某锁闭机构耐久性试验研究 |
| |
引用本文: | 徐梅香,张辉.某锁闭机构耐久性试验研究[J].直升机技术,2012(4):61-64. |
| |
作者姓名: | 徐梅香 张辉 |
| |
作者单位: | 1. 中国直升机设计研究所,江西景德镇,333001 2. 中航工业综合技术研究所,北京,100028 |
| |
摘 要: | 为了验证某直升机用锁闭机构的耐久性能,在没有现行标准的情况下,作者采用逐步加载的方法确定预紧力进行耐久性试验,该方法为耐久性试验的具体实施提供了一种解决思路。
|
关 键 词: | 锁闭机构 耐久性试验 预紧力 |
An Endurance Test Research of a Hook Latch |
| |
Authors: | XU Meixiang ZHANG Hui |
| |
Institution: | 1.China Helicopter Research and Development Institute, Jingdezhen 333001,China; 2.China Aero Polytechnical Establishment, Beijing 100028,China) |
| |
Abstract: | To verify a hook latch' s endurance, the author put forward a new test method under no existing standard. This method confirmed the tension preload of the endurance test by loading to the hook latch step by step, and it provided a new idea of how operating the endurance test to hook latches. |
| |
Keywords: | hook latch endurance test tension preload |
本文献已被 CNKI 维普 万方数据 等数据库收录! |