Shell Aviation News n 254 Aug 1959 p 14-18. Technical considerations involved in determination of 250-hp engine design, developed by General Motors for small helicopters and light military aircraft; unique features are reviewed such as free turbine, selection of engine pressure ratio and turbine inlet temperature, engine air flow, matching of components, selection of compressor configuration, control system, and mechanical configuration. (see also abstract in SAE -- J v 67 n 7 July 1959 p 54-6)


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    Titel :

    Design approach to Allison model 250 engine


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Hall, R.S. (Autor:in)

    Kongress:

    SAE Meeting ; 1959 Allison



    Erscheinungsdatum :

    1959


    Format / Umfang :

    26 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    DESIGN APPROACH TO THE ALLISON MODEL 250 ENGINE

    HALL, R. S. | SAE Technical Papers | 1959


    ALLISON: AIRCRAFT ENGINE PIONEER

    Jensen, D. T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003


    The ALLISON AIRCRAFT-ENGINE DEVELOPMENT

    HAZEN, R. M. | SAE Technical Papers | 1941


    Evolution of the Allison Model 250 Engine

    Stevens, E. C. / Conn, F. E. | SAE Technical Papers | 1980