The introduction of a new product in the aeronautical sector implies conducting characterization tests in an automated, safe and sustainable way. This paper describes a dedicated test bench design and validation that allows characterizing a swashplate Helicopter Electro Mechanical Actuation System (HEMAS). The test bench replicates the operating conditions that the actuator will encounter in service simulating the aerodynamic force by a hydraulic counter load system. The results obtained in validation tests show the ability of the test bench to replicate specified test cases. The validation was performed using a hydraulic cylinder to replicate the motion profile that will be followed by the actuator. The test campaign with the actuator will be performed during 2015.


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    Titel :

    Test bench for helicopter electro mechanical actuation system validation: Design and validation of dedicated test bench for aeronautical electromechanical actuators


    Beteiligte:
    Echevarria, Imanol (Autor:in) / Lasa, Joseba (Autor:in) / Casado, Pablo (Autor:in) / Dominguez, Alberto (Autor:in) / Eguizabal, Inigo (Autor:in) / Lizeaga, Mikel (Autor:in) / Perez, Raul (Autor:in) / Berenguer, Oscar (Autor:in)


    Erscheinungsdatum :

    01.03.2015


    Format / Umfang :

    2134077 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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