Fretting Fatigue Cracking of a Center Guide Bolt Supporting the Combustion Chamber in a Heavy-duty Gas Turbine Engine
-
, and
Abstract
The slotted center guide bolt of the center guide feature of the lower part of the outer shell of an annular combustion chamber was found fractured in a heavy-duty gas turbine engine used for power generation, after approximately 5.500 operating hours. The incident was a one-off event and not a recurring incident. No similar events were reported from the fleet; hence the failure was not considered a field issue. The metallurgical root cause investigation that was ordered to determine the failure mechanism revealed that the incident center guide bolt failed by fretting fatigue cracking, a high cycle fatigue (HCF) phenomenon.
Kurzfassung
In einer Großgasturbine, die der Stromerzeugung dient, wies der geschlitzte Führungsbolzen der Führungseinrichtung im Unterteil der Außenschale einer Ringbrennkammer nach ca. 5.500 Betriebsstunden einen Bruch auf. Bei dem Vorkommnis handelte es sich um einen Einzelfall und nicht um ein sich wiederholendes Phänomen. Ähnliche Vorkommnisse innerhalb der Anlagenflotte wurden nicht berichtet; das Versagen wurde also nicht als ein systematischer maschinenseitiger Fehler angesehen. Die metallurgische Ursachenanalyse, die zur Bestimmung des Versagensmechanismus in Auftrag gegeben wurde, zeigte, dass der betreffende Führungsbolzen aufgrund eines durch Reiboxidation induzierten Schwingbruches versagte, einem Phänomen der hochzyklischen Ermüdung (HCF).
References / Literatur
[1] Waterhouse, R. B. (ed.): Fretting Fatigue. Applied Science Publishers, London1981Search in Google Scholar
[2] Waterhouse, R. B.; Lindley, T. C. (ed.): Fretting Fatigue. Mechanical Engineering Publications Limited, London1994. (Papers presented at the International Symposium on Fretting Fatigue held at the University of Sheffield)Search in Google Scholar
[3] Nowell, D.; Dini, D.; Hills, D. A.: Recent developments in the understanding of fretting fatigue. Engineering Fracture Mechanics73 (2006) 207–22210.1016/j.engfracmech.2005.01.013Search in Google Scholar
[4] Christiner, T.; Reiser, J.; Godór, I.; Eichlseder, W.; Trieb, F.; Stühlinger, R.: The fatigue endurance limit of a high strength Cr-Ni steel in a fretting dominated regime. Tribology International59 (2013) 97–10310.1016/j.triboint.2012.01.014Search in Google Scholar
[5] Shin, K. S.: Prediction of fretting fatigue behavior under elastic-plastic conditions. Journal of Mechanical Science and Technology23 (2009) 2714–272110.1007/s12206-009-0723-7Search in Google Scholar
[6] Koiprasert, H.; Dumrongrattana, S.; Niranatlumpong, P.: Thermally sprayed coatings for protection of fretting wear in land-based gas-turbine engine. Wear257 (2004) 1–710.1016/S0043-1648(03)00174-1Search in Google Scholar
[7] Chan, P. C.; Thornley, J. C.: Common Features of Fretting-Fatigue Cracking in Steels. Practical Failure Analysis, Volume 2(6) December 2002, PFANF8 (2002) 6:85–9010.1007/BF02715504Search in Google Scholar
[8] Hoeppner, D. W.: Fretting fatigue case studies of engineering components. Tribology International39 (2006) 1271–127610.1016/j.triboint.2006.02.051Search in Google Scholar
[9] Neu, R. W.: Progress in standardization of fretting fatigue terminology and testing. Tribology International44 (2011) 1371–137710.1016/j.triboint.2010.12.001Search in Google Scholar
[10] Murthy, H.; Gao, G.; Farris, T. N.: Fretting fatigue of single crystal nickel at 600 °C. Tribology International39 (2006) 1227–124010.1016/j.triboint.2006.02.050Search in Google Scholar
[11] Ghosh, S. J.: Failure Investigation of a Low-Pressure Turbine Blade. Practical Failure Analysis, Volume 4(3) June 2004, JFAPBC (2004) 3:73–7710.1007/s11668-996-0018-6Search in Google Scholar
[12] Golden, P. J.; Hutson, A. L.; Bartha, B. B.; Nicholas, T.: Fatigue Loading and Life Prediction in Three Fretting Fatigue Fixtures. Experimental Mechanics (2008) 48:253–26310.1007/s11340-008-9130-8Search in Google Scholar
[13] Fischer, B.; Neidel, A.: Metallurgical Failure Investigation of Fractured Stage 15 Compressor Disk Rim in Köln-Niehl Gas Turbine Engine. Internal report GT BLN QM / 2013 / 0505, October 4, 2013.Search in Google Scholar
© 2018, Carl Hanser Verlag, München
Articles in the same Issue
- Contents/Inhalt
- Contents
- Editorial
- Editorial
- Technical Contributions/Fachbeiträge
- Heat Treatment and Microstructural Contrasting on Low-Alloy Copper-Based Alloys
- Analysis, Modeling and Simulation of Tomographic Image Data for the 3D Microstructure of Electrode Material in Lithium-Ion Batteries
- Detailed Metallographic Analysis of the Surface Layer Structure of Carbonitrided Case-Hardening Steels after Varied Tempering Treatments
- Fretting Fatigue Cracking of a Center Guide Bolt Supporting the Combustion Chamber in a Heavy-duty Gas Turbine Engine
- Meeting Diary/Veranstaltungskalender
- Meeting Diary
Articles in the same Issue
- Contents/Inhalt
- Contents
- Editorial
- Editorial
- Technical Contributions/Fachbeiträge
- Heat Treatment and Microstructural Contrasting on Low-Alloy Copper-Based Alloys
- Analysis, Modeling and Simulation of Tomographic Image Data for the 3D Microstructure of Electrode Material in Lithium-Ion Batteries
- Detailed Metallographic Analysis of the Surface Layer Structure of Carbonitrided Case-Hardening Steels after Varied Tempering Treatments
- Fretting Fatigue Cracking of a Center Guide Bolt Supporting the Combustion Chamber in a Heavy-duty Gas Turbine Engine
- Meeting Diary/Veranstaltungskalender
- Meeting Diary