Indium Oxide Co-Stabilized Thermal Barrier Coating

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Solution Overview

Problem

Conventional thermal barrier coatings for high-temperature metallic components, such as those in industrial gas turbines, face challenges in stabilizing the cubic phase of zirconia and resisting corrosion from fuel impurities like sodium, sulfur, and vanadium, leading to premature degradation and reduced lifespan.

Innovation Solution

A corrosion-resistant thermal barrier coating material is developed by blending indium oxide with indate forming oxides, forming a co-stabilized mixture with zirconia or hafnia, and using a combination of air plasma sprayable or electron beam physical vapor deposition processes to create a stable coating that resists chemical attacks and maintains the tetragonal and cubic phases of zirconia or hafnia.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If scandia stabilized zirconia is used as a thermal barrier coating, then the coating has high resistance to corrosives and effective thermal barrier properties, but the cost becomes extremely expensive making it impractical for widespread use

Engineering Contradiction:
Improvecorrosion resistanceVSAvoidcost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent changes the chemical composition parameters by substituting scandia with a combination of indium oxide and indate forming oxides (such as lanthanum oxide, cerium oxide, or yttrium oxide). This parameter substitution maintains the stabilizing function while dramatically reducing cost, as indium and the selected indate forming oxides are significantly cheaper than scandia while still providing effective corrosion resistance and thermal barrier properties

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs cheaper alternative materials (indium oxide combined with indate forming oxides) that can provide comparable performance to expensive scandia stabilized zirconia. This principle allows replacement of high-cost materials with lower-cost alternatives that achieve the same functional objectives, making thermal barrier coatings economically viable for widespread industrial application

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

2Ease of manufacture

If indium stabilized zirconia is used as a thermal barrier coating, then the coating can be cost effective, but the indium is so volatile that it boils off during plasma spraying or electron beam physical deposition and does not remain in the thermal barrier coating

Engineering Contradiction:
ImprovecostVSAvoidcompositional stability
Core Design Contradiction:
Ease of manufactureVSStability of the object's composition

Solution Approach 1:

The patent merges indium oxide with indate forming oxides (such as lanthanum oxide, cerium oxide, or yttrium oxide) to create a composite stabilizing system. This combination allows the indium to be present in lower concentrations that do not cause excessive volatility, while the indate forming oxides provide structural stability and prevent indium loss during plasma spraying or electron beam physical deposition processes

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The indate forming oxides act as intermediary substances that stabilize the zirconia structure and prevent indium volatilization. These intermediaries form a stable matrix that retains the indium within the coating structure during high-temperature deposition processes, ensuring the indium remains in the final thermal barrier coating to provide corrosion resistance

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of manufacture

If conventional thermal barrier coating methods are used, then the coating can be applied, but impurities in fuels such as sodium, sulfur, phosphorus, and vanadium corrode the coating causing spalling and reducing component lifetime

Engineering Contradiction:
Improvecoating applicabilityVSAvoidcorrosion resistance
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent uses a composite material system consisting of indium oxide combined with indate forming oxides (such as lanthanum oxide, cerium oxide, or yttrium oxide) stabilized zirconia. This composite composition provides enhanced corrosion resistance against fuel impurities (sodium, sulfur, phosphorus, and vanadium) compared to conventional single-stabilizer coatings, while maintaining the ability to be applied through standard plasma spraying or electron beam physical deposition processes

Inventive Principle:
Principle #40Composite materials

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 solution effectively prevents the transformation of zirconia or hafnia to the monoclinic phase, thereby preventing cracking, spalling, and chemical attack, extending the lifespan and efficiency of the thermal barrier coating and the underlying metallic components.

Implementation Method 1

blending indium oxide with indate forming oxides, forming a co-stabilized mixture with zirconia or hafnia, and using a combination of air plasma sprayable or electron beam physical vapor deposition processes to create a stable coating that resists chemical attacks and maintains the tetragonal and cubic phases of zirconia or hafnia

Methodology Applied
Scientific EffectPhase stabilization:

Implementation Method 2

air plasma sprayable processes

Methodology Applied
Scientific EffectPlasma spray: Plasma Spray

Implementation Method 3

electron beam physical vapor deposition processes

Methodology Applied
Scientific EffectPhysical vapor deposition: Physical Vapour Deposition

Implementation Method 4

a corrosion-resistant thermal barrier coating material is developed by blending indium oxide with indate forming oxides, forming a co-stabilized mixture with zirconia or hafnia

Methodology Applied
Scientific EffectCorrosion resistance:

Data Source

PatentUS7534290B2Corrosion resistant thermal barrier coating material
Publication Date: 2009.05.19 ALLUMAX TTI LLC
  • US7534290B2 patent drawing
  • US7534290B2 patent drawing
  • US7534290B2 patent drawing

AI summary

According to one exemplary embodiment, a method for forming a corrosion resistant thermal barrier coating material includes steps of blending indium oxide with at least one hydrate forming oxide to form a mechanical mixture, heating the mechanical mixture to a sufficiently high temperature to form an indate precursor, and blending the indate precursor with at least one non-hydrate forming oxide to form a co-stabilized mixture. In one embodiment, the co-stabilized mixture can be changed into an APS powder by using a powder forming method. In another embodiment, the co-stabilized mixture can be formed into a desired shape and heated to form an EB-PVD ingot.