Ceramic Composite Repair Inserts for Thermomechanical Integrity

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Solution Overview

Problem

Existing methods for repairing ceramic composite components, particularly those used in high-temperature applications like gas turbine engines, are inadequate in addressing non-conforming or damaged areas effectively, especially in terms of maintaining thermomechanical properties and structural integrity.

Innovation Solution

A method involving the use of additive manufacturing to fabricate a monolithic ceramic repair insert with a CMC face sheet, which is bonded and consolidated with the component using heat treatment and chemical processes like pyrolysis and melt-infiltration, tailored to the specific geometry of the repair area.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional repair methods are used for ceramic composite components, then the repair process is simpler, but the thermomechanical properties and structural integrity are compromised

Engineering Contradiction:
Improvestructural integrityVSAvoidrepair process complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The repair insert is divided into distinct functional zones: a monolithic ceramic body for structural support and CMC face sheets for surface integration. This segmentation allows each zone to be optimized for its specific function while maintaining overall structural integrity during repair

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The repair insert is pre-fabricated with the exact geometry matching the damaged area using additive manufacturing. This preliminary action ensures precise fit and minimizes differential shrinkage before the actual repair process begins

Inventive Principle:
Principle #10Preliminary action

Solution Approach 3:

The repair insert combines monolithic ceramic and CMC materials in a single component. This composite structure allows the insert to match the thermomechanical properties of the original ceramic composite component, ensuring compatibility and structural integrity

Inventive Principle:
Principle #40Composite materials

2Manufacturing precision

If a generic repair insert is used, then the manufacturing process is easier, but the fit and performance in specific repair areas are inadequate

Engineering Contradiction:
Improvegeometry matchingVSAvoidcustom fabrication
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The additive manufacturing process allows for precise control of geometric parameters of the repair insert. By changing parameters such as lattice structure, density, and dimensional tolerances during fabrication, the insert achieves exact geometry matching with the damaged area while maintaining manufacturability

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The repair insert features locally optimized properties: the monolithic ceramic body provides structural strength in the core region, while CMC face sheets provide surface compatibility. This local quality differentiation achieves precise geometry matching without requiring the entire component to be custom-fabricated

Inventive Principle:
Principle #3Local quality

3Stability of the object's composition

If materials with different thermal expansion coefficients are used in repair, then material selection is easier, but differential shrinkage and stress are increased

Engineering Contradiction:
Improvethermomechanical compatibilityVSAvoidmaterial selection flexibility
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The repair insert uses a composite structure combining monolithic ceramic and CMC materials. This allows selection of materials with matched thermal expansion coefficients to the original component, ensuring thermomechanical compatibility and minimizing differential shrinkage while maintaining structural versatility

Inventive Principle:
Principle #40Composite materials

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 method provides improved thermomechanical properties and minimizes differential shrinkage, ensuring the repaired component maintains structural integrity and performance in extreme conditions.

Implementation Method 1

bonding and consolidated with the component through heat treatment and chemical processes like pyrolysis and melt-infiltration

Methodology Applied
Scientific EffectPyrolysis: Pyrolysis

Implementation Method 2

bonding and consolidated with the component through heat treatment and chemical processes like pyrolysis and melt-infiltration

Methodology Applied
Scientific EffectMelt-infiltration: Melting

Data Source

PatentUS20250276941A1Method for repairing ceramic composite components
Publication Date: 2025.09.04 GENERAL ELECTRIC CO
  • US20250276941A1 patent drawing
  • US20250276941A1 patent drawing
  • US20250276941A1 patent drawing

AI summary

A method for repairing a component that comprises a ceramic matrix composite (“CMC”) material includes forming a repair insert defined by a repair geometry where the repair geometry is based on a repair area of the component, and the repair insert comprises a monolithic ceramic. Inserting the repair insert into the repair area and applying a CMC face sheet to the repair insert. The method further includes bonding the repair insert to the CMC face sheet, the repair insert to the component, and the CMC face sheet to the component. The method also includes thermally processing and densifying at least one of the repair insert or the CMC face sheet in the repair area.