首页> 外国专利> METHOD FOR SIMULTANEOUS OPERATION OF DRIVES FOR MOVING AIRCRAFT LATCHES, DEVICE FOR AIRCRAFT LATCH DRIVES AND AIRCRAFT EQUIPPED WITH SUCH DEVICE

METHOD FOR SIMULTANEOUS OPERATION OF DRIVES FOR MOVING AIRCRAFT LATCHES, DEVICE FOR AIRCRAFT LATCH DRIVES AND AIRCRAFT EQUIPPED WITH SUCH DEVICE

机译:用于同时移动飞机闩锁的驱动器的方法,用于飞机闩锁驱动器的设备以及配备有这种设备的飞机

摘要

1. A method for the simultaneous operation of drives for moving at least two movable aerodynamic surfaces of an aircraft, including: - controlling drives for moving movable aerodynamic surfaces in the direction of a given position; - detecting, during movement, the slowest drive; and - adaptation of the drive control to fit it under the action of the slowest drive. 2. The method according to claim 1, wherein when the drive reaches a predetermined position, this drive is stopped and braked to hold it in a predetermined position. The method according to claim 1, wherein each drive comprises an electric motor, the method comprising the step of detecting a failure due to a combination of at least some of the following parameters: position of the aerodynamic surface; engine position; motor power supply current; drive load 4. The method according to claim 3, in which each drive contains a brake, while the parameters used in the failure detection mode also contain a braking torque. The method according to claim 3, in which, in case of failure of at least one of the drives, all the drives are stopped. The method according to claim 3, which is designed to control at least four aerodynamic surfaces distributed over both wings of the aircraft, while in case of failure of at least one of the drives of one of the aerodynamic surfaces on one of the wings, the drives of this aerodynamic surface are stopped , as well as the drives of the corresponding aerodynamic surface located on the other wing. 7. The method according to claim 6, in which the drives dr
机译:1.一种用于使飞行器的至少两个可移动空气动力学表面运动的驱动器同时运行的方法,包括:-控制用于沿给定位置的方向移动可移动空气动力学表面的驱动器; -在运动过程中检测最慢的驱动; -在最慢的驱动器的作用下使驱动器控制适合它。 2.根据权利要求1所述的方法,其中,当驱动器到达预定位置时,该驱动器被停止和制动以将其保持在预定位置。 2.根据权利要求1所述的方法,其中,每个驱动器包括电动机,所述方法包括检测由于以下至少一些参数的组合而引起的故障的步骤:所述空气动力学表面的位置;发动机位置;电机电源电流; 4.根据权利要求3所述的方法,其中,每个驱动器包括制动器,而在故障检测模式中使用的参数还包括制动转矩。 4.根据权利要求3所述的方法,其中,在至少一个驱动器发生故障的情况下,所有驱动器都被停止。 4.根据权利要求3所述的方法,其被设计成控制分布在所述飞机的两个机翼上的至少四个空气动力学表面,而在所述机翼之一上的空气动力学表面之一的驱动器中的至少一个驱动器失效的情况下,停止了该空气动力学表面的驱动以及位于另一侧翼上的相应空气动力学表面的驱动。 7.根据权利要求6所述的方法,其中,驱动器dr

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