The invention discloses a rotor air refueling pod which comprises a shell, a ram-type air turbine is arranged at the front end of the shell, a refueling machine fuel supply port, a control interface and a connecting port are formed in the top of the shell, a pod camera base is arranged below the rear end of the shell, and a pod camera is installed on the pod camera base. An oil conveying system, a refueling system, a refueling taper sleeve, a rotor wing, a refueling pod controller and a power supply assembly are arranged in the shell. According to the rotor air refueling pod, under the condition that normal refueling can be guaranteed, refueling operation can be conducted on more aircrafts, the taper sleeve is provided with the rotor, the refueling operation process can be faster and more intelligent, and the refueling operation efficiency can be improved.

    本发明公开了一种旋翼空中加油吊舱,包括外壳,外壳的前端设置有冲压式空气涡轮,外壳顶部设置有加油机燃料供应口、控制接口、连接口,外壳的后端下方设置有吊舱摄像头基座,吊舱摄像头基座上面安装有吊舱摄像头,外壳内部包括有输油系统、加油系统、加油锥套、旋翼、加油吊舱控制器、电源总成。本发明的一种旋翼空中加油吊舱,在保证能正常加油的条件下,还可以给更多的飞行器进行加油作业,锥套带有旋翼可以使加油作业过程更加快速智能,能够提高加油作业的效率。


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    Titel :

    Rotor air refueling pod


    Weitere Titelangaben:

    一种旋翼空中加油吊舱


    Beteiligte:
    WANG XUEFENG (Autor:in) / WU CHENGFEI (Autor:in) / LIU DAN (Autor:in)

    Erscheinungsdatum :

    2022-01-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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