Diffusion barrier to prevent super alloy depletion into nickel-CBN blade tip coating

Patent metadata

Field	Value
Publication number	US-11225876-B2
Application number	US-201916720844-A
Country	US
Kind code	B2
Filing date	Dec 19, 2019
Priority date	Dec 19, 2019
Publication date	Jan 18, 2022
Grant date	Jan 18, 2022

Abstract

A diffusion barrier coating on a nickel-based alloy substrate comprising the diffusion barrier being coupled to the substrate between the substrate and a composite material opposite the substrate, wherein the diffusion barrier comprises a nickel phosphorus alloy material.

First claim

What is claimed is:

1. A diffusion barrier coating on a nickel-based alloy substrate comprising:
the diffusion barrier coupled to the substrate between the substrate and a composite material opposite the substrate, wherein the diffusion barrier comprises a nickel phosphorus alloy material configured as a lamellar layer coating comprising a lamellar structure that includes multiple layers with grain boundaries having a twisted grain boundary orientation instead of and in the absence of columnar grain structures, wherein said grain boundaries are aligned with a surface of the substrate.

2. The diffusion barrier coating on a substrate according to claim 1 , wherein said diffusion barrier consists of plated layers.

3. The diffusion barrier coating on a substrate according to claim 1 , wherein said composite material comprises a nickel-cubic boron nitride material.

4. The diffusion barrier coating on a substrate according to claim 1 , wherein said diffusion barrier comprises a bond coat between said substrate and said composite material.

5. A gas turbine engine component comprising:
a compressor integrally bladed rotor having a blade with an airfoil section and a tip having a substrate;
a diffusion barrier coupled to the substrate between the substrate and a composite material opposite the substrate, wherein the diffusion barrier comprises a nickel phosphorus alloy material configured as a lamellar layer coating comprising a lamellar structure that includes multiple layers with grain boundaries having a twisted grain boundary orientation instead of and in the absence of columnar grain structures, wherein said grain boundaries are aligned with a surface of the tip.

6. The gas turbine engine component according to claim 5 , wherein said substrate comprises a nickel-based alloy.

7. The gas turbine engine component according to claim 5 , wherein said integrally bladed rotor is located in a high pressure compressor section of the gas turbine engine.

8. A process for diffusion inhibition in a nickel-based alloy substrate of a gas turbine engine component comprising:
applying a diffusion barrier coupled to the substrate, wherein the diffusion barrier comprises a nickel phosphorus alloy material configured as a lamellar layer coating comprising a lamellar structure that includes multiple layers with grain boundaries having a twisted grain boundary orientation instead of and in the absence of columnar grain structures;
wherein said grain boundaries are aligned with a surface of said nickel-based alloy substrate, reducing available rapid diffusion pathways through the diffusion barrier thickness;
coating said diffusion barrier with a matrix composite; and
subjecting said gas turbine engine component with nickel-based alloy substrate to at least one of a heat treatment and an engine operation.

9. The process of claim 8 , further comprising:
plating the diffusion barrier in layers.

10. The process of claim 8 , wherein said matrix composite comprises a nickel-cubic boron nitride material.

11. The process of claim 8 , further comprising: preventing Cr, Al, and Ti depletion from the nickel-based alloy substrate by reducing diffusion between said nickel-based alloy substrate and said matrix composite with said diffusion barrier, wherein said preventing Cr, Al, and Ti depletion comprises said reducing available rapid diffusion pathways through the diffusion barrier thickness by aligning said grain boundaries with the surface of said nickel-based alloy substrate.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Jin Lei
• Joost William J
• Brodeur Ryan M

Classifications

• F05D2300/609

  Grain size · CPC title

• C25D5/617

  Crystalline layers · CPC title

• C25D5/14

  two or more layers being of nickel or chromium, e.g. duplex or triplex layers · CPC title

• B22F7/08

  with one or more parts not made from powder {(B22F7/062 takes precedence)} · CPC title

• C23C28/028

  Including graded layers in composition or in physical properties, e.g. density, porosity, grain size · CPC title