[1] ZHAO H, JIANG Z M, DING H. Tool path planning for profiling grinding of aero-engine blade edge[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(10): 524318 (in Chinese). 赵欢, 姜宗民, 丁汉. 航空发动机叶片叶缘随形磨抛刀路规划[J]. 航空学报, 2021, 42(10): 524318.
[2] YANG J J, ZHENG X M, YANG X Y. Load scatter factors affecting aero engine structure life[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(5): 524339 (in Chinese). 杨俊杰, 郑小梅, 杨兴宇. 影响航空发动机结构寿命的载荷分散系数[J]. 航空学报, 2021, 42(5): 524339.
[3] ZHAO F T, JING X D, YANG M S, et al. Experimental study of rotor blades vibration and noise in multistage high pressure compressor and their relevance[J]. Chinese Journal of Aeronautics, 2020, 33(3): 870-878.
[4] ZHANG S, ZHANG Q B, ZHANG X M. Identification of foreign object impact on aero-engine fan blades with variance analysis[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(5): 524196 (in Chinese). 张帅, 张强波, 张霞妹. 基于方差分析的航空发动机风扇叶片外物撞击识别[J]. 航空学报, 2021, 42(5): 524196.
[5] WANG W M, CHEN Z W, ZHANG X L, et al. Fault diagnosis method of rotor rubbing impact based on blade tip timing[J/OL]. Acta Aeronautica et Astronautica Sinica, (2021-02-26)[2021-06-23].
http://kns.cnki.net/kcms/detail/11.1929.v.20210225.1634.032.html. DOI:
10.7527/S1000-6893.2021.25031.(inChinese). 王维民, 陈子文, 张旭龙, 等. 基于叶端定时的转子碰摩故障诊断方法[J/OL]. 航空学报, (2021-02-26)[2021-06-23].
http://kns.cnki.net/kcms/detail/11.1929.v.20210225.1634.032.html. DOI:
10.7527/S1000-6893.2021.25031.
[6] BUNKER R S. Axial turbine blade tips: Function, design, and durability[J]. Journal of Propulsion and Power, 2006, 22(2): 271-285.
[7] BOOTH T C, DODGE P R, HEPWORTH H K. Rotor-tip leakage: Part Ⅰ—basic methodology[J]. Journal of Engineering for Gas Turbines and Power, 1982, 104(1): 154-161.
[8] HUANG C F, HOU M J. Technology for measurement of blade tip clearance in an aeroengine[C]//Proceedings of the 2008 Aeronautical Test Technology Summit, 2008: 35-40, 47 (in Chinese). 黄春峰, 侯敏杰. 航空发动机叶尖间隙测量技术研究[C]//2008年航空试验测试技术峰会论文集, 2008: 35-40, 47.
[9] WISEMAN M W, GUO T H. An investigation of life extending control techniques for gas turbine engines[C]//Proceedings of the 2001 American Control Conference. (Cat. No. 01CH37148). Piscataway: IEEE Press, 2001: 3706-3707.
[10] HAO J. The investigation about civil aviation engine surge problem: The final solution for PW4000-94"engine group 3 surge[C]//The 13th session of the 15th Annual meeting of China Association for Science and Technology: Proceedings of the Aeroengine Design, Manufacturing and Application Technology Symposium, 2013: 8-12 (in Chinese). 郝杰. 民用航空发动机喘振问题研究: 普惠PW4000-94英寸发动机第三类喘振最终解决措施[C]//第十五届中国科协年会第13分会场: 航空发动机设计、制造与应用技术研讨会论文集, 2013: 8-12.
[11] XIE F. Effect of tip clearance on stall and circumferential single grooves improving the stability on axial-flow compressors[D]. Xi'an: Northwestern Polytechnical University, 2015: 3-10 (in Chinese). 谢芳. 轴流压气机叶尖间隙影响失速的机理及周向单槽机匣处理扩稳研究[D]. 西安: 西北工业大学, 2015: 3-10.
[12] DANISH S N, QURESHI S R, IMRAN M M, et al. Effect of tip clearance and rotor-stator axial gap on the efficiency of a multistage compressor[J]. Applied Thermal Engineering, 2016, 99: 988-995.
[13] FRITH P C. The effect of compressor rotor tip crops on turboshaft engine performance[J]. Journal of Engineering for Gas Turbines and Power, 1994, 116(1): 184-189.
[14] GRAF M B, WONG T S, GREITZER E M, et al. Effects of nonaxisymmetric tip clearance on axial compressor performance and stability[J]. Journal of Turbomachinery, 1998, 120(4): 648-661.
[15] SHAO H J. Investigation on the turbine blade tip clearance measurement active clearance control and dumping identification[D]. Beijing: Beijing University of Chemical Technology, 2017: 3 (in Chinese). 邵化金. 涡轮叶片叶尖间隙监测、主动控制与阻尼识别方法研究[D]. 北京: 北京化工大学, 2017: 3.
[16] WU J, WEN B, ZHANG Q, et al. A novel blade tip clearance measurement method based on event capture technique[J]. Mechanical Systems and Signal Processing, 2020, 139: 106626.
[17] SANG Z L. Experimental study on influence of blade tip geometries on the tip clearance flow of compressor cascade[D]. Dalian: Dalian Maritime University, 2017: 12 (in Chinese). 桑则林. 叶尖几何形状对压气机叶栅间隙流场影响的实验研究[D]. 大连: 大连海事大学, 2017: 12.
[18] ZHANG J L. Research on blade tip clearance and blade tip-timing measurement based on microwave sense[D]. Tianjin: Tianjin University, 2017: 13 (in Chinese). 张济龙. 基于微波传感的叶尖间隙及叶尖定时测量方法研究[D]. 天津: 天津大学, 2017: 13.
[19] YE L Q. Research on transient response of blade tip clearance of high pressure turbine based on temperature and revolution[D]. Guanghan: Civil Aviation Flight University of China, 2020: 2-6 (in Chinese). 叶林青. 基于温度和转速的高压涡轮叶尖间隙瞬态响应研究[D]. 广汉: 中国民用航空飞行学院, 2020: 2-6.
[20] LATTIME S, STEINETZ B. Turbine engine clearance control systems: Current practices and future directions[C]//38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2002.
[21] XIANG HH, GE N, GAO J, et al. Effect of circumferential non-uniform tip clearance on performance of axial compressor[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(2): 121491 (in Chinese). 向宏辉, 葛宁, 高杰, 等. 周向非均匀叶尖间隙对轴流压气机性能的影响[J]. 航空学报, 2018, 39(2): 121491.
[22] ZHENG C, ZHU M C. Application of image measuring technology in blade tip clearance measurement[J]. Journal of Applied Optics, 2014, 35(5): 835-840 (in Chinese). 郑臣, 朱目成. 影像测量技术在叶尖间隙测量中的应用[J]. 应用光学, 2014, 35(5): 835-840.
[23] MIL-HDBK-1783B Engine structural integrity program (ENSIP)[S]. Washington, D.C. : Department of Defense, 2004.
[24] ZHANG B C. Aeroengine test technologies[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2005: 29-32 (in Chinese). 张宝诚. 航空发动机试验和测试技术[M]. 北京: 北京航空航天大学出版社, 2005: 29-32.
[25] MA Y Z. The key technique research of blade tip clearance measurement for rotational blades[D]. Tianjin: Tianjin University, 2007: 1-3 (in Chinese). 马玉真. 旋转叶片叶尖间隙测量的关键技术研究[D]. 天津: 天津大学, 2007: 1-3.
[26] LIU Y, TAN L, WANG B. A review of tip clearance in propeller, pump and turbine[J]. Energies, 2018, 11(9): 2202.
[27] YU B, KE H W, SHEN E Y, et al. A review of blade tip clearance-measuring technologies for gas turbine engines[J]. Measurement and Control, 2020, 53(3-4): 339-357.
[28] JIA B H, HE L, FENG Y, et al. The development of aero-engine tip-clearance measurement technology: A simple review[C]//2017 13th IEEE International Conference on Electronic Measurement & Instruments (ICEMI). Piscataway: IEEE Press, 2017: 565-570.
[29] CAO S Z. Research on rotating blade tip clearancenoncontacting measurement in the aero-engine[D]. Tianjin: Tianjin University, 2007: 10-11 (in Chinese). 曹素芝. 发动机叶片叶尖间隙非接触检测技术研究[D]. 天津: 天津大学, 2007: 10-11.
[30] MASLOVSKIY A, BAKULIN M, SNITKO M. Microwave blade tip clearance measurements: Principles, current practices and future opportunities[C]//Proceedings of ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, 2013: 849-853.
[31] DENG C. Research on rotating blade tip clearance signal acquisition & high speed data acquisition & processing technology[D]. Tianjin: Tianjin University, 2018: 13-20 (in Chinese). 邓澈. 旋转叶片叶尖间隙信号获取及高速采集处理技术研究[D]. 天津: 天津大学, 2018: 13-20.
[32] DAVIDSON D P, DEROSE R D, WENNERSTROM A J. The measurement of turbomachinery stator-to-drum running clearances[C]//Proceedings of ASME 1983 International Gas Turbine Conference and Exhibit, 2015.
[33] SHEARD A G, TURNER S R. Electromechanical measurement of turbomachinery blade tip-to-casing running clearance[C]//Proceedings of ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, 2015.
[34] SHEARD A G, KILLEEN B. A blade-by-blade tip clearance measurement system for gas turbine applications[J]. Journal of Engineering for Gas Turbines and Power, 1995, 117(2): 326-331.
[35] WATANABE T, MATSUKI M. Study of tip clearance measurement system[J]. Transactions of the Japan Society of Mechanical Engineers Series C, 1994, 60(574): 2090-2095.
[36] WATANABE T. Measurement of tip clearance of all blades and the maximum tip clearance using discharge-type tip clearance measurement system[J]. Transactions of the Japan Society of Mechanical Engineers Series C, 2001, 67(657): 1478-1483.
[37] YU B, WANG J Q, SHEN E Y, et al. Blade tip gap measuring system and method based on AC discharging: China, CN106091914B[P]. 2017-12-22 (in Chinese). 于兵, 王继强, 申恩玉, 等. 一种基于交流放电的叶尖间隙测量系统及测量方法: 中国, CN106091914B[P]. 2017-12-22.
[38] YU B, ZHANG T, KE H W, et al. Research on the tip clearance measuring method based on AC discharge[J]. IEEE Access, 2020, 8: 60355-60363.
[39] AOKI S, TESHIMA K, ARAI M, et al. Results from the phase Ⅱ test using the high-temperature developing unit (HTDU)[J]. Journal of Engineering for Gas Turbines and Power, 1988, 110(2): 251-258.
[40] XIONG Y F. Rotor tip-clearance measurement in aeroengine[J]. Measurement & Control Technology, 2004, 23(1): 5-7 (in Chinese). 熊宇飞. 航空发动机转子叶尖间隙测量[J]. 测控技术, 2004, 23(1): 5-7.
[41] DHADWAL H S, MEHMUD A, KHAN R, et al. Integrated fiber optic light probe: Measurement of static deflections in rotating turbomachinery[J]. Review of Scientific Instruments, 1996, 67(2): 546-552.
[42] MA Y Z, DUAN F J, CAO S Z, et al. Optical fiber sensor for blade tip clearance measurement[J]. Opto-Electronic Engineering, 2005, 32(7): 85-88 (in Chinese). 马玉真, 段发阶, 曹素芝, 等. 叶片叶尖间隙测量的光纤传感器[J]. 光电工程, 2005, 32(7): 85-88.
[43] MA Y Z, DUAN F J, WANG Z, et al. Application of optical fiber sensor in tip clearance measurement[J]. Chinese Journal of Sensors and Actuators, 2007, 20(12): 2724-2727 (in Chinese). 马玉真, 段发阶, 王仲, 等. 光纤传感器在叶尖间隙测量中的应用[J]. 传感技术学报, 2007, 20(12): 2724-2727.
[44] GARCÍA I, BELOKI J, ZUBIA J, et al. An optical fiber bundle sensor for tip clearance and tip timing measurements in a turbine rig[J]. Sensors, 2013, 13(6): 7385-7398.
[45] DURANA G, AMOREBIETA J, FERNANDEZ R, et al. Design, fabrication and testing of a high-sensitive fibre sensor for tip clearance measurements[J]. Sensors, 2018, 18(8): 2610.
[46] YANG S D, YANG X, LIU Q R. Analysis of elimination effect of shape factor of reflecting surface by end structure of optical fiber sensor[J]. Measurement & Control Technology, 2020, 39(2): 14-19 (in Chinese). 杨盛德, 杨训, 刘悄然. 光纤传感器端面结构对反射面形状因子的消除作用分析[J]. 测控技术, 2020, 39(2): 14-19.
[47] JIA B H, FENG Y, JIA W H. Application of optical sensor with two-circle reflective coaxial fiber in tip clearance measurement[J]. Laser & Optoelectronics Progress, 2015, 52(10): 100603 (in Chinese). 贾丙辉, 冯勇, 贾文华. 双圈同轴式光纤传感器在叶尖间隙测量中的应用[J]. 激光与光电子学进展, 2015, 52(10): 100603.
[48] JIA B H, HE L. An optical fiber measurement system for blade tip clearance of engine[J]. International Journal of Aerospace Engineering, 2017, 2017: 1-9.
[49] XIE S Y, ZHANG X D, XIONG Y W, et al. Design and modeling of three-dimensional tip clearance optical probe[J]. Chinese Journal of Scientific Instrument, 2018, 39(11): 180-187 (in Chinese). 谢思莹, 张小栋, 熊逸伟, 等. 三维叶尖间隙光纤探头设计及输出特性研究[J]. 仪器仪表学报, 2018, 39(11): 180-187.
[50] ZHANG X D, XIONG Y W, XIE S Y, et al. Optical-fiber-based dynamic measurement system for 3D tip clearance of rotating blades[J]. Optics Express, 2019, 27(22): 32075-32095.
[51] LIU H C, ZHANG X D, XIONG Y W, et al. Design andanalysis of grouped symmetric optical fiber sensor for demodulating three-dimensional tip clearance[J]. Chinese Journal of Sensors and Actuators, 2020, 33(4): 485-491 (in Chinese). 刘洪成, 张小栋, 熊逸伟, 等. 解调三维叶尖间隙的分组对称光纤传感器设计与分析[J]. 传感技术学报, 2020, 33(4): 485-491.
[52] FORD M J, HONEYCATT R E, NORDLUND R E, et al. Advanced optical blade tip clearance measurement system: NASA CR-159402[R]. West Palm Beach: NASA, 1978.
[53] BARRANGER J P, FORD M J. Laser-optical blade tip clearance measurement system[J]. Journal of Engineering for Gas Turbines and Power, 1981, 103(2): 457-460.
[54] BI S M. Technology for measurement of blade tip clearance in the gas turbine[D]. Harbin: Harbin Engineering University, 2011: 38-42 (in Chinese). 毕思明. 燃气轮机叶尖间隙测量技术研究[D]. 哈尔滨: 哈尔滨工程大学, 2011: 38-42.
[55] DHADWAL H S, KURKOV A P. Dual-laser probe measurement of blade-tip clearance[J]. Journal of Turbomachinery, 1999, 121(3): 481-485.
[56] YE D C, DUAN F J, OUYANG T, et al. Blade tip clearance measurement using tip timing of multi-beam[J]. Journal of Optoelectronics Laser, 2011, 22(4): 570-573 (in Chinese). 叶德超, 段发阶, 欧阳涛, 等. 基于多光束叶尖定时原理的叶尖间隙测量技术[J]. 光电子·激光, 2011, 22(4): 570-573.
[57] WANG K. Rotating blade tip clearance measuring technique using blade tip-timing and dual-frequency laser phase ranging[D]. Tianjin: Tianjin University, 2014: 31-39 (in Chinese). 王凯. 基于叶尖定时和双频激光相位测距的叶尖间隙测量技术[D]. 天津: 天津大学, 2014: 31-39.
[58] DUAN F J, ZHANG J L, JIANG J J, et al. Method to improve the blade tip-timing accuracy of fiber bundle sensor under varying tip clearance[J]. Optical Engineering, 2016, 55(1): 014106.
[59] DIAMOND D H, HEYNS P S, OBERHOLSTER A J. Constant speed tip deflection determination using the instantaneous phase of blade tip timing data[J]. Mechanical Systems and Signal Processing, 2021, 150: 107151.
[60] PFISTER T, BVTTNER L, CZARSKE J. Laser Doppler profile sensor with sub-micrometre position resolution for velocity and absolute radius measurements of rotating objects[J]. Measurement Science and Technology, 2005, 16(3): 627-641.
[61] NEUMANN M, DREIER F, GUNTHER P, et al. A laser-optical sensor system for blade vibration detection of high-speed compressors[J]. Mechanical Systems and Signal Processing, 2015, 64-65: 337-346.
[62] PFISTER T, BVTTNER L, CZARSKE J, et al. Turbo machine tip clearance and vibration measurements using a fibre optic laser Doppler position sensor[J]. Measurement Science and Technology, 2006, 17(7): 1693-1705.
[63] PFISTER T, BVTTNER L, CZARSKE J, et al. Fiber optic laser Doppler distance sensor for in-situ tip clearance and vibration monitoring of turbo machines[C]//Proceedings of the 14th International Symposium on Applications of Laser Techniques to Fluid Mechanics, 2008: 1-6.
[64] LIU YY, LI L, HUANG Y F. The use of diffractive elements in Doppler tip clearance detection system[J]. Optical Technique, 2011, 37(3): 381-384 (in Chinese). 刘园园, 李林, 黄一帆. 衍射透镜在多普勒叶尖间隙检测系统中的应用[J]. 光学技术, 2011, 37(3): 381-384.
[65] KEMPE A, SCHLAMP S, RÖSGEN T, et al. Low-coherence interferometric tip-clearance probe[J]. Optics Letters, 2003, 28(15): 1323-1325.
[66] VAKHTIN A, CHEN S J, MASSICK S. Optical probe for monitoring blade tip clearance[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2009: 507.
[67] YE D C. Tip clearance measurements of rotating blades using dual frequency laser with large frequency difference[D]. Tianjin: Tianjin University, 2012: 13-27 (in Chinese). 叶德超. 基于大频差双频激光的旋转叶片叶尖间隙测量技术[D]. 天津: 天津大学, 2012: 13-27.
[68] WANG K, DUAN F J, GUO H T, et al. Blade tip clearance measurement using dual frequency laser with large frequency difference[J]. Journal of Optoelectronics Laser, 2013, 24(10): 1984-1988 (in Chinese). 王凯, 段发阶, 郭浩天, 等. 基于大频差双频激光的发动机叶尖间隙测量技术[J]. 光电子·激光, 2013, 24(10): 1984-1988.
[69] GUO H T, DUAN F J, WU G X, et al. Blade tip clearance measurement of the turbine engines based on a multi-mode fiber coupled laser ranging system[J]. Review of Scientific Instruments, 2014, 85(11): 115105.
[70] BI C, LI D, FANG J G, et al. Application of chromatic confocal displacement sensor in measurement of tip clearance[C]//Proc SPIE 10155, Optical Measurement Technology and Instrumentation, 2016, 1015: 101551S.
[71] Hood Technology. Sensors[EB/OL]. (2010-05-07)[2021-06-23].
https://www.hoodtech.com/bvm/sensors.html.
[72] SMARTMENS. Optical fiber sensor[EB/OL]. (2016-09-02)[2021-06-23].
http://www.smartmens.com/product/277384094 (in Chinese). 善测(天津)科技有限公司. 光纤传感器[EB/OL]. (2016-09-02)[2021-06-23].
http://www.smartmens.com/pro-duct/277384094.
[73] И. Е. Заблоцкий. Noncontact vibration measurement on turbines rotor blades[M]. WU S X, ZHENG S C, translated. Beijing: National Defense Industry Press, 1986: 75-81 (in Chinese). И. Е. 萨勃洛斯基. 涡轮机叶片振动的非接触测量[M]. 吴士祥郑叔琛, 译. 北京: 国防工业出版社, 1986: 75-81.
[74] SARMA G R, BARRANGER J P. Capacitance-type blade-tip clearance measurement system using a dual amplifier with ramp/DC inputs and integration[J]. IEEE Transactions on Instrumentation and Measurement, 1992, 41(5): 674-678.
[75] HAASE W C, HAASE Z S. High-Speed, capacitance-based tip clearance sensing[C]//2013 IEEE Aerospace Conference. Big Sky, MT, USA. Piscataway: IEEE Press, 2013: 1-8.
[76] SATISH T N, VIVEK A, ANAGHA S N, et al. Novel resistor-capacitor (RC) network-based capacitance signal conditioning circuit for tip clearance measurement on gas turbine engine[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 234(2): 342-360.
[77] BARRANGER J P. Low-cost FM oscillator for capacitance type of blade tip clearance measurement system: TP-2746[R]. Cleveland: NASA, 1987.
[78] LONG C, DUAN F J, OUYANG T. Application of superheterodyne FM reception in measurement of blade tip clearance[J]. Transducer and Microsystem Technologies, 2009, 28(3): 108-110 (in Chinese). 龙成, 段发阶, 欧阳涛. 超外差调频接收技术在叶尖间隙测量中的应用[J]. 传感器与微系统, 2009, 28(3): 108-110.
[79] DUAN F J, YE D C, LONG C. Technique for capacitance-type blade tip clearance measurement based on PLL carrier frequency tracking[J]. Journal of Tianjin University, 2011, 44(4): 283-286 (in Chinese). 段发阶, 叶德超, 龙成. 基于PLL载频跟踪的电容式叶尖间隙测量技术[J]. 天津大学学报, 2011, 44(4): 283-286.
[80] ADDABBO T, FORT A, MUGNAINI M, et al. A system for the dynamic response characterization of turbomachinery tip clearance measurement instruments based on capacitive probes[C]//2015 IEEE Sensors Applications Symposium (SAS). Piscataway: IEEE Press, 2015: 1-5.
[81] CHIVERS J. A technique for the measurement of blade tip clearance in a gas turbine[C]//25th Joint Propulsion Conference. Reston: AIAA, 1989.
[82] MU¨LLER D, SHEARD A G, MOZUMDAR S, et al. Capacitive measurement of compressor and turbine blade tip to casing running clearance[J]. Journal of Engineering for Gas Turbines and Power, 1997, 119(4): 877-884.
[83] SHEARD A G. Blade by blade tip clearance measurement[J]. International Journal of Rotating Machinery, 2011, 2011: 1-13.
[84] ROTADATA. Capacitance probes overview[EB/OL]. (2021-06-23)[2021-06-23].
https://www.rotadata.com/Blade_Tip_Clearance_Capacitance_Probes.
[85] LAWSON C P, IVEY P C. Tubomachinery blade vibration amplitude measurement through tip timing with capacitance tip clearance probes[J]. Sensors and Actuators A: Physical, 2005, 118(1): 14-24.
[86] BARRANGER J. An in-place recalibration technique to extend the temperature capability of capacitance-sensing, rotor-blade-tip-clearance measurement systems[C]//SAE Technical Paper Series. 400 Commonwealth Drive. Warrendale: SAE International, 1978: 781003.
[87] FOGALE TURBO. Capablade fusion with MC925[EB/OL]. (2021-06-23)[2021-06-23].
http://www.fogale.fr/turbomachinery/index.php.
[88] SMARTMENS. BCMS[EB/OL]. (2016-09-02)[2021-06-23].
http://www.smartmens.com/product/277384485 (in Chinese). 善测(天津)科技有限公司. 叶尖间隙测量系统[EB/OL]. (2016-09-02)[2021-06-23].
http://www.smartmens.com/product/277384485.
[89] ZHANG X, DUAN F J, YE D C, et al. Tip clearance signal processing method for rotary blade based on RMS[J]. Automation & Instrumentation, 2019, 34(11): 42-46 (in Chinese). 张鑫, 段发阶, 叶德超, 等. 基于RMS的旋转叶片叶尖间隙信号处理方法[J]. 自动化与仪表, 2019, 34(11): 42-46.
[90] SHAO X C, DUAN F J, JIANG J J, et al. Denoising method of blade tip clearance signal based on adaptive moving average and wavelet threshold[J]. Chinese Journal of Sensors and Actuators, 2021, 34(1): 34-40 (in Chinese). 邵兴臣, 段发阶, 蒋佳佳, 等. 基于自适应滑动均值和小波阈值的叶尖间隙信号降噪方法[J]. 传感技术学报, 2021, 34(1): 34-40.
[91] LI J, GUO G H, DUAN F J, et al. A novel self-adaptive, multi-peak detection algorithm for blade tip clearance measurement based on a capacitive probe[J]. Measurement Science and Technology, 2021, 32(8): 085006.
[92] RICKMAN J. Eddy current turbocharger blade speed detection[J]. IEEE Transactions on Magnetics, 1982, 18(5): 1014-1021.
[93] ROESELER C, VON FLOTOW A, TAPPERT P. Monitoring blade passage in turbomachinery through the engine case (no holes)[C]//Proceedings, IEEE Aerospace Conference. Piscataway: IEEE Press, 2002: 6.
[94] HAASE W C, HAASE Z S. Advances in through-the-case eddy current sensors[C]//2013 IEEE Aerospace Conference. Piscataway: IEEE Press, 2013: 1-5.
[95] TOMASSINI R, ROSSI G, BROUCKAERT J F. Blade tip clearance and blade vibration measurements using a magnetoresistive sensor[C]//Proceedings of the 11th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, 2015: 256.
[96] TOMASSINI R. Blade tip timing and blade tip clearance measurement system based on magnetoresistive Sensors[D]. Padova: Università degli Studi di Padova, 2016: 83-90.
[97] TOMASSINI R, ROSSI G, BROUCKAERT J F. On the development of a magnetoresistive sensor for blade tip timing and blade tip clearance measurement systems[J]. Review of Scientific Instruments, 2016, 87(10): 102505.
[98] DUAN F J, HUANG T T, JIANG J J, et al. High-speed vortex sensor: China, CN107121153A[P]. 2017-09-01 (in Chinese). 段发阶, 黄婷婷, 蒋佳佳, 等. 高速电涡流传感器: 中国, CN107121153A[P]. 2017-09-01.
[99] SUTCLIFFE H. Principles of eddy-current distance gauges[J]. Proceedings of the Institution of Electrical Engineers, 1977, 124(5): 479.
[100] WANG W M, SHANG W, YAO J F, et al. A blade tip-timing measurement study basedon eddy current technology[J]. Journal of Beijing University of Chemical Technology (Natural Science Edition), 2014, 41(3): 102-107 (in Chinese). 王维民, 尚文, 姚剑飞, 等. 基于电涡流技术的叶尖间隙及定时测量研究[J]. 北京化工大学学报(自然科学版), 2014, 41(3): 102-107.
[101] WANG W M, SHAO H J, CHEN L F, et al. Investigation on the turbine blade tip clearance monitoring based on eddy current pulse-trigger method[C]//Proceedings of ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, 2016.
[102] WANG W M, SHAO H J, CHEN L F, et al. Investigation on the blade tip clearance monitoring of turbomachinery based on the pulse-trigger method[J]. Journal of Vibration, Measurement & Diagnosis, 2017, 37(3): 583-587, 634 (in Chinese). 王维民, 邵化金, 陈立芳, 等. 基于触发脉冲的涡轮机械叶尖间隙监测方法[J]. 振动测试与诊断, 2017, 37(3): 583-587, 634.
[103] SMARTMENS. Condition Monitoring and Health Management of Rotating Machinery[EB/OL]. (2016-09-02)[2021-06-23].
http://www.smartmens.com/xzjxztjchjkgl (in Chinese). 善测(天津)科技有限公司. 旋转机械状态监测和健康管理[EB/OL]. (2016-09-02)[2021-06-23].
http://www.smartmens.com/xzjxztjchjkgl.
[104] CHANA K S, CARDWELL M T, SULLIVAN J S. The development of a hot section eddy current sensor for turbine tip clearance measurement[C]//Proceedings of ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. 2013.
[105] SRIDHAR V, CHANA K S. Tip-clearance measurements on an engine high pressure turbine using an eddy current sensor[C]//Proceedings of ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, 2017.
[106] DU L, ZHU X L, ZHE J. A high sensitivity inductive sensor for blade tip clearance measurement[J]. Smart Materials and Structures, 2014, 23(6): 065018.
[107] HAN Y, ZHONG C, ZHU X L, et al. Online monitoring of dynamic tip clearance of turbine blades in high temperature environments[J]. Measurement Science and Technology, 2018, 29(4): 045102.
[108] ZHAO Z Y, LIU Z X, LYU Y G, et al. Experimental investigation of high temperature-resistant inductive sensor for blade tip clearance measurement[J]. Sensors, 2018, 19(1): 61.
[109] ZHAO Z Y, LIU Z X, LV Y G, et al. Design and verification of high resolution eddy current sensor for blade tip clearance measurement[J]. Chinese Journal of Scientific Instrument, 2018, 39(6): 132-139 (in Chinese). 赵梓妤, 刘振侠, 吕亚国, 等. 高分辨率转子叶尖间隙测量传感器的设计及验证[J]. 仪器仪表学报, 2018, 39(6): 132-139.
[110] LIU Z X, ZHAO Z Y, LYU Y G, et al. Experimental investigation of inductive sensor characteristic for blade tip clearance measurement at high temperature[J]. Sensors, 2019, 19(17): 3694.
[111] BOROVIK S Y, PODLIPNOV P E, SEKISOV Y N, et al. Influence of disturbing factors in a system for measuring radial clearances in gas-turbine engines with temperature self-compensation[J]. Optoelectronics, Instrumentation and Data Processing, 2019, 55(4): 388-398.
[112] CHANA K S. Eddy current sensors: US 20100171491[P]. 2010-07-08.
[113] JIAO D, NI L W, ZHU X L, et al. Measuring gaps using planar inductive sensors based on calculating mutual inductance[J]. Sensors and Actuators A: Physical, 2019, 295: 59-69.
[114] WU J, WEN B, ZHOU Y, et al. Eddy current sensor system for blade tip clearance measurement based on a speed adjustment model[J]. Sensors, 2019, 19(4): 761.
[115] MANDACHE C, MCELHINNEY T, MRAD N. Aircraft engine blade tip monitoring using pulsed eddy current technology[C]//Proceedings of the 4th International Symposium on NDT in Aerospace, 2012: 1-9.
[116] GRZYBOWSKI R, FOYT G, KNOELL H, et al. Microwave blade tip clearance measurement system[C]//Proceedings of ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, 2015.
[117] WENGER J, NOWECK M, STOTZ M, et al. An MMIC-based microwave sensor for accurate clearance measurements in aircraft engines[C]//1997 27th European Microwave Conference. Piscataway: IEEE Press, 1997: 1122-1126.
[118] ASLINEZHAD M, A HEJAZI M. Turbine blade tip clearance determination using microwave measurement and k-nearest neighbour classifier[J]. Measurement, 2020, 151: 107142.
[119] ZHANG T, REN L, JU X Y, et al. Design of sensor for measuring turbine engine blade tip clearance[C]//2017 IEEE International Conference on Signal Processing, Communications and Computing (ICSPCC). Piscataway: IEEE Press, 2017: 1-5.
[120] LU X, TAN Q L. A new type of microwave blade tip clearance sensor[J]. Micronanoelectronic Technology, 2020, 57(1): 49-53, 65 (in Chinese). 路晓, 谭秋林. 一种新型微波叶尖间隙传感器[J]. 微纳电子技术, 2020, 57(1): 49-53, 65.
[121] WAGNER M, SCHULZE A, VOSSICK M, et al. Novel microwave vibration monitoring system for industrial power generating turbines[C]//1998 IEEE MTT-S International Microwave Symposium Digest (Cat. No. 98 CH36-192). Piscataway: IEEE Press, 1998: 1211-1214.
[122] VIOLETTI M, SKRIVERVIK A K, XU Q, et al. New microwave sensing system for blade tip clearance measurement in gas turbines[C]//Sensors, 2012 IEEE. Piscataway: IEEE Press, 2012: 1-4.
[123] NASA. New sensor gaining interest on industry radar screen[EB/OL]. (2003-01-01)[2021-06-23].
http://spinoff.nasa.gov/spinoff2003/ip_10.html.
[124] ZHANG J L, DUAN F J, NIU G Y, et al. A blade tip timing method based on a microwave sensor[J]. Sensors, 2017, 17(5): 1097.
[125] ZHANG J L, DUAN F J, NIU G Y. Blade tip clearance and blade tip timing measurement based on microwave sensors[J]. Control Engineering of China, 2019, 26(7): 1233-1238 (in Chinese). 张济龙, 段发阶, 牛广越. 基于微波传感器的叶尖间隙与叶尖定时测量[J]. 控制工程, 2019, 26(7): 1233-1238.
[126] PERZ M, PRZYSOWA R, DZIECIOL E. Turbojet engine blades health/maintenance monitoring using a microwave probe[C]//2006 International Conference on Microwaves, Radar & Wireless Communications. Piscataway: IEEE Press, 2006: 255-258.
[127] ROKICKI E, WERYN'SKI P, SZCZEPANIK R. Differential antenna: Poland, P391806[P]. 2008-09-01 (in Polish).
[128] SCHICHT A, HUBER K, ZIROFF A, et al. Absolute phase-based distance measurement for industrial monitoring systems[J]. IEEE Sensors Journal, 2009, 9(9): 1007-1013.
[129] XIE X J, WU Y H, ZHU Z Y. Design and calculation of microwave sensor for tip clearance measurement on aircraft engine[J]. Transducer and Microsystem Technologies, 2015, 34(5): 63-65 (in Chinese). 谢兴娟, 吴娅辉, 朱振宇. 航空发动机叶尖间隙测试微波传感器设计与计算[J]. 传感器与微系统, 2015, 34(5): 63-65.
[130] XIE X J, WU Y H. Analysis and simulation of microwave iip clearance measurement sensor[J]. Metrology & Measurement Technology, 2016, 36(6): 47-50 (in Chinese). 谢兴娟, 吴娅辉. 微波叶尖间隙测量传感器的计算分析[J]. 计测技术, 2016, 36(6): 47-50.
[131] ZHA X S, WU Y H. Design of digital down converter in microwave measurement system of tip clearance[J]. Radio Communications Technology, 2017, 43(6): 71-76 (in Chinese). 查祥胜, 吴娅辉. 叶尖间隙微波测量系统中数字下变频设计[J]. 无线电通信技术, 2017, 43(6): 71-76.
[132] PAN Y J. A pulse radar front-end research for tip clearance measurement[D]. Chengdu: University of Electronic Science and Technology of China, 2017: 26-54 (in Chinese). 潘跃静. 叶尖间隙微波测量系统前端研究[D]. 成都: 电子科技大学, 2017: 26-54.
[133] ZHAI D Y, XIE M, YUAN J D, et al. Application of high level synthesis in the blade tip clearance measurement system[C]//2018 11th International Congress on Image and Signal Processing, BioMedical Engineering and Informatics (CISP-BMEI). Piscataway: IEEE Press, 2018: 1-5.
[134] MASLOVSKIY A. Microwave turbine tip clearance measuring system for gas turbine engines[C]//Proceedings of ASME Turbo Expo 2008: Power for Land, Sea, and Air, 2009: 105-114.
[135] SCHICHT A, SCHWARZER S, SCHMIDT L P. Tip clearance measurement technique for stationary gas turbines using an autofocusing millimeter-wave synthetic aperture radar[J]. IEEE Transactions on Instrumentation and Measurement, 2012, 61(6): 1778-1785.
[136] NIU G Y, DUAN F J, ZHOU Q, et al. A dynamic measurement method of blade tip clearance by microwave phase difference ranging[J/OL]. Acta Aeronautica et Astronautica Sinica, (2021-04-06)[2021-06-23].
http://kns.cnki.net/kcms/detail/11.1929.V.20210429.1424.044.html. DOI:
10.7527/S10-00-6893.2021.25396.(inChinese). 牛广越, 段发阶, 周琦, 等. 基于微波相位差测距的叶尖间隙动态测量方法[J/OL]. 航空学报, (2021-04-06)[2021-06-23].
http://kns.cnki.net/kcms/detail/11.1929.V.20210429.1424.044.html. DOI:
10.7527/S10-00-6893.2021.25396.
[137] HOLST T A. Analysis of spatial filtering in phase-based microwave measurements of turbine blade tips[D]. Atlanta: Georgia Institute of Technology, 2005: 34-45.
[138] KWAPISZ D, HAFNER M, QUELOZ S. Calibration and characterization of a CW radar for blade tip clearance measurement[C]//The 7th European Radar Conference. Piscataway: IEEE Press, 2010: 320-323.
[139] YANG J S, XU G L, DONG W D, et al. Study on the signal calibration of microwave blade tip clearance sensor[J]. Chinese Journal of Scientific Instrument, 2018, 39(10): 193-201 (in Chinese). 杨季三, 徐贵力, 董文德, 等. 微波叶尖间隙传感器信号校准研究[J]. 仪器仪表学报, 2018, 39(10): 193-201.
[140] HOLMQUIST E B, JALBERT P L. Turbine blade tip clearance measurement instrumentation[C]//Proceedings of ASME Turbo Expo 2007: Power for Land, Sea, and Air, Montreal, 2009: 605-611.
[141] GEISHEIMER J, HOLST T. Novel sensors to enable closed-loop active clearance control in gas turbine engines[C]//SPIE Defense+Security. Proc SPIE 9083, Micro-and Nanotechnology Sensors, Systems, and Applications VI, 2014, 9083: 908310.
[142] ABDUL-AZIZ A, WOIKE M R, ANDERSON R C, et al. Propulsion health monitoring assessed by microwave sensor performance and blade tip timing[C]//Smart Structures and NDE for Energy Systems and Industry 4.0, 2019: 109730Q.
[143] STEINER A. Techniques for blade tip clearance measurements with capacitive probes[J]. Measurement S