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.


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    Title :

    Utilization of Exhaust Gas of Aircraft Engines


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Pre-1964 SAE Technical Papers ; 1906



    Publication date :

    1946-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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