Blade failures in gas turbine engines often lead to loss of all downstream stages and can have a dramatic effect on the availability of the turbine engines. Thorough failure investigation is essential for the effective management of engine airworthiness. In this paper blade fatigue failures are inve
Failure analysis of gas turbine buckets
β Scribed by Jung-Chel Chang; Young-Hoon Yun; Chel Choi; Jae-Chul Kim
- Publisher
- Elsevier Science
- Year
- 2003
- Tongue
- English
- Weight
- 756 KB
- Volume
- 10
- Category
- Article
- ISSN
- 1350-6307
No coin nor oath required. For personal study only.
β¦ Synopsis
The failure of a gas turbine first stage bucket was investigated by visual inspection and finite element analysis. The failure of a major bucket cooling passage was a critical cause of the separation of a bucket segment and caused microstructural deterioration of the neighboring regions by serious thermal load. Changes of microstructural morphologies of the damaged buckets under the thermal and mechanical stress were observed. After coating stripping, the bucket surface condition was evaluated through visual inspection and finite element analysis. The TMF (thermalmechanical fatigue) cracking of surface coatings on the suction and pressure sides of the bucket was described.
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