The invention relates to a wing integrated with distributed ducted fans. The wing integrated with the distributed ducted fans comprises the distributed ducted fans and a wing body, wherein the distributed ducted fans are integrated on an inner wing section of the wing body; the nacelles partially surround the distributed ducted fans; and the lift force balancing device is arranged at the outer side end part of the nacelle in the spanwise direction, the lift force balancing device comprises at least one wing panel, and the at least one wing panel generates the device lift force in the device spanwise length of the lift force balancing device in the spanwise direction.

    本发明涉及一种集成有分布式涵道风扇的机翼。该集成有分布式涵道风扇的机翼包括:分布式涵道风扇,分布式涵道风扇集成到机翼的内段翼上;短舱,短舱部分地包围分布式涵道风扇;以及升力均衡装置,升力均衡装置设在短舱在展向方向上的外侧端部处,其中升力均衡装置包括至少一个翼片,并且至少一个翼片在升力均衡装置在展向方向上的装置展向长度上产生装置升力。


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    Title :

    Wing integrated with distributed ducted fans


    Additional title:

    集成有分布式涵道风扇的机翼


    Contributors:
    XIE RUIXUAN (author) / CHEN ZHIYU (author) / DING LING (author) / WANG QIMIN (author) / JIN DING (author) / XU NANBO (author)

    Publication date :

    2024-04-12


    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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