CN1740361A - Low temperature super elastic four-component Ni-Ti alloy - Google Patents

Low temperature super elastic four-component Ni-Ti alloy Download PDF

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Publication number
CN1740361A
CN1740361A CN 200410073026 CN200410073026A CN1740361A CN 1740361 A CN1740361 A CN 1740361A CN 200410073026 CN200410073026 CN 200410073026 CN 200410073026 A CN200410073026 A CN 200410073026A CN 1740361 A CN1740361 A CN 1740361A
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CN
China
Prior art keywords
alloy
low temperature
super elastic
titanium
component
Prior art date
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Pending
Application number
CN 200410073026
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Chinese (zh)
Inventor
杨宏进
曹继敏
杨冠军
杨华斌
牛中杰
高维娜
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XI'AN SAITE METAL MATERIAL DEVELOPMENT Co Ltd
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XI'AN SAITE METAL MATERIAL DEVELOPMENT Co Ltd
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Priority to CN 200410073026 priority Critical patent/CN1740361A/en
Publication of CN1740361A publication Critical patent/CN1740361A/en
Pending legal-status Critical Current

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Abstract

The present invention relates to one kind of low temperature super elastic four-component Ti-Ni alloy and its preparation and application. The present invention features that the alloy consists of Ni 55.3-56 wt%, V 0.40-0.90 wt%, Al 0.05-0.15 wt%, except Ti and inevitable impurities, including C not more than 0.070 wt%, H not more than 0.005 wt% and O not more than 0.050 wt%. The alloy is especially suitable for use in making spectacle frame, cellphone antenna and other devices needing low temperature elasticity.

Description

A kind of low temperature super elastic four-component Ni-Ti alloy
Technical field
The present invention relates to be applied to a kind of super-elasticity titanium nickel (TiNi) alloy product and preparation method thereof under the cold condition.
Background technology
Titanium nickel TiNi alloy not only has peculiar shape memory effect, but also has superior superelastic properties, and mainly is used widely in spectacle frame, antenna for mobile phone field.The TiNi alloy can show excellent non-linear superelastic properties after certain technology special processing, the maximum elastic strain amount can reach 8%, presents than the much bigger elasticity of other metallic substance (general recoverable strain amount is no more than 1%).The binary Ti-Ni alloy of real world applications presents the temperature of 5% non-linear superelastic properties more than 5 ℃, 5 ℃ of obvious variation of the non-linear superelastic properties of following temperature alloy.
When titanium nickel (TiNi) alloy is applied to spectacle frame, antenna for mobile phone, require to present non-linear preferably superelastic properties under low-temperature condition, i.e.-10 ℃~40 ℃ temperature ranges, after 6% recoverable deformation, recovery rate is greater than 95% after the requirement silk material cold working timeliness; After the cold working straight line was handled ,-25 ℃~40 ℃ temperature ranges, after 5% recoverable deformation, recovery rate was greater than 90%.Reality needs the use temperature interval to present the new Ti-Ni alloy goods and the preparation method of good non-linear superelastic properties in above scope.
Summary of the invention
The objective of the invention is at the deficiencies in the prior art, a kind of low temperature super elastic titanium nickel (TiNi) quad alloy is provided.
Can take following technical scheme to realize purpose.
The Ni-based quad alloy goods of titanium, by weight percentage, it consists of: nickel: 55.3%~56.3%; Vanadium: 0.40%~0.90%; Aluminium: 0.05%~0.18%, surplus is titanium and unavoidable impurities, wherein low gap constituent content carbon C≤0.070%; Hydrogen H≤0.005%; Oxygen O≤0.050%.
Low temperature super elastic of the present invention adopts a certain proportion of aluminium vanadium (AlV) alloy as additive with new titanium nickel (TiNi) alloy, reduces the martensitic transformation temperature of alloy, improves the homogeneity of ingot casting composition simultaneously.
Alloy preparation process of the present invention is that the element that will reduce martensitic transformation temperature adds with aluminium vanadium (AlV) alloy form, and element titanium (Ti) adds with the titanium sponge form, and elemental nickel (Ni) adds with the electrolytic nickel strips.The melting in vacuum induction furnace of batching back, by forge, rolling, swage, stretch, align preparation all size rod silk material.

Claims (3)

1, a kind of low temperature super elastic is characterized in that by weight percentage, it consists of: nickel: 55.3%~56.3% with titanium nickel (TiNi) quad alloy; Vanadium: 0.40%~0.90%; Aluminium: 0.05%~0.18%, surplus is titanium and unavoidable impurities, wherein low gap constituent content carbon C≤0.070%; Hydrogen H≤0.005%; Oxygen O≤0.050%.
2, the application of a kind of titanium nickel according to claim 1 (TiNi) quad alloy goods is characterized in that: make spectacle frame, antenna for mobile phone.
3, aluminium element, v element add with the aluminum-vanadium alloy form.
CN 200410073026 2004-08-25 2004-08-25 Low temperature super elastic four-component Ni-Ti alloy Pending CN1740361A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200410073026 CN1740361A (en) 2004-08-25 2004-08-25 Low temperature super elastic four-component Ni-Ti alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200410073026 CN1740361A (en) 2004-08-25 2004-08-25 Low temperature super elastic four-component Ni-Ti alloy

Publications (1)

Publication Number Publication Date
CN1740361A true CN1740361A (en) 2006-03-01

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200410073026 Pending CN1740361A (en) 2004-08-25 2004-08-25 Low temperature super elastic four-component Ni-Ti alloy

Country Status (1)

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CN (1) CN1740361A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100460548C (en) * 2007-09-30 2009-02-11 北京航空航天大学 Titanium-nickel-aluminum-base high-temperature alloy material and preparation method thereof
CN102888535A (en) * 2011-07-21 2013-01-23 西安赛特金属材料开发有限公司 Wear-resistant nickel-titanium-based alloy and preparation method thereof
CN103088234A (en) * 2011-10-28 2013-05-08 西安赛特金属材料开发有限公司 Low interstitial titanium-nickel-aluminum-vanadium shape memory alloy material for low temperature hyperelasticity
CN114908265A (en) * 2022-06-02 2022-08-16 西安斯塔克材料科技有限公司 Preparation method of TiNiAlV quaternary alloy filament

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100460548C (en) * 2007-09-30 2009-02-11 北京航空航天大学 Titanium-nickel-aluminum-base high-temperature alloy material and preparation method thereof
CN102888535A (en) * 2011-07-21 2013-01-23 西安赛特金属材料开发有限公司 Wear-resistant nickel-titanium-based alloy and preparation method thereof
CN103088234A (en) * 2011-10-28 2013-05-08 西安赛特金属材料开发有限公司 Low interstitial titanium-nickel-aluminum-vanadium shape memory alloy material for low temperature hyperelasticity
CN114908265A (en) * 2022-06-02 2022-08-16 西安斯塔克材料科技有限公司 Preparation method of TiNiAlV quaternary alloy filament
CN114908265B (en) * 2022-06-02 2023-10-27 西安斯塔克材料科技有限公司 Preparation method of TiNiAlV quaternary alloy filament

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