain low concentrations of such contaminants as sulfur, phosphorus and ash.
  • impregnation of the compact may be accomplished by mixing the impregnant with the powders prior to their cold compaction, in which event the impregnant also acts as a die lubricant for the cold compacting operation.
  • One may alternatively impregnate the compact after the powders have been consolidated, this being accomplished by soaking the compact in oil to cause the oil to fill the pores by capillary action.
  • Another technique which results in deeper impregnation is to first immerse the compacts in oil, the vessel containing both the oil and compact being evacuated to drive the oil under pressure into the voids of the compact and into the interconnected pores thereof. Thereafter, the pressure in the vessel is returned to atmosphere.
  • impregnant onto the compact immediately before it enters the pro-heated furnace so that only the outer surfaces thereof are coated, the depth of oil penetration depending on the volume of oil relative to the volume and surface area of the compact and the time interval between spraying of the compact and its entry into the furnace.
  • the amount of impregnant used will of course be determined by the amount of time the heated body is subject to an oxidizing atmosphere.
  • the powder compacts are heated in air or reducing atmospheres, using conventional heating apparatus 12. Heating may be carried out in gas-fired furnaces, induction heated or electric resistance furnaces or in special electrode arrangements wherein an electric current is conveyed through the compact to produce internal heating by virtue of the resistivity of the compact.
  • the heating acts not only to bring the metal to its hot working point but it also results in the thermal decomposition or combustion of the impregnant, with the result that protective vapors are evolved from the pores which envelop the compact with an air excluding blanket.
  • the heated .compact is transferred as rapidly as possible by means of conveyor belts or rollers or other means to the hot working equipment. By this technique it is possible to protect the compact from oxidation during the transfer operation.
  • the pro-heat time to ensure protection of the com pact from oxidation during preheating and transference may be determined visually, that is by observing the size of the flame occurring from oxidation of the protective vapors. It may also be determined empirically, that is by preheating the compacts for varying periods and measuring the mechanical or physical properties of the end product to arrive at optimum conditions.
  • Such materials include iron, steel and ferrous alloys, as well as titanium and the refractory metals such as tungsten, molybdenum, columbium and their alloys.
  • the method is also useful for non-ferrous metals and their alloys. The reason the method is most applicable to metals which oxidize rapidly at temperatures above their recrystallization temperatures is that it is in this very range that metal is hot worked.
  • the pre-heated compact may be hot worked by any rnown process 13, such as rolling, swaging, extrusion and forging.
  • the technique has been described herein in connection with protecting powder-fabricated materials from oxidation during various processing stages (i.e., preheating after cold pressing, pre-heating after hot pressing or pre-heating after forming a sinter cake in a protective atmosphere), the technique is not limited to powder or particle fabricated materials and may be employed to protect small cast wrought forging billets from contamination and scaling during pre-heating as well as during transfer from the pro-heating furnace to the forging press.
  • the technique in accordance with the invention has the same objective as conventional techniques making use of protective atmospheres; namely it seeks to prevent oxidation and nitrogenation of powder fabricated or cast wrought materials when pre-heating the material and transferring it to hot working equipment.
  • the instant technique has many advantages, among which are:
  • the method of hot working metals comprising the steps of forming a coherent body of oxidation sensitive materials, coating at least the surface of said body with a hydrocarbon compound, preheating said coated body to a hot working temperature, said compound having the property of evolving a protective atmosphere at said hot working temperature and hot working said preheated body while said protective atmosphere is being evolved.
  • the method of hot Working an oxidation sensitive metal comprising the steps of cold compacting particles of said metal into a porous compact, impregnating the pores of said compact with a hydrocarbon compound which evolves into a protective vapor at the hot working 7.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Powder Metallurgy (AREA)

Description

Oct. 13, 1964 s. STORCHHEIM 3,152,893
PROCESS FOR PREVENTING OXIDATION OF HOT WORKED PARTS Filed Feb. 23, 1962 Pqocsss Fa firm-"rave 041041-10 OF l/or- A/OQ/(EO B91975 Commnou Or Rayncus 76 Foqn CbnPncr hinges/mm OF Commer- Mr HYQQGCAQbO/Y Campos/n05 Pgwnrwe Or /MPQ5GIYA r50 Conpncr INVEN TOR. Samuel sropwllsln' Ame/vex United States Patent .0
3,152,893 PRQCESS FOR PREVENTING OXIDATEGN HOT WORKED PARTS Samuel Storchheim, Forest Hills, N.Y., assignor to Alloys Research & Manufacturing Corporation, Woodside,
N.Y., a corporation of Delaware Filed Feb. 23, 1962, Ser. No. 175,235 16 Claims. (Cl. 75223) This invention relates generally to the hot working of metals and more particularly to an improved method for inhibiting the oxidation of metal parts being hot worked.
In hot working certain oxidation-sensitive metals, it is conventional to use protective atmospheres when preheating the metal part and also when hot working the part. This practice is essential in order to preclude excessive scaling and to avoid contamination with the nitrogen and oxygen in the air. Such contamination is ordinarily encountered with cast-wrought materials, but it is particularly acute in the the case of powder-fabricated metal parts. I
In fabricating metal parts by powder metallurgy techniques, the parts normally possess some degree of porosity during certain phases of the operation, as for example, after cold compaction. Because the pores may be partially interconnecting, even the innermost regions of the powder fabricated part can be penetrated by contaminants such as oxygen and nitrogen. By reason of this fact and because a porous metal compact presents a greater amount of exposed surface area to the heating atmosphere, the extent of contamination arising in porous metals may be severe as compared to that occurring in cast wrought materials exposed to an oxidizing atmosphere.
The extent of oxidation is also affected by the nature of the furnace used. In fuel furnaces, the main'constituents of combustion gases are 00,, nitrogen, water vapor and CO or 0 The relative amounts depend upon the degree of mixing and the quantities of fuel introduced into the burners. In general, it has been found that the scaling or oxidizing gases in a furnace atmosphere are CO water vapor and 0 while the reducing constitucuts are CO and H and unburned hydrocarbons from the fuel. The scaling action of the atmosphere at any temperature and for any time of contact depends upon the relative proportions of these gases in the atmosphere. In electric or mufile furnaces, on the other hand, the atmosphere is normally air which in the case of steel, for example, forms a heavy free scale at all temperatures above 1200 F., the amount of scale increasing with temperature.
It has therefore been therpractice to pre-heat porous compacts in protective atmospheres, and also when trans:
ferring the compact to hot working equipment, to make 3,152,893 Patented Oct. '13, I964- It is also an object of the invention to provide a method of the above type which makes it possible to use relatively inexpensive heating equipment and to effect a transfer of the heated part in air. While the method is of particular value with powder-fabricated parts, it is also useful with cast wrought materials.
Briefly stated, these objects are accomplished by a low costtechnique utilizing thermal decomposition or combustion of hydrocarbon compounds which are impregnated in the body being processed or are contained on the surface thereof to prevent their oxidation during pro-heating and hot working. The metals being processed may consist of powder or particulate-fabricated or cast-wrought materials in the form of discontinuous billets, ingots or continuous slabs.
Whereas pre-heating and hot working of oxidationsensitive materials. is usually carried out in protective atmospheres, the technique in' accordance with the invention acts to generate a protective gaseous blanket about the part being worked and thereby permit the operations to be conduced in air.
For a better understanding of the invention, aswell as other objects and further features thereof, reference is made to the following detailed description to be read in conjunction with the accompanying drawingwhose single figure is a flow sheet illustrative of the process in accordance with the invention.
Compaction Referring now to drawing, the first step 10 in the process, involves compaction of oxidation-sensitive metal powder or'finely divided particles above powder size to form a compact. 'Such particles may be formed in the conventional way by atomization of molten metal by the use of air, steam or an inert gas, or by centrifugal spinning, shooting, graining or machining.
The compacts may be prepared in various ways, as by cold pressing, hot pressing or by sintering. In cold pressing, the powders are placed in a die and then subjected to pressure at room temperature, this resulting in partial consolidation and conversion into handleable compacts having up to 98% of the density of the cast-wrought metal. Cold pressing may be eifected by such methods as forging, rolling or explosive compacting. i
In hot pressing, hot powders are placed in a'die or suitable containerand subjected to pressure. This technique has the advantage of requiring less pressure than cold compaction to produce a useable compact. Alternatively,
the powder may be heatedwithin the die, this being more feasible where the powders are highly sensitive to oxidae tion. v a
The use of comp-acting dies may be avoided'by sintering loose powders for a period oftime and at a temperature appropriate to the metal, to produce a sinter cake through inter-particle bonding, the sinter cake being equivalent to a handleable compact. e 1
, g I l npregnation I In the second step 11, the powder compacts are impregnated with a hydrocarbon liquid or solid having the prop- I erty of evolving protective vapors during pre-heating. The
protective vapors are generated either through thermal decomposition of the impregnant or by its combinaiton.
with the oxygen in the air to formcarbon dioxide carbon 2 monoxide, hydrogen, finely divided carbon particles or mixtures thereof. Among the useful low cost impregnants for this purpose are petroleum oils, both distillates and residuums, petroleum waxes and greases, and such hydrocarbon compounds as camphor, coal tars, pitches and various distillates.
The choice of impregnant must be such as to have a suitable boiling range relative to the temperature used for preheating the metal compact, and that it contain low concentrations of such contaminants as sulfur, phosphorus and ash.
impregnation of the compact may be accomplished by mixing the impregnant with the powders prior to their cold compaction, in which event the impregnant also acts as a die lubricant for the cold compacting operation. One may alternatively impregnate the compact after the powders have been consolidated, this being accomplished by soaking the compact in oil to cause the oil to fill the pores by capillary action.
Another technique which results in deeper impregnation is to first immerse the compacts in oil, the vessel containing both the oil and compact being evacuated to drive the oil under pressure into the voids of the compact and into the interconnected pores thereof. Thereafter, the pressure in the vessel is returned to atmosphere.
It is also feasible merely to spray the impregnant onto the compact immediately before it enters the pro-heated furnace so that only the outer surfaces thereof are coated, the depth of oil penetration depending on the volume of oil relative to the volume and surface area of the compact and the time interval between spraying of the compact and its entry into the furnace. The amount of impregnant used will of course be determined by the amount of time the heated body is subject to an oxidizing atmosphere.
Subsequent to impregnation, the powder compacts are heated in air or reducing atmospheres, using conventional heating apparatus 12. Heating may be carried out in gas-fired furnaces, induction heated or electric resistance furnaces or in special electrode arrangements wherein an electric current is conveyed through the compact to produce internal heating by virtue of the resistivity of the compact.
The heating acts not only to bring the metal to its hot working point but it also results in the thermal decomposition or combustion of the impregnant, with the result that protective vapors are evolved from the pores which envelop the compact with an air excluding blanket. The heated .compact is transferred as rapidly as possible by means of conveyor belts or rollers or other means to the hot working equipment. By this technique it is possible to protect the compact from oxidation during the transfer operation.
The pro-heat time to ensure protection of the com pact from oxidation during preheating and transference may be determined visually, that is by observing the size of the flame occurring from oxidation of the protective vapors. It may also be determined empirically, that is by preheating the compacts for varying periods and measuring the mechanical or physical properties of the end product to arrive at optimum conditions.
H 0! Working The technique described herein can be used in conjunction with any type of oxidation-sensitive material, but its greatest applicability is with respect to the processing of materials which oxidize readily at temperatures above their recrystallization temperatures.
Such materials include iron, steel and ferrous alloys, as well as titanium and the refractory metals such as tungsten, molybdenum, columbium and their alloys. The method is also useful for non-ferrous metals and their alloys. The reason the method is most applicable to metals which oxidize rapidly at temperatures above their recrystallization temperatures is that it is in this very range that metal is hot worked.
The pre-heated compact may be hot worked by any rnown process 13, such as rolling, swaging, extrusion and forging.
While the technique has been described herein in connection with protecting powder-fabricated materials from oxidation during various processing stages (i.e., preheating after cold pressing, pre-heating after hot pressing or pre-heating after forming a sinter cake in a protective atmosphere), the technique is not limited to powder or particle fabricated materials and may be employed to protect small cast wrought forging billets from contamination and scaling during pre-heating as well as during transfer from the pro-heating furnace to the forging press.
Thus the technique in accordance with the invention has the same objective as conventional techniques making use of protective atmospheres; namely it seeks to prevent oxidation and nitrogenation of powder fabricated or cast wrought materials when pre-heating the material and transferring it to hot working equipment. However the instant technique has many advantages, among which are:
(1) It eliminates the use of protective furnace atmospheres, so that the material to be hot worked may be pie-heated in air with a consequent reduction in the cost of furnace operation.
(2) It requires a less expensive furnace, for no provision need be made for the furnace to contain a protective atmosphere.
(3) It permits the use of low cost heat sources, such as gas or oil operated furnaces rather than the more expensive electrical types.
(4) It does away with the need for shielded conveyors to transfer the pre-heated work, for the transfer may be carried out in air.
(5) It eliminates the hazards incident to the use of combustible protective atmospheres, such as hydrogen, during pre-heating and transfer operations.
(6) It is a low cost process for the impregnants contribute very little to the overall cost of processing.
While there have been disclosed preferred processes in accordance with the invention, it will be obvious that many changes may be made therein without departing from the essential spirit of the invention as set forth in the appended claims.
What is claimed is:
1. The method of hot working metals comprising the steps of forming a coherent body of oxidation sensitive materials, coating at least the surface of said body with a hydrocarbon compound, preheating said coated body to a hot working temperature, said compound having the property of evolving a protective atmosphere at said hot working temperature and hot working said preheated body while said protective atmosphere is being evolved.
2. The method set forth in claim 1 wherein said body is formed by cold rolling powder into a compact.
3. The method set forth in claim 1 wherein said body is cast wrought. V
4. The method set forth in'claim 1 wherein said body is formed by hot rolling powder into a compact.
5. The method set forth in claim 1 wherein said body is formed by sintering metal particles into sinter cake.
6. The method of hot Working an oxidation sensitive metal comprising the steps of cold compacting particles of said metal into a porous compact, impregnating the pores of said compact with a hydrocarbon compound which evolves into a protective vapor at the hot working 7. The method of hot working a metal, as set forth in claim 6, wherein the impregnant is mixed with said powders prior to their compacting.
8. The method as set forth in claim 6, wherein the compact is soaked in a fluid impregnant which fills the pores thereof by capillary action.
9. The method, as set forth in claim 6, wherein the compact is immersed in said impregnant and is introduced by pressure into the pores of said compact.
10. The method, as set forth in claim 6, wherein said impregnant is sprayed on the surface of said compact.
11. The method, as set forth in claim 6, wherein said impregnant is a petroleum product.
12. The method, as set forth in claim 6, wherein said impregnant is camphor.
13. The method, as set forth in claim 6, wherein said impregnant is coal tar.
5 14. The method, as set forth in claim 6-, wherein said impregnant is pitch.
15. The method as set forth in claim 1, wherein said hot working is effected by forging said body.
16. The method as set forth in claim 1, wherein said hot working is effected by extruding said body.
References (fitted in the file of this patent UNITED STATES PATENTS Sherwood Aug. 23, 1932

Claims (1)

1. THE METHOD OF HOT WORKING METALS COMPRISING THE STEPS OF FORMING A COHERENT BODY OF OXIDATION SENSITIVE MATERIALS, COATIG AT LEAST THE SURFACE OF SAID BODY WITH A HYDROCARBON COMPOUND, PREHEATING SAID COATED BODY TO A HOT WORKING TEMPERATUE, SAID COMPOUND HAVING THE PROPERTY OF EVOLVING A PROTECTIVE ATMOSPHERE AT SAID HOT WORKING TEMPERATURE AND HOT WORKING SAID PREHEATED BODY WHILE SAID PROTECTIVE ATMOSPHERE IS BEING EVOLVED.
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3334408A (en) * 1964-10-08 1967-08-08 Metal Innovations Inc Production of powder, strip and other metal products from refined molten metal
US3479258A (en) * 1965-07-01 1969-11-18 Int Nickel Co Method for coating steel with nickel
US4423004A (en) * 1983-03-24 1983-12-27 Sprague Electric Company Treatment of tantalum powder
EP0256116A1 (en) * 1986-02-07 1988-02-24 Aluminum Company Of America Method of heat treatment
EP0368789A1 (en) * 1988-11-10 1990-05-16 Lanxide Technology Company, Lp. A method of thermo-forming a novel metal matrix composite body

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1873223A (en) * 1929-11-13 1932-08-23 Sherwood Patents Ltd Porous metal and method of forming the same
US1974173A (en) * 1930-11-13 1934-09-18 Chrysler Corp Porous metal bearing composition
US2155651A (en) * 1937-06-17 1939-04-25 Hardy Metallurg Corp Manufacture of aluminum alloys
US2187086A (en) * 1938-02-10 1940-01-16 Gen Motors Corp Metallic element and method of making same
US3050386A (en) * 1958-11-22 1962-08-21 Accumulatoren Fabrik Ag Method of producing sinter electrodes

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1873223A (en) * 1929-11-13 1932-08-23 Sherwood Patents Ltd Porous metal and method of forming the same
US1974173A (en) * 1930-11-13 1934-09-18 Chrysler Corp Porous metal bearing composition
US2155651A (en) * 1937-06-17 1939-04-25 Hardy Metallurg Corp Manufacture of aluminum alloys
US2187086A (en) * 1938-02-10 1940-01-16 Gen Motors Corp Metallic element and method of making same
US3050386A (en) * 1958-11-22 1962-08-21 Accumulatoren Fabrik Ag Method of producing sinter electrodes

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3334408A (en) * 1964-10-08 1967-08-08 Metal Innovations Inc Production of powder, strip and other metal products from refined molten metal
US3479258A (en) * 1965-07-01 1969-11-18 Int Nickel Co Method for coating steel with nickel
US4423004A (en) * 1983-03-24 1983-12-27 Sprague Electric Company Treatment of tantalum powder
EP0256116A1 (en) * 1986-02-07 1988-02-24 Aluminum Company Of America Method of heat treatment
EP0256116A4 (en) * 1986-02-07 1989-09-19 Aluminum Co Of America Method of heat treatment.
EP0368789A1 (en) * 1988-11-10 1990-05-16 Lanxide Technology Company, Lp. A method of thermo-forming a novel metal matrix composite body

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