A new generation of transport aircraft will be powered by efficient, advanced turboprop propulsion systems. Systems that develop 5,000 to 15,000 horsepower have been studied. Reduction gearing for these advanced propulsion systems is discussed. Allison Gas Turbine Division's experience with the 5,000 horsepower reduction gearing for the T56 engine is reviewed and the impact of that experience on advanced gear systems is considered. The reliability needs for component design and development are also considered. Allison's experience and their research serve as a basis on which to characterize future gear systems that emphasize low cost and high reliability.


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    Titel :

    Gear Systems for Advanced Turboprops


    Beteiligte:
    D. A. Wagner (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Gear systems for advanced turboprops

    Wagner, D.A. | Tema Archiv | 1987


    Tensile buckling of advanced turboprops

    CHAMIS, C. C. / AIELLO, R. A. | AIAA | 1983


    Parametric studies of advanced turboprops

    FERTIS, D. G. / AIELLO, R. A. / CHAMIS, C. C. et al. | AIAA | 1990


    Parametric studies of advanced turboprops

    FERTIS, D. / AIELLO, R. / CHAMIS, C. | AIAA | 1988


    Tensile buckling of advanced turboprops

    Chamis, C. C. / Aiello, R. A. | NTRS | 1983