Composite Layup Forming With Vacuum Control for Wrinkle Reduction

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Solution Overview

Problem

Existing methods of forming composite materials, such as dry carbon fabrics and non-crimped fabrics, often result in inconsistencies like wrinkles due to the bulk of the materials and limitations in tooling options.

Innovation Solution

A method involving a composite layup sealed in a vacuum envelope, formed onto a tool under vacuum, with controlled vacuum levels and heating to reduce wrinkles, using sweepers like inflatable bladders or compliant wipers to apply pressure and maintain shape, followed by resin infusion.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If dry composite fabrics are formed into a part shape before infusion and cure, then the composite structure can be manufactured, but wrinkles and inconsistencies are generated during forming

Engineering Contradiction:
Improvemanufacturability of composite structureVSAvoidsurface quality of composite
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The composite layup is debulked in advance within the vacuum envelope before forming, removing excess bulk and potential wrinkle sources prior to the shaping operation. This preliminary debulking action prevents wrinkles from forming during the subsequent forming process.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

Vacuum pressure is applied through the vacuum envelope during forming to hold the composite layup against the tool. The controlled vacuum pressure ensures uniform contact and prevents wrinkle formation while maintaining the ability to form complex shapes.

Inventive Principle:
Principle #29Pneumatics and hydraulics

2Manufacturing precision

If the bulk of dry composite fabrics is reduced, then forming quality improves, but the complexity of the forming process increases

Engineering Contradiction:
Improveforming quality of compositeVSAvoidcomplexity of forming process
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The vacuum envelope serves multiple functions simultaneously: it debulks the composite layup, applies vacuum pressure during forming, and maintains the formed shape. By combining these operations in a single apparatus, the process complexity is reduced despite the multiple functions performed.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The vacuum level within the envelope is dynamically adjusted during the process - initially lower vacuum for debulking, then increased vacuum for forming and shape maintenance. This parameter change allows optimization of each process stage without requiring separate equipment.

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If composite layup is held under vacuum during forming, then wrinkles are reduced, but the control of vacuum levels becomes more complex

Engineering Contradiction:
Improvereduction of wrinkles in compositeVSAvoidvacuum control system
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The vacuum level is dynamically adjusted during the forming process - starting with lower vacuum for debulking, then increasing to higher vacuum for forming and shape maintenance. This dynamic adjustment optimizes wrinkle reduction while managing system complexity through a single controllable parameter.

Inventive Principle:
Principle #15Dynamics

4Manufacturing precision

If composite layup is debulked before forming, then forming precision improves, but the forming time increases

Engineering Contradiction:
Improveprecision of formed shapeVSAvoidforming cycle time
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

Debulking is performed as a preliminary action within the vacuum envelope before the main forming operation. By completing the debulking step in advance, the subsequent forming process proceeds more efficiently with reduced risk of wrinkles, overall optimizing the balance between precision and time.

Inventive Principle:
Principle #10Preliminary action

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 effectively reduces wrinkles and bulk in composite layups by controlling vacuum and applying pressure, ensuring precise shaping and consistent material integrity.

Implementation Method 1

A composite layup is sealed in a vacuum envelope... the composite layup is formed onto a tool while the composite layup is held under vacuum in the vacuum envelope

Methodology Applied
Scientific EffectVacuum: Vacuum

Implementation Method 2

Heating the composite layup may comprise melting at least one of a thermoplastic veil or thermoplastic stitching in the composite layup

Methodology Applied
Scientific EffectMelting: Melting

Implementation Method 3

The composite layup may be heated while under vacuum to maintain the formed shape in the composite layup by tacking the composite layup

Methodology Applied
Scientific EffectHeating: Heating

Data Source

PatentEP4606544A1Composite forming
Publication Date: 2025.08.27 THE BOEING CO
  • EP4606544A1 patent drawingFigure 1
  • EP4606544A1 patent drawingFigure 2
  • EP4606544A1 patent drawingFigure 3

AI summary

Methods of creating a formed shape into composite layups with reduced wrinkling. A composite layup is sealed in a vacuum envelope, the composite layup comprising at least one of a resin or a thermoplastic material. The composite layup is formed onto a tool while the composite layup is held under vacuum in the vacuum envelope to create a formed shape in the composite layup.