摘要
当舵面的轴向惯性载荷有多个接头承载时,且各个接头处的承载结构细节不相同时,文章通过结构分析把舵面惯性载荷分配在各个承载接头上,以确定各个接头上轴承的轴向承载许用值。
When Aircraft rudder inertia load supported by several fittings with different details, this paper uses structure analysis method to allocate rudder surface inertial load into different bearing joints to make sure their bearing axial static limit load.
出处
《江苏科技信息》
2016年第20期68-69,共2页
Jiangsu Science and Technology Information
关键词
舵面惯性载荷
结构设计
飞机
rudder inertia load
structure design
plane
