The two newest internal combustion engine technologies which have demonstrated the most promise in the last 25 years are the direct-injection stratified-charge (DISC) rotary engine [1] and the adiabatic diesel engine [2]. The (DISC) engine is particularly attractive for aviation applications [3] because of its light weight, multi-fuel capability and potential for low fuel consumption. However, one disadvantage with the DISC engine is the weight and size of the liquid cooling system. NASA Lewis Research Center has supported a technology enablement program to advance the DISC rotary engine for general aviation applications and recognizes the importance of improvement in fuel consumption and reductions in the coolant system weight [4].


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    Titel :

    Analysis and Test of Insulated Components for Rotary Engine


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Doup, Douglas (Autor:in) / Badgley, Patrick R. (Autor:in) / Kamo, Roy (Autor:in)

    Kongress:

    SAE International Congress and Exposition ; 1989



    Erscheinungsdatum :

    1989-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Analysis and test of insulated components for rotary engine

    Badgley, P.R. / Doup, D. / Kamo, R. | Tema Archiv | 1989


    Analysis and test of insulated components for rotary engines

    Badgley,P.R. / Doup,D. / Kamo,R. et al. | Kraftfahrwesen | 1989


    Designing ceramic insulated components for the adiabatic engine

    Woods, M.E. / Mandler, W.F. / Scofield, T.L. | Tema Archiv | 1985


    Heat Insulated Turbocompound Engine

    Toyama, Kosuke / Shimauchi, Tomoki / Nishiyama, Toshihiko et al. | SAE Technical Papers | 1983


    Heat insulated turbocompound engine

    Toyama,K. / Yoshimitsu,T. / Nishiyama,T. et al. | Kraftfahrwesen | 1983