The design of an aircraft engine capable of developing 186 kW shaft power at a 7620 m altitude is described. The 186 kW design takes into account expected new developments in aircraft designs resulting in a reassessment of the power requirements at the cruise mode operation. Based on the results of this analysis a three phase technology development program is projected resulting in production dates of 1985, 1992, and 2000.


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    Titel :

    Design study: A 186 kW lightweight diesel aircraft engine


    Beteiligte:

    Erscheinungsdatum :

    01.04.1980


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Lightweight, low compression aircraft diesel engine

    Gaynor, T. L. / Bottrell, M. S. / Eagle, C. D. et al. | NTRS | 1977



    Lightweight, Low Compression Aircraft Diesel Engine

    T. L. Gaynor / M. S. Bottrell / C. D. Eagle et al. | NTIS | 1977