Multilayered erosion resistant coating for gas turbines
AssigneeHoneywell International Inc.
InventorsDerek A. Rice, Adrienne Lamm
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AssigneeHoneywell International Inc.
InventorsDerek A. Rice, Adrienne Lamm
Estimating the term…
A coating system is used on an engine component having an outer surface configured to be exposed to a first plurality of particles impinging against the outer surface at an angle within a first angle range and a second plurality of particles impinging at an angle in a second angle range. The system includes a bond layer overlying the engine component outer surface, a first erosion-resistant layer comprising a first material that is more resistant to erosion by particles impinging the component outer surface at an angle within the first angle range than by particles impinging within the second angle range, an interlayer overlying the first erosion-resistant layer, and a second erosion-resistant layer comprising a second material that is more resistant to erosion by particles impinging the component outer surface at an angle within the second angle range than by particles impinging within the first angle range.
An erosion-resistant coating system for use on an engine component having an outer surface that is configured to be exposed to a first plurality of particles impinging against the outer surface at an angle within a first angle range and a second plurality of particles impinging against the outer surface at an angle in a second angle range that is different than the first angle range, the system comprising:
The coating system of claim 8, wherein the transition metal is doped with a material selected from the group consisting of boron, carbon, nitrogen, and oxygen.
An erosion-resistant coating system for use on an engine component having an outer surface that is configured to be exposed to a first plurality of particles impinging against the outer surface at an angle within a first angle range and a second plurality of particles impinging against the outer surface at an angle in a second angle range that is different than the first angle range, the system comprising:
The coating system of claim 11, wherein the interlayer is a graded structure.
The coating system of claim 12, wherein the interlayer has a first side and a second side, the first side comprising the first crystallographic structure and the second side comprising the second crystallographic structure.
The coating system of claim 15, wherein the transition metal is doped with at least one material selected from the group consisting of boron, carbon, nitrogen, and oxygen.
A method of coating an engine component having an outer surface, the coating configured to be exposed to a first plurality of particles impinging against the outer surface at an angle within a first angle range and a second plurality of particles impinging against the outer surface at an angle in a second angle range that is different than the first angle range, the method comprising the steps of:
A method of coating an engine component having an outer surface that is configured to be exposed to a first plurality of particles impinging against the outer surface at an angle within a first angle range and a second plurality of particles impinging against the outer surface at an angle within a second angle range that is different than the first angle range, the method comprising the steps of:
Dependencies are inferred from the claim text.