TREATED GAS TURBINE COMPONENTS AND PROCESSES OF TREATING GAS TURBINE SYSTEMS AND GAS TURBINE COMPONENTS
A process of treating a component (101) includes mechanically removing surface debris (109) from a base coating (105) of the component (101), identifying at least one surface feature (113) in the base coating (105), and applying an overlay coating layer (115) over the surface feature (113) of the ba...
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Main Authors | , , , , |
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Format | Patent |
Language | English French German |
Published |
27.12.2017
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Subjects | |
Online Access | Get full text |
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Summary: | A process of treating a component (101) includes mechanically removing surface debris (109) from a base coating (105) of the component (101), identifying at least one surface feature (113) in the base coating (105), and applying an overlay coating layer (115) over the surface feature (113) of the base coating (105) without stripping off the base coating (105). A process of treating a gas turbine component (101) includes mechanically removing surface debris (109) from a base coating (105) of the gas turbine component (101), identifying at least one surface feature (113) in the base coating (105) of corrosion pits, dents, spalls, and combinations thereof, and applying an overlay coating layer (115) over the surface feature (113) of the base coating (105) without stripping off the base coating (105). A treated gas turbine component (101) includes a gas turbine component substrate (103) and a base coating (105) on the gas turbine component substrate (103) having at least one healed surface feature (113). The healed surface feature (113) includes an overlay coating layer (115) on the base coating (105). |
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Bibliography: | Application Number: EP20160461527 |