Retractable propulsor assemblies for aircraft are described that generate lift during vertical take-off, hover, and vertical landing. The retractable propulsor assemblies are deployed from a compartment in a fuselage of the aircraft to transition the aircraft into vertical flight, and are stowed in the compartment during cruise flight to reduce aerodynamic drag on the aircraft. One embodiment comprises a method of operating a VTOL aircraft. The method comprises deploying the retractable propulsor assembly from the compartment of the fuselage to provide the lift for vertical flight. The methodfurther comprises transitioning the VTOL aircraft from the vertical flight to cruise flight, and stowing the retractable propulsor assembly in the compartment during the cruise flight to reduce the aerodynamic drag on the VTOL aircraft.

    描述了用于飞机的可伸缩推进器组件,其在垂直起飞、悬停和垂直降落期间产生升力。可伸缩推进器组件从飞机机身的隔室中展开以将飞机转换为垂直飞行,并且在巡航飞行期间被收起在隔室中以减少飞机上的空气动力阻力。一个实施例包括一种操作VTOL飞机的方法。该方法包括从机身的隔室展开可伸缩推进器组件以提供用于垂直飞行的升力。该方法还包括使VTOL飞机从垂直飞行转换到巡航飞行,以及在巡航飞行期间将可伸缩推进器组件收起在所述隔室中以减少VTOL飞机上的空气动力阻力。


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    Titel :

    RETRACTABLE PROPULSOR ASSEMBLIES FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT


    Weitere Titelangaben:

    垂直起降(VTOL)飞机的可伸缩式推进器组件


    Beteiligte:
    CORNES OLIVIER (Autor:in)

    Erscheinungsdatum :

    02.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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