The paper presents the results of compliance assessment of the values of reliability and fault tolerance of the helicopter's electric traction based on the project requirements. As a comprehensive parameter for the assessment of fault tolerance of the components with a number of degradation states, it is proposed to use the parameter degree of fault tolerance. On the basis of such a criterion the transition probabilities for the Multi-State System reliability Markov Models have been computed. The simulation and assessment results allow a conclusion about the feasibility of the traction drive topology and its compliance with the design requirements on the reliability and the future operational conditions of electrical helicopters.


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    Titel :

    Fault tolerant traction drive of electrical helicopter with battery electric energy storage


    Beteiligte:


    Erscheinungsdatum :

    01.06.2017


    Format / Umfang :

    500132 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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