| Citation: | FAN Xiaoqian, WANG Yangbing, LIU Yiming, et al. Effect of throat size of turbine guide on performance of gas turbine starter[J]. Journal of Aerospace Power, 2024, 39(9):20230775 doi: 10.13224/j.cnki.jasp.20230775 |
A gas turbine guide on a gas turbine starter was taken as the research object, and the effects of throat size of gas turbine guide on the performance of gas turbine starter and components were studied using experimental methods and numerical simulation. The results of experimental research on A, B, C types of gas turbine guide (average outer diameter of the throat was 111.27, 111.94, 112.34 mm) indicated: type C′ starter compared with type A′ starter, normal starting time became shorter by 14%, output shaft disengagement speed of lose efficacy starting increased by 7.1%, maximum output power increased by 11.6%, the performance of starter was improved significantly. Numerical research results indicated: type C″ compared with type A″, the flow rate of turbine stage increased by 3.6%, maximum output power of power turbine increased by 12.2%. The increase in power turbine power was attributed to the combined effect of increased flow rate, increased temperature and increased temperature drop. In summary, the outer diameter of gas turbine guide throat changed the matching point of entire gas turbine by affecting the performance of turbine stage, then the overall performance exhibited a certain degree of dispersion.
| [1] |
HAROLD E R. Analytical determination of radial inflow turbine design geometry for maximum efficiency[R]. NASA TN D-4384, 1968.
|
| [2] |
REICHERT A W, SIMON H. Design and flow field calculations for transonic and supersonic radial inflow turbine guide vanes[J]. Journal of Turbomachinery, 1997, 119(1): 103-113. doi: 10.1115/1.2840999
|
| [3] |
REICHERT A W, SIMON H. Numerical investigations on the optimum design of radial inflow turbine guide vanes: 94-GT-061[R]. Hague, Netherlands: ASME, 1994.
|
| [4] |
邓清华, 丰镇平. 微型燃气轮机向心透平导向器的流场分析与设计研究[J]. 西安交通大学学报, 2005, 39(9): 962-965. DENG Qinghua, FENG Zhenping. Flow analysis and design of radial inflow turbine guide vanes for microturbine[J]. Journal of Xi’an Jiaotong University, 2005, 39(9): 962-965. (in Chinese
DENG Qinghua, FENG Zhenping. Flow analysis and design of radial inflow turbine guide vanes for microturbine[J]. Journal of Xi’an Jiaotong University, 2005, 39(9): 962-965. (in Chinese)
|
| [5] |
宣建光, 邱建, 夏晨, 等. 一种微型涡轮发动机导向器改进方案[J]. 航空动力学报, 2010, 25(12): 2690-2696. XUAN Jianguang, QIU Jian, XIA Chen, et al. Improvement of a micro-turbine nozzle[J]. Journal of Aerospace Power, 2010, 25(12): 2690-2696. (in Chinese
XUAN Jianguang, QIU Jian, XIA Chen, et al. Improvement of a micro-turbine nozzle[J]. Journal of Aerospace Power, 2010, 25(12): 2690-2696. (in Chinese)
|
| [6] |
周逊, 韩万金, 王仲奇. 低压涡轮导向器气动性能的实验研究[J]. 热力透平, 2007, 36(2): 92-96. ZHOU Xun, HAN Wanjin, WANG Zhongqi. Experimental investigation of aerodynamic characteristics of LP turbine guide vane[J]. Thermal Turbine, 2007, 36(2): 92-96. (in Chinese
ZHOU Xun, HAN Wanjin, WANG Zhongqi. Experimental investigation of aerodynamic characteristics of LP turbine guide vane[J]. Thermal Turbine, 2007, 36(2): 92-96. (in Chinese)
|
| [7] |
朱兰, 张剑, 卿雄杰. 高压涡轮导向器扇形叶栅试验及改进设计验证[J]. 燃气涡轮试验与研究, 2014, 27(5): 19-24. ZHU Lan, ZHANG Jian, QING Xiongjie. Experiment and improved design verification on the sector cascade of high pressure turbine nozzle[J]. Gas Turbine Experiment and Research, 2014, 27(5): 19-24. (in Chinese
ZHU Lan, ZHANG Jian, QING Xiongjie. Experiment and improved design verification on the sector cascade of high pressure turbine nozzle[J]. Gas Turbine Experiment and Research, 2014, 27(5): 19-24. (in Chinese)
|
| [8] |
安柏涛, 韩万今, 王松涛, 等. 几何参数对涡轮低压导向器变工况性能的影响[J]. 航空动力学报, 2004, 19(1): 94-100. AN Baitao, HAN Wanjin, WANG Songtao, et al. Effects of geometry parameters on incidence characteristics of turbine low pressure guide vane[J]. Journal of Aerospace Power, 2004, 19(1): 94-100. (in Chinese
AN Baitao, HAN Wanjin, WANG Songtao, et al. Effects of geometry parameters on incidence characteristics of turbine low pressure guide vane[J]. Journal of Aerospace Power, 2004, 19(1): 94-100. (in Chinese)
|
| [9] |
郑涛, 赵克云, 吴仁辉. 水流法测量涡轮导向器喉道面积[J]. 推进技术, 1997, 18(4): 106-108. ZHENG Tao, ZHAO Keyun, WU Renhui. Measurement of turborotor throat area by water flow[J]. Journal of Propulsion Technology, 1997, 18(4): 106-108. (in Chinese
ZHENG Tao, ZHAO Keyun, WU Renhui. Measurement of turborotor throat area by water flow[J]. Journal of Propulsion Technology, 1997, 18(4): 106-108. (in Chinese)
|
| [10] |
屈云凤, 张志强, 曾令玉, 等. 型线法测量涡轮导向器喉道面积的原理和应用[J]. 测控技术, 2015, 34: 160-163. QU Yunfeng, ZHANG Zhiqiang, ZENG Lingyu, et al. Principle and application of turbine nozzle throat area measurement by profile method[J]. Measurement & Control Technology, 2015, 34: 160-163. (in Chinese
QU Yunfeng, ZHANG Zhiqiang, ZENG Lingyu, et al. Principle and application of turbine nozzle throat area measurement by profile method[J]. Measurement & Control Technology, 2015, 34: 160-163. (in Chinese)
|
| [11] |
王振兴, 范明争, 张盛珺, 等. 涡轮导向器喉道面积三坐标测量不确定度评估[J]. 航空制造技术, 2022, 65(5): 68-74. WANG Zhenxing, FAN Mingzheng, ZHANG Shengjun, et al. Measurement uncertainty evaluation of turbine nozzle throat area measured by coordinate measurement machine[J]. Aeronautical Manufacturing Technology, 2022, 65(5): 68-74. (in Chinese
WANG Zhenxing, FAN Mingzheng, ZHANG Shengjun, et al. Measurement uncertainty evaluation of turbine nozzle throat area measured by coordinate measurement machine[J]. Aeronautical Manufacturing Technology, 2022, 65(5): 68-74. (in Chinese)
|
| [12] |
闻雪友, 钱振岳. 涡轮导向器面积调整对燃气轮机性能的影响[J]. 舰船科学技术, 1981, 3(12): 74-88, 93. WEN Xueyou, QIAN Zhenyue. Influence of turbine guide area adjustment on gas turbine performance[J]. Ship Science and Technology, 1981, 3(12): 74-88, 93. (in Chinese
WEN Xueyou, QIAN Zhenyue. Influence of turbine guide area adjustment on gas turbine performance[J]. Ship Science and Technology, 1981, 3(12): 74-88, 93. (in Chinese)
|
| [13] |
DENTON J D. The 1993 IGTI scholar lecture: loss mechanisms in turbomachines[J]. Journal of Turbomachinery, 1993, 115(4): 621-656. doi: 10.1115/1.2929299
|
| [14] |
ROSE M G, HARVEY N W. Turbomachinery wakes: differential work and mixing losses[J]. Journal of Turbomachinery, 2000, 122(1): 68-77. doi: 10.1115/1.555429
|
| [15] |
WALTERS D K, LEYLEK J H. Impact of film-cooling jets on turbine aerodynamic losses[J]. Journal of Turbomachinery, 2000, 122(3): 537-545. doi: 10.1115/1.1303818
|
| [16] |
石德永, 宋文艳, 浮强. 导向器叶片尾缘厚度对涡轮性能影响研究[J]. 机械设计与制造, 2013(11): 102-104, 108. SHI Deyong, SONG Wenyan, FU Qiang. Research of stator trailing edge thickness effects on turbine performance[J]. Machinery Design & Manufacture, 2013(11): 102-104, 108. (in Chinese doi: 10.3969/j.issn.1001-3997.2013.11.031
SHI Deyong, SONG Wenyan, FU Qiang. Research of stator trailing edge thickness effects on turbine performance[J]. Machinery Design & Manufacture, 2013(11): 102-104, 108. (in Chinese) doi: 10.3969/j.issn.1001-3997.2013.11.031
|
| [17] |
徐志伟, 郭昊雁, 郑振江, 等. 向心涡轮导向器设计改进及应用[J]. 推进技术, 2017, 38(10): 2358-2364. XU Zhiwei, GUO Haoyan, ZHENG Zhenjiang, et al. Improvement of design technology for a radial inflow turbine guide vane and its application[J]. Journal of Propulsion Technology, 2017, 38(10): 2358-2364. (in Chinese
XU Zhiwei, GUO Haoyan, ZHENG Zhenjiang, et al. Improvement of design technology for a radial inflow turbine guide vane and its application[J]. Journal of Propulsion Technology, 2017, 38(10): 2358-2364. (in Chinese)
|
| [18] |
陈靖华, 徐伟祖, 李传鹏. 空气涡轮起动机性能数值仿真和试验研究[J]. 南京航空航天大学学报, 2022, 54(4): 654-661. CHEN Jinghua, XU Weizu, LI Chuanpeng. Numerical simulation and experimental investigation on performance of air turbine starter[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2022, 54(4): 654-661. (in Chinese
CHEN Jinghua, XU Weizu, LI Chuanpeng. Numerical simulation and experimental investigation on performance of air turbine starter[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2022, 54(4): 654-661. (in Chinese)
|
| [19] |
陈靖华, 徐伟祖, 李传鹏. 空气涡轮起动机优化设计和匹配特性[J]. 南京航空航天大学学报, 2023, 55(2): 226-232. CHEN Jinghua, XU Weizu, LI Chuanpeng. Optimization design and matching performance of air turbine starter[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2023, 55(2): 226-232. (in Chinese
CHEN Jinghua, XU Weizu, LI Chuanpeng. Optimization design and matching performance of air turbine starter[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2023, 55(2): 226-232. (in Chinese)
|
| [20] |
黄维娜, 邹正平, 李维, 等. 航空发动机涡轮设计[M]. 北京: 科学出版社, 2022. HUANG Weina, ZOU Zhengping, LI Wei. Turbine design of aero-engine[M]. Beijing: Science Press, 2022. (in Chinese
HUANG Weina, ZOU Zhengping, LI Wei. Turbine design of aero-engine[M]. Beijing: Science Press, 2022. (in Chinese)
|