The invention discloses an oil-driven ducted aircraft. The oil-driven ducted aircraft comprises a ducted body with an encircling effect, a power system arranged in the ducted body and a control surface mechanism arranged in the ducted body; the duct body comprises an anti-twist blade and a duct; the power system is erected in the duct through a power frame, and the power frame is fixed to the upper portion of the duct; the power system comprises an output shaft, and the output shaft is connected with a ducted paddle mechanism used for providing lift force; and the control surface mechanism is positioned below the ducted propeller mechanism and is used for controlling the aircraft to steer. According to the oil-driven ducted aircraft, the ducted propeller mechanism and the control surface mechanism are both mounted in the ducted body, and the ducted propeller mechanism and the control surface mechanism can be well protected by the ducted body, so that the safety of the oil-driven ducted aircraft in flight is improved, and the service life of the oil-driven ducted aircraft in flight is prolonged; and the main mounting and fixing positions and the main force bearing parts of all the mechanisms are rigid main force bearing rings, and due to the design, the rigidity of a ducted surface material can be improved, so that the weight of the whole oil-driven ducted aircraft is reduced.

    本发明公开了一种油动涵道飞行器,包括具有环括作用的涵道体、设置在所述涵道内部的动力系统和设置在所述涵道内部的舵面机构;所述涵道体包括反扭叶片和涵道;所述动力系统通过动力架架设在涵道内部,所述动力架固定在涵道上方;所述动力系统包括输出轴,所述输出轴连接有用于提供升力的涵道桨机构;所述舵面机构位于所述涵道桨机构的下方,用于控制飞行器转向;本发明的涵道桨机构和舵面机构均安装在涵道体内部,涵道可以对上述两机构起到很好的保护作用,以提高油动涵道飞行器在飞行中的安全性和使用寿命;上述所有机构的主要安装固定位置和主要承力部位为刚性主承力环,此类设计可以涵道表面材料的刚性从而减轻整个油动涵道飞行器的重量。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Oil-driven ducted aircraft


    Weitere Titelangaben:

    一种油动涵道飞行器


    Beteiligte:
    LIN HAIYING (Autor:in) / CUI HANZHANG (Autor:in) / LI ZEYU (Autor:in) / WU JIANGHAO (Autor:in)

    Erscheinungsdatum :

    2022-01-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



    Ducted aircraft

    ZHANG LIHUI / WANG CHAOSONG | Europäisches Patentamt | 2021

    Freier Zugriff

    Ducted aircraft

    ZHEN PENGFEI / XU BIN / FAN WEI et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Ducted aircraft

    WANG BIN / ZHANG JIANFEI / WEN XIAOQING et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Ducted lifting body and ducted aircraft

    LIU ZHENCHEN / FU HAIYU / LI RUIBIN | Europäisches Patentamt | 2022

    Freier Zugriff

    Dish-shaped ducted aircraft driven by electromagnetic force

    CHEN JICHANG / ZOU WENYANG / LU ZHIWEI et al. | Europäisches Patentamt | 2023

    Freier Zugriff