C/C Friction Disk Coating for Oxidation and Wear Protection

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Solution Overview

Problem

Aircraft carbon/carbon (C/C) friction disks face challenges with oxidation protection and wear improvement, leading to reduced performance and increased maintenance needs.

Innovation Solution

A method involving the application of multiple coatings to densified C/C friction disks, including a first coating of boron carbide powder, a second coating of aluminum and silicon, and additional coatings of aluminum oxide, phosphoric acid derivatives, and glass compositions, to provide comprehensive oxidation protection and wear improvement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multiple coating layers are applied to the C/C friction disk, then oxidation resistance and wear durability are significantly enhanced, but the manufacturing complexity and process time increase

Engineering Contradiction:
Improveoxidation resistance and wear durabilityVSAvoidmanufacturing complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The protective coating system is divided into multiple functional layers: a first coating containing boron carbide powder applied to non-wear surfaces for oxidation protection, and a second coating containing aluminum and silicon applied to wear surfaces for wear resistance. Each layer serves a specific protective function, allowing the system to achieve comprehensive protection while maintaining manageable manufacturing complexity through functional segmentation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs composite coating materials combining different substances with complementary properties. The first coating uses boron carbide powder known for its oxidation resistance, while the second coating uses aluminum and silicon compounds for wear protection. These composite material combinations enable the C/C friction disk to simultaneously achieve both oxidation resistance and wear durability without requiring a single complex material.

Inventive Principle:
Principle #40Composite materials

2Reliability

If multiple coating layers are applied to the C/C friction disk, then oxidation resistance and wear durability are significantly enhanced, but the production time and processing steps increase

Engineering Contradiction:
Improvewear durabilityVSAvoidproduction time
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The coating components are prepared as pre-formulated mixtures containing the necessary powders, surfactants, and carrier fluids before application. The first coating mixture is prepared with boron carbide powder and applied to non-wear surfaces, followed by the second coating mixture with aluminum and silicon applied to wear surfaces. This preliminary preparation of coating mixtures streamlines the manufacturing process and reduces overall production time.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent specifies controlled thickness parameters for each coating layer (0.0002 to 0.003 inches) and uses carrier fluids that facilitate uniform application and controlled drying. By optimizing these parameters, the multi-layer coating process achieves efficient production with reduced processing time while maintaining the required protective performance.

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 coating method significantly enhances the oxidation resistance and wear durability of C/C friction disks, leading to increased landings per overhaul (LPO) and reduced oxidation fallout during maintenance.

Implementation Method 1

a first coating to a radially inward non-wear surface and a radially outward non-wear surface of the densified C/C friction disk... The first coating is a mixture including boron carbide (B4C) powder

Methodology Applied
Scientific EffectOxidation protection: Oxidation

Implementation Method 2

a second coating to the radially inward non-wear surface, the radially outward non-wear surface, and the wear surfaces of the densified C/C friction disk... the second coating is a mixture including aluminum (Al), silicon (Si)

Methodology Applied
Scientific EffectWear improvement: Wear

Implementation Method 3

a third coating to the to the radially inward non-wear surface and the radially outward non-wear surface of the densified C/C friction disk... the third coating is a mixture of aluminum oxide (Al2O3)

Methodology Applied
Scientific EffectOxidation resistance: Oxidation

Data Source

PatentUS20250154996A1Coating of a carbon/carbon (c/c) disk providing oxidation protection and wear improvement
Publication Date: 2025.05.15 GOODRICH CORP
  • US20250154996A1 patent drawing
  • US20250154996A1 patent drawing
  • US20250154996A1 patent drawing

AI summary

A method is provided for providing oxidation protection and wear improvement for a densified carbon/carbon (C/C) friction disk. The method includes applying a first coating to a radially inward non-wear surface and a radially outward non-wear surface of the densified C/C friction disk and applying a second coating to the radially inward non-wear surface, the radially outward non-wear surface, and the wear surfaces of the densified C/C friction disk.