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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    Title :

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


    Contributors:


    Publication date :

    2017-06-01


    Size :

    500132 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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