Silicon Source Coating for High-Temperature Oxidation Resistance

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Solution Overview

Problem

Conventional environmental barrier coatings (EBCs) for silicon-bearing materials in high-temperature applications, such as gas turbines, are limited by the melting point of silicon in the bond layer, leading to mechanical instability and restricted temperature capability, while silicide coatings face thermal stress issues due to mismatched thermal expansion coefficients and gaseous by-product formation.

Innovation Solution

A coating architecture using a substrate with a first layer comprising a silicon source material and a secondary material with a lower thermal expansion coefficient, which diffuses silicon to form a protective silica layer, mitigating thermal stresses and by-product disruption, and a second layer acting as a membrane for silicon transport, ensuring sustained protection and reduced thermal expansion mismatch.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conventional EBC bond layer containing silicon is used, then the coating provides chemical stability and protection in high-temperature water vapor environments, but the melting point of silicon limits the maximum operating temperature and causes mechanical instability at elevated temperatures

Engineering Contradiction:
Improvecoating protection capabilityVSAvoidmaximum operating temperature
Core Design Contradiction:
ReliabilityVSTemperature

Solution Approach 1:

The bond layer composition is modified by reducing free silicon content and adjusting the SiO2-Si-Al2O3 system parameters to elevate the melting point and maintain structural stability at higher temperatures while preserving chemical protection capabilities

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The bond layer is designed as a composite material combining SiO2, Si, and Al2O3 in specific proportions to achieve both chemical stability against water vapor attack and enhanced high-temperature structural integrity through the complementary properties of each component

Inventive Principle:
Principle #40Composite materials

2Stability of the object's composition

If silicide coatings are applied to reduce thermal expansion mismatch, then thermal stress is reduced, but gaseous by-products are formed during oxidation that can disrupt coating integrity

Engineering Contradiction:
Improvethermal expansion compatibilityVSAvoidgaseous by-products from oxidation
Core Design Contradiction:
Stability of the object's compositionVSObject-generated harmful factors

Solution Approach 1:

The harmful silicide layer that generates gaseous by-products is removed from the coating system, replacing it with a silicon-based bond layer that achieves thermal expansion compatibility through controlled silicon diffusion and SiO2 formation without producing disruptive gases

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The potential harm of silicon oxidation is converted into a benefit by controlling the oxidation process to form a protective SiO2 layer that provides both thermal expansion matching and chemical protection, eliminating the gaseous by-product issue while maintaining thermal compatibility

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

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 proposed solution enhances high-temperature oxidation resistance and extends the temperature capability of coated components by reducing thermal stresses and maintaining coating integrity over time, thereby improving the service life and performance of materials in demanding environments.

Implementation Method 1

silicon is provided from the first layer and diffuses through the second layer to the surface of the second layer

Methodology Applied
Scientific EffectDiffusion: Diffusion

Implementation Method 2

a first layer over the substrate. The first layer includes a silicon source material and a secondary material... reducing thermal stresses

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentUS11066339B2Article for high temperature service
Publication Date: 2021.07.20 GENERAL ELECTRIC CO
  • US11066339B2 patent drawing

AI summary

An article comprises a substrate comprising a ceramic matrix composite; a first layer disposed over the substrate, the first layer comprising a substantially interconnected silicon source material, and a secondary material; and a second layer disposed over the first layer, the second layer comprising a membrane material in mass transfer communication with the silicon source material.