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首页> 外文期刊>Engineering failure analysis >Bending fatigue tests on a metallic wire rope for aircraft rescue hoists
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Bending fatigue tests on a metallic wire rope for aircraft rescue hoists

机译:飞机救援提升机用金属钢丝绳的弯曲疲劳试验。

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摘要

During normal operation, the ends of helicopter rescue hoist ropes, to which a hook is attached, can be subject to bending stress caused by vibrations. This happens in the event of partial or total recovery of the hook into its lodging without a spring-loaded blocking system. The swinging of the rope end consequently causes bending of the rope near the terminal, with resultant fatigue stress that can lead quickly to breakage or damage of the rope. A series of alternating bending fatigue tests using a constant load, similar to those known as BoS (bending over sheave) tests, were carried out. These simulate the effective working conditions of a rescue hoist. This paper describes modifications to test machinery, the test method and the data obtained; statistical analysis of this data enabled us to make a rope life prediction which was then experimentally confirmed by run-outs on test ropes.
机译:在正常操作过程中,直升飞机救援提升绳的末端(附有钩子)可能会因振动而产生弯曲应力。在没有弹簧加载的锁止系统的情况下,如果钩子部分或全部恢复到其容纳状态,则会发生这种情况。绳索端部的摆动因此导致绳索在终端附近弯曲,从而产生疲劳应力,该疲劳应力会迅速导致绳索断裂或损坏。进行了一系列使用恒定载荷的交替弯曲疲劳测试,类似于已知的BoS(滑轮弯曲)测试。这些模拟了救援起重机的有效工作条件。本文介绍了对测试设备,测试方法和获得的数据的修改;对这些数据的统计分析使我们能够做出绳索寿命预测,然后通过测试绳索跳动通过​​实验确认。

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