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某型直升机旋翼轴载荷测试方法研究
引用本文:张文军,吕伯平.某型直升机旋翼轴载荷测试方法研究[J].航空计测技术,2006,26(1):42-43,51.
作者姓名:张文军  吕伯平
作者单位:空军第一航空学院,河南信阳464000
摘    要:某型直升机旋翼轴是驱动旋翼旋转的关键疲劳部件,本文主要介绍了对该型直升机主旋翼轴载荷的测试方法:应变片的选择及测点布置,测试原理,测试结果及分析.

关 键 词:直升机  旋翼轴  测试方法
文章编号:1002-6061(2006)01-0042-02
收稿时间:2005-05-30
修稿时间:2005-05-30

Research of Testing Method of Rotor Shaft Loading of One Type of Helicopter
ZHANG Wen-jun,LV Bo-ping.Research of Testing Method of Rotor Shaft Loading of One Type of Helicopter[J].Aviation Metrology & Measurement Technology,2006,26(1):42-43,51.
Authors:ZHANG Wen-jun  LV Bo-ping
Institution:The First Aeronautic Institute of Air Force,Xinyang 464000,China
Abstract:One type of helicopter rotor shaft is the key fatigue part that drives rotor to revolve. This paper principally introduces the testing method of the type of helicopter rotor shaft loading, including the choice of strain gauge, deploying of measuring point ,testing principle, testing result and analysis.
Keywords:helicopter  rotor shaft  testing method
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