ANALYSIS OF REPAIRED GAS TURBINE AND COMPRESSOR BLADES
نویسندگان
چکیده
منابع مشابه
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High cycle fatigue (HCF) cracks generated by compressor blade vibrations are a common source of failure in gas turbine engines. Current methods for crack detection are costly, time consuming, and prone to errors. In-situ blade vibration detection would help operators avoid critical engine speeds, and help infer the presence of cracks via a change in the mode of a blade. Blade vibrations can be ...
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ژورنال
عنوان ژورنال: Aviation
سال: 2008
ISSN: 1648-7788,1822-4180
DOI: 10.3846/1648-7788.2008.12.46-50