본 발명은 비행체에 장착되고, 내부 공간을 갖는 하우징, 상기 하우징의 내부 공간에서 회전력을 형성하는 구동 모터, 상기 구동 모터의 회전력을 전달받고, 상기 구동 모터의 회전축과 교차되어 치합되는 제1 샤프트, 상기 제1 샤프트와 동축 상에 배치되는 제2 샤프트, 상기 제1 샤프트와 제2 샤프트의 회전 동력을 선택적으로 단속하는 클러치 및 상기 제2 샤프트의 회전력을 전달받는 보빈을 포함하는, 비행체용 윈치를 제공한다.
An objective of the present invention is to provide a winch for a flight vehicle that can be supplied at high speed by free fall in the case of an emergency in the process of supplying projectiles using the winch mounted on the flight vehicle. According to the present invention, provided is a winch for a flight vehicle, which comprises: a housing mounted on a flight vehicle and having an inner space; a drive motor forming a rotational force in the inner space of the housing; a first shaft which receives the rotational force of the drive motor and intersects with a rotational axis of the drive motor to be engaged; a second shaft disposed coaxially with the first shaft; a clutch which selectively regulates the rotational force of the first shaft and the second shaft; and a bobbin receiving the rotational force of the second shaft.
WINCH PROVIDED IN FLYING OBJECT
비행체용 윈치
2023-06-28
Patent
Electronic Resource
Korean
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