The UACL JT15D-1 engine is a 2200 lb thrust turbofan engine of the high bypass ratio type, the first small engine of the type to be certified and placed in production. The engine is briefly described, and the scope of development testing and resources applied is reviewed. A selection of major development problems is covered, and future developments are indicated.


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    Titel :

    Development of the JT15D-1 Turbofan Engine


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Cook, D. L. (Autor:in)

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1972



    Erscheinungsdatum :

    1972-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Further Development of the JT15D Turbofan

    Cook, D. L. / Anschutz, R. H. | SAE Technical Papers | 1973


    “Quiet” Aspects of the Pratt & Whitney Aircraft JT15D Turbofan

    Plucinsky, J. C. | SAE Technical Papers | 1973


    Predicted and Observed Modal Radiation Patterns from JT15D Engine with Inlet Rods

    M.F. Heidmann / A.V. Saule / J.G. McArdle | AIAA | 1980



    Turbofan engine and aircraft comprising turbofan engine

    GARDES PASCAL / MENOU FABIEN / GOUGEON PASCAL et al. | Europäisches Patentamt | 2021

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