The impact on a commercial transport aircraft of using fuels which have relaxed property limits relative to current commercial jet fuel was assessed. The methodology of the study is outlined, fuel properties are discussed, and the effect of the relaxation of fuel properties analyzed. Advanced fuel system component designs that permit the satisfactory use of fuel with the candidate relaxed properties in the subject aircraft are described. The two fuel properties considered in detail are freezing point and thermal stability. Three candidate fuel system concepts were selected and evaluated in terms of performance, cost, weight, safety, and maintainability. A fuel system that incorporates insulation and electrical heating elements on fuel tank lower surfaces was found to be most cost effective for the long term.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Study of advanced fuel system concepts for commercial aircraft and engines


    Beteiligte:
    Versaw, E. F. (Autor:in) / Brewer, G. D. (Autor:in) / Byers, W. D. (Autor:in) / Fogg, H. W. (Autor:in) / Hanks, D. E. (Autor:in) / Chirivella, J. (Autor:in)

    Erscheinungsdatum :

    01.01.1983


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Commercial aircraft engines

    Dickinson, H.C. | Engineering Index Backfile | 1929


    Engines for Commercial Aircraft

    Emerald Group Publishing | 1987


    Studies of advanced fuel injection concepts for diesel engines

    Beck,N.J. / Hom,K. / Maxson,J.A. et al. | Kraftfahrwesen | 1989


    Gasoline requirements of commercial aircraft engines

    Cummings, H.K. | Engineering Index Backfile | 1930