Multilayer Environmental Barrier Coating for Silicon Carbide

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Solution Overview

Problem

Silicon-containing ceramics used in high-temperature applications like gas turbine engines are prone to rapid recession due to reaction with water vapor and oxidizing gases, leading to coating loss and reduced efficiency.

Innovation Solution

A multilayer system comprising a substrate coated with a first layer of rare earth silicate and cordierite, and a second layer of rare earth silicate, with varying amounts of cordierite, to provide thermal expansion matching and stress reduction, enhancing durability and resistance to environmental and thermal conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a single-layer coating is applied to silicon-containing ceramics, then the coating provides basic protection, but interlayer stresses develop due to thermal expansion mismatch leading to coating spallation

Engineering Contradiction:
Improvecoating protectionVSAvoidcoating bond strength
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The coating system is divided into multiple layers with different compositions. The first layer contains rare earth silicate and cordierite, while the second layer contains rare earth silicate with reduced cordierite content. This segmentation allows each layer to contribute differently to stress management and protection, preventing spallation while maintaining reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The cordierite content is varied between layers to optimize thermal expansion matching. The first layer has higher cordierite content (up to 12 wt%) to match the substrate thermal expansion, while the second layer has reduced cordierite content (0-12 wt%) to reduce interlayer stresses. This parameter change resolves the contradiction between bond strength and stress prevention.

Inventive Principle:
Principle #35Parameter changes

2Temperature

If ceramics are exposed to high temperature combustion environments, then they can operate at higher temperatures improving engine efficiency, but water vapor and oxidizing gases cause rapid recession of the ceramic surface

Engineering Contradiction:
Improveoperating temperatureVSAvoidceramic recession
Core Design Contradiction:
TemperatureVSLoss of substance

Solution Approach 1:

The coating uses a composite material system combining rare earth silicate and cordierite in specific proportions. This composite provides both high-temperature stability and resistance to water vapor and oxidizing gases. The rare earth silicate forms a protective barrier while cordierite provides structural stability, allowing the ceramic to operate at elevated temperatures without rapid recession.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The coating composition is optimized for the specific high-temperature combustion environment. The rare earth silicate-rich outer layer provides localized protection against water vapor and oxidizing gases where they contact the ceramic surface, while the cordierite content is adjusted to maintain structural integrity at operating temperatures.

Inventive Principle:
Principle #3Local quality

3Stability of the object's composition

If cordierite content is increased in the coating to match thermal expansion, then thermal stress is reduced, but the coating becomes more susceptible to chemical reactions with water vapor forming liquid silicates

Engineering Contradiction:
Improvethermal expansion matchingVSAvoidchemical reaction with water vapor
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The coating is segmented into two layers with different cordierite contents. The first layer has higher cordierite content (up to 12 wt%) for thermal expansion matching, while the second layer has reduced cordierite content (0-12 wt%) to minimize chemical reactions with water vapor. This segmentation resolves the contradiction by assigning different functional priorities to different layers.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The cordierite content parameter is changed between layers to balance thermal expansion matching and chemical stability. By reducing cordierite content in the outer layer, the coating becomes less susceptible to water vapor reactions while the inner layer maintains thermal expansion compatibility with the substrate.

Inventive Principle:
Principle #35Parameter changes

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 multilayer system effectively reduces interlayer stresses, improves bond strength, and decreases recession rates, maintaining component integrity under severe conditions such as high temperatures and humidity.

Implementation Method 1

varying amounts of cordierite, to provide thermal expansion matching and stress reduction

Methodology Applied
Scientific EffectThermal expansion matching: Thermal Expansion

Implementation Method 2

Silicon containing ceramics typically form a slow forming silica (SiO2) scale in clean oxidizing environments. However, water vapor, molten salts, or a reducing atmosphere present in the environment may react with the silica scale to form liquid silicates. Oxygen may then diffuse through the liquid silicate and oxidize the ceramic substrate.

Methodology Applied
Scientific EffectOxidation resistance: Oxidation

Data Source

PatentUS8334062B1Environmental barrier coating
Publication Date: 2012.12.18 SAINT GOBAIN CERAMICS & PLASTICS INC
  • US8334062B1 patent drawing
  • US8334062B1 patent drawing
  • US8334062B1 patent drawing

AI summary

The present invention relates generally to a multi-layered article suitable for service in severe environments. The article may be formed of a substrate, such as silicon carbide and/or silicon nitride. The substrate may have a first layer of a mixture of a rare earth silicate and Cordierite. The substrate may also have a second layer of a rare earth silicate or a mixture of a rare earth silicate and cordierite.