This paper examines why large aircraft engines are started the way they are today, and why that may all change in the not too distant future.Electric starting of aircraft engines and Auxiliary Power Units (APU) has been limited to 28 VDC battery systems, with starting power typically under 10 kW. Above this power level the very high battery currents, and resulting voltage drops, make the approach less and less practical.Large engines for commercial transports may require more than 100 kW to start so low voltage battery starting will not be an option.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Electric Starting of Large Aircraft Engines


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    World Aviation Congress & Exposition ; 2002



    Erscheinungsdatum :

    05.11.2002




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Electric Starting of Large Aircraft Engines

    Taylor, C. M. / Society of Automotive Engineers of New York | British Library Conference Proceedings | 2002


    Starting systems for large aircraft engines

    Burgoine, A.C. | Engineering Index Backfile | 1923


    Starting of aircraft engines

    Gosslau, F. | Engineering Index Backfile | 1928


    Starting of Aircraft Gas Turbine Engines

    M. A. Alabin / B. M. Kats / Y. A. Litvinov | NTIS | 1972


    ELECTRICAL SYSTEM WITH DOUBLE SECONDARY ELECTRIC MAINS FOR STARTING AIRCRAFT ENGINES

    MARIOTTO DAMIEN / JAMOT MICHEL / LOGEAIS JEAN-FRANCOIS | Europäisches Patentamt | 2019

    Freier Zugriff