A novel bending fatigue test device based on self-excited vibration principle and its application to superelastic Nitinol microwire study

被引:7
|
作者
Leng, Jiaming [1 ,2 ,3 ]
Yan, Xiaojun [1 ,2 ,3 ,4 ]
Zhang, Xiaoyong [1 ,2 ,3 ,4 ]
Qi, Mingjing [1 ]
Liu, Zhiwei [1 ]
Huang, Dawei [1 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[2] Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China
[3] Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China
[4] Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
bending fatigue; superelastic Nitinol microwire; self-excited vibration; strain amplitude; SHAPE-MEMORY ALLOY; ELECTROSTATIC ACTUATORS; STRUCTURAL FATIGUE; CONSTITUTIVE MODEL; WIRES; STRAIN; BEAM;
D O I
10.1088/1361-665X/aa7bdf
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Most Nitinol-alloy-based biomedical devices are usually manufactured from straight drawn microwires or microbeams. Fatigue due to cyclic bending is interpreted as the primary failure mechanism in these devices. However, the bending fatigue performance of a Nitinol microwire is rarely studied because of the lack of test devices. Therefore, we firstly establish a bending fatigue test device based on the self-excited vibration principle. Then, we further improve and experimentally verify the device in three aspects to enlarge the strain amplitude: electrode distance optimization, electrode placement angle optimization and local stiffness enhancement. Based on these improvements, the strain amplitude is increased to 6%, successfully meeting the requirements of Nitinol microwire bending fatigue tests. Using the improved test device, a group of superelastic Nitinol (55.8% Ni-44.2% Ti) microwires with a diameter of 50.8 mu m are tested. The test results show that the fatigue strain limit for the chosen life (1 x 10(6) cycles) is around 1.9%, and the inflexion appears at a strain amplitude of 2.3%. SEM observation shows the typical features of low-cycle and high-cycle fatigue on the fracture surfaces.
引用
收藏
页数:9
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