Pin Array for Ceramic Matrix Composite Preform Compression

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Solution Overview

Problem

The processing of ceramic matrix composites (CMCs) faces challenges with uneven matrix infiltration due to tortuous pore networks and surface deformations caused by z-channel formation, leading to defects in composite properties, particularly in gas turbine engines.

Innovation Solution

A pin array is used to apply a compressive force on the preform surface through infiltration holes in a tooling fixture, minimizing surface deformations and facilitating uniform matrix densification by aligning pins with z-channels to prevent fraying and excess matrix formation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If z-channels are formed to create direct pathways for reactant gases, then infiltration efficiency is improved, but surface deformations and defects are created

Engineering Contradiction:
Improveinfiltration efficiencyVSAvoidsurface deformation
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The pin array is introduced to apply preliminary compressive force to the preform surface during or after z-channel formation, counteracting the surface deformations and fiber fraying that occur during needle perforation. This preliminary anti-action prevents the formation of defects that would otherwise compromise the preform surface quality.

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The pin array serves as an intermediary element between the z-channel formation process and the final preform surface quality. By inserting pins into the preform during perforation, the pins mediate the mechanical stresses and distribute forces uniformly, preventing direct damage to the fiber structure and reducing surface deformations.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Manufacturing precision

If compressive force is applied to minimize surface deformations, then manufacturing precision is improved, but additional process complexity is introduced

Engineering Contradiction:
Improvesurface deformationVSAvoidprocess complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The compressive force application is segmented into discrete pin locations corresponding to z-channel positions, rather than applying uniform compression across the entire preform surface. This segmentation allows targeted intervention only where needed, simplifying the overall process while maintaining precision.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The pin array is designed to be self-aligning with the z-channel locations, where pins automatically position themselves at the correct locations during the perforation process. This self-service mechanism eliminates the need for complex alignment systems or additional positioning steps, reducing process complexity while maintaining manufacturing precision.

Inventive Principle:
Principle #25Self-service

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 ensures more uniform densification of CMCs, reducing thermal and aerodynamic impacts by minimizing surface defects and promoting even matrix infiltration, thereby enhancing the properties of CMCs for aerospace applications.

Implementation Method 1

pushing a pin array against a surface of the preform through infiltration holes in the tooling fixture to apply a compressive force on the preform

Methodology Applied
Scientific EffectCompressive force: Compression

Implementation Method 2

The pore network through a woven system is often highly tortuous for infiltrating reactant vapors, which leads to uneven deposition through the thickness of the preform

Methodology Applied
Scientific EffectVapor infiltration: Permeation

Data Source

PatentEP4446076A1A method of forming a ceramic matrix composite, and a pin array
Publication Date: 2024.10.16 RTX CORP
  • EP4446076A1 patent drawingFigure 1
  • EP4446076A1 patent drawingFigure 2
  • EP4446076A1 patent drawingFigure 3

AI summary

A method of forming a ceramic matrix composite includes arranging a plurality of ceramic fibers into a preform (10), mounting the preform (10) within a tooling fixture (18), perforating the preform (10) to form a plurality of z-channels (16), each of the plurality of z-channels (16) extending completely through a thickness of the preform (10), pushing a pin array (24) against a surface (12) of the preform (10) through infiltration holes (20) in the tooling fixture (18) to apply a compressive force on the preform (10), and subsequently, removing the pin array (24) from the surface (12) of the preform (10). The pin array (24) includes a plurality of pins (26) extending from a backplate (28). Each of the plurality of pins (26) is aligned with a respective infiltration hole (20) of the tooling fixture (18).