Laser powder weld reconditioning of gas turbine engine blades
نویسندگان
چکیده
منابع مشابه
Vibration and Crack Detection in Gas Turbine Engine Compressor Blades using Eddy Current Sensors
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: VESTNIK of Samara University. Aerospace and Mechanical Engineering
سال: 2017
ISSN: 2541-7533,2542-0453
DOI: 10.18287/2541-7533-2016-15-3-60-69