GB846530A - Hot-worked aluminium base alloy powder article - Google Patents

Hot-worked aluminium base alloy powder article

Info

Publication number
GB846530A
GB846530A GB13543/58A GB1354358A GB846530A GB 846530 A GB846530 A GB 846530A GB 13543/58 A GB13543/58 A GB 13543/58A GB 1354358 A GB1354358 A GB 1354358A GB 846530 A GB846530 A GB 846530A
Authority
GB
United Kingdom
Prior art keywords
hot
worked
aluminium
alloy
base alloy
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
Application number
GB13543/58A
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.)
Howmet Aerospace Inc
Original Assignee
Aluminum Company of America
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 Aluminum Company of America filed Critical Aluminum Company of America
Publication of GB846530A publication Critical patent/GB846530A/en
Expired 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium

Abstract

A hot-worked aluminium-base alloy powder article free from oxide except as an incidental impurity is formed from atomized powder of an aluminium alloy containing at least 70% of aluminium, 2.5-20% iron, and 0-10% of one or more of manganese, nickel, cobalt, chromium, titanium, zirconium and vanadium, the iron-containing constituent being present in the hot-worked article being in the form of fine uniformly distributed insoluble particles having a maximum thickness of 0.4 micron. Particles of alloy passing through a 100 mesh sieve, and the majority passing through a 200 mesh sieve, are formed by drastically chilling a spray of molten alloy. The powder is compressed at a temperature in the range 700-900 DEG F., e.g. at 30,000-120,000 p.s.i. The compact is then hot-worked as by extrusion, forging or rolling, preferably in the same temperature range. A cold-working operation may follow. Specifications 404,463 and 625,364 are referred to.
GB13543/58A 1957-05-08 1958-04-29 Hot-worked aluminium base alloy powder article Expired GB846530A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US846530XA 1957-05-08 1957-05-08

Publications (1)

Publication Number Publication Date
GB846530A true GB846530A (en) 1960-08-31

Family

ID=22186339

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13543/58A Expired GB846530A (en) 1957-05-08 1958-04-29 Hot-worked aluminium base alloy powder article

Country Status (1)

Country Link
GB (1) GB846530A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2494722A1 (en) * 1980-11-24 1982-05-28 United Technologies Corp PRECIPITATION-CURABLE ALUMINUM ALLOY ARTICLE AND METHOD OF MANUFACTURE
GB2173214A (en) * 1985-04-02 1986-10-08 Aluminum Co Of America Powder metallurgy
GB2179369A (en) * 1985-08-06 1987-03-04 Secretary Trade Ind Brit Sintered aluminium alloy
EP0271424A1 (en) * 1986-10-27 1988-06-15 United Technologies Corporation Age hardenable dispersion strengthened high temperature aluminum alloy

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2494722A1 (en) * 1980-11-24 1982-05-28 United Technologies Corp PRECIPITATION-CURABLE ALUMINUM ALLOY ARTICLE AND METHOD OF MANUFACTURE
GB2173214A (en) * 1985-04-02 1986-10-08 Aluminum Co Of America Powder metallurgy
GB2179369A (en) * 1985-08-06 1987-03-04 Secretary Trade Ind Brit Sintered aluminium alloy
EP0271424A1 (en) * 1986-10-27 1988-06-15 United Technologies Corporation Age hardenable dispersion strengthened high temperature aluminum alloy

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