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 |