Influence of Rotor Tip Blockage on Near Stall Blade Vibrations in an Axial Compressor Rig

被引：15
|
作者：
Moeller, Daniel [1 ]
Juengst, Maximilian [1 ]
Schiffer, Heinz-Peter [1 ]
Giersch, Thomas [2 ]
Heinichen, Frank [2 ]
机构：
[1] Tech Univ Darmstadt, Inst Gas Turbines & Aerosp Prop, D-64287 Darmstadt, Germany
[2] Rolls Royce Deutschland, D-15827 Blankenfelde Mahlow, Germany
来源：
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 2018年 / 140卷 / 02期
关键词：
INTEGRATED NONLINEAR APPROACH; FORCED RESPONSE PREDICTION;
D O I：
10.1115/1.4038316
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
Rotor blade vibrations observed in the Darmstadt transonic compressor rig are investigated in this paper. The vibrations are nonsynchronous and occur in the near stall (NS) operating region. Rotor tip flow fluctuations traveling near the leading edge (LE) against the direction of rotation (in the rotor relative frame of reference) with about 50% blade tip speed are found to be the reason for the occurrence of the vibrations. The investigations show that the blockage at the rotor tip is an important factor for the aeroelastic stability of the compressor in the NS region. It is found that by application of a recirculating tip injection (TI) casing treatment, the aeroelastic stability increases as a result of reduced blockage in the rotor tip region.
引用
收藏
页数：12
相关论文
共 50 条
  • [21] Blockage development in a transonic, axial compressor rotor
    Suder, K.L.
    Journal of Turbomachinery, 1998, 120 (03): : 465 - 476
  • [22] STATOR-AVERAGED, ROTOR BLADE-TO-BLADE NEAR-WALL FLOW IN A MULTISTAGE AXIAL COMPRESSOR WITH TIP CLEARANCE VARIATION
    MOYLE, IN
    WALKER, GJ
    SHREEVE, RP
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1992, 114 (03): : 668 - 674
  • [23] A correlation for tip leakage blockage in compressor blade passages
    Hoeger, M
    Lahmer, M
    Dupslaff, M
    Fritsch, G
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 426 - 432
  • [24] INFLUENCE OF BLADE TIP FILLET STRUCTURE ON AERODYNAMIC PERFORMANCE OF A COMPRESSOR ROTOR
    Wang, Haohao
    Zhao, Lei
    Gao, Limin
    Li, Yongzeng
    Ma, Chi
    PROCEEDINGS OF THE ASME TURBO EXPO 2020: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2A, PT II, 2020,
  • [25] ON ROTOR BLADE LOADING AND TIP LEAKAGE PHENOMENA IN A LOW SPEED AXIAL COMPRESSOR WITH FORWARD BLADE SWEEP
    Ramakrishna, P., V
    Govardhan, M.
    PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON POWER ENGINEERING 2009 (ICOPE-09), VOL 2, 2009, : 491 - 497
  • [26] Partial Stall Effects on the Failure of an Axial Compressor Blade
    Poursaeidi, E.
    Arhani, M. R. Mohammadi
    Hosseini, S.
    Darayi, M.
    Arablu, M.
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 137 (12):
  • [27] Numerical Investigation of the Behavior of Tip Leakage Flow in a Low-speed Axial Compressor Rotor at Near-Stall Condition
    Duan, Zhenzhen
    Liu, Yangwei
    Lu, Lipeng
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 8, PTS A-C, 2012, : 461 - 471
  • [28] Stall-Induced Vibrations of the AVATAR Rotor Blade
    Stettner, M.
    Reijerkerk, M. J.
    Luenenschloss, A.
    Riziotis, V.
    Croce, A.
    Sartori, L.
    Riva, R.
    Peeringa, J. M.
    SCIENCE OF MAKING TORQUE FROM WIND (TORQUE 2016), 2016, 753
  • [29] Influence of rotor-stator axial clearance on compressor rotating stall characteristics
    Li, Hefei
    Zheng, Qun
    Jiang, Bin
    AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 139
  • [30] STUDY ON UNSTEADY FLOW CHARACTERISTIC IN A TRANSONIC AXIAL COMPRESSOR ROTOR AT NEAR STALL CONDITION
    Zhang, Ziyun
    Wu, Yanhui
    Li, Ziliang
    PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 10A, 2022,
12345