The invention relates to a tilt rotor propulsion system for an aircraft. A method for operating a propulsion system of an aircraft includes moving a plurality of forward propellers and aft propellers to a vertical thrust position. When in the vertical thrust position, the method further includes providing a first fore-aft electrical power ratio to the plurality of fore and aft propellers. The method further includes moving the plurality of forward thrusters and aft thrusters to a forward thrust position. When in the forward thrust position, the method further includes providing a second forward-to-aft electrical power ratio to the plurality of forward propellers and aft propellers. The first fore-aft electrical power ratio is different from the second fore-aft electrical power ratio to provide certain efficiency for the aircraft.

    本申请涉及用于飞行器的倾转旋翼推进系统。一种用于操作飞行器的推进系统的方法包括将多个前推进器和后推进器移动到垂直推力位置。当处于垂直推力位置时,该方法还包括向多个前推进器和后推进器提供第一前后电功率比率。该方法还包括将多个前推进器和后推进器移动到向前推力位置。当处于向前推力位置时,该方法还包括向多个前推进器和后推进器提供第二前后电功率比率。第一前后电功率比率不同于第二前后电功率比率以为飞行器提供一定的效率。


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    Title :

    Tilt rotor propulsion system for aircraft


    Additional title:

    用于飞行器的倾转旋翼推进系统



    Publication date :

    2022-11-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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