| Citation: | CAO Chuanjun, GU Zhixiang, XU Feng. Digital calibration method and application of compressor variable stator vanes[J]. Journal of Aerospace Power, 2024, 39(12):20220932 doi: 10.13224/j.cnki.jasp.20220932 |
In order to improve the angle precision of variable stator vane (VSV), the process and method of digital calibration for VSV were established. The main steps include: zero calibration of angular resolver, angle measurement of extreme position, length adjustment of connecting rod, angle checking of extreme position, vane’s angle and liner displacement of actuator, and angle checking of difference for all speeds. The platform system was also founded for VSV digital calibration. The method proposed avoided the impact from personal operation deviation and precision of calibration tool. The test results showed that, the new digital VSV calibration improved the angle precision at half degree. The improvement of angle precision promoted the matching performance of compressor and the accuracy of compressor performance evaluation.
| [1] |
桂幸民. 航空压气机气动热力学理论与应用[M]. 上海: 上海交通大学出版社,2014. GUI Xingmin. Compressor aerothermodynamics and its applications in aircraft engines[M]. Shanghai: Shanghai Jiao Tong University Press,2014. (in Chinese
GUI Xingmin. Compressor aerothermodynamics and its applications in aircraft engines[M]. Shanghai: Shanghai Jiao Tong University Press, 2014. (in Chinese)
|
| [2] |
曹传军,刘天一,朱伟,等. 民用大涵道比涡扇发动机高压压气机技术进展[J]. 航空学报,2023,44(12): 027824. CAO Chuanjun,LIU Tianyi,ZHU Wei,et al. Technology development in high pressure compressor of civil high bypass-ratio turbofan engine[J]. Acta Aeronautica et Astronautica Sinica,2023,44(12): 027824. (in Chinese
CAO Chuanjun, LIU Tianyi, ZHU Wei, et al. Technology development in high pressure compressor of civil high bypass-ratio turbofan engine[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(12): 027824. (in Chinese)
|
| [3] |
熊劲松,侯安平,袁巍,等. 可调叶片的发展趋势及其气动问题的探讨[J]. 航空动力学报,2008,23(1): 112-116. XIONG Jinsong,HOU Anping,YUAN Wei,et al. Some discuss on technology trend and aerodynamics problem of adjustable blade[J]. Journal of Aerospace Power,2008,23(1): 112-116. (in Chinese
XIONG Jinsong, HOU Anping, YUAN Wei, et al. Some discuss on technology trend and aerodynamics problem of adjustable blade[J]. Journal of Aerospace Power, 2008, 23(1): 112-116. (in Chinese)
|
| [4] |
LONG Bingxiang,CHEN Qin,REN Zebin,et al. Effectiveness of variable rotor blades technique & variable stator vanes technique in adjusting axial-flow compressor[J]. IOP Conference Series: Materials Science and Engineering,2020,751(1): 012003. doi: 10.1088/1757-899X/751/1/012003
|
| [5] |
张健,任铭林. 静叶角度调节对压气机性能影响的试验研究[J]. 航空动力学报,2000,15(1): 27-30. ZHANG Jian,REN Minglin. Experimental investigation on effect of stator vane angle adjustment on compressor performance[J]. Journal of Aerospace Power, 2000,15(1): 27-30. (in Chinese
ZHANG Jian, REN Minglin. Experimental investigation on effect of stator vane angle adjustment on compressor performance[J]. Journal of Aerospace Power, 2000, 15(1): 27-30. (in Chinese)
|
| [6] |
胡晏铭,聂超群. 轴流压气机变工况导叶/静叶/转速联调规律探索[J]. 中国科学: 技术科学,2010,40(7): 765-771. HU Yanming,NIE Chaoqun. Exploration of combined adjustment laws about IGV,stator and rotational speed in off-design conditions in an axial compressor[J]. Scientia Sinica (Technologica),2010,40(7): 765-771. (in Chinese doi: 10.1360/ze2010-40-7-765
HU Yanming, NIE Chaoqun. Exploration of combined adjustment laws about IGV, stator and rotational speed in off-design conditions in an axial compressor[J]. Scientia Sinica (Technologica), 2010, 40(7): 765-771. (in Chinese) doi: 10.1360/ze2010-40-7-765
|
| [7] |
曹志鹏,刘波,丁伟. 静叶角度调节对组合压气机性能优化机理[J]. 北京航空航天大学学报,2007,33(8): 878-881,893. CAO Zhipeng,LIU Bo,DING Wei. Stator setting angles adjustment on performance improvement of axial-centrifugal compressor[J]. Journal of Beijing University of Aeronautics and Astronautics,2007,33(8): 878-881,893. (in Chinese
CAO Zhipeng, LIU Bo, DING Wei. Stator setting angles adjustment on performance improvement of axial-centrifugal compressor[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(8): 878-881, 893. (in Chinese)
|
| [8] |
王赫,杨纯辉,韩文俊,等. 核心机压气机进口可调静子叶片角度控制规律[J]. 航空发动机,2022,48(3): 20-24. WANG He,YANG Chunhui,HAN Wenjun,et al. Control law of compressor inlet variable stator vanes angle of a core engine[J]. Aeroengine,2022,48(3): 20-24. (in Chinese
WANG He, YANG Chunhui, HAN Wenjun, et al. Control law of compressor inlet variable stator vanes angle of a core engine[J]. Aeroengine, 2022, 48(3): 20-24. (in Chinese)
|
| [9] |
POHL D,JANSSEN J,JESCHKE P,et al. Variable stator vane penny gap aerodynamic measurements and numerical analysis in an annular cascade wind tunnel[J]. International Journal of Gas Turbine,Propulsion and Power Systems,2020,11(2): 44-55. doi: 10.38036/jgpp.11.2_44
|
| [10] |
WOLLMANN T,NITSCHKE S,KLAUKE T,et al. Investigating the friction,wear and damage behaviour of plain bearing bushes of the variable stator vane system[J]. Tribology International,2022,165: 107280. doi: 10.1016/j.triboint.2021.107280
|
| [11] |
杨伟,徐伟. ADAMS参数化分析在高压压气机调节机构设计中的初步应用[J]. 燃气涡轮试验与研究,2012,25(4): 20-24. YANG Wei,XU Wei. Preliminary application of parameterized analysis based on ADAMS in VSV’s adjusting mechanism design of high pressure compressor[J]. Gas Turbine Experiment and Research,2012,25(4): 20-24. (in Chinese
YANG Wei, XU Wei. Preliminary application of parameterized analysis based on ADAMS in VSV’s adjusting mechanism design of high pressure compressor[J]. Gas Turbine Experiment and Research, 2012, 25(4): 20-24. (in Chinese)
|
| [12] |
张晓宁,赵雷,杨勇刚. 联调机构虚拟样机运动学动力学仿真[J]. 航空发动机,2014,40(4): 56-60. ZHANG Xiaoning,ZHAO Lei,YANG Yonggang. Kinematics and dynamics simulation of jointly adjusting mechanism based on virtual prototype technology[J]. Aeroengine,2014,40(4): 56-60. (in Chinese
ZHANG Xiaoning, ZHAO Lei, YANG Yonggang. Kinematics and dynamics simulation of jointly adjusting mechanism based on virtual prototype technology[J]. Aeroengine, 2014, 40(4): 56-60. (in Chinese)
|
| [13] |
张少平,杨川,张一彬. 压气机静叶调节机构的柔性多体建模及仿真[J]. 燃气涡轮试验与研究,2018,31(4): 12-18. ZHANG Shaoping,YANG Chuan,ZHANG Yibin. Modeling and simulation of the adjusting mechanism of stators through flexible multibody approach[J]. Gas Turbine Experiment and Research,2018,31(4): 12-18. (in Chinese
ZHANG Shaoping, YANG Chuan, ZHANG Yibin. Modeling and simulation of the adjusting mechanism of stators through flexible multibody approach[J]. Gas Turbine Experiment and Research, 2018, 31(4): 12-18. (in Chinese)
|
| [14] |
郑彦,钟明桥. 联动环支架间隙和数量对静子叶片调节精度的影响[J]. 燃气涡轮试验与研究,2020,33(5): 20-25. ZHENG Yan,ZHONG Mingqiao. Analysis of clearance and number influence of linkage ring brackets on stator vane adjustment accuracy[J]. Gas Turbine Experiment and Research,2020,33(5): 20-25. (in Chinese
ZHENG Yan, ZHONG Mingqiao. Analysis of clearance and number influence of linkage ring brackets on stator vane adjustment accuracy[J]. Gas Turbine Experiment and Research, 2020, 33(5): 20-25. (in Chinese)
|
| [15] |
张哲,王汉平,孙浩然,等. VSV调节机构阻滞力和调节精度的归因分析[J]. 航空学报,2020,41(12): 380-390. ZHANG Zhe,WANG Hanping,SUN Haoran,et al. Attribution analysis of blocking force and adjustment accuracy of adjusting mechanism of variable stator vane[J]. Acta Aeronautica et Astronautica Sinica,2020,41(12): 380-390. (in Chinese
ZHANG Zhe, WANG Hanping, SUN Haoran, et al. Attribution analysis of blocking force and adjustment accuracy of adjusting mechanism of variable stator vane[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(12): 380-390. (in Chinese)
|
| [16] |
张宝振,王汉平,徐峰,等. VSV调节机构的仿真提速和精度补偿措施研究[J]. 航空学报,2022,43(9): 499-512. ZHANG Baozhen,WANG Hanping,XU Feng,et al. Research on simulation speed-up and accuracy compensation measures of adjusting mechanism of variable stator vane[J]. Acta Aeronautica et Astronautica Sinica,2022,43(9): 499-512. (in Chinese
ZHANG Baozhen, WANG Hanping, XU Feng, et al. Research on simulation speed-up and accuracy compensation measures of adjusting mechanism of variable stator vane[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(9): 499-512. (in Chinese)
|
| [17] |
张学宝,张一彬,孙登科,等. 基于系统工程的压气机调节机构精益研发[J]. 航空动力,2022(1): 55-58. ZHANG Xuebao,ZHANG Yibin,SUN Dengke,et al. Lean research and development of compressor adjusting mechanism based on systems engineering[J]. Aerospace Power,2022(1): 55-58. (in Chinese
ZHANG Xuebao, ZHANG Yibin, SUN Dengke, et al. Lean research and development of compressor adjusting mechanism based on systems engineering[J]. Aerospace Power, 2022(1): 55-58. (in Chinese)
|
| [18] |
张延,陈栋权,欧阳醌,等. 航空发动机可调叶片角度校准工装设计方法[J]. 航空精密制造技术,2019,55(5): 21-27. ZHANG Yan,CHEN Dongquan,OU Yangkun,et al. Analysis of calibration tooling design about adjustable stator blade angle[J]. Aviation Precision Manufacturing Technology,2019,55(5): 21-27. (in Chinese
ZHANG Yan, CHEN Dongquan, OU Yangkun, et al. Analysis of calibration tooling design about adjustable stator blade angle[J]. Aviation Precision Manufacturing Technology, 2019, 55(5): 21-27. (in Chinese)
|