According to an embodiment of the present invention, a tail-sitter aircraft having a rotating cockpit may comprise: an aircraft body; a canopy installed on the aircraft body and having an accommodation space therein; a support frame connected to the aircraft body and attached to an outer surface of the canopy; a rotating rod protruding from the support frame toward the accommodation space of the canopy and rotatably connected to the support frame; a control frame provided in the accommodation space and connected to the rotating rod; a cockpit installed on the control frame; and an interface installed on the control frame and provided in front of the cockpit. There are advantages of a tail-sitter aircraft that can take off and land in a narrow space such as a parking lot or a private house without using a runway, while securing the visibility, comfort, range and maneuverability of a pilot without changing the external shape of the aircraft during take-off and landing.

    일 실시 예에 따른 회전 조종석을 갖는 테일시터 항공기는, 항공기 바디; 상기 항공기 바디에 설치되고, 내부에 수용 공간을 갖는 캐노피; 상기 항공기 바디에 연결되고, 상기 캐노피의 외측면에 부착되는 지지 프레임; 상기 지지 프레임으로부터 상기 캐노피의 수용 공간을 향해 돌출되고, 상기 지지 프레임에 대해 회전 가능하게 연결되는 회전 로드; 상기 수용 공간에 마련되고, 상기 회전 로드에 연결되는 조종 프레임; 상기 조종 프레임 상에 설치되는 조종석; 및 상기 조종 프레임 상에 설치되고, 상기 조종석의 전방에 마련되는 인터페이스를 포함할 수 있다.


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    Titel :

    TAIL-SITTER AIRCRAFT WITH A ROTATING COCKPIT


    Weitere Titelangaben:

    회전 조종석을 갖는 테일시터 항공기


    Erscheinungsdatum :

    2021-11-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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