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1·Fretting fatigue usually occurs in lap joints of aircraft structure.

搭接件是飞机结构中容易产生微动疲劳损伤的部位。

2·Fretting wear and fretting fatigue of steel wires in steel ropes have been identified as a major cause of reducing the life of the rope.

钢丝绳内部钢丝的微动磨损和微动疲劳是造成钢缆寿命降低的主要原因之一。

3·This article describes the phenomenon, effect factors and distinguishable characteristics of fretting fatigue damage failure by real case.

介绍了微动疲劳损伤失效的现象，影响因素，鉴别特征，并举例说明。

4·The fretting fatigue life under complex loads monotonously decreases with the increase of the high cycle load while the low cycle loads keep constant.

复合载荷下，低周幅值不变，增加高周载荷的幅值，微动疲劳寿命随幅值比的增加而降低。

5·In this paper, the failure mechanism and control technology of fretting fatigue have been studied by means of fatigue testing and finite element analysis.

为了研究行人碰撞事故中人体下肢的生物力学响应和损伤机理，建立了一个人体下肢有限元模型。

6·By analyzing the working condition and failure mechanism of packing box, it is proved in theory that fretting fatigue results in the failure of packing box.

通过对填料盘工作状况和失效机制的理论分析，进而在理论上证明了填料盘的开裂是由于微动疲劳造成的。

7·The fretting fatigue behavior of TC4 alloy was investigated using cylinder-plane configuration. Based on the experimental results, the damage mechanism of fretting fatigue failure was discussed.

研究了TC4 合金在柱面-平面接触条件下的微动疲劳行为，分析了其微动疲劳损伤机制。

8·Based on the experiment research and finite element analysis, the fretting wear mechanism and the influence factors on fatigue life are made clear in this paper.

在数值模拟结果与试验结果基础上，总结分析了微动疲劳损伤机理及寿命的影响因素及原因。

9·Fretting wear and its induced fatigue and fracture of wires was one of the major failure modes of the hoisting ropes.

钢丝间的微动磨损以及由此引起的钢丝的疲劳断裂是提升钢丝绳失效的主要原因之一。

10·The results show that the fatigue life with fretting damage is markedly decreased compared with the fatigue life without fretting damage.

计算结果表明：有微动损伤的车轴疲劳寿命比无微动损伤的疲劳寿命明显减少。