首页> 外国专利> METHOD FOR CONTROLLING THE THRUST OF THE JET ENGINES OF AN AIRCRAFT DURING THE TAKE-OFF PHASE, CONTROLLING DEVICE AND CORRESPONDING AIRCRAFT

METHOD FOR CONTROLLING THE THRUST OF THE JET ENGINES OF AN AIRCRAFT DURING THE TAKE-OFF PHASE, CONTROLLING DEVICE AND CORRESPONDING AIRCRAFT

机译:在起飞阶段控制飞机喷气发动机推力的方法,控制装置及相应的飞机

摘要

The present invention relates to a control of the engine thrust of a multi-reactor process plane (1), during aircraft take-off phase, which successively comprises a first step of controlling the reactor at a first thrust level P1, until the aircraft (1) reaches a first predetermined speed VA, and a second step of controlling the reactor at a second thrust level P2, less than the first level P1 thrust, when the aircraft (1 ) has a higher speed than the first predetermined speed VA, the first predetermined speed VA being selected less than the minimum control ground speed V MCG said aircraft (1) when the reactors are the second thrust level P2.
机译:[0001]本发明涉及在飞机起飞阶段期间对多反应堆工艺平面(1)的发动机推力的控制,该控制依次包括将反应堆控制在第一推力水平P1直至飞机( 1)达到第一预定速度VA,以及第二步骤,当飞机(1)的速度高于第一预定速度VA时,将反应堆控制在小于第一水平P1推力的第二推力水平P2上,当反应堆为第二推力水平P2时,将第一预定速度VA选择为小于所述飞机(1)的最小控制地面速度V

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