环形燃烧室冷热态发散冷却性能的对比实验

摘要/Abstract

摘要： 针对燃烧室发散冷却性能的研究，设计了3头部扇段模型燃烧室进行冷热态对比实验.通过对模型环形燃烧室内外环面上的温度进行测量，讨论冷热态时综合冷却效率分布差异，并考察了冷却空气量与主流空气量之比对综合冷却效率的影响规律.结果表明：发散冷却在冷热态时的综合冷却性能差异显著，主要是由于燃烧反应的发生改变了燃烧室内流场和温度场，进而引起壁面热负荷变化；无论冷态还是热态，在旋流主流的作用下，内环面上的发散气膜相比于外环面更易吹离壁面.随着无量纲流量比的增加，面积平均综合冷却效率均随之增加，但增加幅度逐渐降低.

关键词: , 发散冷却；低污染燃烧室；综合冷却效率

Abstract: Threenozzle annular model combustor is designed to investigate the effusion cooling characteristics under nonreacting and reacting flow conditions. Temperature was measured on both outer and inner liners of the combustor, and then difference of overall cooling effectiveness distribution with or without combustion is analyzed. The effect of coolant to mainstream air flowrate ratio on the overall cooling effectiveness is studied. Results showed that effusion cooling behavior under reacting condition looks distinctly different from that under nonreacting condition. Specifically, cooling effectiveness showed laterally nonuniform distribution and skewed towards the micro rotation direction result from three separate coswirling flows merge. The most significant phenomenon at reacting flow condition is that low cooling effectiveness region shows up. This is because of the swirling flame impinging on the combustor liners.

Key words: effusion cooling, lowemission combustion, overall cooling effectiveness

中图分类号:

V 231.2

吉雍彬1，杜世强2，虞江鹏1，葛冰1，臧述升1. 环形燃烧室冷热态发散冷却性能的对比实验 [J]. 上海交通大学学报（自然版）, 2017, 51(8): 962-969.

JI Yongbin1，DU Shiqiang2，YU Jiangpeng1，GE Bing1， ZANG Shusheng1. Comparative Experimental Investigation of Effusion Cooling
Performance on the Annular Combustor Liners at
Nonreacting/Reacting Flow Conditions[J]. Journal of Shanghai Jiaotong University, 2017, 51(8): 962-969.

参考文献

［1］SCHULZ A. Combustor liner cooling technology in scope of reduced pollutant formation and rising thermal efficiencies［J］. Heat Transfer in Gas Turbine Systems, 2001，934(1): 135146.
［2］KREWINKEL R. A review of gas turbine effusion cooling studies［J］. International Journal of Heat and Mass Transfer, 2013, 66: 706722.
［3］林宇震. 燃烧室多斜孔壁气膜冷却研究［D］. 北京: 北京航空航天大学能源动力与工程学院, 1997.
［4］LEGER B, MIRON P, EMIDIO J M. Geometric and aerothermal influences on multiholed plate temperature: Application on combustor wall［J］. International Journal of Heat and Mass Transfer, 2003, 46: 12151222.
［5］OGUNTADE H I, ANDREWS G E, BURNS A D, et al. The influence the number of holes on effusion cooling effectiveness for an X/D of 4.7［C］∥Proceeding of ASME TURBO EXPO. Montreal: ASME，2015, GT201542248.
［6］HUANG Z, XIONG Y B, LIU Y Q, et al. Experimental investigation of fullcoverage effusion cooling through perforated flat plates［J］. Applied Thermal Engineering, 2015, 76: 7685.
［7］GOLDSTEIN R J, STONE L D. Rowofholes film cooling of curved walls at low injection angles［J］. Journal of Turbomachinery, 1997, 119(3): 574579.
［8］KOC I, PARMAKSIZOGLU C, CAKAN M. Numerical investigation of film cooling effectiveness on the curved surface［J］. Energy Conversion and Management, 2006, 47(9/10): 12311246.
［9］PATIL S, ABRAHAM S, TAFTI D, et al. Experimental and numerical investigation of convective heat transfer in a gas turbine can combustor［J］. Journal of Turbomachinery, 2011, 133(1): 011028.
［10］PATIL S, SEDALOR T, TAFTI D, et al. Study of flow and convective heat transfer in a simulated scaled up low emission annular combustor［J］. Journal of Thermal Science and Engineering Applications, 2011, 3(3): 031010.
［11］GOMEZ R D, KUMAR V, EKKAD S, et al. Flow field and liner heat transfer for a model annular combustor equipped with radial swirlers［C］∥50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. Cleveland: AIAA，2014: 3436.
［12］CARMACK A, EKKAD S, KIM Y, et al. Comparison of flow and heat transfer distributions in a can combustor for radial and axial swirlers under cold flow conditions［J］. Journal of Thermal Science and Engineering Applications, 2013, 5(3): 031012.
［13］WURM B, SCHULZ A, BAUER H J. A new test facility for investigating the interaction between swirl flow and wall cooling films in combustors［C］∥Proceeding of ASME TURBO EXPO. Orlando: ASME，2009: 59961.
［14］WURM B, SCHULZ A, BAUER H J, et al. Cooling efficiency for assessing the cooling performance of an effusion cooled combustor liner［C］∥Proceeding of ASME TURBO EXPO. San Antonio: ASME, 2013: 94304.
［15］WURM B, SCHULZ A, BAUER H J, et al. Impact of swirl flow on the penetration behaviour and cooling performance of a starter cooling film in modern lean operating combustion chambers［C］∥Proceeding of ASME TURBO EXPO. Dusseldorf: ASME，2014: 25520.
［16］ANDREINI A, BECCHI R, FACCHINI B, et al. Adiabatic effectiveness and flow field measurements in a realistic effusion cooled lean burn combustor［J］. Journal of Engineering for Gas Turbines and Power, 2016, 138(3): 031506.
［17］ANDREINI A, FACCHINI B, BECCHI R, et al. Effect of slot injection and effusion array on the liner heat transfer coefficient of a scaled leanburn combustor with representative swirling flow［J］. Journal of Engineering for Gas Turbines and Power, 2016, 138(4): 041501.
［18］ANDREINI A, SOGHE R D, FACCHINI B, et al. Local source based CFD modeling of effusion cooling holes: Validation and application to an actual combustor test case［J］. Journal of Engineering for Gas Turbines and Power, 2014, 136(1): 011506.
［19］ANDREINI A, FACCHINI B, INSINNA M, et al. Hybird RansLes modeling of a hot streak generator oriented to the study of combustorturbine interaction［C］∥Proceeding of ASME TURBO EXPO. Montreal: ASME，2015: 42402.

[1]	王聚团, 戚晓宁, 黄志明. 水下生产管汇测试技术及其改进研究[J]. 海洋工程装备与技术, 2022, 9(2): 43-49.
[2]	袁振钦, 邹科, 孙亚峰, 刘刚, 屈衍, 李居跃. 基于时域分析法的动态电缆疲劳分析[J]. 海洋工程装备与技术, 2022, 9(2): 50-55.
[3]	王娟, 杨明旺, 郑茂尧, 刘凌云, 赵立君. 高强钢在大型半潜式平台组块建造中的应用[J]. 海洋工程装备与技术, 2022, 9(1): 27-31.
[4]	陈欣, 赵晓磊, 王立坤, 肖德明, 张腾月. 深水大型吸力锚建造技术研究[J]. 海洋工程装备与技术, 2022, 9(1): 32-36.
[5]	尹彦坤, 易涤非. 半潜式生产平台船体结构关键节点工程临界评估[J]. 海洋工程装备与技术, 2022, 9(1): 52-57.
[6]	MA Qunsheng (马群圣), CEN Xingxing (岑星星), YUAN Junyi (袁骏毅), HOU Xumin (侯旭敏). Word Embedding Bootstrapped Deep Active Learning Method to Information Extraction on Chinese Electronic Medical Record[J]. J Shanghai Jiaotong Univ Sci, 2021, 26(4): 494-502.
[7]	ZHANG Shengfa (张胜发), TANG Na (唐纳), SHEN Guofeng (沈国峰), WANG Han (王悍), QIAO Shan (乔杉). Universal Software Architecture of Magnetic Resonance-Guided Focused Ultrasound Surgery System and Experimental Study[J]. J Shanghai Jiaotong Univ Sci, 2021, 26(4): 471-481.
[8]	安庆升, 孙立东, 武秋生. 碳纤维增强复合材料发射筒设计研究[J]. 空天防御, 2021, 4(2): 13-.
[9]	KONG Xiangqiang (孔祥强), MENG Xiangxi (孟祥熙), LI Jianbo (李见波), SHANG Yanping (尚燕平), CUI Fulin (崔福林) . Comparative Study on Two-Stage Absorption Refrigeration Systems with Different Working Pairs[J]. J Shanghai Jiaotong Univ Sci, 2021, 26(2): 155-162.
[10]	ZHUANG Weimin (庄蔚敏), WANG Pengyue (王鹏跃), AO Wenhong (熬文宏), CHEN Gang (陈刚) . Experiment and Simulation of Impact Response of Woven CFRP Laminates with Different Stacking Angles[J]. J Shanghai Jiaotong Univ Sci, 2021, 26(2): 218-230.
[11]	ZHOU Xuhui (周旭辉), ZHANG Wenguang (张文光), XIE Jie (谢颉). Effects of Micro-Milling and Laser Engraving on Processing Quality and Implantation Mechanics of PEG-Dexamethasone Coated Neural Probe[J]. J Shanghai Jiaotong Univ Sci, 2021, 26(1): 1-9.
[12]	HUANG Ningning (黄宁宁), MA Yixin (马艺馨), ZHANG Mingzhu (张明珠), GE Hao (葛浩), WU Huawei (吴华伟). Finite Element Modeling of Human Thorax Based on MRI Images for EIT Image Reconstruction[J]. J Shanghai Jiaotong Univ Sci, 2021, 26(1): 33-39.
[13]	WANG Xianjin, GAO Xu, YU Kuigang . Fixture Locating Modelling and Optimization Research of Aluminum Alloy Sidewall in a High-Speed Train Body[J]. J Shanghai Jiaotong Univ Sci, 2020, 25(6): 706-713.
[14]	QIAO Xing, MA Dan, YAO Xuliang, FENG Baolin. Stability and Numerical Analysis of a Standby System[J]. J Shanghai Jiaotong Univ Sci, 2020, 25(6): 769-778.
[15]	WU Jin, MIN Yu, YANG Xiaodie, MA Simin . Micro-Expression Recognition Algorithm Based on Information Entropy Feature[J]. Journal of Shanghai Jiao Tong University(Science), 2020, 25(5): 589-599.