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内燃波转子影响涡轴发动机性能研究
成本林1,2, 李建中1,2, 巩二磊1, 温泉2, 张堃元1
1.南京航空航天大学 能源与动力学院,江苏 南京 210016;2.中国航空动力机械研究所,湖南 株洲 421002
摘要:
内燃波转子涡轴发动机是一种集波转子增压技术、等容燃烧技术和涡轴发动机技术为一体的新概念发动机。介绍了内燃波转子的结构和工作原理,建立内燃波转子涡轴发动机热力循环分析数学模型,开展内燃波转子通道出口气流马赫数变化对涡轴发动机性能的影响研究,探讨内燃波转子涡轴发动机热力循环状态参数变化规律,验证了内燃波转子技术能够显著提高涡轴发动机性能,内燃波转子涡轴发动机比功率和热循环效率最大提高了35.79%,耗油率SFC最大减少了26.37%。
关键词:  涡轴发动机  内燃波转子  热力循环  性能  出口马赫数
DOI:
分类号:
基金项目:国家自然科学基金(50876041);高等学校博士学科点专项科研基金(20093218120013)。
Impact of Internal Combustion Wave Rotor on Performance of Turboshaft Engine
CHENG Ben-lin1,2, LI Jian-zhong1,2, GONG Er-lei1, WEN Quan2, ZHANG Kun-yuan1
1.College of Energy and Power, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2.Chinese Aviation Powerplant Research Institute,Zhuzhou 421002, China
Abstract:
The internal combustion wave rotor turboshaft engine is a new concept engine which combines many technologies of wave rotor pressure increase and high thermodynamic cycle efficiency with constant-volume combustion and turboshaft engine. The structure and work principium of the internal combustion wave rotor were introduced and the thermo-cycle analysis mode of an internal combustion wave rotor turboshaft engine was established. When the exit Mach number of the internal combustion wave rotor channel was changed, the effects on performance of the internal combustion wave rotor turboshaft engine were investigated and the variable disciplinarian of thermo-cycle parameter of the internal combustion wave rotor was discussed.It was validated that the technology of the internal combustion wave rotor could enhance performance of turboshaft engine.The specifc cycle work and thermal efficiency maximally increase by 35.79% and specific fuel consumption mostly decreases by 26.37% for the internal combustion wave rotor turboshaft engine.
Key words:  Turboshaft engine  Internal combustion wave rotor  Thermodynamic cycle  Performance  Exit Mach number