IL34411A - Improvements in alloys - Google Patents

Improvements in alloys

Info

Publication number
IL34411A
IL34411A IL34411A IL3441170A IL34411A IL 34411 A IL34411 A IL 34411A IL 34411 A IL34411 A IL 34411A IL 3441170 A IL3441170 A IL 3441170A IL 34411 A IL34411 A IL 34411A
Authority
IL
Israel
Prior art keywords
alloy
shape
heat
temperature
recoverable
Prior art date
Application number
IL34411A
Other languages
Hebrew (he)
Other versions
IL34411A0 (en
Original Assignee
Fulmer Res Inst Ltd
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 Fulmer Res Inst Ltd filed Critical Fulmer Res Inst Ltd
Publication of IL34411A0 publication Critical patent/IL34411A0/en
Publication of IL34411A publication Critical patent/IL34411A/en

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/007Alloys based on nickel or cobalt with a light metal (alkali metal Li, Na, K, Rb, Cs; earth alkali metal Be, Mg, Ca, Sr, Ba, Al Ga, Ge, Ti) or B, Si, Zr, Hf, Sc, Y, lanthanides, actinides, as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C28/00Alloys based on a metal not provided for in groups C22C5/00 - C22C27/00
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C43/00Alloys containing radioactive materials

Claims (1)

1. ' CLAIMS 34411/2 1, A method of making an article from a heat-recoverable alloy, which alloy when s itably heat-treated is one shape, and caused to deform at an appropriate temperature into another shape at least partially recovers ite first shape upon sufficiently raising the temperature of the article, comprising the step of applying^., a strain to the alloy in its high temperature phase which produces a stress which induces a desired shape in its low temper ure phas 2. A method according to c a.±n 1 in which said strain is applied by deforming the alloy in its high-temperature pliase partly towards the shape required for the low-temperature phase. β. A method according to claim 2 in which the temperature is ubsequen l lowered so that alloy changes into its lovf-temperature phase and assumes the required shape, , A method aepprcjing to claim, \ in which h° alloy is defprmed^ into a desired shape in its low-temperature phase and said strain is applied by raising t|ie temperature sp that i tfie a¾loy changes iptP its high-temperature phase while restraint is applied, to the alloy to prevent a change in shape, 5, A method pf making a hea -recoverable article from a heat-recoverable alloy, which method, includes the stops of Shaping the alloy at an elevated tem er tu e into a first shape, cooling to a lower temperature, deforming the alloy at the lower temperature intp a second shape, said temperatures being such that if reheated without restraint to an appropriate temperature the alloy would at least partly resume its firs shape, and reheating the alloy tp said appropriate temperature while subjecting it to restraint which prevents a change of 6. A method according to claim 5 in which the alloy is cooled to the lower temperature after said reheating, still retaining the second shape. 7. A method according to any preceding claim in which the alloy is a binary alloy of uranium containing 2 to 7% by weight molybdenum, 3 to 11% by weight niobium or 2. to 7% by weight rhenium. 8. A method according to claim 7 in which the alloy is a binary alloy of uranium containing 3 to 6.5% by weight molybdenum. 9. A method according to claim 7 in which the alloy is a binary alloy of uranium containing 4 to 10% by weight niobium 10. A method according to any of claims 1 to 6 in which the alloy is a manganese-copper binary alloy containing 5 to 50% by weight copper. 11. A method according to claim 10 in which the alloy contains 5 to 30% by weight copper. 12.. A method according to any of claims 1 to 6 in which the alloy is a nickel-titanium binary alloy containing 52 to 56% by weight nickel. 13. A heat-recoverable alloy as defined in any of claims 7 to 11. 14. A method of making a heat-recoverable article from a heat-recoverable alloy according to claim 13, which, method . includes the steps of shaping the alloy at an elevated temperature into a first shape, cooling to a lower temperature, and causing the alloy to deform at the lower temperature into a second shape, said temperatures being such that if reheated to an appropriate temperature the alloy would at least partly regain its first shape. 15. A heat-recoverable article made by a method according to any of claims 1 to 12. and 14. 16. A heat-recoverable article made of a heat-recoverable alloy, which article has, when the alloy is in its high- temperature phase, internal stress which promotes a desired change of shape in the low-temperature phase. 17. Apparatus including a heat-recoverable article according to claim 15 or claim 16, the article performing a function in said apparatus by virtue of its property of changing shape with temperature. 18. A method of making a heat-recoverable article from a heat-recoverable :>alloy2 using restraint on reheating substantially as hereinbefore described in the Examples. ' · · . 19. A method of making a heat-recoverable article from a heat-recoverable alloy using partial initial deformation above the transformation temperature substantially as hereinbefore described in the Examples. 20. A heat-recoverable uranium-molybdenum, uranium-niobium, uranium-rhenium or manganese-copper binary alloy substantially as hereinbefore described in the Examples. 21. A heat-recoverable article made by a method and/or from an alloy according to any Of claims 18 to 20.
IL34411A 1969-05-01 1970-04-29 Improvements in alloys IL34411A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2237269 1969-05-01

Publications (2)

Publication Number Publication Date
IL34411A0 IL34411A0 (en) 1970-06-17
IL34411A true IL34411A (en) 1976-03-31

Family

ID=10178310

Family Applications (1)

Application Number Title Priority Date Filing Date
IL34411A IL34411A (en) 1969-05-01 1970-04-29 Improvements in alloys

Country Status (12)

Country Link
US (1) US3802930A (en)
JP (1) JPS4815130B1 (en)
AT (1) AT315524B (en)
BE (1) BE749851A (en)
CA (1) CA929084A (en)
CH (2) CH567103A5 (en)
DE (1) DE2021348C3 (en)
FR (1) FR2044754A1 (en)
GB (1) GB1315652A (en)
IL (1) IL34411A (en)
NL (1) NL172971C (en)
SE (1) SE389688B (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4067752A (en) * 1973-11-19 1978-01-10 Raychem Corporation Austenitic aging of metallic compositions
JPS53925B2 (en) * 1974-05-04 1978-01-13
JPS51126323A (en) * 1975-02-18 1976-11-04 Raychem Corp Articles able to heat recovery and making method of them
US4036669A (en) * 1975-02-18 1977-07-19 Raychem Corporation Mechanical preconditioning method
US4010455A (en) * 1975-07-17 1977-03-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Cyclical bi-directional rotary actuator
US4002954A (en) * 1975-12-11 1977-01-11 The United States Of America As Represented By The Secretary Of The Army Trigger circuit
US4493737A (en) * 1980-05-21 1985-01-15 The United States Of America As Represented By The United States Department Of Energy Method for fabricating uranium alloy articles without shape memory effects
US4448824A (en) * 1982-01-28 1984-05-15 Raychem Corporation Wraparound protective closure
WO1988002787A1 (en) * 1986-10-14 1988-04-21 Cvi/Beta Ventures, Inc. Shape-memory alloy resetting method and apparatus
US4758285A (en) * 1986-10-14 1988-07-19 Cvi/Beta Ventures, Inc. Shape-memory alloy resetting method
GB8720025D0 (en) * 1987-08-25 1987-09-30 Raychem Pontoise Sa Article
US5133721A (en) * 1991-03-19 1992-07-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Device for removing foreign objects from anatomic organs
US6068623A (en) 1997-03-06 2000-05-30 Percusurge, Inc. Hollow medical wires and methods of constructing same
US8414714B2 (en) 2008-10-31 2013-04-09 Fort Wayne Metals Research Products Corporation Method for imparting improved fatigue strength to wire made of shape memory alloys, and medical devices made from such wire
CN104195484A (en) * 2014-08-20 2014-12-10 西安钢研功能材料有限责任公司 Preparation method of Mn72Ni10Cu18 alloy strip

Also Published As

Publication number Publication date
CH567103A5 (en) 1975-09-30
SE389688B (en) 1976-11-15
CA929084A (en) 1973-06-26
DE2021348C3 (en) 1980-06-04
GB1315652A (en) 1973-05-02
DE2021348A1 (en) 1971-01-14
US3802930A (en) 1974-04-09
DE2021348B2 (en) 1979-09-20
NL172971C (en) 1983-11-16
CH555892A (en) 1974-11-15
FR2044754A1 (en) 1971-02-26
NL7006402A (en) 1970-11-03
AT315524B (en) 1974-05-27
BE749851A (en) 1970-10-30
JPS4815130B1 (en) 1973-05-12
IL34411A0 (en) 1970-06-17

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