| 发明名称 | Aircraft pylon and aircraft | ||
| 摘要 | To provide an aircraft pylon capable of being mounted to a wing without exertion of preload while ensuring that redundancy is provided in the pylon. An aircraft pylon 50 includes: a pylon strut 11 for supporting an engine of an aircraft; a pin joint mechanism for connecting the pylon strut 11 to a main wing of the aircraft; a link member 15 disposed between the pylon strut 11 and the main wing of the aircraft, wherein the link member 15 includes a collection of plural independent link elements. | ||
| 申请公布号 | US9499274(B2) | 申请公布日期 | 2016.11.22 |
| 申请号 | US201414162044 | 申请日期 | 2014.01.23 |
| 申请人 | MITSUBISHI AIRCRAFT CORPORATION | 发明人 | Takeuchi Akira |
| 分类号 | B64C27/26;B64D27/26;B64D27/18 | 主分类号 | B64C27/26 |
| 代理机构 | Pearne & Gordon LLP | 代理人 | Pearne & Gordon LLP |
| 主权项 | 1. An aircraft pylon comprising: a pylon strut for supporting an engine of an aircraft; a pin joint mechanism for connecting the pylon strut to a main wing of the aircraft; and a link member disposed between the pylon strut and the main wing of the aircraft, wherein the link member comprises a collection of plural independent link elements, wherein the plural independent link elements are separately attached to the pylon strut, and the plural independent link elements are attached to each other and partly butted against each other. | ||
| 地址 | Aichi JP | ||