THIS paper-relates to the recovery of energy from the exhaust gas of aircraft reciprocating engines by means of the exhaust jet, the steady-flow turbine, and the blowdown turbine.The performance of a reciprocating engine compounded with these energy-recovery devices is discussed in detail.The operating conditions for maximum performance are presented, and the effects of engine cooling and knock limit on these conditions are considered.A comparison is made of the overall weight of the engine plus fuel for the various exhaust energy-recovery systems at several operating conditions and durations.THIS paper-relates to the recovery of energy from the exhaust gas of aircraft reciprocating engines by means of the exhaust jet, the steady-flow turbine, and the blowdown turbine.The performance of a reciprocating engine compounded with these energy-recovery devices is discussed in detail.The operating conditions for maximum performance are presented, and the effects of engine cooling and knock limit on these conditions are considered.A comparison is made of the overall weight of the engine plus fuel for the various exhaust energy-recovery systems at several operating conditions and durations.THIS paper-relates to the recovery of energy from the exhaust gas of aircraft reciprocating engines by means of the exhaust jet, the steady-flow turbine, and the blowdown turbine.The performance of a reciprocating engine compounded with these energy-recovery devices is discussed in detail.The operating conditions for maximum performance are presented, and the effects of engine cooling and knock limit on these conditions are considered.A comparison is made of the overall weight of the engine plus fuel for the various exhaust energy-recovery systems at several operating conditions and durations.THIS paper-relates to the recovery of energy from the exhaust gas of aircraft reciprocating engines by means of the exhaust jet, the steady-flow turbine, and the blowdown turbine.The performance of a reciprocating engine compounded with these energy-recovery devices is discussed in detail.The operating conditions for maximum performance are presented, and the effects of engine cooling and knock limit on these conditions are considered.A comparison is made of the overall weight of the engine plus fuel for the various exhaust energy-recovery systems at several operating conditions and durations.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Utilization of Exhaust Gas of Aircraft Engines


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1946




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    NACA Study of the Utilization of Exhaust Gas of Aircraft Engines

    PINKEL, BENJAMIN | SAE Technical Papers | 1946


    EXHAUST-VALVES AND GUIDES FOR AIRCRAFT ENGINES

    HERON, S D | SAE Technical Papers | 1924


    Exhaust emissions reduction for intermittent combustion aircraft engines

    Rezy, B. J. / Stuckas, K. J. / Tucker, J. R. et al. | NTRS | 1982


    Exhaust Emissions Reduction for Intermittent Combustion Aircraft Engines

    B. J. Rezy / K. J. Stuckas / J. R. Tucker et al. | NTIS | 1982