THE CF6 engine is a dual rotor, high bypass ratio turbofan engine designed for airline operation. It incorporates a variable stator, high pressure ratio compressor, an annular combustor, an air-cooled core engine turbine and a co-axial front fan driven by a five-stage low pressure turbine (Fig. 1). The core engine has an exhaust thrust spoiler which operates in conjunction with the fan cascade reverser during landing roll.


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    Titel :

    Potential Technology Improvements for the CF6 Turbofan


    Untertitel :

    The status of the CF6 development programme and its potential growth as described in a Society of Automotive Engineers paper presented at Los Angeles in October 1968


    Beteiligte:
    Payzer, R.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.02.1969


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Potential technology improvements for CF6 turbofan

    Payzer, R.J. | Engineering Index Backfile | 1968


    POTENTIAL TECHNOLOGY IMPROVEMENTS FOR THE CF6 TURBOFAN

    PAYZER, R. J. | SAE Technical Papers | 1968