Ceramic-Coated Carbon-Carbon Seal Ring for Oxidation Resistance

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Solution Overview

Problem

Gas turbine engine components, particularly seals, experience wear and oxidation issues that reduce their lifetime and effectiveness, necessitating improved wear protection and oxidation resistance.

Innovation Solution

A carbon-carbon composite seal ring with a monoaluminum phosphate binder layer and a ceramic layer, such as SiC or Si3N4, applied via atomic layer deposition, provides enhanced oxidation resistance and fills sub-surface porosity to extend the seal's lifetime.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If carbon-carbon composite seal ring is used, then wear resistance is improved, but oxidation resistance deteriorates

Engineering Contradiction:
Improvewear resistanceVSAvoidoxidation resistance
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The seal ring uses a composite structure combining carbon-carbon composite material with ceramic coating layers. The carbon-carbon composite provides wear resistance while the ceramic coating (such as silicon carbide, silicon nitride, or oxidation-resistant ceramic) provides oxidation resistance, creating a multi-functional composite material system that resolves the contradiction between wear resistance and oxidation resistance.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The ceramic coating is applied selectively to specific surfaces of the seal ring that are most susceptible to oxidation, while maintaining the carbon-carbon composite structure in areas requiring high wear resistance. This localized application optimizes both properties where needed most.

Inventive Principle:
Principle #3Local quality

2Object-affected harmful factors

If ceramic layer is applied to protect seal ring, then oxidation resistance is improved, but manufacturing complexity increases

Engineering Contradiction:
Improveoxidation resistanceVSAvoidmanufacturing complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The ceramic coating is applied as a pre-manufacturing step during the seal ring production process, before the seal ring is installed in the engine. This preliminary application of protective coating integrates the oxidation protection into the manufacturing workflow, reducing the need for separate post-manufacturing treatment steps and maintenance interventions.

Inventive Principle:
Principle #10Preliminary action

3Strength

If binder layer is applied on seal ring surface, then adhesion is improved, but surface finish complexity increases

Engineering Contradiction:
ImproveadhesionVSAvoidsurface finish complexity
Core Design Contradiction:
StrengthVSManufacturing precision

Solution Approach 1:

A binder layer (such as aluminum phosphate binder) is introduced as an intermediary substance between the carbon-carbon composite seal ring substrate and the ceramic coating. This binder layer enhances the adhesion and bonding between the two materials, ensuring the ceramic coating remains firmly attached to the seal ring during operation, while the binder is selected to be compatible with both surfaces.

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 carbon-carbon composite seal ring with a ceramic layer significantly improves oxidation resistance and wear protection, extending the seal's operational life and maintaining sealing effectiveness.

Implementation Method 1

applying a ceramic layer over the binder layer on at least one surface of the seal by atomic layer deposition

Methodology Applied
Scientific EffectAtomic layer deposition:

Data Source

PatentUS20260043354A1Protective treatment and method of applying the same
Publication Date: 2026.02.12 RTX CORP
  • US20260043354A1 patent drawing
  • US20260043354A1 patent drawing
  • US20260043354A1 patent drawing

AI summary

A sealing system includes a shaft, a rotor configured to rotate with respect to the shaft, and a carbon-carbon composite seal ring arranged around the shaft such that it seals against the rotor. The carbon-carbon composite seal ring includes a monoaluminum phosphate binder layer disposed on at least one surface of the carbon-carbon composite seal ring and a ceramic layer disposed over the monoaluminum phosphate binder layer on the least one surface of the carbon-carbon composite seal ring. A method of manufacturing a seal is also disclosed.