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Usin segmented compression exponent to calculate the exhaust temperature of the single stage high pressure ratio air ocmpressor

机译:使用分段压缩指数计算单级高压比空压机的排气温度

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Today,to claculate the terminal temeprature of compression of the single stage high pressure ratio compressor,the traditional method is using hte constant process exponent.This calculation mehtod creastes a lage error in the result compared with the measruemnts.To eliminate the error the author brings out a calculation method which separates the high compresison process into server segments.The new method segments the whole compression process of the cylinder into entropy increment porcess,isentropic process and entropy decrement process which are all have a low pressure ratio and it is suitable for engineering uses.By using different exponent of process,the calculation result is more closely to the real process.Based on this mehtod,the paper leads out the equations of the compression terminal temperature and the exhaust temperature of the high pressure ratio compressor with considerations of suction,discharge pressure loss,suction temeprature rise and discharge temperature drop.
机译:如今,为了解决单级高压比压缩机的压缩末端特性,传统方法是使用恒定过程指数。这种计算方法与测量方法相比会增加结果误差。为消除误差,作者消除了误差提出了一种将高压缩过程分为多个服务器段的计算方法。新方法将汽缸的整个压缩过程分为熵增量过程,等熵过程和熵递减过程,它们均具有较低的压力比,适合于工程设计。通过使用不同的过程指数,计算结果与实际过程更加接近。在此方法的基础上,本文提出了考虑吸力的高压比压缩机的压缩端温度和排气温度方程。 ,排气压力损失,吸油温度升高,排气温度下降。

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