一种民机静力试验平尾加载假件的设计  

Design of Horizontal Tail Load Dummy for Civil Aircraft in Static Test

作　　者：刘佳[1] 

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《工程与试验》2013年第3期38-40,共3页Engineering and Test

摘　　要：本文提出了一种民用飞机静力试验平尾加载假件的设计思路。通过机身后段静力试验各种载荷工况的考核,证明了该假件的刚度和强度满足设计的要求,可以为民用飞机机体结构静力试验的假件设计提供参考。A design method of horizontal tail load dummy for a civil aircraft in static test is introduced in this paper. Several load conditions are evaluated in the static test for the after-fuselage of a civil aircraft. The test results show that the dummy has enough stiffness and strength to meet the design requirement. Such method could provide reference for the dummy design of full-scale airframe in static test.

关 键 词：民用飞机 静力试验 水平尾翼 假件设计 

分 类 号：V216.1[航空宇航科学与技术—航空宇航推进理论与工程]