| 发明名称 |
AIRCRAFT ENGINE PYLON |
| 摘要 |
An aircraft engine pylon having an upper fitting, an upper panel located below the upper fitting, a shear pin at least partially coupling the upper fitting and the upper panel, and tension fasteners at least partially coupling the upper fitting and the upper panel with the shear pin defining a shear force load path and the tension fasteners defining tension force load paths. |
| 申请公布号 |
US2016159487(A1) |
申请公布日期 |
2016.06.09 |
| 申请号 |
US201314907233 |
申请日期 |
2013.07.26 |
| 申请人 |
KANG Yanxiang;YUAN Mingchao;FANG Xueliang;MRA SYSTEMS, INC. |
发明人 |
Kang Yanxiang;Yuan Mingchao;Fang Xueliang |
| 分类号 |
B64D27/26 |
主分类号 |
B64D27/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft engine pylon comprising:
an upper fitting; an upper panel located below the upper fitting; a shear pin at least partially coupling the upper fitting and the upper panel; and tension fasteners at least partially coupling the upper fitting and the upper panel; wherein the shear pin defines a primary shear force load path for shear forces acting between the upper fitting and the upper panel, and the tension fasteners define a primary tension force load path for tension forces acting between the upper fitting and the upper panel. |
| 地址 |
Shanghai CN |
