This paper briefly reviews the basic design concepts of the RB.211-22 high by-pass turbofan engine. It summarises the facilities available for developing the engine. It concludes with a status report of the engine development programme, including comments on the fan blade, combustion development and smoke levels, the H.P. turbine blade, oil sealing, structural rig testing, the three-shaft configuration, modular build, borescope inspection, achieved performance and noise levels.


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    Titel :

    Development of the Rolls-Royce RB.211 turbofan for airline operation


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Keen, J.M.S. (Autor:in)

    Kongress:

    National Air Transportation Meeting ; 1970



    Erscheinungsdatum :

    01.02.1970




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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