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复合材料舵翼面静力加载方式研究
引用本文:杨蓉,孙金云,吴兵,李晓峰,杜珺.复合材料舵翼面静力加载方式研究[J].强度与环境,2012(2):1-8.
作者姓名:杨蓉  孙金云  吴兵  李晓峰  杜珺
作者单位:北京强度环境研究所,北京100076
摘    要:随着新材料及新工艺的不断发展,复合材料以其低质量高力学性能的优势,被广泛应用到各种飞行器结构中.本文主要针对 C/C、C/SiC 等复合材料舵翼面静力试验的加载方式进行了调研,发现拉式及压式杠杆组合加载的方式较为常用,而且早期国外的研究中,就对压式杠杆中载荷橡胶垫的力学性能进行过专门描述

关 键 词:复合材料  翼面  静强度

The investigation on static loading method of composite wing
YANG Rong,SUN Jinyun,WU Bing,LI Xiaofeng,DU.The investigation on static loading method of composite wing[J].Structure & Environment Engineering,2012(2):1-8.
Authors:YANG Rong  SUN Jinyun  WU Bing  LI Xiaofeng  DU
Institution:Jun(Beijing Institute of Structure and Environment Engineering,Beijing 100076,China)
Abstract:With the development of the new materials and new technology,low-quality composite material with high mechanical properties of its advantages,this has been widely applied to various aircraft structure.In this paper,investigation of static loading method about rudder wing surface with C/C and C/SiC composite material was conducted,it was found that the lever of tension and compression have been used usually,in addition,foreigners had special studies on the mechanical properties of load pad in the early.
Keywords:composite  wing surface  static strength
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