| 发明名称 |
AIRCRAFT |
| 摘要 |
An aircraft with a turbofan engine including an engine body and a fan, wherein the turbofan engine is supported on an airframe via a pylon, an igniter cable is interposed between an ignition plug of the engine and an ignition control unit that controls power supply to the ignition plug, and at least a part of the igniter cable is passed through an inside of the pylon. |
| 申请公布号 |
US2015232188(A1) |
申请公布日期 |
2015.08.20 |
| 申请号 |
US201514614650 |
申请日期 |
2015.02.05 |
| 申请人 |
MITSUBISHI AIRCRAFT CORPORATION |
发明人 |
TATEIWA Jingo |
| 分类号 |
B64D27/12;B64D29/02 |
主分类号 |
B64D27/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising a turbofan engine including an engine body and a fan,
wherein the turbofan engine is supported on an airframe via a pylon, an igniter cable is interposed between an ignition plug of the engine and an ignition control unit that controls electric power supply to the ignition plug, and at least a part of the igniter cable is passed through an inside of the pylon. |
| 地址 |
Aichi JP |
