A hybrid electric aircraft equipped with gyrostable control is provided. In one aspect, a hybrid electric aircraft includes a turbine generator having a gas turbine engine and a generator operably coupled thereto to generate electrical power. The turbine generator defines an axis of rotation. The aircraft also includes one or more electrically driven thrusters for generating thrust to the aircraft. In addition, the aircraft includes a pivot mount operably coupled with the turbine generator. To provide gyroscopic stabilization control of an aircraft, a pivot mount is controlled to adjust an axis of rotation of a turbine generator relative to a primary stabilization axis of the aircraft. Additionally or alternatively, the rotational speed of the turbine generator may be varied to provide gyrostable control of the aircraft.

    提供了一种配备有陀螺稳定控制的混合电动飞行器。在一个方面,一种混合电动飞行器包括涡轮发电机,该涡轮发电机具有燃气涡轮发动机和可操作地联接到其以产生电力的发电机。涡轮发电机限定旋转轴线。该飞行器还包括一个或多个电驱动推进器,用于为飞行器产生推力。此外,飞行器包括与涡轮发电机可操作地联接的枢轴安装件。为了提供飞行器的陀螺稳定控制,控制枢轴安装件以相对于飞行器的主要稳定轴线调节涡轮发电机的旋转轴线。附加地或替代地,可以改变涡轮发电机的旋转速度以提供飞行器的陀螺稳定控制。


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    Title :

    Hybrid electric aircraft with gyrostable control


    Additional title:

    具有陀螺稳定控制的混合电动飞行器


    Contributors:

    Publication date :

    2023-01-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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