TURBINE BLADE CREEP MONITORING

A method of monitoring turbine blade creep in a gas turbine engine is provided. The method includes: receiving stereo images of a turbine blade of a row of turbine blades, the images having been obtained using a stereo borescope located in the engine adjacent the row of turbine blades; identifying s...

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Bibliographische Detailangaben
Hauptverfasser: NASSER, Bilal M, PULISCIANO, Adriano
Format: Patent
Sprache:eng
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