Polygonal Tow Preforms for Ceramic Matrix Composites

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Solution Overview

Problem

Conventional three-dimensional textile preform fabrication processes for ceramic matrix composites (CMCs) face challenges in controlling filament packing and minimizing damage to filaments, leading to suboptimal mechanical and physical properties due to the abrasive nature of the processes and difficulties in matrix infiltration.

Innovation Solution

The process involves producing tows with predetermined polygonal cross-sectional shapes embedded in a temporary matrix, allowing for controlled filament packing and protection during fabrication, with the temporary matrix being removable to facilitate uniform infiltration by a ceramic matrix material.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If conventional three-dimensional textile preform fabrication processes are used, then the preform can be manufactured, but filament packing control is poor and filament damage occurs due to the abrasive nature of the process

Engineering Contradiction:
Improvefilament packing controlVSAvoidfilament damage
Core Design Contradiction:
Manufacturing precisionVSObject-affected harmful factors

Solution Approach 1:

A sizing agent is applied to the tow as an intermediary substance between the filament and the weaving/braiding process. This sizing agent reduces friction and abrasion during preform fabrication, protecting the filament while enabling controlled packing through the combination of sizing and subsequent debonding steps.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The tow is pre-shaped and sized before the actual preform fabrication process. This preliminary preparation establishes controlled filament packing and protective coating in advance, preventing damage during the abrasive weaving or braiding operations that follow.

Inventive Principle:
Principle #10Preliminary action

2Volume of moving object

If large tow sizes are used to obtain desired part dimensions, then the part dimensions can be achieved, but filament breakage increases due to the abrasive preforming process

Engineering Contradiction:
Improvepart dimensionsVSAvoidfilament integrity
Core Design Contradiction:
Volume of moving objectVSReliability

Solution Approach 1:

The sizing agent serves as a protective intermediary that enables the use of large tow sizes without proportionally increasing filament breakage. The sizing reduces abrasion during handling and preforming, allowing large tows to maintain filament integrity while achieving the required part dimensions.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The filament surface properties are changed through application of sizing agents with specific friction-reducing characteristics. This parameter change protects filaments during the mechanical stress of large tow preforming while maintaining the structural integrity needed for large part dimensions.

Inventive Principle:
Principle #35Parameter changes

3Volume of moving object

If large tow sizes are used, then part dimensions can be achieved, but matrix infiltration becomes difficult

Engineering Contradiction:
Improvepart dimensionsVSAvoidmatrix infiltration uniformity
Core Design Contradiction:
Volume of moving objectVSManufacturing precision

Solution Approach 1:

The tow is pre-shaped with a specific cross-sectional geometry and filament packing structure before preform fabrication. This preliminary shaping creates optimal conditions for subsequent matrix infiltration by ensuring uniform spacing and accessibility, enabling complete infiltration even with large tow sizes.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The tow structure is optimized locally with specific filament packing densities and cross-sectional shapes in different regions. This local optimization ensures that matrix material can infiltrate uniformly throughout the preform while maintaining the large overall dimensions required for the part.

Inventive Principle:
Principle #3Local quality

4Shape

If mechanical or ultrasonic fluffing techniques are used on two-dimensional fabrics, then fiber spreading is achieved, but these techniques are not effective for three-dimensional fabrics

Engineering Contradiction:
Improvefiber spreadingVSAvoidapplicability to three-dimensional fabrics
Core Design Contradiction:
ShapeVSAdaptability or versatility

Solution Approach 1:

The desired fiber spreading and tow shape are achieved during the preform fabrication process itself through the interaction of sized tows with the weaving or braiding mechanism. This preliminary action eliminates the need for subsequent fluffing operations and directly creates the optimal structure for matrix infiltration in three-dimensional fabrics.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS8663778B2Preforms, composite components formed therewith, and processes therefor
Publication Date: 2014.03.04 GENERAL ELECTRIC CO
  • US8663778B2 patent drawing
  • US8663778B2 patent drawing

AI summary

A three-dimensional preform, composite components formed with the preform, and processes for producing the preform and composite materials. The three-dimensional preform includes first and second sets of tows containing filaments. Each tow of the first set has a predetermined polygonal cross-sectional shape and is embedded within a temporary matrix. The preform is fabricated from the first and second sets of tows, in which the second set of tows are transverse to the first set of tows, adjacent tows of the second set are spaced apart to define interstitial regions therebetween, and the polygonal cross-sectional shapes of the first set of tows are substantially congruent to the cross-sectional shapes of the interstitial regions so as to substantially fill the interstitial regions.