METHOD FOR MODIFYING AN AIRFOIL SHROUD
A turbine engine, bucket and method for modifying an airfoil shroud of turbine bucket is disclosed. A reference location is located in a second end edge of the airfoil shroud proximate a seal rail of the airfoil shroud. A relief cut is formed in the airfoil shroud to remove the reference location. A...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
29.05.2014
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Subjects | |
Online Access | Get full text |
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Summary: | A turbine engine, bucket and method for modifying an airfoil shroud of turbine bucket is disclosed. A reference location is located in a second end edge of the airfoil shroud proximate a seal rail of the airfoil shroud. A relief cut is formed in the airfoil shroud to remove the reference location. Additionally, another reference location may be located in a first end edge of the airfoil shroud proximate the seal rail. Another relief cut may be formed in the airfoil shroud to remove the other reference location. |
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Bibliography: | Application Number: US201314046417 |