Aeroengine Safety - 12:126:1261:12612<a style="color:#000" href="https://www.tugraz.at/institute/ittm">Institute of Thermal Turbomachinery and Machine Dynamics</a></br><a href="https://www.tugraz.at">Graz University of Technology</a>
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2026-06-21T14:31:24+00:00Aeroengine Safety
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https://aeroenginesafety.tugraz.at/lib/exe/fetch.php?media=wiki:logo.pngtext/html2020-08-18T18:34:37+00:00Anonymous (anonymous@undisclosed.example.com)12.6.1.2 Damages due to LCF
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12.6.1.2 Damages due to LCF
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[ Damage due to LCF ]
Damages due to LCF loads are already treated in the part-specific chapters (compressor, combustion chamber, and turbine). In Volume 2, Chapter 8.2 also deals with LCF in the context of fragment containment. Volume 2, Chapter 6.2 contains examples of the influence of fretting on LCF (Ills. 6.2-6 and 6.2-7). The special situation of thermal fatigue is dealt with in Chapter 12.6.3. Therefore, the following are merely…