发明名称 |
Method for optimising the performance of an aircraft, device and aircraft |
摘要 |
<p>The method involves defining two levels of performance of an aircraft (1), and determining a power margin based on a rotational speed of a gas generator (2'). Another power margin is determined based on a temperature of the gas. Each power margin is compared to a threshold to determine whether a target level of performance is equal to one of the levels of performance, and the target level of performance is displayed so that a pilot controls the aircraft depending on the target level of performance established before the flight. An independent claim is also included for a device for optimizing the performance of a rotary wing aircraft.</p> |
申请公布号 |
EP2623746(A1) |
申请公布日期 |
2013.08.07 |
申请号 |
EP20120007806 |
申请日期 |
2012.11.19 |
申请人 |
EUROCOPTER |
发明人 |
EVRARD, JEAN-PHILIPPE;CORPRON, ALBAN |
分类号 |
F02C9/00;B64D31/00;G05B23/02;G07C5/08 |
主分类号 |
F02C9/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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