The general situation of the development of aircraft braking system are introduced, aiming at the shortcomings of traditional hydraulic braking system, a kind of suitable for civil aircraft electric brake system is designed, using electromechanical actuator to replace the traditional hydraulic pressure mechanism, and through MATLAB simulation and inertia test, verify the electrical brake system simplifies the system composition, reduce the weight of the system, the system performance, safety testing and maintenance, etc. compared with the existing brake system has made great progress.


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    Titel :

    Study on electric brake system of civil aircraft


    Beteiligte:
    Liu, Jinsong (Autor:in) / Yang, Jinri (Autor:in) / Xiao, Yang (Autor:in)


    Erscheinungsdatum :

    01.10.2016


    Format / Umfang :

    509409 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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