A brief summary of previous significant aircraft diesel engine development and application is presented along with a comparison with the then contemporary state-of-the-art aircraft gasoline engine. Performance results for an Advanced Variable Cycle Diesel (AVCD) engine obtained from a computer simulator code are presented and comparisons made with an identical fixed cycle engine. Some operational benefits of an AVCD engine are discussed along with an alternate method of controlling the engine's turbocompressor. Finally, a description of a 750 SHP AVCD aircraft engine suitable for use on a medium size subsonic business transport plane and its projected performance is presented.


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    Titel :

    The Variable Cycle Diesel as an Aircraft Engine, Part 2


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aerospace Atlantic Conference & Exposition ; 1990



    Erscheinungsdatum :

    1990-04-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Variable Cycle Diesel as an Aircraft Engine, Part 1

    Johnston, Richard P. | SAE Technical Papers | 1989


    The variable cycle diesel as an aircraft engine

    Johnston, R.P. | Tema Archiv | 1989


    The variable cycle diesel as an aircraft engine

    Johnston, R.P. | Tema Archiv | 1990


    Two-cycle diesel aircraft engine development in France

    Wilkinson, P.H. | Engineering Index Backfile | 1939


    A variable cycle jet engine for ASTOVL aircraft

    Wood, A. / Pilidis, P. | British Library Online Contents | 1997