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- W2369912698 abstract "The control system tightwire in an aircraft fractured during the deceleration of the engine. In order to find out the cause of the fracture,macro and micro observation of the fracture surface,chemical composition analysis,ultimate tension tests,surface trace observation and fatigue tests were carried out. The results show that the fracture of the tightwire is fatigue fracture mainly controlled by bending stress. The abrasion between the tightwire and pulley,as well as that between the steel wires,promoted the initiation of the fatigue cracks. The fatigue life of the control system can be enhanced by choosing the pulley of proper size and improving the lubricating condition between the tightwire and the pulley." @default.
- W2369912698 created "2016-06-24" @default.
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- W2369912698 date "2009-01-01" @default.
- W2369912698 modified "2023-09-23" @default.
- W2369912698 title "Failure Analysis of Control System Tightwire in Aircraft" @default.
- W2369912698 hasPublicationYear "2009" @default.
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