GB782148A - Improvements in and relating to the heat treatment of titanium alloys - Google Patents

Improvements in and relating to the heat treatment of titanium alloys

Info

Publication number
GB782148A
GB782148A GB30840/55A GB3084055A GB782148A GB 782148 A GB782148 A GB 782148A GB 30840/55 A GB30840/55 A GB 30840/55A GB 3084055 A GB3084055 A GB 3084055A GB 782148 A GB782148 A GB 782148A
Authority
GB
United Kingdom
Prior art keywords
temperature
hours
etching
relating
coarsening
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
GB30840/55A
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 GB782148A publication Critical patent/GB782148A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/183High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • ing And Chemical Polishing (AREA)

Abstract

Titanium base alloys having compositions within one of the following ranges in per cent by weight. Al 2.0-8.0, Si 0.1-1.5, V 2.0-6.0 or Mo 1.0-6.0 or Mo and V 1.0-6.0; Al 4.0-6.0, Si 0.3-0.5, V 3.0-5.0; Al 4.0-6.0, Si 0.3-0.5, Mo 3.0-4.0; Al 2.0-8.0, Mo 1.0-6.0 the remainder in each case being Ti together with impurities O up to 0.2, N up to 0.1, C up to 0.25 and H up to 0.02, the Al content being at least as great as that of Mo or V or the combination thereof, are heated to a temperature high in the polyphase field to coarsen the microstructure and to form a continuous alpha phase, then quickly cooled and aged at a temperature below the coarsening temperature till the beta phase is dark etching. The final condition of the beta phase is determined by etching with a solution of 60 cc. glycerine, 20 cc. concentrated nitric acid and 20 cc. precipitated hydrofluoric acid. The coarsening treatment may be at 1500-1650 DEG F. for 4-24 hours, the alloy being rapidly cooled in inert atmosphere or air or by quenching to room temperature or to the ageing temperature of 1000-1200 DEG F. at which it is held e.g. for 4-48 hours.
GB30840/55A 1954-10-27 1955-10-27 Improvements in and relating to the heat treatment of titanium alloys Expired GB782148A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US782148XA 1954-10-27 1954-10-27

Publications (1)

Publication Number Publication Date
GB782148A true GB782148A (en) 1957-09-04

Family

ID=22142661

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30840/55A Expired GB782148A (en) 1954-10-27 1955-10-27 Improvements in and relating to the heat treatment of titanium alloys

Country Status (1)

Country Link
GB (1) GB782148A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2584094A1 (en) * 1985-06-27 1987-01-02 Mitsubishi Metal Corp HIGH STRENGTH TITANIUM ALLOY MATERIAL HAVING IMPROVED OUVABILITY AND PROCESS FOR PRODUCING THE SAME
GB2203755A (en) * 1987-04-22 1988-10-26 Nippon Kokan Kk Corrosion resistant titanium alloy
GB2498408A (en) * 2012-01-12 2013-07-17 Titanium Metals Corp A titanium alloy comprising aluminium, vanadium, molybdenum, silicon and oxygen

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2584094A1 (en) * 1985-06-27 1987-01-02 Mitsubishi Metal Corp HIGH STRENGTH TITANIUM ALLOY MATERIAL HAVING IMPROVED OUVABILITY AND PROCESS FOR PRODUCING THE SAME
GB2178758A (en) * 1985-06-27 1987-02-18 Mitsubishi Metal Corp Titanium base alloy
US4889170A (en) * 1985-06-27 1989-12-26 Mitsubishi Kinzoku Kabushiki Kaisha High strength Ti alloy material having improved workability and process for producing the same
GB2203755A (en) * 1987-04-22 1988-10-26 Nippon Kokan Kk Corrosion resistant titanium alloy
GB2203755B (en) * 1987-04-22 1991-08-14 Nippon Kokan Kk High strength and corrosion resistant titanium alloy having excellent corrosion-wear properties
GB2498408A (en) * 2012-01-12 2013-07-17 Titanium Metals Corp A titanium alloy comprising aluminium, vanadium, molybdenum, silicon and oxygen
GB2498408B (en) * 2012-01-12 2013-12-18 Titanium Metals Corp Titanium alloy with improved properties
US10119178B2 (en) 2012-01-12 2018-11-06 Titanium Metals Corporation Titanium alloy with improved properties

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