An extended tail wing according to an embodiment of the present invention comprises: an extending body which can be extended in a longitudinal direction, and connected to a launching body in a compressed state; a fixating means locking the extending body such that the compressed state of the extending body may be maintained, and unlocking the extending body such that the extending body may be extended when the launching body is launched; and a tail wing connected to a rear side of the extending body.

    일 실시 예에 따른 확장형 꼬리 날개는, 길이 방향으로 연장 가능하고, 발사체에 압축 상태로 연결되는 연장체; 상기 연장체의 압축 상태가 유지되도록 상기 연장체를 구속하고, 상기 발사체가 발사되면 상기 연장체가 연장되도록 상기 연장체에 대한 구속을 해제하는 고정 수단; 및 상기 연장체의 후측에 연결되는 꼬리 날개를 포함할 수 있다.


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    Titel :

    EXTENDED TAIL WING


    Weitere Titelangaben:

    확장형 꼬리 날개


    Beteiligte:
    LEE HAN JIN (Autor:in) / SONG MIN SUP (Autor:in) / BANG JAE WON (Autor:in)

    Erscheinungsdatum :

    21.03.2019


    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



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