Failure analysis of steam turbine blade
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
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Title |
Failure analysis of steam turbine blade
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Creator |
Madan, M
Suresh Kumar, M Venkataswamy, MA Sujata, M Parameswara, MA Bhaumik, SK |
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Subject |
Aeronautics (General)
Chemistry and Materials (General) |
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Description |
The steam turbine blade had failed by fatigue. The fatigue crack had initiated at the blade root T-joint fillet. Fatigue appears to be of high cycle – low stress type. From the evidences, the most probable reason for fatigue crack initiation appears to be presence of nonmetallic inclusions in the blade material and/or excessive clearance between the blade guiding rib on the disc and the blade root.
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Publisher |
National Aerospace Laboratories
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Date |
2005
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Type |
Proj.Doc/Technical Report
NonPeerReviewed |
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Identifier |
Madan, M and Suresh Kumar, M and Venkataswamy, MA and Sujata, M and Parameswara, MA and Bhaumik, SK (2005) Failure analysis of steam turbine blade. Project Report. National Aerospace Laboratories, Bangalore.
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Relation |
http://nal-ir.nal.res.in/10000/
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