A ducted wing is configured to be connected to an aircraft. The ducted wing includes an integrated array of jet wings. Each jet wing includes a propeller fan, an upper wing portion, and a lower wing portion extending beyond an end of the upper wing portion. Each jet wing includes a duct formed between the upper wing portion and the lower wing portion, with a propeller located within the duct. Further, each jet wing may have one or more flaps at a leading edge or a trailing edge of the jet wing. The jet wing may have a flap that controls an inlet area or an outlet area of the propeller fan and a flap that controls whether the aircraft is operable in one of a plurality of different takeoff modes.

    一种管道式机翼被构造成连接到飞行器。该管道式机翼包括集成喷气翼阵列。每个喷气翼包括推进器风扇、上翼部分和延伸超过该上翼部分的端部的下翼部分。每个喷气翼包括形成在该上翼部分和该下翼部分之间的管道,其中推进器位于该管道内。此外,每个喷气翼可在该喷气翼的前缘处或后缘处具有一个或多个襟翼。该喷气翼可具有控制该推进器风扇的入口面积或出口面积的襟翼以及控制该飞行器是否可在多个不同起飞模式中的一个起飞模式中操作的襟翼。


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    Titel :

    Tubular wing with flap


    Weitere Titelangaben:

    具有襟翼的管道式机翼


    Beteiligte:
    MOORE MICHAEL DAVID (Autor:in) / VILLAR IVAN A (Autor:in) / JEDANSKY DANIEL (Autor:in) / HAHN ALEXANDER S (Autor:in) / FEI XIAOFAN (Autor:in) / PERRY AARON THOMAS (Autor:in)

    Erscheinungsdatum :

    11.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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