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波转子对小型燃气涡轮发动机性能的影响
引用本文:成本林,李建中,温 泉,等.波转子对小型燃气涡轮发动机性能的影响[J].南京航空航天大学学报,2012,44(4):431-437.
作者姓名:成本林  李建中  温 泉  
作者单位:1. 南京航空航天大学能源与动力学院,南京,210016;中航工业航空动力机械研究所,株洲,421002
2. 中航工业航空动力机械研究所,株洲,421002
3. 南京航空航天大学能源与动力学院,南京,210016
基金项目:高等学校博士学科点专项科研基金,中央高校基本科研业务费专项
摘    要:波转子是一种自冷却动压交换设备,具有提高各种发动机和机械的性能与运行特性的特有优势。本文建立基于波转子技术的小型燃气涡轮发动机热力循环分析模型。研究了压气机、涡轮压比、燃烧工作条件变化等5种热力循环方案情况下波转子技术对小型燃气涡轮发动机性能的影响。探讨波转子嵌入燃气涡轮发动机后导致燃烧室工作环境的变化规律。在相同压气机压比、相同涡轮进口温度热力循环方案情况下,波转子技术提高燃气涡轮发动机性能最高,获得了基于波转子技术小型燃气涡轮发动机最佳性能优化区和燃烧室工作环境变化规律。

关 键 词:小型燃气涡轮发动机  波转子  热力循环  性能

Impact of Wave Rotor on Performance of Small Gas Turbine Engine
Cheng Benlin , Li Jianzhong , Wen Quan , Gong Erlei , Zhang Kunyuan.Impact of Wave Rotor on Performance of Small Gas Turbine Engine[J].Journal of Nanjing University of Aeronautics & Astronautics,2012,44(4):431-437.
Authors:Cheng Benlin  Li Jianzhong  Wen Quan  Gong Erlei  Zhang Kunyuan
Institution:Cheng Benlin1,2,Li Jianzhong1,2,Wen Quan2,Gong Erlei1,Zhang Kunyuan1(1.College of Energy and Power Engineering,Nanjing University of Aeronautics &Astronautics,Nanjing,210016,China;2.China Aviation Powerplant Research Institute,Zhuzhou,421002,China)
Abstract:The wave rotor is a self-cooled dynamic pressure exchange machine that can improve the engine performance and fit diversified course.In this paper,the thermo-cycle analysis mode of a wave-rotor-topped small gas turbine engines is established.When the compressor,the turbine pressure ratio,and the turbine inlet temperature vary in the thermodynamic calculation according to the anticipated design objectives in the five considered cases,the influence of wave rotor on the performance of small gas turbine engines is investigated.The variable laws of wave rotor-applied combustor work condition is discussed.The best performance is obtained in the topped engine operates with the same compressor pressure ratio,inlet temperature and physical compressor like that of the baseline engine.The prime performance optimized region and the combustor work condition of the wave-rotor-topped small gas turbine engines are obtained.
Keywords:small gas turbine engine  wave rotor  thermodynamic cycle  performance
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