Fretting Fatigue Cracking of an Arresting Feature in a Turbine Disk of a Heavy-Duty Gas Turbine Engine

被引:2
|
作者
Neidel, A. [1 ]
Giller, M. [1 ]
Riesenbeck, S. [1 ]
机构
[1] Gasturbinenwerk Berlin, Energy Sect, Werkstoffpruflabor, Huttenstr 12, D-10548 Berlin, Germany
来源
关键词
D O I
10.3139/147.110348
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
A check for surface cracks under application of the magnetic flux leakage method (MT testing) was performed on the turbine wheel disk of a heavy-duty turbine gas turbine engine for energy generation. It revealed unacceptable findings on the bearing surface of the sealing plate groove. In order to identify the damage-causing mechanism of the material, a metallographic examination was performed. The findings during non-destructive material testing were caused by a gaping material separation which was also easily detectable to the naked eye. The material separation is a high-cycle fatigue crack induced by fretting. Hence, the damage causing mechanism was fretting fatigue cracking.
引用
收藏
页码:37 / 46
页数:10
相关论文
共 50 条
  • [1] Fretting Fatigue Cracking of a Center Guide Bolt Supporting the Combustion Chamber in a Heavy-duty Gas Turbine Engine
    Neidel, A.
    Fischer, B.
    Gaedicke, T.
    [J]. PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2018, 55 (03): : 158 - 175
  • [2] Uncharacteristic Circumferential TMF Cracking in a Heavy-duty Stationary Gas Turbine Engine Burner Outlet
    Neidel, A.
    Ullrich, Th.
    Wallich, S.
    [J]. PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2015, 52 (06): : 334 - 341
  • [3] Erosion Damage to Last-Stage Compressor Disk of a Heavy-duty Gas Turbine Engine
    Neidel, Andreas
    Gaedicke, Tobias
    Wallich, Sebastian
    [J]. PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2015, 52 (10): : 607 - 614
  • [4] High Cycle Fatigue Failure of Burner Feeder Line in a Heavy-duty Gas Turbine Engine
    Neidel, A.
    Giller, M.
    Riesenbeck, S.
    Woehl, E.
    [J]. PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2019, 56 (01): : 48 - 60
  • [5] Integrity of heavy-duty gas turbine rotors
    Becker, B
    Termuehlen, H
    [J]. PROCEEDINGS OF THE AMERICAN POWER CONFERENCE, VOL 58, PTS I AND II, 1996, 58 : 720 - 726
  • [6] AERODYNAMIC ANALYSIS AND REDESIGN OF AN INLET SEGMENT FOR A HEAVY-DUTY GAS TURBINE ENGINE
    Abdel-Wahab, Samer
    Vogel, Gregory
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, 2010, : 1275 - 1282
  • [7] Hydrogen Induced Stress Corrosion Cracking of Fuel Oil Premix Burner Nozzles in a Heavy-duty Gas Turbine Engine
    Neidel, A.
    Gadicke, T.
    Wallich, S.
    [J]. PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2018, 55 (11): : 773 - 786
  • [8] Material testing for fatigue design of heavy-duty gas turbine blading with film cooling
    Pan, Y
    Bischoff-Beiermann, B
    Schulenberg, T
    [J]. FATIGUE DESIGN 1998, VOL II, 1998, 182 : 433 - 440
  • [9] Material testing for fatigue design of heavy-duty gas turbine blading with film cooling
    Pan, Y
    Bischoff-Beiermann, B
    Schulenberg, T
    [J]. FATIGUE DESIGN AND RELIABILITY, 1999, 23 : 155 - 162
  • [10] Metallurgical Failure Investigation of HCF Cracking in a Premix Fuel Oil Manifold of a Heavy-duty Combined Cycle Gas Turbine Engine
    Neidel, A.
    Fischer, B.
    Cagliyan, E.
    [J]. PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2016, 53 (04): : 237 - 247