江苏科技信息 ›› 2016, Vol. 33 ›› Issue (20): 23-24.doi: 10.3969/j.issn.1004-7530.2016.20.026
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田会杰
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Tian Huijie
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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。
关键词: 舵面惯性载荷, 结构设计
Abstract: 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.
田会杰. 民用飞机舵面接头轴向承载结构分析[J]. 江苏科技信息, 2016, 33(20): 23-24.
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链接本文: https://qkcb.jssti.cn/jskj/CN/10.3969/j.issn.1004-7530.2016.20.026
https://qkcb.jssti.cn/jskj/CN/Y2016/V33/I20/23