This paper describes the design, construction and testing of a dual-output power converter concept where the large components, such as the DC link capacitor and heat-sink, are shared between two actuators which are used sequentially in the deployment of aircraft landing gear. This mutual component approach combines the advantages of dual-use power converters with the flexibility of one power converter per application. Practical results of the converter operating are presented for a range of test conditions in order to validate the simulation study.


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    Title :

    An Electromechanically Actuated Nose Landing Gear Using a Dual-Output Motor Control Unit


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Power Systems Conference ; 2010



    Publication date :

    2010-11-02




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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