The present invention relates to a controller for controlling the selection of a front-wheel steering device for an aircraft and a selection controlling method thereof and, more specifically, to a controller for controlling the selection of a front-wheel steering device for an aircraft composed of first and second selection switches (110, 120) positioned in a front seat and a rear seat by being formed into a momentary type switch; a weight-on-wheel (WOW) limit switch (130) selecting a cutoff of an oil pressure supply to the front-wheel steering device in a flight by determining whether the aircraft flies or not; a switching unit (100) selecting whether to supply the oil pressure to the front-wheel steering device for the aircraft or not; and a control unit (200) controlling the oil pressure supply by determining front-wheel steering device selection signals according to the selection of the switching unit (100). The control unit (200) controls the oil pressure supply by determining odd-numbered selection signals as front-wheel steering device selection signals when the odd-numbered selection signals are inputted by the first or second selection switch (110, 120) and even-numbered selection signals as front-wheel steering device selection releasing signals when the even-numbered selection signals are inputted by the first or second selection switch (110, 120). The purpose of the present invention is to provide the controller for controlling the selection of the front-wheel steering device for the aircraft and the selection controlling method thereof enabling a pilot to use the front-wheel steering device while reducing a workload of the pilot.

    본 발명은 항공기용 전륜조향장치 선택 제어기 및 그 선택의 제어 방법에 관한 것으로, 더욱 상세하게는 모멘터리(Momentary) 타입 스위치로 형성되어 전방석 및 후방석에 위치하는 제 1 및 제 2 선택 스위치(110, 120)와, 항공기의 비행 여부를 판단하여 비행 중 전륜조향장치에 유압 공급 차단을 선택하는 WOW(Weight On Wheel) 제한 스위치(130)로 이루어지며, 항공기용 전륜조향장치에 유압 공급 여부를 선택하는 스위칭부(100) 및 상기 스위칭부(100)의 선택 여부에 따라, 항공기용 전륜조향장치 선택 신호를 판단하여 유압 공급을 제어하는 제어부(200)를 포함하여 구성되며, 상기 제어부(200)는 상기 제 1 또는 제 2 선택 스위치(110, 120)에서 홀수번째 선택 신호가 입력될 경우, 항공기용 전륜조향장치 선택 신호로 판단하고, 상기 제 1 또는 제 2 선택 스위치(110, 120)에서 짝수번째 선택 신호가 입력될 경우, 항공기용 전륜조향장치 선택 해제 신호로 판단하여 유압 공급을 제어하는 것을 특징으로 하는 항공기용 전륜조향장치 선택 제어기에 관한 것이다.


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    Title :

    NOSE WHEEL STEERING TAKE CONTROLLER FOR AN AIRPLANE


    Additional title:

    항공기용 전륜조향장치 선택 제어기 및 그 선택의 제어 방법


    Contributors:
    IM GANG BIN (author)

    Publication date :

    2016-06-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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