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应变测试技术应用于发动机质心偏移研究
引用本文:王文龙,赵政社,混平,刘英元.应变测试技术应用于发动机质心偏移研究[J].火箭推进,2011,37(2):76-80.
作者姓名:王文龙  赵政社  混平  刘英元
作者单位:西安航天动力试验技术研究所,陕西,西安,710100
摘    要:为研究液体火箭发动机的质心偏移情况,在发动机传力构件上合理分布测量点,对发动机机架、推力室与机架连接压杆、推力室头部等多个区域的缓应变参数进行了测量,通过对测量数据的处理与分析,得出了发动机质心偏移情况的初步判断.

关 键 词:发动机试车  缓应变  质心偏移

Application of strain testing technology in research on centroid shift of rocket engine
WANG Wen-long,ZHAO Zheng-she,HUN Ping,LIU Ying-yuan.Application of strain testing technology in research on centroid shift of rocket engine[J].Journal of Rocket Propulsion,2011,37(2):76-80.
Authors:WANG Wen-long  ZHAO Zheng-she  HUN Ping  LIU Ying-yuan
Institution:(Xi' an Aerospace Propulsion Test Technique Institute, Xi'an 710100, China)
Abstract:The method of slow strain testing for the liquid-propellant rocket engine is introduced in the paper. In order to research the centroid shift of the liquid-propellant rocket engine, the detecting points are reasonably collocated on the force transmission constructional elements to detect the slow strain parameters of the engine frame, pressure lever between thrust chamber and engine frame, and front-end of thrust chamber. The preliminary judgement for the centroid shift of the liquid-propellant rocket engine was achieved after the processing and analysis of the detected data.
Keywords:rocket engine test  slow strain  centroid shift
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