Sacrificial Overwrap for Wound-Tape Carbon Preform Densification

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Solution Overview

Problem

Carbon/carbon composites used in high-temperature applications face thermal-shock induced mechanical failure due to nonuniform thermal insulative and expansion characteristics, leading to interlaminar failure during densification, which is costly to prevent with multi-directional reinforcement.

Innovation Solution

Applying a sacrificial tape overwrap under tension to form-holding hoop stress on preforms before densification, preventing inter-layer delamination and failure without requiring additional inter-layer reinforcement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multi-directional reinforcement is used to control thermal expansion and prevent mechanical failure, then reliability is improved, but manufacturing cost increases significantly

Engineering Contradiction:
Improvepreform integrity during densificationVSAvoidmanufacturing cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

A sacrificial overwrap is applied to the preform before the densification process begins. This overwrap pre-establishes compressive hoop stress in the preform walls, which counteracts the thermal-shock induced tensile stresses that would otherwise cause interlaminar failure during densification. The overwrap is removed after densification, having served its protective function.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The sacrificial overwrap is a temporary, low-cost component that is applied before processing and removed afterward. It provides essential mechanical support during the critical densification phase but is not part of the final product, allowing cost-effective protection without permanent complexity in the carbon/carbon component.

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

2Temperature

If thick-walled fabric-based laminates are densified to produce carbon/carbon composites, then thermal protection performance is improved, but interlaminar failure occurs due to thermal-shock induced stress

Engineering Contradiction:
Improvethermal protection capabilityVSAvoidpreform integrity during densification
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The sacrificial overwrap applies compressive stress to the preform walls before thermal shock occurs. This preliminary anti-action counterbalances the tensile stresses that develop during rapid heating and densification, preventing the interlaminar cracking that would otherwise occur in thick-walled laminates.

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The overwrap changes the stress state parameters of the preform from tensile-dominant (which causes failure) to compressive-dominant (which prevents failure). By modifying the mechanical boundary conditions through the overwrap, the material can withstand the thermal shock without interlaminar failure.

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

Enables the production of low-cost, thick-walled carbon/carbon composites for thermal protection systems by controlling thermal-shock induced mechanical loading, eliminating interlaminar failure and defects during densification.

Implementation Method 1

applying a sacrificial tape overwrap to the first preform in a tensioned manner to form a second preform having the layers of preform tape subject to form-holding hoop stress by the tape overwrap

Methodology Applied
Scientific EffectTension: Tension

Implementation Method 2

layers of preform tape subject to form-holding hoop stress by the tape overwrap

Methodology Applied
Scientific EffectHoop stress:

Implementation Method 3

The second preform is then densified in a densification process to produce the densified carbon component

Methodology Applied
Scientific EffectDensification:

Data Source

PatentUS20250236047A1Manufacturing carbon-densified component using sacrificial overwrapping of wound-tape preform
Publication Date: 2025.07.24 TEXTRON SYSTEMS CORP
  • US20250236047A1 patent drawing
  • US20250236047A1 patent drawing
  • US20250236047A1 patent drawing

AI summary

A method of making a densified carbon component includes wrapping a preform tape of carbon material about a mandrel to form a first preform having a laminated, multi-layer structure, and applying a sacrificial tape overwrap to the first preform in a tensioned manner to form a second preform having the layers of preform tape subject to form-holding hoop stress by the tape overwrap. The second preform is then densified in a densification process to produce the densified carbon component. During densification, the presence of the overwrap helps to prevent undesired delamination or similar defects from occurring.