Method for repairing an apertured gas turbine component
A method is disclosed for repairing defects in a gas turbine component 10 that comprises a substrate 58 and an existing coating 44 on the substrate 58. The article 10 includes cooling holes 18 having a predetermined air flow requirement and an outer shaped portion 52 and an inner metering portion 60...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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