Method for endowing Ni-enriched TiNi shape memory alloy with two-way shape memory characteristic

A technology of memory alloy and memory, which is applied in the field of endowing Ni-rich TiNi shape memory alloy with two-way memory characteristics, which can solve problems such as difficulty in realizing memory performance, and achieve strong cycle deformation stability, reduced energy consumption, and short response time Effect

Active Publication Date: 2018-12-11
AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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Problems solved by technology

At present, it is difficult to achieve the two-way shape memory performance of "thermal e

Method used

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  • Method for endowing Ni-enriched TiNi shape memory alloy with two-way shape memory characteristic
  • Method for endowing Ni-enriched TiNi shape memory alloy with two-way shape memory characteristic

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[0024] The technical solution of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments:

[0025] See Figure 1~2 As shown, the method for imparting the two-way memory characteristic of the Ni-rich TiNi shape memory alloy is characterized in that: the two-way memory characteristic refers to the "thermal expansion and contraction" type two-way shape memory performance. The steps of the method are Yes:

[0026] (1) The chemical composition and atomic percentage in the Ni-rich TiNi shape memory alloy are: Ni50.8-60.0%, the balance is Ti, and the mass percentage of impurities C and O in the Ni-rich TiNi shape memory alloy should be Less than 0.3%;

[0027] (2) The Ni-rich TiNi shape memory alloy adopts tube 1 as the training object, the wall thickness of tube 1 is 0.3-50mm, the outer diameter is 5-350mm, and the length is 10-300mm;

[0028] (3) The tube 1 of TiNi shape memory alloy is aged in a muffle furnace: the ag...

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Abstract

The invention discloses a method for endowing a Ni-enriched TiNi shape memory alloy with a two-way shape memory characteristic. The method comprises the following steps: applying high-energy electrical stimulation to a constrained cold-formed TiNi shape memory alloy, coupling a Joule heating effect caused in a low temperature range of 150-250 DEG C with the electron wind effect, promoting the internal defects (such as dislocation) of the alloy to be in directional arrangement along a constraint stress direction, enabling a martensite variant to be in orientated growth, then 'memorizing' the cold forming state as a high temperature shape, 'memorizing' a high-temperature aging state as a low temperature shape, matching a mechanical training method to form the electrical stimulation-mechanical training method, and endowing the Ni-enriched TiNi shape memory alloy with the 'thermal expansion and cold contraction' type two-way shape memory characteristic. According to the method, the high-energy electrical stimulation and martensitic phase transition alternative cycle period duration can be greatly shortened, the production efficiency is improved, and the energy consumption is reduced.

Description

technical field [0001] The invention is a method for imparting two-way memory characteristics of a Ni-rich state TiNi shape memory alloy, which belongs to Background technique: [0002] Shape memory alloy is a material with integrated structure and function, and has the dual functions of sensing and driving at the same time. It is the best choice for realizing lightweight and intelligent mechanical structures. TiNi-based shape memory alloys have martensitic phase transformation characteristics, so they have excellent shape memory properties, superelastic properties and high damping properties; in addition, TiNi-based shape memory alloys are intermetallic compounds with good mechanical properties and corrosion resistance , has the most application prospect as a solid-state drive. The one-way shape memory and superelastic properties of TiNi-based shape memory alloys belong to the intrinsic properties of alloy materials, while the two-way shape memory properties do not belong ...

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Application Information

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IPC IPC(8): C22C19/03C22F1/10
CPCC22C19/03C22F1/002C22F1/006C22F1/10
Inventor 官磊成波刘大博
Owner AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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