Gas turbine engine component

A gas turbine engine component coating having superior abradability and erosion resistance is disclosed. The coating includes a base coat foundation layer, a graded interlayer and an abradable top layer for an overall thickness of preferably about 50 mils. The coating is characterized by a plurality...

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Bibliographische Detailangaben
Hauptverfasser: NISSLEY, DAVID M, HARTER, HAROLD D, GODIN, DANIEL R, FOSTER, GEORGE E
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A gas turbine engine component coating having superior abradability and erosion resistance is disclosed. The coating includes a base coat foundation layer, a graded interlayer and an abradable top layer for an overall thickness of preferably about 50 mils. The coating is characterized by a plurality of vertical microcracks. By precisely controlling the deposition parameters, composition of the layers and layer particle morphology, segmentation is achieved, as well as superior abradability and erosion resistance.