The invention relates to a bypass power device and an aircraft. A rotor wing is arranged in a bypass which is divided into an intake section and an exhaust section, a length adjusting mechanism is used for adjusting the length of the bypass and enabling the specific value of the intake section and the exhaust section to change. By the arrangement of the length adjusting mechanism, the length of the bypass can be adjusted in the axial direction, the specific value of the intake section and the exhaust section can be changed, and the location of the rotor wing in the axial direction of the bypass can be assuredly optimized. The bypass power device is adopted to the aircraft.


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    Titel :

    Bypass power device and aircraft


    Beteiligte:
    HE CHUNWANG (Autor:in)

    Erscheinungsdatum :

    24.06.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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