| 发明名称 |
EMERGENCY OPERATING MODE FOR A PISTON ENGINE IN AN AIRPLANE |
| 摘要 |
A method is provided for operating a piston engine in an airplane in an emergency operating mode, in which a minimum power output of the piston engine is ensured in that an emergency operating mode is activated that is as much as possible independent of measured values of respective sensors provided for an operation of the piston engine, in which the measured values of the sensors are substituted with firmly specified values. A corresponding airplane is provided as well as to an emergency operation control unit for carrying out the provided method. |
| 申请公布号 |
US2015252740(A1) |
申请公布日期 |
2015.09.10 |
| 申请号 |
US201514640723 |
申请日期 |
2015.03.06 |
| 申请人 |
Robert Bosch GmbH |
发明人 |
HEYL Andreas;DAMM Daniel;HERBORD Markus;WETTIG Matthias;FEUCHTER Wilfried;SOMMER Nicolas |
| 分类号 |
F02D29/02 |
主分类号 |
F02D29/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for operating at least one piston engine in an airplane in an emergency operating mode, in which a minimum power output of the at least one piston engine is ensured, the method comprising:
activating the emergency operating mode that is as much as possible independent of measured values of respective sensors provided for an operation of the at least one piston engine; and substituting the measured values of the sensors with firmly specified values. |
| 地址 |
Stuttgart DE |
