Possibilities to further improve the third generation transport aircraft engines Rolls Royce RB 211, Pratt & Whitney JT 9D, and General Electric CF6/50, notably as regards losses in the thermodynamic cycle, are discussed. The following topics are dealt with: reduction of compressor losses; reduction of turbine losses; mixers and exchangers; and energy saving.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Amelioration of Various Components of a Subsonic Transport Aircraft Engine l'Amelioration des Differents Composants de l'Installation Motrice d'UN Avion Subsonique de Transport


    Contributors:
    J. Devriese (author)

    Publication date :

    1977


    Size :

    21 pages



    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Utilisation des Methodes de Calcul pour Optimiser l'Installation Motrice des Avions de Transport

    Monthus, X. / Colin, P. / Mogilka, P. et al. | British Library Conference Proceedings | 1993




    RESEAU DE DISTRIBUTION D'ENERGIE ELECTRIQUE D'UN VEHICULE DE TRANSPORT, TEL QU'UN AVION, AINSI QU'UNE INSTALLATION ELECTRIQUE D'UN AVION

    PERJU CATALIN / CUILLER CLAUDE / WAIDELICH KATHRYN et al. | European Patent Office | 2015

    Free access

    Amelioration des procedes de signalisation terre-avion

    Bourgues | Engineering Index Backfile | 1934