Page 227 - 《振动工程学报》2026年第3期
P. 227

第 3 期                 唐新姿,等: 非谐分流叶片对离心压气机叶轮气弹稳定性影响分析                                       827

                   WANG  Yanzhong,  QI  Ronghua.  Aerodynamic  damp⁃  pressor[J]. Journal of Engineering for Thermal Energy
                   ing simulation of impeller with split blade[J]. Computer   and Power, 2022, 37(1): 49-56.
                   Simulation, 2019, 36(6): 77-82.              [16] 康达, 何卫东, 徐毅 . 分流叶片长度和周向位置对高
             [6] 郭雪莲, 李琳 . 亚声速叶片与跨声速叶片的气动阻尼                          压比离心压气机性能的影响[J]. 推进技术, 2020, 41
                   比较[J]. 推进技术, 2010, 31(3): 296-300.               (12): 2709-2719.
                   GUO  Xuelian,  LI  Lin.  Comparison  on  aerodynamic   KANG  Da,  HE  Weidong,  XU  Yi.  Effects  of  splitter
                   damping  between  subsonic  blade  and  transonic  blade  blade  length  and  circumferential  position  on  perfor⁃
                  [J]. Journal of Propulsion Technology, 2010, 31(3):   mance of high pressure ratio centrifugal compressor[J].
                   296-300.                                          Journal of Propulsion Technology, 2020, 41(12): 2709-
             [7] 杨晓东, 侯安平, 李漫露, 等 . 栅距非谐对跨声速压气                       2719.
                   机转子气动阻尼的影响[J]. 推进技术, 2017, 38(1):            [17] 陈春刘, 原野, 韩剑英, 等 . 分流叶片长度及周向位置
                   94-102.                                           对氢气离心压气机气动性能的影响[J]. 天津理工大学
                   YANG Xiaodong, HOU Anping, LI Manlu, et al. Ef⁃   学报,2025, 41(1): 29-35.
                   fects  of  pitch  mistuning  on  rotor  damping  of  transonic   CHEN Chunliu, YUAN Ye, HAN Jianying, et al. In⁃
                   compressor[J]. Journal of Propulsion Technology, 2017,   fluence of splitting blade length and circumferential posi⁃
                   38(1): 94-102.                                    tion  on  the  aerodynamic  performance  of  hydrogen  cen⁃
             [8] LENG  Y  J,  KEY  N  L.  Effects  of  nonuniform  blade   trifugal compressor[J]. Journal of Tianjin University of
                   spacing  on  compressor  rotor  forced  response  and  aero⁃  Technology, 2025, 41(1): 29-35.
                   acoustics[J].  Journal  of  Propulsion  and  Power,  2020,   [18] 冯瑞, 连晋毅, 李杰 . 分流叶片周向偏移对高速离心
                   36(5): 721-731.                                   压 气 机 内 部 流 场 和 性 能 的 影 响 分 析[J]. 机 械 设 计 ,
             [9] EKICI K, KIELB R E, HALL K C. The effect of aero⁃   2022, 39(8): 85-91.
                   dynamic asymmetries on turbomachinery flutter[J]. Jour⁃  FENG Rui, LIAN Jinyi, LI Jie. Analysis on influence
                   nal of Fluids and Structures, 2013, 36: 1-17.     of  circumferential  deviation  of  splitter  blade  on  internal
             [10] PHAN  H,  HE  L.  Phasing  structural  and  aerodynamic   flow  field  and  performance  of  high-speed  centrifugal
                   mistuning  for  leveraging  aeroelastic  performance[C]//  compressor[J].  Journal  of  Machine  Design,  2022,  39
                   ASME  Turbo  Expo  2022:  Turbomachinery  Technical   (8): 85-91.
                   Conference  and  Exposition.  Rotterdam,  Netherlands:   [19] LANE F. System mode shapes in the flutter of compres⁃
                   American  Society  of  Mechanical  Engineers,  2022:   sor  blade  rows[J].  Journal  of  the  Aeronautical  Scienc⁃
                   V08AT21A016.                                      es, 1956, 23(1): 54-66.
             [11] ZHANG W H, LIAO X L, FAN W Y, et al. Model⁃   [20] MOFFATT S, NING W, LI Y S, et al. Blade forced
                   ing of the unsteady aerodynamic force of turbine blades   response prediction for industrial gas turbines[J]. Jour⁃
                   considering  nonuniform  vane  pitch[J].  Physics  of  Flu⁃  nal of Propulsion and Power, 2005, 21(4): 707-714.
                   ids, 2024, 36: 017141.                       [21] 李颂, 杨新乐, 李惟慷, 等 . 叶片梯度角对压气机叶轮
             [12] 牛永红, 侯安平, 张明明, 等 . 非均匀静子布局对转子                      固 有 频 率 的 影 响 规 律[J]. 中 国 机 械 工 程 , 2022, 33
                   叶片振动的影响[J]. 推进技术, 2015, 36(7): 1078-1084.        (2): 243-251.
                   NIU  Yonghong,  HOU  Anping,  ZHANG  Mingming,    LI  Song,  YANG  Xinle,  LI  Weikang,  et  al.  Influence
                   et al. Effects of asymmetric vane spacing on rotor blade   laws  of  blade  gradient  angle  on  natural  frequency  of
                   vibration[J]. Journal of Propulsion Technology, 2015,   compressor  impellers[J].  China  Mechanical  Engineer⁃
                   36(7): 1078-1084.                                 ing, 2022, 33(2): 243-251.
             [13] 郑赟, 崔健, 高庆哲, 等 . 导叶非均匀布局对气动激励                 [22] BENDIKSEN O, KIELB R E, HALL K C. Turboma⁃
                   的影响[J]. 航空动力学报, 2022, 37(11): 2627-2635.          chinery aeroelasticity[J]. Encyclopedia of Aerospace En⁃
                   ZHENG Yun, CUI Jian, GAO Qingzhe, et al. Effects   gineering, 2010. DOI: 10.1002/9780470686652.
                   of inlet guide vanes asymmetry layouts on aerodynamic   [23] PHAN  H  M.  A  spatial-temporal  analysis  approach  for
                   excitation[J].  Journal  of  Aerospace  Power,  2022,  37  flutter  predictions  using  decoupled  and  fully-coupled
                  (11): 2627-2635.                                   methods[J].  Journal  of  Fluids  and  Structures,  2021,
             [14] SAJEDIN A, ALLPORT J, AMOOZGAR M, et al.           107: 103412.
                   Blade thickness effects on viscous flutter in a radial tur⁃  [24] DUAN  X  B,  CONG  J  Q,  DAI  Z  Z,  et  al.  Influence
                   bocharger  turbine[J].  Engineering  Failure  Analysis,   mechanism and quantificational evaluation of key factors
                   2022, 136: 106139.                                affecting flutter stability of a transonic fan[J]. Aerospace
             [15] 张书玮, 姜玉廷, 林洪飞, 等 . 分流叶片长度和周向位                      Science and Technology, 2023, 138: 108312.
                   置对氦氙离心压气机性能的影响[J]. 热能动力工程,
                                                                第一作者: 唐新姿(1981―),女,博士,教授。
                   2022, 37(1): 49-56.
                   ZHANG Shuwei, JIANG Yuting, LIN Hongfei, et al.       E-mail: xinzitang@163.com
                   Effects of splitter blade length and circumferential posi⁃  通信作者: 彭锐涛(1982―),男,博士,教授。
                   tion  on  performance  of  helium-xenon  centrifugal  com⁃  E-mail: pengruitao@163.com
   222   223   224   225   226   227   228   229   230   231   232