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Study of Lug Strength under Axial Tension Loads
Author(s): 
Pages: 30-32
Year: Issue:  3
Journal: AIRCRAFT DESIGN

Keyword:  轴向拉伸单耳片双耳片强度计算;
Abstract: 耳片是飞机结构的重要连接元件,是结构主要传力通道上的重要环节,是飞机结构强度计算和细节分析的重点部位.多年来,许多国内外学者、专家对其进行了大量试验研究工作.大量的试验表明,随着加载角度的增大,耳片的静拉伸破坏载荷降低,所以,现在在设计中,都尽量采用受轴向载荷的耳片.本文对受轴向拉伸载荷作用下的单、双耳片进行了强度分析研究,并进行了归纳总结.
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