The present invention relates to a bending modification-type control wing of a guided missile, capable of precisely controlling a trajectory of the guided missile, by controlling the control wing of the guided missile in the direction curved by a piezoelectric unit in an unfolded state of the control wing of the guided missile. According to the present invention, the bending modification-type control wing of a guided missile relates to a guided missile equipped with a body (10), and a control wing (20) installed with a plurality of wing units (21) to control the trajectory along the circumference of the body (10). The wing units (21) include a piezoelectric driving unit (22) integrally attached to the wing units (21), expanded or contracted when being applied to a voltage, for bending and modifying the wing units (21) to bend the remaining portion in any one direction in comparison with the front end of the wing units (21).

    본 발명은 유도탄의 조종날개가 전개된 상태에서 상기 유도탄의 조종날개를 압전부에 의해 만곡되는 방향을 제어함으로써, 상기 유도탄의 탄도를 정밀하게 제어할 수 있는 유도탄의 굽힘 변형식 조종날개에 관한 것이다. 본 발명에 따른 유도탄의 굽힘 변형식 조종날개는, 몸체(10)와 상기 몸체(10)의 둘레를 따라 탄도를 제어하도록 복수로 날개부(21)가 설치되는 조종날개(20)를 구비한 유도탄에 있어서, 상기 날개부(21)에는, 상기 날개부(21)에 일체로 부착되고, 전압이 인가되면 팽창되거나 수축되면서, 상기 날개부(21)의 전단에 비하여 나머지 부분이 어느 한 방향으로 휘어지도록 상기 날개부(21)를 굽힘변형시키는 압전구동부(22)를 포함하는 것을 특징으로 한다.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    BENDING TYPE CONTROL WING OF MISSILE


    Weitere Titelangaben:

    유도탄의 굽힘 변형식 조종날개


    Beteiligte:
    LEE SANG KYU (Autor:in) / CHAE JE WOOK (Autor:in) / CHOE EUI JUNG (Autor:in)

    Erscheinungsdatum :

    01.04.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    Bending type control wing of missile

    Europäisches Patentamt | 2016

    Freier Zugriff

    WING-FUSELAGE FUSION TYPE VARIABLE OBLIQUE WING PLUS TERMINAL WING MISSILE

    SUZUKI KAZUTAKA | Europäisches Patentamt | 2017

    Freier Zugriff

    WING, MISSILE, AND MANUFACTURING METHOD FOR WING

    KANAZAWA MASARU / KATSUNAGA KENTA / OGIMURA KOJI | Europäisches Patentamt | 2021

    Freier Zugriff

    Ring Wing for a Compressed Missile

    August, H. | Online Contents | 1996


    Ring Wing for an Underwater Missile

    August, H. | Online Contents | 1996