| 摘要 |
<p>The method involves measuring current values (N1c1-N1c4) of driving parameters associated to external engines (M1, M4) and internal engines (M2, M3). Detection is made whether difference between the current values of the driving parameters associated with each engine and a determined intermediate setpoint value (N1x) is equal to a predefined threshold. Operating speed of the engines is raised to determined take-off speed such that the driving parameters associated with the engine reach a takeoff setpoint value when the difference is equal to the predefined threshold. An independent claim is also included for a device for controlling operating speed of engines of an aircraft during take-off phase.</p> |
