Page 223 - 《振动工程学报》2025年第11期
P. 223

第 11 期                  杨斯骞,等:基于叶尖定时的低转速动叶片裂纹在线识别方法                                        2681

                  Crack  fault  monitoring  of  high-speed  rotor  blades  based  on  569-580.
                  non-contact measurement[J]. Journal of Aerospace Power,1-  AO  Chunyan, QIAO  Baijie, LIU  Meiru, et  al.  Dynamic
                  12[2025-10-15]. https://doi.org/10.13224/j.cnki.jasp.20240726.  strain  reconstruction  method  of  rotating  blades  based  on  no-
              [8]  许敬晖,乔百杰,刘美茹,等. 基于叶端定时的转子叶片                       contact measurement[J]. Journal of Aerospace Power,2020,
                  裂纹监测与诊断     [J]. 推进技术,2022,43(2):374-382.         35(3):569-580.
                                                                [14]  ZHANG F Y,GUO S P,LI X J,et al. Characterization of
                  XU Jinghui,QIAO Baijie,LIU Meiru,et al. Crack moni-
                  toring and diagnosis of rotor blades using blade tip timing[J].  crack on the outer edge of the disk based on blade tip timing
                                                                    technology[J].  Measurement  Science  and  Technology,
                  Journal of Propulsion Technology,2022,43(2):374-382.
              [9]  WU S M,WANG Z K,LI H Q,et al. Blade crack detec-  2023,34(9):095119.
                                                                [15]  ZHANG F L,YU H T,WANG J J. A novel damage identifi-
                  tion  using  blade  tip  timing[J].  IEEE  Transactions  on  Instru-
                                                                    cation  method  for  flue  gas  turbine  blades  based  on  tip
                  mentation and Measurement,2021,70:6502813.
                                                                    timing[J]. ISA Transactions,2023,135:537-550.
              [10]  XU  J  H, QIAO  B  J, LIU  M  R, et  al.  Crack  propagation
                                                                [16]  DIAMOND  D  H, HEYNS  P  S, OBERHOLSTER  A  J.
                  monitoring   of   rotor   blades   using   synchroextracting
                                                                    Improved  blade  tip  timing  measurements  during  transient
                  transform[J].  Journal  of  Sound  and  Vibration, 2021, 509:
                                                                    conditions using a state space model[J]. Mechanical Systems
                  116253.
                                                                    and Signal Processing,2019,122:555-579.
              [11]  XU J H,QIAO B J,LIU M R,et al. Blade tip timing for
                                                                [17]  盛昌文,姜永正,黄磊,等. 基于叶尖定时的风机叶片裂
                  monitoring  crack  propagation  of  rotor  blades  using  Block-
                                                                    纹故障识别研究     [J]. 仪器仪表学报,2024,45(4):57-65.
                  AOLS[J].  Mechanical  Systems  and  Signal  Processing,
                                                                    SHENG Changwen,JIANG Yongzheng,HUANG Lei,et
                  2022,181:109498.
                                                                    al. Research on fan blade crack fault identification based on tip
              [12]  FAN Z F,LI H K,CAO H W,et al. Research on running
                                                                    timing[J].  Chinese  Journal  of  Scientific  Instrument, 2024,
                  status monitoring and rotating blade crack detection of large-
                                                                    45(4):57-65.
                  scale  centrifugal  compressor  based  on  blade  tip  timing  tech-
                  nique[J]. IEEE Transactions on Instrumentation and Measure-  第一作者:杨斯骞(2002—),男,硕士研究生。
                  ment,2022,72:3501011.                                 E-mail:1583792863@qq.com
              [13]  敖春燕,乔百杰,刘美茹,等. 基于非接触式测量的旋转                  通信作者:张继旺(1991—),男,博士,高级工程师。
                  叶片动应变重构方法        [J]. 航空动力学报,2020,35(3):              E-mail:zhangjiwang@csei.org.cn
   218   219   220   221   222   223   224   225   226   227   228