The fatiguefracturemechanism of main bearing cage is analysed and investigated for aircraft engine taking WP6 for example.
以WP6发动机轴承为例,对航空发动机主轴轴承保持架疲劳断裂的机理进行了分析探讨。
2
The mechanism of the shat-blast enhancing technology and its eldest on improving resisfemle to fatigue and stress corrosion fracture are describe briefly in this paper.
本文简要介绍喷丸强化工艺的机理,及在改善金属零部件疲劳断裂和应力腐蚀断裂抗力中的强化效果;
3
The toughening mechanism of ADI was investigated by microstructure analysis and fracture characteristics of the specimens under tensile test. contact fatigue and stress fatigue.