Single Layer Bond Coat for Gas Turbine Substrates

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Solution Overview

Problem

Conventional bi-layer bond coats for gas turbine components are time-consuming and costly due to the need for separate processes and equipment, with the coarse powder layer being unsuitable as a protective coating system and prone to oxidation damage, while the fine powder layer lacks adequate adhesion for ceramic materials.

Innovation Solution

A single layer bond coat is applied using a homogeneous powder composition with a specific particle size distribution, applied via HVOF process, achieving comparable properties to bi-layer coats, including surface roughness, density, and tensile strength, and optionally followed by a ceramic thermal barrier layer.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a bi-layer bond coat is applied with separate fine and coarse powder layers, then the protective properties and adhesion are improved, but the process complexity and time consumption increase

Engineering Contradiction:
Improveprotective properties and adhesionVSAvoidprocess complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines the fine powder layer and coarse powder layer into a single homogeneous powder composition with a specific particle size distribution (10-100 μm). This single layer achieves both the protective properties of the fine layer and the adhesion benefits of the coarse layer, eliminating the need for separate deposition processes and equipment configurations.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The single layer bond coat performs multiple functions simultaneously: it provides oxidation and corrosion protection like the fine powder layer, creates adequate surface roughness for ceramic adhesion like the coarse powder layer, and maintains density and mechanical properties. This universal layer replaces the specialized functions of two separate layers.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Reliability

If a coarse powder layer is deposited to achieve surface roughness for ceramic adhesion, then adhesion is improved, but the protective properties deteriorate due to porosity and oxidation susceptibility

Engineering Contradiction:
Improveceramic adhesionVSAvoidoxidation damage and porosity
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The single layer bond coat has non-uniform particle size distribution within the layer, creating local variations in density and roughness. The finer particles (10-30 μm) provide dense protective regions, while coarser particles (40-100 μm) create surface roughness for adhesion, with both present throughout the layer rather than in separate layers.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The bond coat uses a composite powder composition containing particles of different sizes (10-100 μm range) within a single layer. This composite structure provides both the density and protection of fine particles and the surface roughness and adhesion of coarse particles, eliminating the need for separate layers with conflicting properties.

Inventive Principle:
Principle #40Composite materials

3Object-affected harmful factors

If a fine powder layer is deposited to provide oxidation protection, then protective properties are improved, but the surface roughness is insufficient for adequate ceramic adhesion

Engineering Contradiction:
Improveoxidation and corrosion protectionVSAvoidceramic adhesion
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The single layer bond coat has non-uniform particle size distribution within the layer, creating local variations in density and roughness. The finer particles (10-30 μm) provide dense protective regions, while coarser particles (40-100 μm) create surface roughness for adhesion, with both present throughout the layer rather than in separate layers.

Inventive Principle:
Principle #3Local quality

4Manufacturing precision

If separate HVOF and APS processes are used for bi-layer bond coat deposition, then the desired properties are achieved, but the equipment requirements and inventory complexity increase

Engineering Contradiction:
Improvecoating propertiesVSAvoidequipment configurations
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent combines the fine powder layer and coarse powder layer into a single homogeneous powder composition with a specific particle size distribution (10-100 μm). This single layer achieves both the protective properties of the fine layer and the adhesion benefits of the coarse layer, eliminating the need for separate deposition processes and equipment configurations.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The single layer bond coat performs multiple functions simultaneously: it provides oxidation and corrosion protection like the fine powder layer, creates adequate surface roughness for ceramic adhesion like the coarse powder layer, and maintains density and mechanical properties. This universal layer replaces the specialized functions of two separate layers.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The single layer bond coat provides improved adhesion and durability, reducing oxidation and increasing the effective life of thermal barrier coatings by maintaining mechanical properties and thermal insulation, while simplifying the application process and reducing material inventory.

Implementation Method 1

The bond coat is applied in a thermal spray process, for example a high velocity oxy-fuel (HVOF) process

Methodology Applied
Scientific EffectThermal spray deposition: Plasma Spray

Implementation Method 2

high velocity oxy-fuel (HVOF) spray processes

Methodology Applied
Scientific EffectHigh velocity oxy-fuel spray: Fluid Spray

Implementation Method 3

thermal barrier coating (TBC) systems formed on the exposed surfaces of high temperature components have found wide use

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Implementation Method 4

The bond coat is typically formed from an oxidation-resistant aluminum-containing alloy to promote adhesion of the ceramic layer to the component

Methodology Applied
Scientific EffectAdhesion: Adhesive

Implementation Method 5

the bond coat having oxidation resistance, adequate surface roughness, and density

Methodology Applied
Scientific EffectOxidation resistance: Oxidation

Data Source

PatentUS8053089B2Single layer bond coat and method of application
Publication Date: 2011.11.08 GE INFRASTRUCTURE TECH LLC
  • US8053089B2 patent drawing
  • US8053089B2 patent drawing
  • US8053089B2 patent drawing

AI summary

A protective coating system for metal components includes a superalloy metal substrate, such as a component of a gas turbine. A single layer bond coat is applied to the superalloy metal substrate in a thermal spray process from a homogeneous powder composition having a particle size distribution wherein about 90% of the particles by volume are within a range of about 10 μm to about 100 μm. The percentage of particles within any 10 μm band within the range does not exceed about 20% by volume, and the percentage of particles within any two adjacent 10 μm bands within the range does not deviate by more than about 8% by volume.