US2287251A - Manufacture of nonporous metal articles - Google Patents

Manufacture of nonporous metal articles Download PDF

Info

Publication number
US2287251A
US2287251A US343492A US34349240A US2287251A US 2287251 A US2287251 A US 2287251A US 343492 A US343492 A US 343492A US 34349240 A US34349240 A US 34349240A US 2287251 A US2287251 A US 2287251A
Authority
US
United States
Prior art keywords
manufacture
magnesium
manganese
aluminium
pressing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US343492A
Inventor
Jones William David
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of US2287251A publication Critical patent/US2287251A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0408Light metal alloys
    • C22C1/0416Aluminium-based alloys
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S29/00Metal working
    • Y10S29/031Pressing powder with other step

Definitions

  • an aluminium alloy powder containing a small proportion of one or more of the elements manganese, magnesium, antimony or titanium or a mixture of an aluminium or aluminium alloy powder and a powder of one or more of the aforesaid elements or an alloy containing the same is subjected to pressure at an elevated temperature of at least 300 C. but below the point of general fusion, for example a temperature of between 400 and 600 C.
  • a particularly suitable group of alloys are those containing up to 20% of magnesium and up to 5% of manganese for example alloys containing 0.2 to 3.5% of manganese and 1.5 to 6% of magnesium the balance being aluminium.
  • the process according to the invention may be eflected without the use of protective atmosphere although if desired a protective atmosphere may be used.
  • the powders will be subjected to pressing in the cold before subjecting them to pressure at an elevated temperature and such cold pressure may if'desired be efiected at a high pressure, for example more than 5 tons per square inch.
  • the particles of the powders employed may be of varying shape; for example they may be spherical or angular, for example in the form of lamellae.
  • the particles should not be finer than about 20 microns or even 40 microns but on the other hand they should pass through a 100 mesh sieve.
  • Powder particles of lamellae form are particles such as rectangular chips having one long dimension and two short dimensions as distinguished from flakes, spheroids or granules.
  • the powders may, if desired, be mixed with other elements or alloys or compounds for example metals which would tend to rupture or dissolve oxide films or metals which would be molten cr-which would react with the aluminium titanium up to 5%, silicon up to 5%, iron up to 1%, cerium up to 1%, copper up to 5% and sodium up to 1%.
  • calcium hydride, titanium hydride, zirconium hydride, or alkali metal hydrides may be added as described in my United Kingdom Specification No. 503,874, whilst furthermore non-metallic elements or fluxes such as mixtures of fluorides and chlorides may be added.
  • a temperature of between about 400 and 600 C. is particularly advantageous since these are lower temperatures than those employed in die casting and are so low that metal dies will withstand the temperatures.
  • the heating may be effected electrically by resistance or induction.
  • the die in which the hot pressing is effected may, if desired, be non-metallic.
  • the speed of operation may in some cases be of importance.
  • the speed of pressing it is possible to obtain a better cohesion of the particles if the speed of pressing is so adjusted that air is expelled whilst at the same time the powder is not blown out of the die whilst, furthermore, it is possible to arrange by suitably choosing. the speed of pressing that the lamellae shapedparticles are all disposed substantially parallel to each other,
  • the powdered aluminium alloy can be manufactured by comminuting by ball milling, disintegrating, or grinding the massive alloy in a protective atmosphere so that no oxidation takes place, and then introducing the powder into dies and cold pressing it in dies and then hot pressing, conducting the whole operaor with each other to produce a liquid phase tions in a protective atmosphere.
  • the rate of cooling of the product can be controlled, or separate heat treatments may be applied in order to modify the mechanical properties thereof.
  • the product After the hot pressing the product can be brought to the desired size if necessary in a press and it can also be mechanically treated to modify its density or to alter its physical constitution such as by forging, stamping and rolling, if desired whilst still hot.
  • the product of the invention may have a different composition in difl'erent parts thereof for example by using layers of powders of different composition as the initial material.
  • suitable alloys for use in the process of the present invention are alloys containing 1.0 to 1.2% of manganese, 1.8 to 2.0% magnesium, up to 0.2% of antimony, 0.7% of silicon and the rest aluminium, 5.0 to 10% of magnesium and the rest aluminium, 2% of magnesium, 1.2 to
  • the process of the present invention has numerous advantages for example cheapness of manufacture, excellent mechanical properties of the product, particularly strength and ductility,
  • a metal article comprising a non-porous, compacted, agglomerated mass of particles of metal powder consisting of 1.0 to 1.2% manganese, 1.8 to 2.0% magnesium, 0.2% antimony, 0.7% silicon and the rest aluminum having a tensile strength of 17 tons per square inch and an elongation of 14%.
  • a process forthe manufacture of non-porous metal articles of, high density, high tensile strength and high elongation comprising cold pressing a pulverulent mass of an aluminum alloy consisting of 1.5 to.6% magnesium, 2 to 3.5% manganese, an eilective amount up to 5% silicon, an effective amount up to 1% antimony and the balance aluminum at a pressure of more than five tons per square inch to form a compact, and again pressing the compact at a pressure less than that employed in the cold pressing while at a temperature of about 400 to 600 C. to convert the compact into a non-porous body of high density and high tensile strength.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Description

Patented June 23, 1942 UNITED STATES PATENT OFFICE MANUFACTURE di zi r ironous METAL William David Jones, London, England No Drawing. Application July 1, 1940, Serial No. 343,492. In- Great Britain July '1, 1939 2 Claims. (01. 15- 22 This invention relates" to the-manufacture of metal articles ormasses and has as its principal object to produce non-porous articles or masses having a high tensile strength and elongation from aluminium alloy powders.
According to the process of the present invention an aluminium alloy powder containing a small proportion of one or more of the elements manganese, magnesium, antimony or titanium or a mixture of an aluminium or aluminium alloy powder and a powder of one or more of the aforesaid elements or an alloy containing the same is subjected to pressure at an elevated temperature of at least 300 C. but below the point of general fusion, for example a temperature of between 400 and 600 C.
A particularly suitable group of alloys are those containing up to 20% of magnesium and up to 5% of manganese for example alloys containing 0.2 to 3.5% of manganese and 1.5 to 6% of magnesium the balance being aluminium.
The process according to the invention may be eflected without the use of protective atmosphere although if desired a protective atmosphere may be used. In general the powders will be subjected to pressing in the cold before subjecting them to pressure at an elevated temperature and such cold pressure may if'desired be efiected at a high pressure, for example more than 5 tons per square inch.
The particles of the powders employed may be of varying shape; for example they may be spherical or angular, for example in the form of lamellae. Preferably the particles should not be finer than about 20 microns or even 40 microns but on the other hand they should pass through a 100 mesh sieve.
Powder particles of lamellae form are particles such as rectangular chips having one long dimension and two short dimensions as distinguished from flakes, spheroids or granules.
In addition to the elements mentioned above, the powders may, if desired, be mixed with other elements or alloys or compounds for example metals which would tend to rupture or dissolve oxide films or metals which would be molten cr-which would react with the aluminium titanium up to 5%, silicon up to 5%, iron up to 1%, cerium up to 1%, copper up to 5% and sodium up to 1%.
An alloy containing 1.5 to 6% of magnesium, 0.2 to 3.5% of manganese, an effective amount upon to 5% of silicon, an effective amount up to 1% of antimony and the balance aluminum was found to be desirable.-
If desired, calcium hydride, titanium hydride, zirconium hydride, or alkali metal hydrides may be added as described in my United Kingdom Specification No. 503,874, whilst furthermore non-metallic elements or fluxes such as mixtures of fluorides and chlorides may be added.
The use of a temperature of between about 400 and 600 C. is particularly advantageous since these are lower temperatures than those employed in die casting and are so low that metal dies will withstand the temperatures.
The heating may be effected electrically by resistance or induction.
The die in which the hot pressing is effected may, if desired, be non-metallic.
In effecting the hot pressing the speed of operation may in some cases be of importance. Thus for example when using powders having lamellae shaped particles it is possible to obtain a better cohesion of the particles if the speed of pressing is so adjusted that air is expelled whilst at the same time the powder is not blown out of the die whilst, furthermore, it is possible to arrange by suitably choosing. the speed of pressing that the lamellae shapedparticles are all disposed substantially parallel to each other,
thus giving better cohesive properties.
In cases where oxide content is very detrimental there is the possibility of obtaining a pressing which contains no oxide at all. This can be effected by combining together a process of powder manufacture with the process of pressing. For example the powdered aluminium alloy can be manufactured by comminuting by ball milling, disintegrating, or grinding the massive alloy in a protective atmosphere so that no oxidation takes place, and then introducing the powder into dies and cold pressing it in dies and then hot pressing, conducting the whole operaor with each other to produce a liquid phase tions in a protective atmosphere.
After the hot pressing operation the rate of cooling of the product can be controlled, or separate heat treatments may be applied in order to modify the mechanical properties thereof.
After the hot pressing the product can be brought to the desired size if necessary in a press and it can also be mechanically treated to modify its density or to alter its physical constitution such as by forging, stamping and rolling, if desired whilst still hot.
If desired the product of the invention may have a different composition in difl'erent parts thereof for example by using layers of powders of different composition as the initial material.
The following examples illustrate how the process of the invention may be carried into effect:
1. An alloy containing 0.3% of manganese, 2.2% of magnesium, 0.2% of antimony, 0.7% of silicon and the rest aluminium, in the form of spherical shaped particles was first cold pressed at 8 tons per square inch to form a compact and this compact was then subjected to pressure at 4 tons per square inch without the use of a protective atmosphere at 575 C. The product had a tensile strength of 17 tons per square inch and an elongation of 14%.
2. An alloy containing 0.36% of silicon, 1.3% of iron, 2.03% of magnesium, 1.32% of manganese, 0.168% of antimony and the rest aluminium in the form of granular particles was first cold pressed at 10 tons per square inch to form a compact and this compact was then sub jected to pressure at 4.5 tons per square inch without the use of a protective atmosphere at 580 C.
Other suitable alloys for use in the process of the present invention are alloys containing 1.0 to 1.2% of manganese, 1.8 to 2.0% magnesium, up to 0.2% of antimony, 0.7% of silicon and the rest aluminium, 5.0 to 10% of magnesium and the rest aluminium, 2% of magnesium, 1.2 to
1.5% of manganese, 0.2% of antimony or.titanii um and the rest aluminium, 7.5% of magnesium, 0.3% of manganese and the rest aluminium and 2.5 to 5% of magnesium, up to 0.5% of manganese and the rest aluminium.
The process of the present invention has numerous advantages for example cheapness of manufacture, excellent mechanical properties of the product, particularly strength and ductility,
freedom from casting defects such as pinholes, controlled. grain size and shape, controlled distribution of the alloying constituents, the possibility of adding constituents which do not or pre-iormed component, e. g. metallic or nonmetallic components, or inclusions of higher or lower density than the main body of the article in order to obtain specialised mechanical or balance characteristics, and the possibility of obtaining alloys-having physical or chemical characteristics that are unobtainable by casting methods.
The expression articles as used in the appended claims includes masses."
What I claim is:
1 A metal article comprising a non-porous, compacted, agglomerated mass of particles of metal powder consisting of 1.0 to 1.2% manganese, 1.8 to 2.0% magnesium, 0.2% antimony, 0.7% silicon and the rest aluminum having a tensile strength of 17 tons per square inch and an elongation of 14%.
2. A process forthe manufacture of non-porous metal articles of, high density, high tensile strength and high elongation comprising cold pressing a pulverulent mass of an aluminum alloy consisting of 1.5 to.6% magnesium, 2 to 3.5% manganese, an eilective amount up to 5% silicon, an effective amount up to 1% antimony and the balance aluminum at a pressure of more than five tons per square inch to form a compact, and again pressing the compact at a pressure less than that employed in the cold pressing while at a temperature of about 400 to 600 C. to convert the compact into a non-porous body of high density and high tensile strength.
WILLIAM DAVID JONES.
US343492A 1939-07-07 1940-07-01 Manufacture of nonporous metal articles Expired - Lifetime US2287251A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2287251X 1939-07-07

Publications (1)

Publication Number Publication Date
US2287251A true US2287251A (en) 1942-06-23

Family

ID=10903072

Family Applications (1)

Application Number Title Priority Date Filing Date
US343492A Expired - Lifetime US2287251A (en) 1939-07-07 1940-07-01 Manufacture of nonporous metal articles

Country Status (1)

Country Link
US (1) US2287251A (en)

Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2545821A (en) * 1948-09-10 1951-03-20 Metal Hydrides Inc Method of reducing refractory oxides
US2659129A (en) * 1950-08-16 1953-11-17 Dow Chemical Co Composite alloy
US2659130A (en) * 1950-08-16 1953-11-17 Dow Chemical Co Composite alloy
US2669929A (en) * 1947-03-13 1954-02-23 George O Shull Safety device
US2674542A (en) * 1951-02-06 1954-04-06 Metal Hydrides Inc Method for producing hard surfaced titanium
US2796660A (en) * 1946-07-17 1957-06-25 Aluminium Ind Ag Method for the production of light metal articles
US2809891A (en) * 1954-10-12 1957-10-15 Aluminum Co Of America Method of making articles from aluminous metal powder
US2963780A (en) * 1957-05-08 1960-12-13 Aluminum Co Of America Aluminum alloy powder product
US2966732A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966735A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966731A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966734A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966736A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966733A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US3004331A (en) * 1960-11-08 1961-10-17 Aluminum Co Of America Aluminum base alloy powder product
US3144330A (en) * 1960-08-26 1964-08-11 Alloys Res & Mfg Corp Method of making electrical resistance iron-aluminum alloys
US3232754A (en) * 1961-11-07 1966-02-01 Alloys Res & Mfg Corp Porous metallic bodies and fabrication methods therefor
US3235959A (en) * 1962-06-25 1966-02-22 Alloys Res & Mfg Corp Brazing aluminum based parts
US3250838A (en) * 1964-08-04 1966-05-10 Alloys Res & Mfg Corp Techniques for compacting aluminum powder mixtures
US3301671A (en) * 1964-03-03 1967-01-31 Alloys Res & Mfg Corp Aluminous sintered parts and techniques for fabricating same
US3359095A (en) * 1964-02-19 1967-12-19 Dow Chemical Co Sintering of loose particulate aluminum metal
US3366479A (en) * 1965-04-28 1968-01-30 Alloys Res & Mfg Corp Powder metallurgy
US3413101A (en) * 1965-06-10 1968-11-26 Reynolds Metals Co Consolidated bodies of different aluminous metals to provide corrosion protection and method of making
US3490959A (en) * 1966-02-11 1970-01-20 Mallory & Co Inc P R Beryllium composite
US3860420A (en) * 1970-12-21 1975-01-14 Air Reduction Method of making welding rods by sintering in the presence of a liquid phase
US3996047A (en) * 1974-03-07 1976-12-07 Airco, Inc. Method and mold for producing round rods by powder metallurgy
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
US5566449A (en) * 1993-08-19 1996-10-22 Sumitomo Electric Industries, Ltd. Process for producing a shaft clamping member
US5845799A (en) * 1994-05-18 1998-12-08 Buckhorn Material Handling Group, Inc. Dispensing gate for knock down bulk box
WO2003064710A1 (en) * 2002-01-29 2003-08-07 Gkn Sinter Metals Gmbh Sinterable metal powder mixture for the production of sintered components
WO2003064083A2 (en) * 2002-01-29 2003-08-07 Gkn Sinter Metals Gmbh Method for producing sintered components from a sinterable material

Cited By (35)

* Cited by examiner, † Cited by third party
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
US2669929A (en) * 1947-03-13 1954-02-23 George O Shull Safety device
US2545821A (en) * 1948-09-10 1951-03-20 Metal Hydrides Inc Method of reducing refractory oxides
US2659129A (en) * 1950-08-16 1953-11-17 Dow Chemical Co Composite alloy
US2659130A (en) * 1950-08-16 1953-11-17 Dow Chemical Co Composite alloy
US2674542A (en) * 1951-02-06 1954-04-06 Metal Hydrides Inc Method for producing hard surfaced titanium
US2809891A (en) * 1954-10-12 1957-10-15 Aluminum Co Of America Method of making articles from aluminous metal powder
US2963780A (en) * 1957-05-08 1960-12-13 Aluminum Co Of America Aluminum alloy powder product
US2966732A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966735A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966731A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966734A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966736A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US2966733A (en) * 1958-03-27 1961-01-03 Aluminum Co Of America Aluminum base alloy powder product
US3144330A (en) * 1960-08-26 1964-08-11 Alloys Res & Mfg Corp Method of making electrical resistance iron-aluminum alloys
US3004331A (en) * 1960-11-08 1961-10-17 Aluminum Co Of America Aluminum base alloy powder product
US3232754A (en) * 1961-11-07 1966-02-01 Alloys Res & Mfg Corp Porous metallic bodies and fabrication methods therefor
US3235959A (en) * 1962-06-25 1966-02-22 Alloys Res & Mfg Corp Brazing aluminum based parts
US3359095A (en) * 1964-02-19 1967-12-19 Dow Chemical Co Sintering of loose particulate aluminum metal
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
US3366479A (en) * 1965-04-28 1968-01-30 Alloys Res & Mfg Corp Powder metallurgy
US3413101A (en) * 1965-06-10 1968-11-26 Reynolds Metals Co Consolidated bodies of different aluminous metals to provide corrosion protection and method of making
US3490959A (en) * 1966-02-11 1970-01-20 Mallory & Co Inc P R Beryllium composite
US3860420A (en) * 1970-12-21 1975-01-14 Air Reduction Method of making welding rods by sintering in the presence of a liquid phase
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
US5566449A (en) * 1993-08-19 1996-10-22 Sumitomo Electric Industries, Ltd. Process for producing a shaft clamping member
US5845799A (en) * 1994-05-18 1998-12-08 Buckhorn Material Handling Group, Inc. Dispensing gate for knock down bulk box
WO2003064710A1 (en) * 2002-01-29 2003-08-07 Gkn Sinter Metals Gmbh Sinterable metal powder mixture for the production of sintered components
WO2003064083A2 (en) * 2002-01-29 2003-08-07 Gkn Sinter Metals Gmbh Method for producing sintered components from a sinterable material
WO2003064083A3 (en) * 2002-01-29 2003-12-24 Gkn Sinter Metals Gmbh Method for producing sintered components from a sinterable material
US20050034559A1 (en) * 2002-01-29 2005-02-17 Rene Lindenau Sinterable metal powder mixture for the production of sintered components
US20050036899A1 (en) * 2002-01-29 2005-02-17 Rene Lindenau Method for producing sintered components from a sinterable material
DE10203283C5 (en) * 2002-01-29 2009-07-16 Gkn Sinter Metals Gmbh Method for producing sintered components from a sinterable material and sintered component

Similar Documents

Publication Publication Date Title
US2287251A (en) Manufacture of nonporous metal articles
US2809891A (en) Method of making articles from aluminous metal powder
US4832741A (en) Powder-metallurgical process for the production of a green pressed article of high strength and of low relative density from a heat-resistant aluminum alloy
US2814566A (en) Boron and carbon containing hard cemented materials and their production
US2254549A (en) Sintered metal composition
US2244608A (en) Process of making alloys of aluminum beryllium
US2966731A (en) Aluminum base alloy powder product
US3385696A (en) Process for producing nickel-magnesium product by powder metallurgy
US2840891A (en) High temperature structural material and method of producing same
US4676830A (en) High strength material produced by consolidation of rapidly solidified aluminum alloy particulates
US4171215A (en) Alloying addition for alloying manganese to aluminum
US4389240A (en) Alloying method
US3189444A (en) Metallic composition and method of making
US3141235A (en) Powdered tantalum articles
US1944183A (en) Alloy
US2966732A (en) Aluminum base alloy powder product
US3196007A (en) Beryllium copper composition and method of producing green compacts and sintered articles therefrom
US2823112A (en) Flux compound
US3010824A (en) Method of manufacture of an aluminum alloy, and the alloy obtained by this process
US3525609A (en) Copper alloy material
US2343978A (en) Manufacture of nonporous metal articles
US3137927A (en) Dispersion hardened materials
US3177573A (en) Method of die-expressing an aluminum-base alloy
US3770392A (en) Molybdenum-base alloys
US2768891A (en) Process for production of bronze alloys