Design objectives and features of advanced turbofan engine on order for Lockheed 1011 three-engined transport aircraft; engine is also offered for 200-seat twin engine transports; specification and performance data; arrangement of engine is as follows -- single stage front fan, without inlet guide vanes, is driven from three-stage low-pressure turbine, system being mechanically independent of gas generator; gas generator consists of seven stage intermediate pressure (i.p.) compressor driven by single stage uncooled i.p. turbine, and six stage h-p compressor driven by single stage air cooled h-p turbine; combustion chamber is annular; installation details, engine test program and component testing; combustion and engine control system; maintainability aspects. (See also Aircraft Eng v 40 n 4 Apr 1968 p 22-4, 26)


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    Titel :

    Rolls-Royce RB.211 three shaft turbofan


    Weitere Titelangaben:

    Flight


    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Rolls-Royce three shaft turbofan engine

    Wilde, G.L. / Pickerell, D.J. | Engineering Index Backfile | 1968


    The Rolls-Royce Three Shaft Turbofan Engine

    Wilde, G.L. / Pickerell, D.J. | Emerald Group Publishing | 1968



    Rolls-Royce RB.211 three shaft turbofan

    Engineering Index Backfile | 1968


    The Rolls-Royce RB.211 Three Shaft Turbofan

    Emerald Group Publishing | 1968