发明名称 HIGH SHEAR CAPABILITY INTERFACE
摘要 A connection between a first component and a second component is provided including a first hole formed in a portion of the first component and a second hole formed in a portion of the second component. The second hole is aligned with the first hole. A pin includes a through hole having a pin hole diameter. The pin extends through a portion of the first hole and into a first portion of the second hole. The pin is configured to absorb a shear load applied to the connection. A bolt extends through the second hole and the pin such that a clearance fit is formed between the bolt and the pin. The bolt is configured to absorb an axial load applied to the connection. A nut connected to the free end of the bolt limits movement of the bolt relative to the first and second component.
申请公布号 US2015147132(A1) 申请公布日期 2015.05.28
申请号 US201314087464 申请日期 2013.11.22
申请人 Sikorsky Aircraft Corporation 发明人 Gmirya Yuriy;Karlak Matthew J.;Meeson, Jr. John H.
分类号 F16B21/10;F16B19/00 主分类号 F16B21/10
代理机构 代理人
主权项 1. A connection between a first component and a second component comprising: a first hole formed in a portion of the first component; a second hole formed in a portion of the second component, the second hole being aligned with the first hole; a pin including a through hole having a pin hole diameter, the pin extending through a portion of the first hole and into a first portion of the second hole, the pin being configured to absorb a shear load applied to the connection; a bolt extending through the second hole and the pin, the bolt having an outer diameter smaller than the pin hole diameter such that a clearance fit is formed between the bolt and the pin, the bolt being configured to absorb an axial load applied to the connection; and a nut connected to a free end of the bolt to limit movement of the bolt relative to the first component and the second component.
地址 Stratford CT US