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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fault Tolerant Electrical Power System. Phase I. Study


    Beteiligte:
    M. W. Dige (Autor:in) / P. J. Leong (Autor:in) / D. L. Sommer (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    52 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Fault-tolerant electrical power system

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


    Fault-Tolerant Electrical Power System

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



    Designing a fault tolerant electrical power system (FTEPS)

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


    Application of a Fault Tolerant Electrical Power System

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