Ceramic Heat Shield Infiltration for Corrosion Resistance

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Solution Overview

Problem

Ceramic heat shields in gas turbines face corrosion and erosion due to the conversion of mullite to secondary corundum under high temperatures, leading to premature coating failure and reduced service life, with existing aluminum oxide coatings exhibiting adhesion issues and limited durability.

Innovation Solution

A porous ceramic heat shield with an infiltration coating of yttrium aluminum garnet (YAG) is applied to close surface pores, preventing hot gas invasion and corrosion, while maintaining elongation tolerance and allowing for improved adhesion of additional coatings, using a method that involves immersing the ceramic body in a YAG-containing suspension under vacuum and subsequent firing to achieve deep penetration and crystalline integration.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If aluminum oxide coating is applied to protect ceramic heat shields from corrosion, then corrosion resistance is improved, but adhesion to the ceramic surface deteriorates

Engineering Contradiction:
Improvecorrosion resistanceVSAvoidadhesion strength
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The patent introduces a transition layer comprising aluminum oxide and mullite between the aluminum oxide coating and the mullite ceramic substrate. This intermediate layer serves as a mediator that provides both corrosion resistance and strong adhesion to the substrate, resolving the contradiction between protection and bonding strength

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The protective system uses composite material structure with multiple layers: aluminum oxide coating, transition layer (aluminum oxide + mullite), and mullite substrate. This composite structure combines the corrosion resistance of aluminum oxide with the adhesion benefits of mullite, achieving both requirements simultaneously

Inventive Principle:
Principle #40Composite materials

2Manufacturing precision

If slurry spray method is used to apply aluminum oxide coating, then coating fineness is improved, but post-sintering cracks and premature sanding occur

Engineering Contradiction:
Improvecoating finenessVSAvoidcoating durability
Core Design Contradiction:
Manufacturing precisionVSReliability

Solution Approach 1:

The patent applies plasma spraying instead of slurry spray, fundamentally changing the coating application method parameters. This produces a coating with different microstructure and bonding characteristics that avoids post-sintering cracks and premature sanding while maintaining appropriate fineness

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If flame spray method is used to apply aluminum oxide coating, then coating density is improved, but coating becomes brittle and cannot follow deformations

Engineering Contradiction:
Improvecoating densityVSAvoidflexibility
Core Design Contradiction:
Manufacturing precisionVSStrength

Solution Approach 1:

The patent uses plasma spraying instead of flame spraying, changing the thermal processing parameters. This produces a coating with appropriate density while maintaining flexibility through controlled microstructure and bonding, allowing the coating to follow substrate deformations without becoming brittle

Inventive Principle:
Principle #35Parameter changes

4Adaptability or versatility

If porous ceramic structure is used to preserve elongation tolerance, then deformation capability is improved, but corrosion and erosion attacks increase

Engineering Contradiction:
Improveelongation toleranceVSAvoidcorrosion and erosion resistance
Core Design Contradiction:
Adaptability or versatilityVSObject-affected harmful factors

Solution Approach 1:

The patent segments the ceramic structure into two distinct zones: a dense surface layer (infiltration layer) that resists corrosion and erosion, and an inner porous structure that provides elongation tolerance. This segmentation allows each zone to fulfill its specific function without compromise

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent applies local quality by creating a dense infiltration layer only at the surface where corrosion and erosion occur, while maintaining porosity in the interior where elongation tolerance is needed. This localized treatment optimizes protection where required without sacrificing overall deformation capability

Inventive Principle:
Principle #3Local quality

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 YAG infiltration coating significantly extends the service life of ceramic heat shields by reducing erosion and particle release, minimizing damage to turbine blades, and enabling protection of lateral faces without altering the heat shield dimensions, while ensuring thermal shock stability and uniform coating application.

Implementation Method 1

the infiltration of a highly porous ceramic surface it is achieved that the porosity of the ceramics on the surface is significantly reduced and corrosive products thus cannot invade

Methodology Applied
Scientific EffectInfiltration: Absorption (physical)

Implementation Method 2

the porosity of the ceramics on the surface is significantly reduced

Methodology Applied
Scientific EffectPorosity reduction: Porosity

Implementation Method 3

immersing the ceramic body in a YAG-containing suspension under vacuum and subsequent firing to achieve deep penetration

Methodology Applied
Scientific EffectCapillary action: Capillary Action

Implementation Method 4

subsequent firing to achieve deep penetration and crystalline integration

Methodology Applied
Scientific EffectSintering: Sintering

Data Source

PatentUS11319257B2Ceramic heat shields having surface infiltration for preventing corrosion and erosion attacks
Publication Date: 2022.05.03 SIEMENS ENERGY GLOBAL GMBH & CO KG
  • US11319257B2 patent drawing
  • US11319257B2 patent drawing
  • US11319257B2 patent drawing

AI summary

An improved ceramic heat shield for a gas turbine is provided. The ceramic heat shield has a porous ceramic body and according to the embodiments an infiltration coating that is provided in a surface layer of the porous ceramic body and contains an infiltration coating material designed to gas-tightly seal pores of the ceramic body.