A wing deployment device for a guided missile may be disclosed. The wing deployment device according to an embodiment may include: a wing assembly in which one end of a wing is rotatably coupled and the wing is deployed; a wing fixing block that fixes the wings until a preset time before and after launch of the missile, and releases the fixation of the wings so that the wings are deployed after a preset time; and an elastic member coupled to the wing fixing block and moving the wing fixing block to fix and release the wing based on a propulsion acceleration of the missile. The present invention may provide the wing deployment device and the wing deployment method for deploying wings after a predetermined time after a guided missile is launched from the inside of a launch tube.

    유도탄의 날개 전개 장치가 개시될 수 있다. 일 실시예에 따른 날개 전개 장치는, 날개의 일단이 회전 가능하게 결합되고 날개를 전개시키는 날개 조립체; 유도탄의 발사 전 및 유도탄의 발사 후 사전 설정된 시간까지 날개를 고정시키고, 사전 설정된 시간 이후 날개가 전개되도록 날개의 고정을 해제하는 날개 고정 블록; 및 날개 고정 블록에 결합되고, 상기 유도탄의 추진 가속도에 기초하여 날개를 고정 및 고정 해제하도록 날개 고정 블록을 이동시키는 탄성 부재를 포함할 수 있다.


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    Title :

    APPARATUS AND METHOD OF DEPLOYING WING OF GUIDED MISSILE


    Additional title:

    유도탄의 날개 전개 장치 및 날개 전개 방법


    Contributors:
    YU SE LIN (author)

    Publication date :

    2022-10-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / B64C AEROPLANES , Flugzeuge / F41G Zielvorrichtungen für Waffen , WEAPON SIGHTS



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