Composite Stiffener Run-Out Drapeability via Fabric Substitution

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Solution Overview

Problem

Manufacturing composite stringers with complex geometry, such as run-out regions, often results in wrinkling and defects due to poor drapeability of non-crimp fabric layers, which can lead to stress points and reduced performance.

Innovation Solution

The use of non-crimp fabric blankets combined with woven fibre layers, where the non-crimp blankets are either dropped off or cut to form darts in the transition region, allowing only woven fibre layers in the run-out region to improve drapeability and stress performance, and a method of co-infusing and co-curing dry fabrics on a mould tool to form the stiffener without intermediate cutting steps.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If non-crimp fabric blankets are used in the run-out region, then load carrying performance is improved, but drapeability deteriorates causing wrinkling and manufacturing defects

Engineering Contradiction:
Improveload carrying performanceVSAvoiddrapeability
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent applies different fabric types in different regions: non-crimp fabric blankets are used in the constant section region where load carrying performance is critical, while woven fabric is used in the run-out region where drapeability is required to conform to the changing geometry without wrinkling. This local differentiation resolves the contradiction between strength and ease of manufacture.

Inventive Principle:
Principle #3Local quality

2Productivity

If non-crimp fabric blankets are used throughout the stiffener, then manufacturing speed is improved, but manufacturing precision deteriorates due to wrinkling and defects in complex geometry regions

Engineering Contradiction:
Improvemanufacturing speedVSAvoidgeometric accuracy
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The patent switches from non-crimp fabric blankets to woven fabric in the run-out region where complex geometry requires high drapeability for accurate forming. This local material substitution maintains manufacturing speed while improving geometric accuracy in the critical termination region.

Inventive Principle:
Principle #3Local quality

3Ease of manufacture

If non-crimp fabric blankets are cut to form darts to accommodate run-out geometry, then drapeability is improved, but manufacturing complexity increases

Engineering Contradiction:
ImprovedrapeabilityVSAvoidmanufacturing process complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The patent extracts the non-crimp fabric blankets from the run-out region entirely, replacing them with woven fabric that inherently provides the required drapeability without requiring dart cutting or other complex modifications. This simplifies the manufacturing process while maintaining ease of forming.

Inventive Principle:
Principle #2Taking out (Extraction)

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

This approach enhances the manufacturability and performance of composite stiffeners by reducing defects and stress points, improving drapeability, and eliminating the need for post-curing cutting, thereby reducing costs and time.

Implementation Method 1

The fibre layers are joined together, e.g. by stitching, to form the blanket.

Methodology Applied
Scientific EffectStitching: Mechanical Fastener

Implementation Method 2

a method of co-infusing and co-curing dry fabrics on a mould tool to form the stiffener

Methodology Applied
Scientific EffectCo-infusing and co-curing: Photopolymerisation

Data Source

PatentEP3702142B1Composite stiffener
Publication Date: 2024.02.14 AIRBUS OPERATIONS LTD
  • EP3702142B1 patent drawingFigure 1~3
  • EP3702142B1 patent drawingFigure 4~6
  • EP3702142B1 patent drawingFigure 7~8

AI summary

A composite stiffener for a stiffener reinforced panel. The stiffener has a longitudinal direction and a run-out region which terminates at an end of the stiffener. The stiffener also has a constant section region inboard of the run-out region in the longitudinal direction and having a constant cross section transverse to the longitudinal direction with a crown between adjacent foot portions. The run-out region has a changing cross section transverse to the longitudinal direction with a crown between adjacent foot portions and the crown reduces in height towards the end of the stiffener forming a ramp. The composite stiffener comprises a number of blankets of non-crimp fabric layers.