GB972532A - Improvements in or relating to titanium base alloys - Google Patents

Improvements in or relating to titanium base alloys

Info

Publication number
GB972532A
GB972532A GB617661A GB617661A GB972532A GB 972532 A GB972532 A GB 972532A GB 617661 A GB617661 A GB 617661A GB 617661 A GB617661 A GB 617661A GB 972532 A GB972532 A GB 972532A
Authority
GB
United Kingdom
Prior art keywords
alloy
relating
base alloys
titanium base
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
GB617661A
Inventor
Allan Jay Hatch
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.)
CONTINENTAL TITANIUM METALS CO
Original Assignee
CONTINENTAL TITANIUM METALS 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 CONTINENTAL TITANIUM METALS CO filed Critical CONTINENTAL TITANIUM METALS CO
Priority to GB617661A priority Critical patent/GB972532A/en
Publication of GB972532A publication Critical patent/GB972532A/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

Abstract

An alloy having fine as-cast grain size contains in percentage by weight .Al.4-8 .V.3-5 .Be.0.05-0.15 .S.0.02-0.07 .Ti.balance An exemplified alloy was forged at 1850 DEG F., and then rolled at 1750 DEG F., followed by annealing for two hours at 1300 DEG F. and air cooling. Subsequent heat treatment consisted of heating for one hour at 1550 DEG F., quenching into water, and then ageing at 900 DEG F. for eight hours and air cooling. Use of the alloy for aircraft components is referred to.
GB617661A 1961-02-20 1961-02-20 Improvements in or relating to titanium base alloys Expired GB972532A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB617661A GB972532A (en) 1961-02-20 1961-02-20 Improvements in or relating to titanium base alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB617661A GB972532A (en) 1961-02-20 1961-02-20 Improvements in or relating to titanium base alloys

Publications (1)

Publication Number Publication Date
GB972532A true GB972532A (en) 1964-10-14

Family

ID=9809800

Family Applications (1)

Application Number Title Priority Date Filing Date
GB617661A Expired GB972532A (en) 1961-02-20 1961-02-20 Improvements in or relating to titanium base alloys

Country Status (1)

Country Link
GB (1) GB972532A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2149617A1 (en) * 2008-07-29 2010-02-03 Hamilton Sundstrand Corporation Method and article for improved adhesion of fatigue-prone components

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2149617A1 (en) * 2008-07-29 2010-02-03 Hamilton Sundstrand Corporation Method and article for improved adhesion of fatigue-prone components
US8065898B2 (en) 2008-07-29 2011-11-29 Hamilton Sundstrand Corporation Method and article for improved adhesion of fatigue-prone components
US8297094B2 (en) 2008-07-29 2012-10-30 Hamilton Sundstrand Corporation Article for improved adhesion of fatigue-prone components

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