GB853539A - Wrought titanium and titanium alloy products - Google Patents

Wrought titanium and titanium alloy products

Info

Publication number
GB853539A
GB853539A GB2802/59A GB280259A GB853539A GB 853539 A GB853539 A GB 853539A GB 2802/59 A GB2802/59 A GB 2802/59A GB 280259 A GB280259 A GB 280259A GB 853539 A GB853539 A GB 853539A
Authority
GB
United Kingdom
Prior art keywords
titanium
wrought
alloy products
hour
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
GB2802/59A
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
Publication of GB853539A publication Critical patent/GB853539A/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Battery Electrode And Active Subsutance (AREA)

Abstract

The impact resistance and resistance to corrosion of wrought titanium and titanium-base alloy products is increased by reducing the hydrogen content to 6-20 p.p.m. Titanium-base alloys containing (1) Al 1.3%, V 8%, Fe 5%, O2 0.4%; (2) Al 6%, V 4%; (3) Al 4%, Mn 4%, and having the above low hydrogen content are referred to in the Specification. Alloy (1) may be annealed by heating to 1250 DEG F. for 1 hour, furnace cooling to 900 DEG F. and then air cooling. It may be hardened by heating to 1375-1400 DEG F. for 1 hour, water quenching and ageing at 1000 DEG F. for 2 hours or 900 DEG F. for 4 hours.
GB2802/59A 1958-02-28 1959-01-26 Wrought titanium and titanium alloy products Expired GB853539A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US853539XA 1958-02-28 1958-02-28

Publications (1)

Publication Number Publication Date
GB853539A true GB853539A (en) 1960-11-09

Family

ID=22191050

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2802/59A Expired GB853539A (en) 1958-02-28 1959-01-26 Wrought titanium and titanium alloy products

Country Status (1)

Country Link
GB (1) GB853539A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4422887A (en) 1980-09-10 1983-12-27 Imi Kynoch Limited Heat treatment
GB2561815A (en) * 2017-03-10 2018-10-31 Ilika Tech Limited Titanium Alloys
CN109161829A (en) * 2018-11-23 2019-01-08 西北有色金属研究院 A method of improving TC4-DT titanium alloy rod bar two-phase section fracture toughness

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4422887A (en) 1980-09-10 1983-12-27 Imi Kynoch Limited Heat treatment
GB2561815A (en) * 2017-03-10 2018-10-31 Ilika Tech Limited Titanium Alloys
CN109161829A (en) * 2018-11-23 2019-01-08 西北有色金属研究院 A method of improving TC4-DT titanium alloy rod bar two-phase section fracture toughness

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