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一类复杂燃气轮机循环的热力学研究
引用本文:昌放辉,陈贤冲,徐水来. 一类复杂燃气轮机循环的热力学研究[J]. 装备制造技术, 2012, 0(6): 28-31
作者姓名:昌放辉  陈贤冲  徐水来
作者单位:1. 海军湛江地区装备修理监修室,广东湛江,524005
2. 海军92337部队,辽宁大连,116031
3. 海军92335部队,福建宁德,352103
摘    要:对一类复杂的燃气轮机循环进行了热力学分析和研究,导出了循环输出功、热效率、熵产和火用效率的解析式;通过数值算例,分别讨论了各个性能目标与中冷压比和总压比的关系,并对中冷压比进行了优化;分析了回热度、循环温比、压气机和涡轮机内效率、中间冷却终点温度等循环参数,对性能目标的影响,所得结果对实际燃气轮机装置的参数选择和优化设计具有一定的参考作用。

关 键 词:燃气轮机循环  热力学第一定律  热力学第二定律  数值算例

Thermodynamics Research a Kind of Complex Gas Turbine Cycle
CHANG Fang-hui , CHEN Xian-chong , XU Shui-lai. Thermodynamics Research a Kind of Complex Gas Turbine Cycle[J]. , 2012, 0(6): 28-31
Authors:CHANG Fang-hui    CHEN Xian-chong    XU Shui-lai
Affiliation:1.Equipment Mend Supervision in Zhanjiang Station,Navy,Zhanjiang Guangdong 524005,China;2.92337 Troops,Navy,Dalian Liaoning 116031,China;3.92335 Troops,Navy,Ningde Fujian 352103,China)
Abstract:Thermodynamics analyses and investigation have been performed for a kind of complex gas turbine cycle.Analytical formulae of the cycle work,thermal efficiency,entropy generation and exergy efficiency are derived.The relations of the performance objectives versus intercooling pressure ratio and total pressure ratio are discussed by numerical examples,and the intercooling pressure ratio is optimized.The effects of cycle parameters(such as degree of regeneration,cycle temperature ratio,efficiencies of compressors and turbine,terminal temperature of intercooling process and so on) on the performance objectives are analyzed.The results obtained in this paper may provide some guidelines for the parameter selection and optimal design of practical gas turbine plant.
Keywords:gas turbine cycle  the first law of thermodynamics  the second law of thermodynamics  numerical examples
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