Power and efficiency optimizations for an open cycle two-shaft gas turbine power plant

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE
Lingen Chen, Huijun Feng, Yanlin Ge, Shuangshuang Shi
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Abstract

In finite-time thermodynamic analyses for various gas turbine cycles, there are two common models: one is closed-cycle model with thermal conductance optimization of heat exchangers, and another is open-cycle model with optimization of pressure drop (PD) distributions. Both of optimization also with searching optimal compressor pressure ratio (PR). This paper focuses on an open-cycle model. A two-shaft open-cycle gas turbine power plant (OCGTPP) is modeled in this paper. Expressions of power output (PP) and thermal conversion efficiency (TCE) are deduced, and these performances are optimized by varying the relative PD and compressor PR. The results show that there exist the optimal values (0.32 and 14.0) of PD and PR which lead to double maximum dimensionless PP (1.75). There also exists an optimal value (0.38) of area allocation ratio which leads to maximum TCE (0.37). Moreover, the performances of three types of gas turbine cycles, such as one-shaft and two-shaft ones, are compared. When the relative pressure drop at the compressor inlet is small, the TCE of third cycle is the biggest one; when this pressure drop is large, the PP of second cycle is the biggest one. The results herein can be applied to guide the preliminary designs of OCGTPPs.

开式循环双轴燃气轮机电厂功率与效率优化
在各种燃气轮机循环的有限时间热力学分析中,常用的模型有两种:一种是采用换热器导热系数优化的闭循环模型,另一种是采用压降分布优化的开循环模型。这两种优化方法还包括寻找最优压缩机压比(PR)。本文主要研究一个开循环模型。本文对双轴开式循环燃气轮机电站进行了建模。推导了功率输出(PP)和热转换效率(TCE)的表达式,并通过改变相对PD和压缩机PR来优化这些性能。结果表明,PD和PR存在最优值(0.32和14.0),从而导致无量纲PP的两倍最大值(1.75)。面积分配比也存在最优值(0.38),导致TCE最大值(0.37)。并对单轴和双轴三种燃气轮机循环的性能进行了比较。当压缩机进口相对压降较小时,第三循环的TCE最大;当压降较大时,第二循环的PP最大。本文的研究结果可用于指导OCGTPPs的初步设计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
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