GB781535A - Improvements in and relating to titanium alloys - Google Patents

Improvements in and relating to titanium alloys

Info

Publication number
GB781535A
GB781535A GB27128/55A GB2712855A GB781535A GB 781535 A GB781535 A GB 781535A GB 27128/55 A GB27128/55 A GB 27128/55A GB 2712855 A GB2712855 A GB 2712855A GB 781535 A GB781535 A GB 781535A
Authority
GB
United Kingdom
Prior art keywords
per cent
alloy
relating
titanium alloys
hours
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
GB27128/55A
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.)
Armour Research Foundation
Original Assignee
Armour Research Foundation
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 Armour Research Foundation filed Critical Armour Research Foundation
Publication of GB781535A publication Critical patent/GB781535A/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)
  • Powder Metallurgy (AREA)

Abstract

A titanium-base alloy has a composition within the following range: Al 2-8 per cent; V 2-6 per cent; Ti and unavoidable impurities the remainder. The alloy may contain, as impurities H up to 0.02 per cent, O up to 0.2 per cent, N up to 0.1 per cent and C up to 0.25 per cent. The alloy may be heated to a temperature high in the alpha-beta phase field e.g. 1400-1700 DEG F. for 1-2 hours, warm worked and then aged at 900-1200 DEG F. for at least 1 hour. High temperature stability is improved by annealing for 12-30 hours at 1000-1200 DEG F. and then air cooling.
GB27128/55A 1954-09-22 1955-09-22 Improvements in and relating to titanium alloys Expired GB781535A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US781535XA 1954-09-22 1954-09-22

Publications (1)

Publication Number Publication Date
GB781535A true GB781535A (en) 1957-08-21

Family

ID=22142261

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27128/55A Expired GB781535A (en) 1954-09-22 1955-09-22 Improvements in and relating to titanium alloys

Country Status (1)

Country Link
GB (1) GB781535A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1171622B (en) * 1960-02-18 1964-06-04 Continental Titanium Metals Co Titanium alloy and process for its heat treatment
US4943412A (en) * 1989-05-01 1990-07-24 Timet High strength alpha-beta titanium-base alloy
US5759484A (en) * 1994-11-29 1998-06-02 Director General Of The Technical Research And Developent Institute, Japan Defense Agency High strength and high ductility titanium alloy

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1171622B (en) * 1960-02-18 1964-06-04 Continental Titanium Metals Co Titanium alloy and process for its heat treatment
US4943412A (en) * 1989-05-01 1990-07-24 Timet High strength alpha-beta titanium-base alloy
US5759484A (en) * 1994-11-29 1998-06-02 Director General Of The Technical Research And Developent Institute, Japan Defense Agency High strength and high ductility titanium alloy

Similar Documents

Publication Publication Date Title
GB1187213A (en) Method of processing Metastable Beta Titanium Alloy
GB997761A (en) Improvements relating to zirconium base alloys
GB911148A (en) Titanium-base alloys and processing thereof
GB781535A (en) Improvements in and relating to titanium alloys
GB880805A (en) Nickel-chromium-cobalt alloys
GB946944A (en) Improvements relating to the heat-treatment of nickel-chromium alloys
GB832438A (en) Process for producing silicon-iron alloy sheets
GB829668A (en) Improvements relating to zirconium alloys
GB988069A (en) Improvements in or relating to zirconium-base alloys
GB870261A (en) Improvements in or relating to aluminium lithium alloys
GB772339A (en) Improvements in or relating to titanium-base alloys
GB782148A (en) Improvements in and relating to the heat treatment of titanium alloys
GB813124A (en) Improvements in or relating to the heat treatment of zirconium alloys
GB766061A (en) Improvements in or relating to uranium alloys
GB873774A (en) Titanium alloys
GB972532A (en) Improvements in or relating to titanium base alloys
GB943228A (en) Improved chromium-tungsten-silicon alloys
GB1141409A (en) Heat treatment and working of titanium alloys
GB815975A (en) Heat treatment of titanium alloys
GB922163A (en) High temperature alpha titanium-zirconium-aluminum alloys
GB727085A (en) Titanium-molybdenum-iron alloys
GB843457A (en) High-strength titanium base aluminum-vanadium-iron alloys
GB853539A (en) Wrought titanium and titanium alloy products
GB850278A (en) Alpha titanium alloys
GB866060A (en) Improvements in high-temperature chromium-tantalum alloys