The invention discloses a general aircraft linear motor traction take-off acceleration launching device, and relates to the application field of linear motors. A launching aircraft is towed by a linear motor to obtain a take-off speed; and a take-off air injection resistance baffle plate is mounted behind the aircraft for providing auxiliary thrust to the aircraft in boosting take-off and providing auxiliary brake force to the linear motor in braking. A ground energy is used for providing energy needed by the take-off phase of the aircraft for the aircraft; and the saved energy is used for prolonging the flight distance of the aircraft or replacing to effective load of the aircraft. The device uses a decentralizing method for changing the high-power linear motor with concentrated power to a group linear motor combined by multiple low-power linear motors to replace the high-power linear motor with concentrated power, so that the manufacturing difficulty of the launching device on such key parts as the linear motor, a current breaker and a direct current-alternating current frequency modulation inverter is reduced, and the system reliability is improved.


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    Titel :

    General aircraft linear motor traction take-off acceleration launching device


    Beteiligte:
    ZHAO YONG (Autor:in)

    Erscheinungsdatum :

    29.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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