The invention relates to the improvement on a clutch control circuit of original invention, and is capable of avoiding a phenomenon that a clutch is out of control; a 'slow engaging-rapid engaging' two-sectional joint way of the clutch is achieved, the impact degree and the sliding-friction work of the clutch in an engaging process are relieved, and the service life of the equipment is prolonged; engine speed is kept stable by virtue of the clutch in the engaging process and a phenomenon of engine shaft damage or flaming-out of an engine is avoided, and therefore the overall performance of an automatic helicopter rotor clutch control system as specified within patent 2010102193000 is enhanced.


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    Titel :

    Improved design of automatic helicopter rotor clutch control system


    Beteiligte:
    MENG ZHIJUN (Autor:in) / ZHOU YAOMING (Autor:in) / WANG CAN (Autor:in) / DOU SHU NAN (Autor:in) / WANG YONGCHAO (Autor:in)

    Erscheinungsdatum :

    2015-07-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



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