| Citation: | WANG Zhihui, MA Chaochen, LIU Xiaojuan, et al. Effect of end-clearance sealed structure of guide vane on variable nozzle turbine performance[J]. Journal of Aerospace Power, 2024, 39(3):20220251 doi: 10.13224/j.cnki.jasp.20220251 |
Based on the traditional variable nozzle turbine guide vane, an end-clearance sealed guide vane (ESGV) was designed. The effect of ESGV on the performance of the turbine was analyzed by numerical simulation under different guide openings. The results showed that ESGV can effectively suppress the end-wall clearance leakage flow of the guide vane and improve the flow state of nozzle ring and rotor channel, and then enhance the turbine efficiency. Finally, the turbine performance tests of the ESGV turbine and the prototype turbine were carried out. The results showed that, when the flow characteristic curves of the two turbines were roughly the same, the efficiency of the ESGV turbine was 5% higher than that of the prototype turbine at the medium opening.
| [1] |
DASGUPTA S,SARMAH P,BORTHAKUR P P. Application of variable geometry turbine turbochargers to gasoline engines-A review[J]. IOP Conference Series: Materials Science and Engineering,2020,943(1): 012010.1-012010.15.
|
| [2] |
FENELEY A J,PESIRIDIS A,ANDWARI A M. Variable geometry turbocharger technology for exhaust energy recovery and boosting-a review[J]. Renewable and Sustainable Energy Reviews,2017,71: 959-975. doi: 10.1016/j.rser.2016.12.125
|
| [3] |
MA Chaochen,HUANG Zhi,QI Mingxu. Investigation on the forced response of a radial turbine under aerodynamic excitations[J]. Journal of Thermal Science,2016,25(2): 130-137. doi: 10.1007/s11630-016-0843-1
|
| [4] |
CHITRAKAR S,NEOPANE H P,DAHLHAUG O G. The numerical and experimental investigation of erosion induced leakage flow through guide vanes of Francis turbine[J]. IOP Conference Series:Earth and Environmental Science,2019,240: 072002.1-072002.10.
|
| [5] |
赵奔,马朝臣,胡良军,等. 导叶间隙不确定性对可调向心涡轮影响数值研究[J]. 推进技术,2014,35(4): 492-498. doi: 10.13675/j.cnki.tjjs.2014.03.003
ZHAO Ben,MA Chaochen,HU Liangjun,et al. Numerical investigation on effects of uncertain nozzle vane clearance on variable geometry radial turbine performance[J]. Journal of Propulsion Technology,2014,35(4): 492-498. (in Chinese) doi: 10.13675/j.cnki.tjjs.2014.03.003
|
| [6] |
ZHAO Ben,WANG Leilei,HOU Hongjun. Numerical analysis for impacts of nozzle end-clearances on aerodynamic performance and forced response in a VNT turbine[J]. Chinese Journal of Aeronautics,2018,31(5): 1030-1040. doi: 10.1016/j.cja.2018.02.015
|
| [7] |
ZHONG Fangpan,ZHOU Chao. Effects of tip gap size on the aerodynamic performance of a cavity-winglet tip in a turbine cascade[J]. Journal of Turbomachinery,2017,139(10): 101009.1-101009.9.
|
| [8] |
FU Yunfeng,CHEN Fu,LIU Huaping,et al. Experimental and numerical study of honeycomb tip on suppressing tip leakage flow in turbine cascade[J]. Journal of Turbomachinery,2018,140(6): 061006.1-061006.10.
|
| [9] |
LI Jun,DU Kun,SONG Liming. Effects of tip cavity geometries on the aerothermal performance of the transonic turbine blade with cavity tip[J]. Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy,2016,230(3): 319-331. doi: 10.1177/0957650915626833
|
| [10] |
MARAL H,ALPMAN E,KAVURMACıOĞLU L,et al. A genetic algorithm based aerothermal optimization of tip carving for an axial turbine blade[J]. International Journal of Heat and Mass Transfer,2019,143: 118419.1-118419.13.
|
| [11] |
GAO Jie,WEI Ming,LIU Pengfei,et al. Improved clearance designs to minimize aerodynamic losses in a variable geometry turbine vane cascade[J]. Proceedings of the Institution of Mechanical Engineers: Part C Journal of Mechanical Engineering Science,2018,232(17): 3085-3101. doi: 10.1177/0954406217729716
|
| [12] |
LIM B, PARK T, KANG Y S. Stall warning using the rotor tip pressure in a transonic axial compressor with circumferential grooves[R]. ASME Paper GT2018-76301, 2018.
|
| [13] |
ALONE D B, KUMAR S S, THIMMAIAH S, et al. Experimental investigation on the effect of porosity of bend skewed casing treatment on a single stage transonic axial flow compressor[R]. ASME Paper GT2014-26102, 2014
|
| [14] |
ZHANG Qianfeng,DU Juan,LI Jichao,et al. Dual stability enhancement mechanisms of axial-slot casing treatment in a high-speed mixed-flow compressor with various tip clearances[J]. Chinese Journal of Aeronautics,2021,34(4): 19-31. doi: 10.1016/j.cja.2020.08.019
|
| [15] |
YANG D, LAO D, YANG C, et al. Investigations on the generation and weakening of shock wave in a radial turbine with variable guide vanes[R]. ASME Paper GT2016-57047, 2016.
|
| [16] |
侯红娟,王磊磊,李延昭. 可调向心涡轮导叶叶顶间隙及其调节方法的研究[J]. 海峡科技与产业,2017(4): 99-100. doi: 10.3969/j.issn.1006-3013.2017.04.036
HOU Hongjuan,WANG Leilei,LI Yanzhao. Study on tip clearance of adjustable centripetal turbine guide vane and its adjustment method[J]. Technology and Industry Across the Straits,2017(4): 99-100. (in Chinese) doi: 10.3969/j.issn.1006-3013.2017.04.036
|
| [17] |
WANG Zhihui,MA Chaochen,HUANG Zhi,et al. A novel variable geometry turbine achieved by elastically restrained nozzle guide vanes[J]. Proceedings of the Institution of Mechanical Engineers: Part D Journal of Automobile Engineering,2020,234(9): 2312-2329. doi: 10.1177/0954407020909662
|
| [18] |
黄文梅. 气动位置控制系统的状态反馈调节[J]. 湖南大学学报(自然科学版),1990,17(1): 11-18.
HUANG Wenmei. State varable feedback control for pneumatical positioning systems[J]. Journal of Hunan University (Natural Science),1990,17(1): 11-18. (in Chinese)
|