The invention discloses a composite jump takeoff system for a heavy gyroplane with jump takeoff capability. The tail end of an output shaft of an engine is connected with a tail vectored thrusting duct through a sliding friction clutch; a first helical bevel gear is placed on the output shaft of the engine; a second helical bevel gear is engaged with the first helical bevel gear; an output end of the second helical bevel gear is connected with a third helical cylindrical gear through an electromagnetic clutch; the third helical cylindrical gear in a first path of transmission is engaged with a fourth helical cylindrical gear; the fourth helical cylindrical gear is connected with a fifth helical cylindrical gear through a spline shaft; the fifth helical cylindrical gear is engaged with a sixth helical cylindrical gear; the sixth helical cylindrical gear is connected with a main rotor through a main rotor shaft; the third helical cylindrical gear in a second path of transmission is connected with a seventh helical cylindrical gear through a spline shaft; the seventh helical cylindrical gear is engaged with an eighth helical cylindrical gear; and the eighth helical cylindrical gear is connected with a flywheel through an overrunning clutch. Through the adoption of the composite jump takeoff system for the heavy gyroplane with the jump takeoff capability, disclosed by the invention, the jump takeoff of the gyroplane can be achieved.


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    Titel :

    Composite jump takeoff system for heavy gyroplane with jump takeoff capability


    Beteiligte:
    XU BIN (Autor:in) / XIANG CHANGLE (Autor:in) / YANG XINGBANG (Autor:in) / WANG YANG (Autor:in) / FAN WEI (Autor:in)

    Erscheinungsdatum :

    2015-10-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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