| 摘要 |
A flight control indicator for twin-engine aircraft, in particular a rotary-wing aircraft comprising two turboengines for driving at least one rotor, intended to provide the power margin available on the engines of the aircraft as a function of the flight conditions. Display means (6) presents a single dial (8) furnished with two needles (91, 92), each of them corresponding to a respective engine, and positioned in such a way that, when the engines are operating normally, the two needles are merged.
|
