Metal Carbide Coating for Oxidation-Resistant Carbon Composites

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Solution Overview

Problem

Carbon-carbon composite materials used in high-temperature applications are susceptible to oxidation, leading to deterioration of their physio-mechanical properties due to surface voids and defects, which existing coatings fail to adequately address.

Innovation Solution

A high-temperature coating comprising a metal carbide antioxidant layer formed by reacting a deposited carbon layer with metals like silicon, titanium, or tungsten using chemical vapor deposition, which seals surface voids and forms a continuous, dense barrier against oxidation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conventional coating is applied to carbon-carbon composite substrate, then the substrate gains some oxidation resistance, but surface voids and defects remain unsealed, allowing oxidation to penetrate through the coating

Engineering Contradiction:
Improveoxidation resistanceVSAvoidoxidation penetration through surface voids
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

A carbon layer is deposited onto the surface of the composite article using chemical vapor deposition before applying the metal slurry. This preliminary carbon layer fills and seals surface voids and defects, creating a smooth, continuous barrier that prevents oxidation from penetrating through to the metal carbide coating and underlying substrate.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The deposited carbon layer serves as an intermediary between the metal carbide coating and the composite substrate. It fills surface voids and provides a continuous, defect-free interface that enhances the sealing effect, preventing oxidation pathways that would otherwise exist through surface defects in the substrate.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Productivity

If metal slurry is applied directly to the composite substrate surface, then the metal carbide forms quickly, but surface voids prevent formation of a continuous coating

Engineering Contradiction:
Improvecoating formation speedVSAvoidcoating continuity
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The carbon layer is deposited onto the composite substrate surface before applying the metal slurry. This preliminary action creates a smooth, continuous surface that eliminates voids and defects, ensuring that when the metal slurry is applied subsequently, it reacts uniformly with the carbon to form a continuous, high-quality metal carbide coating without disruptions from underlying surface defects.

Inventive Principle:
Principle #10Preliminary action

3Object-affected harmful factors

If the carbon layer is made thicker to ensure complete coverage of surface voids, then sealing effectiveness improves, but the amount of material and processing time increases

Engineering Contradiction:
Improvesurface void sealing effectivenessVSAvoidcarbon layer thickness
Core Design Contradiction:
Object-affected harmful factorsVSQuantity of substance

Solution Approach 1:

The mechanical process of building up thick carbon layers is replaced by chemical vapor deposition, which allows precise control of layer thickness and uniform deposition. The CVD process enables formation of an optimally thin yet fully effective carbon layer that seals all surface voids, as the chemical deposition mechanism ensures complete and uniform coverage at controlled thicknesses, avoiding the material waste and extended processing associated with thicker mechanical applications.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 coating effectively protects carbon-carbon composite substrates from oxidation at high temperatures, maintaining their mechanical properties and extending their service life in applications such as aerospace and hypersonic environments.

Implementation Method 1

A relatively thin carbon layer may be deposited onto the surface of the composite article using chemical vapor deposition to smooth the surface voids, seal small surface pores

Methodology Applied
Scientific EffectChemical vapor deposition: Chemical Vapour Deposition

Implementation Method 2

at least a portion of the deposited carbon layer may be reacted with a metal, such as silicon, titanium, or tungsten, in stoichiometric excess. The resulting metal carbide may form a dense antioxidant coating

Methodology Applied
Scientific EffectChemical reaction: Chemical Bonding

Data Source

PatentUS20240279129A1High temperature metal carbide coatings
Publication Date: 2024.08.22 HONEYWELL INTERNATIONAL INC
  • US20240279129A1 patent drawing
  • US20240279129A1 patent drawing
  • US20240279129A1 patent drawing

AI summary

An example method for forming a high temperature coating includes depositing a carbon layer on to a surface of a composite article using chemical vapor deposition. The composite substrate includes a composite substrate including a carbon matrix. The surface of the composite article includes one or more surface voids. The method further includes applying a metal slurry to the surface of the composite article following the deposition of the carbon layer and reacting a metal of the metal slurry with carbon of the carbon layer to form an antioxidant layer of a metal carbide on the composite article.