Disclosed is an actuator for varying the position of a flight control surface on an aircraft, wherein the actuator comprises a no-back device (10) including a backlash adjuster, which is arranged to select a plurality of different backlash lengths. The backlash adjuster may be a nut (20) which moves relative a housing of the no-back device (10) by rotating the nut (20). Also disclosed is a method of adjusting the backlash (B) in a flight control surface actuator, by moving the backlash adjuster axially to adjust the backlash (B) to a desired value.
УСТРОЙСТВО БЛОКИРОВКИ ОБРАТНОГО ХОДА ДЛЯ ПРИВОДА РУЛЯ УПРАВЛЕНИЯ ПОЛЕТОМ
2017-10-13
Patent
Electronic Resource
Russian
IPC: | B64C AEROPLANES , Flugzeuge |
УСТРОЙСТВО, ИСПЫТАТЕЛЬНЫЙ СТЕНД И СПОСОБ ИСПЫТАНИЙ СТРЕЛОЧНОГО ПРИВОДА
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Устройство пневматического привода прислонно-сдвижной двери пассажирского вагона
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