The invention discloses a thrust direction variable power device which comprises a fan, a shell and an adjusting mechanism, an air inlet duct, a first air outlet duct and a second air outlet duct are arranged in the shell, the fan is arranged in the air inlet duct, and the adjusting mechanism is located at the intersection of the air inlet duct, the first air outlet duct and the second air outlet duct. The adjusting mechanism is movably connected to the shell and provided with a guiding air channel, the guiding air channel enables the air inlet channel to communicate with the first air outlet channel and/or the second air outlet channel after the adjusting mechanism moves relative to the shell, and airflow provided by the fan at the position of the air inlet channel can be exhausted to the outside through the first air outlet channel and/or the second air outlet channel. Therefore, the thrust direction is changed, and the thrust direction requirements of the aircraft in different flight states are met.

    本发明公开了一种可变推力方向的动力装置,包括风扇、壳体和调节机构,壳体内设有进风风道、第一出风风道和第二出风风道,风扇设于进风风道,调节机构位于进风风道、第一出风风道和第二出风风道三者之间的相交处,且调节机构活动连接于壳体,调节机构具有引导风道,引导风道在调节机构相对壳体运动后使进风风道连通于第一出风风道和/或第二出风风道,进风风道处的风扇提供的气流即可从第一出风风道和/或第二出风风道排出至外界,以改变推力方向,满足飞行器在不同飞行状态时的推力方向需求。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Power device with variable thrust direction and aircraft


    Weitere Titelangaben:

    可变推力方向的动力装置及飞行器


    Beteiligte:
    HU HUAZHI (Autor:in) / DING KAI (Autor:in)

    Erscheinungsdatum :

    2023-01-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



    POWER PLANT WITH VARIABLE THRUST DIRECTION, AND AIRCRAFT

    HU HUAZHI / DING KAI | Europäisches Patentamt | 2024

    Freier Zugriff


    VARIABLE DIRECTION THRUST UNMANNED AERIAL VEHICLE

    BOEHNKE RYAN L | Europäisches Patentamt | 2016

    Freier Zugriff

    Thrust generating device with adjustable thrust direction

    HWANG KEUM CHEON / CHAE BYUNG CHUL | Europäisches Patentamt | 2018

    Freier Zugriff

    CONTROLLERS AND AIRCRAFT WITH VARIABLE ENGINE THRUST TAKEOFF SYSTEM

    HORNE THOMAS C / LANDERS THOMAS / LAVRISA THOMAS P et al. | Europäisches Patentamt | 2024

    Freier Zugriff