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.


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    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




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