Several engine concepts examined to determine a preferred design which most effectively exploits the characteristics of hydrogen fuel in aircraft tanks received major emphasis. Many candidate designs of tank structure and cryogenic insulation systems were evaluated. Designs of all major elements of the aircraft fuel system including pumps, lines, valves, regulators, and heat exchangers received attention. Selected designs of boost pumps to be mounted in the LH2 tanks, and of a high pressure pump to be mounted on the engine were defined. A final design of LH2-fueled transport aircraft was established which incorporates a preferred design of fuel system. That aircraft was then compared with a conventionally fueled counterpart designed to equivalent technology standards.


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    Titel :

    Study of Fuel Systems for LH2-Fueled Subsonic Transport Aircraft, Volume 1


    Beteiligte:
    G. D. Brewer (Autor:in) / R. E. Morris (Autor:in) / G. W. Davis (Autor:in) / E. F. Versaw (Autor:in) / G. R. Cunnington (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    206 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Study of fuel systems for LH2-fueled subsonic transport aircraft, volume 2

    Brewer, G. D. / Morris, R. E. / Davis, G. W. et al. | NTRS | 1978


    Study of fuel systems for LH2-fueled subsonic transport aircraft, volume 1

    Brewer, G. D. / Morris, R. E. / Davis, G. W. et al. | NTRS | 1978


    Study of Fuel Systems for LH2-Fueled Subsonic Transport Aircraft, Volume 2

    G. D. Brewer / R. E. Morris / G. W. Davis et al. | NTIS | 1978


    Study of LH2 fueled subsonic passenger transport aircraft

    Brewer, G. D. / Morris, R. E. | NTRS | 1976


    Study of LH2 Fueled Subsonic Passenger Transport Aircraft

    G. D. Brewer / R. E. Morris | NTIS | 1976