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不可逆迈索森科往复式布雷顿循环的热力学分析

Thermodynamic Analysis of an Irreversible Maisotsenko Reciprocating Brayton Cycle.

作者信息

Zhu Fuli, Chen Lingen, Wang Wenhua

机构信息

Institute of Thermal Science and Power Engineering, Naval University of Engineering, Wuhan 430033, China.

Military Key Laboratory for Naval Ship Power Engineering, Naval University of Engineering, Wuhan 430033, China.

出版信息

Entropy (Basel). 2018 Mar 5;20(3):167. doi: 10.3390/e20030167.

DOI:10.3390/e20030167
PMID:33265258
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC7512683/
Abstract

An irreversible Maisotsenko reciprocating Brayton cycle (MRBC) model is established using the finite time thermodynamic (FTT) theory and taking the heat transfer loss (HTL), piston friction loss (PFL), and internal irreversible losses (IILs) into consideration in this paper. A calculation flowchart of the power output (P) and efficiency (η) of the cycle is provided, and the effects of the mass flow rate (MFR) of the injection of water to the cycle and some other design parameters on the performance of cycle are analyzed by detailed numerical examples. Furthermore, the superiority of irreversible MRBC is verified as the cycle and is compared with the traditional irreversible reciprocating Brayton cycle (RBC). The results can provide certain theoretical guiding significance for the optimal design of practical Maisotsenko reciprocating gas turbine plants.

摘要

本文运用有限时间热力学(FTT)理论,考虑传热损失(HTL)、活塞摩擦损失(PFL)和内部不可逆损失(IIL),建立了不可逆迈索森科往复布雷顿循环(MRBC)模型。给出了该循环功率输出(P)和效率(η)的计算流程图,并通过详细的数值算例分析了向循环中注水的质量流量(MFR)以及其他一些设计参数对循环性能的影响。此外,验证了不可逆MRBC循环的优越性,并将其与传统不可逆往复布雷顿循环(RBC)进行了比较。研究结果可为实际迈索森科往复式燃气轮机装置的优化设计提供一定的理论指导意义。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/1200e13c93b6/entropy-20-00167-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/4f0e15d12786/entropy-20-00167-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/1eef86ab1c69/entropy-20-00167-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/72742fff7aa7/entropy-20-00167-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/7c3c43a9db0a/entropy-20-00167-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/ac7478aabbc0/entropy-20-00167-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/c0fc795dae0b/entropy-20-00167-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/e8eafb23ea08/entropy-20-00167-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/4e91ea625f9a/entropy-20-00167-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/1200e13c93b6/entropy-20-00167-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/4f0e15d12786/entropy-20-00167-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/1eef86ab1c69/entropy-20-00167-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/72742fff7aa7/entropy-20-00167-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/7c3c43a9db0a/entropy-20-00167-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/ac7478aabbc0/entropy-20-00167-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/c0fc795dae0b/entropy-20-00167-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/e8eafb23ea08/entropy-20-00167-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/4e91ea625f9a/entropy-20-00167-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2237/7512683/1200e13c93b6/entropy-20-00167-g009.jpg

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本文引用的文献

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Finite-time thermodynamics: Engine performance improved by optimized piston motion.有限时间热力学:通过优化活塞运动提高发动机性能。
Proc Natl Acad Sci U S A. 1981 Apr;78(4):1986-8. doi: 10.1073/pnas.78.4.1986.
用于使熵产生最小化的带发热的椭圆圆柱体的构形设计。
Entropy (Basel). 2020 Jun 12;22(6):651. doi: 10.3390/e22060651.
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Optimal Power and Efficiency of Multi-Stage Endoreversible Quantum Carnot Heat Engine with Harmonic Oscillators at the Classical Limit.经典极限下含谐振子的多级内可逆量子卡诺热机的最优功率与效率
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Performance of Universal Reciprocating Heat-Engine Cycle with Variable Specific Heats Ratio of Working Fluid.工作流体比热比可变的通用往复式热机循环性能
Entropy (Basel). 2020 Mar 31;22(4):397. doi: 10.3390/e22040397.