The demand of More Electric Engine/ Aircraft (MEE/ MEA) increases with the need of on-board electrification system for future aircraft. Also, moving towards More Electric Engine/Aircraft (MEE/MEA) concept can achieve better fuel benefit in the engine by controlling the split ratio of the power off-take from each of Low Pressure (LP) and High Pressure (HP) spools. Due to the trend of MEA and MEE integration with the power electronic driven technology, a higher reliability level of electrical power system is required to meet the minimum safety requirement during fault condition. A concept of intelligent system for mitigating the faults by identifying the best fault tolerant system configuration with the minimum load shedding is proposed in this paper. The proposed method not only mitigates the fault elimination from the electrical system but also maintains continuous mechanical power output from LP and HP spools in order to maintain optimum fuel benefit of the engine.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Fault Tolerant More Electric Engine/Aircraft Architecture with Integrated Condition-Based Control


    Contributors:


    Publication date :

    2018-11-01


    Size :

    776234 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Fault-tolerant Control for the More Electric Engine

    Oyori, H. / Morioka, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012


    Fault-tolerant control for the More Electric Engine

    Oyori, Hitoshi / Morioka, Noriko | AIAA | 2012


    FAULT-TOLERANT POWER SYSTEM ARCHITECTURE FOR AIRCRAFT ELECTRIC PROPULSION

    SOLODOVNIK EUGENE V / LACAUX FREDERIC / KARIMI KAMIAR J | European Patent Office | 2021

    Free access


    FAULT-TOLERANT POWER SYSTEM ARCHITECTURE FOR AIRCRAFT ELECTRIC PROPULSION

    EUGENE V SOLODOVNIK / FREDERIC LACAUX / KAMIAR J KARIMI | European Patent Office | 2021

    Free access