Method for optimizing the take-off parameters of an aircraft

• Main Authors: CYRILLE THIERS, JEAN-PIERRE DEMORTIER, CHRISTOPHE HOMEHR, ERIC PETIT, CHRISTIAN LULLA, COLIN HODGES
• Format: Patent
• Language: Chinese; English
• Published: 12.12.2017
• Subjects: CONTROLLING; PHYSICS; REGULATING; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES

A method for optimizing the take-off parameters of an aircraft. The aircraft comprises a system for automatically controlling the high lift devices at the moment when the wheels of the aircraft leave the ground. The method comprises a step of selecting a first configuration of the high lift devices at the start of the take-off phase and a selection of an acceleration speed of the aircraft. The method is advantageous in that, on reception of an actual aircraft take-off detection signal, a control unit is configured to transmit a control command making it possible to bring the high lift devices into a second configuration, in which they are retracted relative to the first position, and consecutively accelerate the speed of the aircraft automatically to an acceleration speed entered by the pilot. 本发明涉及用于优化飞行器的起飞参数的方法。该飞行器(2)包括用于在飞行器的机轮离开地面(E3-E4)时自动控制增升装置的系统，该方法包括在起飞阶段(E1)开始时选择增升装置的第构型(C1)的步骤和选择飞行器的加速速度(V2)。该方法的优点在于，在接收到实际的飞行器起飞(E5)检测信号时，控制单元被配置成用于发送控制命令，使得可以将这些增升装置带入第二构型(C2)中，在该第二构型中它们相对于第位置(C1)收回，并将飞行器的速度自动地加速