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| 1种涡轮叶间补燃室的数值研究 | |
| 引用本文： | 李 明,唐 豪,高大鹏,莫 妲.1种涡轮叶间补燃室的数值研究[J].航空发动机,2012,38(6):24-28. |
| 作者姓名： | 李 明 唐 豪 高大鹏 莫 妲 |
| 作者单位： | 1. 中国轻型燃气轮机开发中心,北京100009 南京航空航天大学能源与动力学院,南京210016 2. 南京航空航天大学能源与动力学院,南京,210016 3. 中国轻型燃气轮机开发中心,北京,100009 4. 中航工业沈阳发动机设计研究所,沈阳,110015 |
| 基金项目： | 国家自然科学基金（51076064）资助 |
| 摘 要： | 为提高燃气涡轮发动机性能，将UCC技术应用在低压涡轮导向器上，建立低压涡轮导向叶片补燃室（TurbineInter-vaneBurners，TIB）模型。通过改变燃烧室结构，设计了3种涡轮叶间补燃室模型，利用计算流体力学软件FLUENT对燃烧室的流动及燃烧进行数值模拟，采用CFD的方法，分析燃烧室的燃烧和流动特性。结果表明：3种结构的涡轮叶间补燃室均提高了燃烧效率，选择的数学模型合理、计算方法可行，其结果可为涡轮叶间补燃室设计提供参考。 |
| 关 键 词： | 涡轮叶间燃烧 超紧凑燃烧 数值模拟 燃气涡轮发动机 |
Numerical Investigation of a Turbine Inter-Vane Burner |
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| Authors: | LI Ming TANG Hao GAO Da-peng MO Da |
| Institution: | 1.China National Light Weight Gas Turbine Development Center, Beijing 100009,China;2.College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;3.AVIC Shenyang Engine Design and Research Institute,Shenyang 110015,China) |
| Abstract: | In order to improve the performance of gas turbine engines, Turbine Inter-Vane Burner (TIB) model was built by the application of Ultra-Compared Combustion (UCC) technology on low-pressure turbine guide vanes .Three TIB models were designed by changing the combustor structure. The computational fluid dynamics (CFD) code FLUENT was used to simulate and analyze the turbulent flow and combustion of the combustor. The results show that the TIB can enhance combustion efficiency. The mathematical models and numerical methods are reasonable and the numerical results provide important reference to the design of TIB. |
| Keywords: | Turbine Inter-vane Burner ultra-compact combustion numerical simulation gas turbines engines |
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