发明名称 |
ENGINE CONTROL COMPUTER OF AIRCRAFT, AND AIRCRAFT |
摘要 |
The invention deals with the restriction on the mode change of an engine due to latching in the case of restarting the engine that has stopped in flight. A FADEC that controls an engine of an aircraft in accordance with a mode, includes a latch operating section that latches the mode, and an in-parking/in-flight determining section that determines whether the aircraft is on the ground or flying off the ground. The latch operating section operates when the in-parking/in-flight determining section determines the aircraft is on the ground, and does not operate when the in-parking/in-flight determining section determines that the aircraft is in fight. |
申请公布号 |
US2017021936(A1) |
申请公布日期 |
2017.01.26 |
申请号 |
US201615288612 |
申请日期 |
2016.10.07 |
申请人 |
MITSUBISHI AIRCRAFT CORPORATION |
发明人 |
NAGASHIMA Yoshihiro |
分类号 |
B64D31/06;F02C7/262;F02C9/28;G05D1/04 |
主分类号 |
B64D31/06 |
代理机构 |
|
代理人 |
|
主权项 |
1. (canceled) |
地址 |
Aichi JP |