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首页> 外文期刊>Russian Aeronautics >Influence of Input Momentum and Losses in the Turbine on the Efficiency of a Turbofan Engine with Periodic Fuel Combustion
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Influence of Input Momentum and Losses in the Turbine on the Efficiency of a Turbofan Engine with Periodic Fuel Combustion

机译:涡轮中输入动量和损失对周期性燃油燃烧的涡扇发动机效率的影响

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摘要

It is shown that research carried out by leading aeroengine manufactures on the use of the thermodynamically high-efficient GTE cycle with the periodic fuel combustion is very urgent. The investigation results are presented and it is disclosed that the advantages of this cycle effectiveness are particularly evident in flight conditions. Owing to a high degree of gas heating, the influence of input momentum and the expansion process efficiency on the economical engine operation is reduced.
机译:结果表明,由领先的航空发动机制造商进行的有关使用热力学高效GTE循环以及周期性燃料燃烧的研究非常紧迫。提出了调查结果,并公开了这种循环有效性的优点在飞行条件下特别明显。由于气体加热程度高,因此减少了输入动量和膨胀过程效率对发动机经济运行的影响。

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