GB843457A - High-strength titanium base aluminum-vanadium-iron alloys - Google Patents

High-strength titanium base aluminum-vanadium-iron alloys

Info

Publication number
GB843457A
GB843457A GB3024658A GB3024658A GB843457A GB 843457 A GB843457 A GB 843457A GB 3024658 A GB3024658 A GB 3024658A GB 3024658 A GB3024658 A GB 3024658A GB 843457 A GB843457 A GB 843457A
Authority
GB
United Kingdom
Prior art keywords
vanadium
strength titanium
iron alloys
titanium base
base aluminum
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
GB3024658A
Inventor
Stanley Abkowitz
Paul Edwin Moorhead
James Richard Gross
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.)
RMI Co
Original Assignee
RMI Co
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 RMI Co filed Critical RMI Co
Priority to GB3024658A priority Critical patent/GB843457A/en
Publication of GB843457A publication Critical patent/GB843457A/en
Expired legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C14/00—Alloys based on titanium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Strip Materials And Filament Materials (AREA)

Abstract

A high-strength titanium-base alloy having a good ductility, and capable of being rolled to sheet or bar form, has a composition in the following range: .Al.0.8-1.8% .V.7.5-8.5% .Fe.4.5-5.5% .O.0.3-0.5% .Ti.and impurities the balance The alloy may be annealed by heating at 1250 DEG F. furnace cooling to 900 DEG F. and then air cooling. The alloy may be hardened by heating to 1375 DEG F., quenching, ageing at 1000 DEG F. for 2 hours and then air cooling.
GB3024658A 1958-09-22 1958-09-22 High-strength titanium base aluminum-vanadium-iron alloys Expired GB843457A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3024658A GB843457A (en) 1958-09-22 1958-09-22 High-strength titanium base aluminum-vanadium-iron alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3024658A GB843457A (en) 1958-09-22 1958-09-22 High-strength titanium base aluminum-vanadium-iron alloys

Publications (1)

Publication Number Publication Date
GB843457A true GB843457A (en) 1960-08-04

Family

ID=10304603

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3024658A Expired GB843457A (en) 1958-09-22 1958-09-22 High-strength titanium base aluminum-vanadium-iron alloys

Country Status (1)

Country Link
GB (1) GB843457A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110964996A (en) * 2019-12-06 2020-04-07 陕西宏远航空锻造有限责任公司 Method for reducing heat treatment residual stress of thick-section titanium alloy forging

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110964996A (en) * 2019-12-06 2020-04-07 陕西宏远航空锻造有限责任公司 Method for reducing heat treatment residual stress of thick-section titanium alloy forging

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