This report documents the results of Phase I, Study, of this five phase program. The objectives of this program are to develop an FTEPS design for an ATF aircraft and to design and fabricate a low cost FTEPS demonstrator with an integrated load simulator. The primary purpose of the program is to develop an electrical power generation and distribution system that can supply electrical power to the various critical systems on the aircraft with a reliability and power quality level commensurate with the requirements of the loads. In Phase I, the electrical loads and their power requirements were defined for the ATF baseline aircraft model. The loads were also located in the baseline aircraft model.


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    Title :

    Fault Tolerant Electrical Power System. Phase I. Study


    Contributors:
    M. W. Dige (author) / P. J. Leong (author) / D. L. Sommer (author)

    Publication date :

    1986


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Fault-Tolerant Electrical Power System

    Mehdi, Ishaque S. / Weimer, Joseph A. | SAE Technical Papers | 1987


    Fault-tolerant electrical power system

    Mehdi, I.S. / Weimer, J.A. | Tema Archive | 1987



    Designing a fault tolerant electrical power system (FTEPS)

    Dige, M.W. / Leong, P.J. / Sommer, D.L. | Tema Archive | 1987


    Application of a Fault Tolerant Electrical Power System

    Sommer, David L. / Maldonado, Miguel A. | SAE Technical Papers | 1990