Metal Carbide Coating for C/C Surface Voids and Oxidation

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Solution Overview

Problem

Carbon-carbon composite materials used in high-temperature applications, such as aerospace, are susceptible to oxidation, leading to deterioration of their physio-mechanical properties, and existing metal carbide-based coatings often fail to form continuous layers due to surface voids and defects.

Innovation Solution

A high temperature coating comprising a metal-rich antioxidant layer of metal carbide is formed by reacting a metal with both the surface portion and carbon powder within surface voids of the carbon-carbon composite substrate, ensuring a continuous and defect-free coating by matching the composition and morphology of the carbon powder with the substrate, thereby extending into and bridging surface voids.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a metal carbide coating is formed on a C/C composite substrate, then oxidation resistance is improved, but surface voids cause discontinuous coating and defects

Engineering Contradiction:
Improveoxidation resistanceVSAvoidcoating continuity
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

Carbon powder is applied to fill surface voids before metal carbide formation, ensuring that the reactive material is pre-positioned in void areas where coating discontinuities would otherwise occur. This preliminary action prevents coating defects rather than correcting them afterward.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

Carbon powder acts as an intermediary material that fills surface voids and provides additional reactive carbon for metal carbide formation. This intermediary substance bridges the gap between the substrate surface and the metal carbide coating, ensuring continuous coverage over void areas.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Manufacturing precision

If carbon powder is used to fill surface voids, then coating density is improved, but additional processing steps are required

Engineering Contradiction:
Improvecoating densityVSAvoidprocess complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The carbon powder application step is merged with the subsequent metal carbide formation process. The carbon powder remains on the surface to react with the metal during the same thermal processing step that forms the metal carbide coating, eliminating the need for separate carbon filling and coating formation operations.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The processing temperature and atmosphere are optimized to enable simultaneous carbon powder reaction and metal carbide formation. By controlling the thermal parameters, both the carbon powder fills voids and reacts to form metal carbide in a single integrated process step.

Inventive Principle:
Principle #35Parameter changes

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 resulting coating provides enhanced resistance to oxidation and environmental attack, maintaining structural integrity at extreme temperatures by forming a dense, uniform, and continuous metal carbide layer that protects the substrate from oxidizing species.

Implementation Method 1

reacting a metal of the metal slurry with carbon of the carbon powder and carbon of the surface portion of the C/C composite substrate to form a metal-rich antioxidant layer of a metal carbide

Methodology Applied
Scientific EffectChemical reaction: Chemical Bonding

Implementation Method 2

applying carbon powder to a surface of a carbon/carbon (C/C) composite substrate to force the carbon powder into one or more surface voids

Methodology Applied
Scientific EffectMechanical force: Mechanical Force

Data Source

PatentUS12172934B2High temperature metal carbide coatings
Publication Date: 2024.12.24 HONEYWELL INTERNATIONAL INC
  • US12172934B2 patent drawing
  • US12172934B2 patent drawing
  • US12172934B2 patent drawing

AI summary

A method for forming a high temperature coating includes applying carbon powder to a surface of a carbon/carbon (C/C) composite substrate to force the carbon powder into one or more surface voids of the surface of the C/C composite substrate. The carbon powder has a substantially same composition and morphology as a surface portion of the C/C composite substrate. The method includes applying a metal slurry to the surface of the C/C composite substrate following the application of the carbon powder and reacting a metal of the metal slurry with carbon of the carbon powder and carbon of the surface portion of the C/C composite substrate to form a metal-rich antioxidant layer of a metal carbide on the C/C composite substrate.