复合材料舵翼面静力加载方式研究  

The investigation on static loading method of composite wing

作　　者：杨蓉[1] 孙金云[1] 吴兵[1] 李晓峰[1] 杜珺[1] 

机构地区：[1]北京强度环境研究所,北京100076

出　　处：《强度与环境》2012年第2期1-8,共8页Structure & Environment Engineering

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。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.

关 键 词：复合材料 翼面 静强度 

分 类 号：V416.1[航空宇航科学与技术—航空宇航推进理论与工程]