Borosilicate Oxidation Coating for Hydrolysis-Resistant Composites

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Solution Overview

Problem

Existing oxidation protection systems for carbon-carbon composite structures, such as those used in aircraft braking systems, face hydrolytic instability due to the formation of water-soluble diboron trioxide (B2O3) at high temperatures, leading to potential material loss and degradation.

Innovation Solution

A method involving the application of a boron slurry and a silicon slurry to a carbon-carbon composite structure, followed by heating, to form a boron-glass and silicon-glass layer. The slurries include boron compounds, glass compounds, glass formers, and carrier fluids, with specific compositions that enhance stability and self-healing properties.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If layers of boron carbide and silicon carbide are used for oxidation protection, then oxidation resistance is improved, but hydrolytic stability deteriorates due to water-soluble diboron trioxide formation

Engineering Contradiction:
Improveoxidation resistanceVSAvoidhydrolytic stability
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

A glass layer acts as an intermediary barrier between the boron carbide/silicon carbide oxidation protection layer and the water-containing environment. This glass intermediary prevents direct contact between water and the hydrolytically unstable B2O3, thereby maintaining both oxidation resistance and hydrolytic stability simultaneously.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The protection system uses a composite structure combining multiple materials: boron carbide, silicon carbide, and glass layers. This composite approach allows each material to perform its specialized function - boron carbide and silicon carbide provide oxidation resistance while the glass layer provides hydrolytic stability, resolving the contradiction between these two requirements.

Inventive Principle:
Principle #40Composite materials

2Loss of substance

If boron carbide and silicon carbide layers are applied for high-temperature protection, then material loss from oxidation is reduced, but water solubility of formed compounds increases leading to degradation

Engineering Contradiction:
Improvecarbon material lossVSAvoidwater stability
Core Design Contradiction:
Loss of substanceVSReliability

Solution Approach 1:

The glass layer serves as a protective intermediary that prevents water from reaching the boron-containing compounds formed during high-temperature operation. This intermediary barrier maintains the benefits of oxidation protection while eliminating the water solubility problem.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The harmful water-soluble diboron trioxide is effectively 'taken out' of the system by blocking its exposure to water through the glass layer. This extraction approach removes the source of degradation while preserving the oxidation protection function.

Inventive Principle:
Principle #2Taking out (Extraction)

3Temperature

If traditional oxidation protection systems are used, then high-temperature oxidation resistance is achieved, but long-term stability in humid environments deteriorates

Engineering Contradiction:
Improvehigh-temperature performanceVSAvoidlong-term stability
Core Design Contradiction:
TemperatureVSDuration of action of stationary object

Solution Approach 1:

The multi-layer composite structure combines materials with complementary properties: boron carbide and silicon carbide for high-temperature oxidation resistance, and glass layers for long-term hydrolytic stability. This composite design allows the system to maintain both high-temperature performance and long-term stability in humid environments.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The glass layer acts as a stable intermediary that protects the underlying oxidation-resistant layers from water attack over long periods, enabling the system to maintain both high-temperature capability and long-term environmental stability.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 method significantly improves the water stability and high-temperature performance of the oxidation protection system, reducing material loss and degradation by forming a stable borosilicate layer that self-heals and resists hydrolysis.

Implementation Method 1

each of the first glass former and the second glass former may comprise colloidal silica

Methodology Applied
Scientific EffectVitrification: Vitrification

Implementation Method 2

forming a stable borosilicate layer that self-heals and resists hydrolysis

Methodology Applied
Scientific EffectChemical Bonding: Chemical Bonding

Implementation Method 3

heating the carbon-carbon composite structure

Methodology Applied
Scientific EffectSintering: Sintering

Implementation Method 4

heating the brake disk at a first temperature

Methodology Applied
Scientific EffectHeat Treatment: Heat Treatment

Implementation Method 5

oxidation protection system on a carbon-carbon composite structure

Methodology Applied
Scientific EffectOxidation resistance: Oxidation

Implementation Method 6

resists hydrolysis

Methodology Applied
Scientific EffectHydrolysis resistance: Hydrolysis

Data Source

PatentUS12344564B2Oxidation protection with improved water resistance for composites
Publication Date: 2025.07.01 GOODRICH CORP
  • US12344564B2 patent drawing
  • US12344564B2 patent drawing
  • US12344564B2 patent drawing

AI summary

Systems and methods for forming an oxidation protection system on a composite structure are provided. In various embodiments, the oxidation protection system comprises a boron-glass layer formed on the composite substrate and a silicon-glass layer formed over the boron-glass layer. Each of the boron-glass layer and the silicon-glass layer includes a glass former.