Optimization study showed that medium pressure ratio turbojet would be best compromise for transatlantic Mach 2.2 civil aircraft; BAC is responsible for intake and nacelle installation, Bristol Siddeley is designing and developing Olympus 593 engine, and SNECMA is responsible for jet pipe, reheat system, primary and secondary nozzles, silencer and thrust reverser; power plants are disposed in 2 twin underwing nacelles positioned outboard of main undercarriage at mid-semi span; arrangements bring intake into region where it is sheltered under wing, which acts as flow-straightener and minimizes effect on intake performance of variation in angle of attack; intake control and engine control system.


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    Titel :

    Concorde powerplant


    Weitere Titelangaben:

    Flight


    Erschienen in:

    Flight ; 84 , n 2854


    Erscheinungsdatum :

    1963


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Concorde A.I.D.S. Powerplant Applications

    WHEELER, P.J. / ESSEX, N.J. | Emerald Group Publishing | 1978


    Concorde AIDS - Powerplant Applications

    Essex, N. J. / Wheeler, P. J. | SAE Technical Papers | 1977


    Concorde AIDS - powerplant application

    Wheeler, P.J. / Esser, N.J. | Tema Archiv | 1977


    Olympus 593 Powerplant in Concorde

    Calder, P.H. | SAE Technical Papers | 1971


    The Olympus 593 Powerplant for Concorde

    John, Derek J. | Emerald Group Publishing | 1967