An aircraft flap deployment system has a track, a carriage supported by the track; an actuator operatively connected to the carriage for moving the carriage along the track between various carriage positions; a flap pivotally connected to the carriage and to a link such that each position of the carriage has a corresponding flap position; and a flap controller communicating with the actuator for controlling actuation of the actuator. In at least one carriage position, the flap is in an intermediate flap position at a negative flap angle and the actuator maintains the carriage and the flap in position. An aircraft wing assembly having the flap deployment system, an aircraft having the aircraft wing assembly, and a method for controlling a position of a flap of an aircraft are also disclosed.
飞机襟翼展开系统。一种飞机襟翼展开系统具有轨道;由轨道支撑的托架;致动器,其在操作上连接到托架,以使托架沿轨道在各个托架位置之间移动;襟翼,其枢转地连接到托架和连杆,使得托架的每个位置具有相应的襟翼位置;襟翼控制器,其与致动器通信,用以控制致动器的致动。在至少一个托架位置中,襟翼以负襟翼角度处于中间襟翼位置中,并且致动器将托架和襟翼保持到位。还公开了一种具有襟翼展开系统的飞机机翼组件、具有该飞机机翼组件的飞机和用于控制飞机的襟翼的位置的方法。
Aircraft flap deployment system
飞机襟翼展开系统
2020-06-30
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |