发明名称 |
CONTROL DEVICE FOR AN ENGINE |
摘要 |
<p>The invention relates to a control device for an engine, comprising means (150) for calculating a blade pitch angle setpoint (160) of at least one propeller of the engine, the calculating means (150) using a propeller performance model, taking into account at least one flight speed (115) in order to adapt a blade pitch angle setpoint by taking into account a shaft horsepower setpoint.</p> |
申请公布号 |
WO2014083259(A1) |
申请公布日期 |
2014.06.05 |
申请号 |
WO2013FR52756 |
申请日期 |
2013.11.15 |
申请人 |
SNECMA |
发明人 |
TANTOT, NICOLAS, JÉRÔME, JEAN;BRICHLER, THIERRY |
分类号 |
B64C11/30;B64D31/06 |
主分类号 |
B64C11/30 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|