Failure analysis of damaged parts of an aeroengine
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Failure analysis of damaged parts of an aeroengine
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| Creator |
Sujata, M
Bhaumik, SK |
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| Subject |
Aeronautics (General)
Chemistry and Materials (General) |
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| Description |
Fractured 1st stage compressor blade and LPTR shaft belonging to an aeroengine were brought to the laboratory for analysis. Fractographic examination indicated that both the components had failed by overload due to impact. There were no evidences of delayed failure like fatigue. No metallurgical abnormalities were found responsible for the failure.
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| Publisher |
National Aerospace Laboratories
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| Date |
2004
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| Type |
Proj.Doc/Technical Report
NonPeerReviewed |
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| Identifier |
Sujata, M and Bhaumik, SK (2004) Failure analysis of damaged parts of an aeroengine. Project Report. National Aerospace Laboratories, Bangalore.
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| Relation |
http://nal-ir.nal.res.in/9680/
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