METHODS FOR COATING GAS TURBINE ENGINE COMPONENTS

The present disclosure relates to methods for coating gas turbine engine components, such as combustor panels. In one embodiment, a method includes forming a first layer to a substrate to form a bond coat, and forming a second layer over the first layer. The second layer may be formed by a material...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: TU JOHN S, LITTON DAVID A, BUTLER AARON S, ZELESKY MARK F, MOURA DENNIS M, KIRSOPP PHILIP J
Format: Patent
Sprache:eng
Schlagworte:
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