The present invention relates to an apparatus of deploying a control fin for a guided weapon, which comprises: a bullet body on which a slot type opening unit for deploying a fin is disposed; a control fin disposed in the bullet body to rotate, elastically supported by an elastic body, and deployed by elasticity of the elastic body; and a fin stopper unit supporting the control fin to be disposed in the bullet body in a folded state, and allowing the control fin to be deployed after a guided weapon is launched. Accordingly, the apparatus of deploying a control fin for a guided weapon prevents accidental deployment of the control fin, and enables the control fin to be deployed only when the guided weapon is actually operated. Therefore, the apparatus of deploying a control fin for a guided weapon can prevent disuse of the entire complete bullet due to a deployment of the control fin, thereby preventing unnecessary consumption of the guided weapon and significantly increasing operation efficiency of the guided weapon.

    본 발명은 유도무기용 조종날개 전개 장치에 관한 것으로 슬롯형태의 날개 전개용 개방부가 위치된 탄 몸체, 상기 탄 몸체 내에 회전 가능하게 위치되고 탄성체에 의해 탄성 지지되고 탄성체의 탄성력에 의해 전개되는 조종날개, 상기 조종날개가 상기 탄 몸체 내에서 접혀진 상태로 위치하도록 지지하고 유도무기의 발사 후 상기 조종날개가 전개되도록 하는 날개 스토퍼부를 포함하여 우발적인 조종날개의 전개를 방지하고, 유도무기의 실제 운용 시에만 조종날개가 전개될 수 있도록 하여 조종날개의 전개로 완성탄의 전체가 불용되는 사고를 방지하여 불필요한 유도무기의 소모를 방지하고, 유도무기의 운용 효율을 크게 향상시킬 수 있다.


    Access

    Download


    Export, share and cite



    Title :

    CANARD DEPLOYING APPARATUS FOR GUIDED MISSILE AND CANARD DEPLOYING METHOD FOR GUIDED MISSILE USING THE SAME


    Additional title:

    유도무기용 조종날개 전개 장치 및 이를 이용한 유도무기용 조종날개 전개방법


    Contributors:
    KIM YONG DUK (author) / PARK EUN JOO (author) / KIM SAN HO (author) / CHOI JAE HYUN (author) / AHN JIN SOO (author)

    Publication date :

    2020-04-24


    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



    APPARATUS AND METHOD OF DEPLOYING WING OF GUIDED MISSILE

    YU SE LIN | European Patent Office | 2022

    Free access

    APPARATUS AND METHOD OF DEPLOYING WING OF GUIDED MISSILE

    European Patent Office | 2023

    Free access

    Aerodynamic performance improvement of a canard control missile

    Tahani, M. / Masdari, M. / Kazemi, M. | Emerald Group Publishing | 2017


    Experimental Flight Characterization of a Canard-Controlled, Subsonic Missile

    Fresconi, Frank / Celmins, Ilmars / Maley, James et al. | AIAA | 2018