Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (15): 131142.doi: 10.7527/S1000-6893.2024.31142
• Fluid Mechanics and Flight Mechanics • Previous Articles
Lei ZHAO(
), Jie LI, Jingying XU
Received:2024-09-02
Revised:2024-09-20
Accepted:2024-11-19
Online:2024-11-26
Published:2024-11-25
Contact:
Lei ZHAO
E-mail:zhaolei@acae.com.cn
CLC Number:
Lei ZHAO, Jie LI, Jingying XU. Effects of low-pressure turbine rig test method on measurement accuracy of efficiency[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(15): 131142.
| [1] | HOWELL R J. Wake-separation bubble interactions in low Reynolds number turbomachinery[D]. Cambridge, East of England: University of Cambridge, 1999. |
| [2] | HOWELL R J, RAMESH O N, HODSON H P, et al. High lift and aft-loaded profiles for low-pressure turbines[J]. Journal of Turbomachinery, 2001, 123(2): 181-188. |
| [3] | 卫刚, 王永明, 王松涛, 等. 高性能低压涡轮设计与试验[J]. 燃气涡轮试验与研究, 2013, 26(2): 6-11. |
| WEI G, WANG Y M, WANG S T, et al. Design and experiment of a high performance low-pressure turbine[J]. Gas Turbine Experiment and Research, 2013, 26(2): 6-11 (in Chinese). | |
| [4] | HASELBACH F, SCHIFFER H P, HORSMAN M, et al. The application of ultra high lift blading in the BR715 LP turbine[J]. Journal of Turbomachinery, 2002, 124(1): 45-51. |
| [5] | HARVEY N W, BRENNAN G, NEWMAN D A, et al. Improving turbine efficiency using non-axisymmetric end walls: Validation in the multi-row environment and with low aspect ratio blading[C]∥ASME Turbo Expo 2002: Power for Land, Sea, and Air, 2009: 119-126. |
| [6] | BRENNAN G, HARVEY N W, ROSE M G, et al. Improving the efficiency of the Trent 500-HP turbine using nonaxisymmetric end walls (part Ⅰ): Turbine design[J]. Journal of Turbomachinery, 2003, 125(3): 497-504. |
| [7] | ROSE M G, HARVEY N W, SEAMAN P, et al. Improving the efficiency of the Trent 500 HP turbine using non-axisymmetric end walls (part Ⅱ): Experimental validation[C]∥ASME Turbo Expo 2001: Power for Land, Sea, and Air, 2014. |
| [8] | GERMAIN T, NAGEL M, Ⅰ RAAB, et al. Improving efficiency of a high work turbine using non-axisymmetric endwalls (Part I): Endwall design and performance[C]∥ASME Turbo Expo 2008: Power for Land, Sea, and Air, 2009: 1109-1119. |
| [9] | JOUINI D B M, LITTLE D, BANCALARI E, et al. Experimental investigation of airfoil wake clocking impacts on aerodynamic performance in a two stage turbine test rig[C]∥ASME Turbo Expo 2003, Collocated with the 2003 International Joint Power Generation Conference, 2009: 351-358. |
| [10] | 中国航空工业集团公司. 航空燃气涡轮发动机轴流涡轮气动性能试验方法: [S]. 北京: 中国航空综合技术研究所, 2013. |
| Aviation Industry Corporation of China. Aerodynamic performance test method of axial turbine for aircraft gas turbine engine: [S]. Beijing: AVIC China Aero-Polytechnology Establishment, 2013 (in Chinese). | |
| [11] | 安兆强, 陈强, 郝晟淳, 等. 大涵道比发动机多级低压涡轮试验技术研究[J]. 航空发动机, 2018, 44(6): 69-73. |
| AN Z Q, CHEN Q, HAO S C, et al. Research on multistage low pressure turbine test technology for high bypass ratio aeroengine[J]. Aeroengine, 2018, 44(6): 69-73 (in Chinese). | |
| [12] | 邸亚超, 胡应交, 张星, 等. 涡轮试验准则数对流场相似性的影响[J]. 航空动力学报, 2018, 33(1): 193-200. |
| DI Y C, HU Y J, ZHANG X, et al. Influence of turbine test criterion parameters on flow similarity[J]. Journal of Aerospace Power, 2018, 33(1): 193-200 (in Chinese). | |
| [13] | 杨帆. 涡轮轮缘封严气流与主流非定常干涉机理及其损失控制研究[D]. 西安: 西北工业大学, 2019: 35-65. |
| YANG F. Investigation of unsteady interaction mechanism and associated loss control between turbine rim seal flow and mainstream[D]. Xi’an: Northwestern Polytechnical University, 2019: 35-65 (in Chinese). | |
| [14] | 张剑. 叶尖间隙对涡轮性能影响的计算与试验研究[J]. 燃气涡轮试验与研究, 2012, 25(2): 33-36. |
| ZHANG J. Calculation and test of influence of rotor tip clearance on turbine performance[J]. Gas Turbine Experiment and Research, 2012, 25(2): 33-36 (in Chinese). | |
| [15] | 王松涛, 刘勋, 周逊, 等. 低压涡轮低雷诺数条件下气动性能分析[J]. 汽轮机技术, 2011, 53(5): 324-327. |
| WANG S T, LIU X, ZHOU X, et al. Aerodynamic performance analysis of low pressure turbine at low Reynolds numbers[J]. Turbine Technology, 2011, 53(5): 324-327 (in Chinese). | |
| [16] | REID K, DENTON J, PULLAN G, et al. The effect of stator-rotor hub sealing flow on the mainstream aerodynamics of a turbine[C]∥ASME Turbo Expo 2006: Power for Land, Sea, and Air, 2008: 789-798. |
| [17] | SCHUEPBACH P, ABHARI R S, ROSE M G, et al. Effects of suction and injection purge-flow on the secondary flow structures of a high-work turbine[J]. Journal of Turbomachinery, 2010, 132(2): 021021. |
| [18] | REGINA K, KALFAS A I, ABHARI R S. Experimental investigation of purge flow effects on a high pressure turbine stage[J]. Journal of Turbomachinery, 2015, 137(4): 041006. |
| [19] | 邹正平, 王松涛, 刘火星, 等. 航空燃气轮机涡轮气体动力学: 流动机理及气动设计[M]. 上海: 上海交通大学出版社, 2014: 183-192. |
| ZOU Z P, WANG S T, LIU H X, et al. Turbine aerodynamics for aero-engine[M]. Shanghai: Shanghai Jiao Tong University Press, 2014: 183-192 (in Chinese). | |
| [20] | VOLINO R J, HULTGREN L S. Measurements in separated and transitional boundary layers under low-pressure turbine airfoil conditions[J]. Journal of Turbomachinery, 2001, 123(2): 189-197. |
| [21] | HODSON H P, HOWELL R J. The role of transition in high-lift low-pressure turbines for aeroengines[J]. Progress in Aerospace Sciences, 2005, 41(6): 419-454. |
| [22] | 张天龙, 陈强, 赵展, 等. 雷诺数对高负荷低速涡轮性能影响的试验研究[J]. 测控技术, 2024, 43(2): 74-79. |
| ZHANG T L, CHEN Q, ZHAO Z, et al. Experimental study on the effect of Reynolds number on the performance of high-load low-speed turbines[J]. Measurement & Control Technology, 2024, 43(2): 74-79 (in Chinese). | |
| [23] | BRINGHENTI C, BARBOSA J R. Effects of turbine tip clearance on gas turbine performance[C]∥ASME Turbo Expo 2008: Power for Land, Sea, and Air, 2009: 1715-1721. |
| [24] | 谷雪花, 郝晟淳, 张东海, 等. 叶尖间隙对涡轮性能影响的试验研究[J]. 航空发动机, 2020, 46(4): 78-81. |
| GU X H, HAO S C, ZHANG D H, et al. Experimental study on influence of tip clearance on turbine performance[J]. Aeroengine, 2020, 46(4): 78-81 (in Chinese). | |
| [25] | YOON S, CURTIS E, DENTON J, et al. The effect of clearance on shrouded and unshrouded turbines at two levels of reaction[C]∥ASME Turbo Expo 2010: Power for Land, Sea, and Air, 2010: 1231-1241. |
| [1] | Shiqi WANG, Qinglan WEN, Peng ZHAO, Yixin CHENG, Liang MA, Zhigang JIA, Quan WEN. Experiments on afterburner combustion performance with self-excited sweeping nozzle in high speed and medium temperature air flow [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(9): 131261-131261. |
| [2] | Lingling CHEN, Yang ZHANG, Yongqiang SHI, Qingzhen YANG. Film cooling performance/nozzle performance/infrared radiation characteristics of a vector nozzle [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(8): 631139-631139. |
| [3] | Chao YANG, Zhicheng ZOU, Changchuan XIE, Chao AN, Cunyi HU. Research progress of RBF dynamic mesh technology and its application in aeroelasticity [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(5): 530945-530945. |
| [4] | Zhuoyuan LI, Xudong YANG, Kai SUN, Junhui XIONG, Shuai SHI. Aerodynamic configuration of distributed ducted fan with complex strong interference effect and performance influence [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(3): 130805-130805. |
| [5] | Yousheng WANG, Liguo SUN, Jinpeng WEI, Wenqian TAN, Yonghao PAN. Optimization of climb trajectory of combined-cycle engine powered aircraft based on improved CSO-Gauss pseudospectral method [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(2): 230737-230737. |
| [6] | Haipeng DING, Zheng LYU, Ke TIAN, Tao YE, Kuangshi CHEN, Jinglei XU. Design and performance analysis of a three-dimensional TBCC exhaust system [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(15): 131104-131104. |
| [7] | Sisi YUAN, Xuming NIU, Zhigang SUN, Yingdong SONG. Load spectrum correction method considering performance degradation [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(12): 231312-231312. |
| [8] | Zonghui WANG, Yunjun YANG, Hongrui ZHAO, Xuechen WANG. Aerodynamic optimization design of tiltrotor under multiple flight conditions [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529024-529024. |
| [9] | Junfu LI, Qing CHEN, Wei WANG, Zhonghua HAN, Yuting TAN, Yulin DING, Lu XIE, Jianling QIAO, Ke SONG, Junqiang AI. Design of low sonic boom high efficiency layout for advanced supersonic civil aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 629613-629613. |
| [10] | Lili CHEN, Jianxia LIU, Juntao ZHANG, Zheng GUO, Anping WU, Zhongxi HOU. Waverider forebody design method with longitudinal segments and multi-stage compression [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 128744-128744. |
| [11] | Wei WANG, Weigang AN, Bifeng SONG, Wenqing YANG. Dynamic soaring performance of albatross-inspired morphing wing [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(24): 630576-630576. |
| [12] | Zhihao ZHU, Xiuming SUI, Jian PU, Long HAO, Wei ZHAO, Qingjun ZHAO. Aerodynamic load of multistage vaneless counterrotating turbine under wake/shock rotor/rotor interactions [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(24): 630582-630582. |
| [13] | Zhe WANG, Zhiping WANG, Kunying DING, Tao ZHANG, Yuanhang WANG. Reliability analysis of thermal barrier coatings on turbine guide vanes of a certain type of aero-engine [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(22): 430141-430141. |
| [14] | Yingzhi ZHANG, Huibin SUN, Cheng YAN, Meng LIU. A digital twin model for rotor tip clearance prediction considering interval uncertainty [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(21): 629775-629775. |
| [15] | Minghui HU, Shaopeng LIU, Hao WANG, Chenyang LI, Weimin WANG, Zhinong JIANG. Characterization and identification of gas turbine blade fracture faults based on broadband vibration [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(20): 230098-230098. |
| Viewed | ||||||
|
Full text |
|
|||||
|
Abstract |
|
|||||
Address: No.238, Baiyan Buiding, Beisihuan Zhonglu Road, Haidian District, Beijing, China
Postal code : 100083
E-mail:hkxb@buaa.edu.cn
Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics
All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341

