Fiber Composite Preform Forming via Tensioned Clamping

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Solution Overview

Problem

Conventional methods for forming composite preforms with aggressive bends result in kinks and wrinkles, particularly at convex curves, due to the tendency of fibers in compression to wrinkle when bent, which can weaken the flange and are difficult to smooth.

Innovation Solution

The method involves displacing the neutral axis of the preform below the flanges by clamping the laminate under tension, ensuring all fibers are under tension during bending, thereby preventing wrinkles by maintaining fibers in tension and avoiding compression-induced wrinkling.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If conventional forming methods are used to create aggressive bends in preforms, then the preform can achieve the desired bent shape, but wrinkles and kinks form at the convex curves of the bend

Engineering Contradiction:
Improvebent shapeVSAvoidsurface quality
Core Design Contradiction:
ShapeVSManufacturing precision

Solution Approach 1:

The method applies preliminary tension to the laminate before bending occurs. By clamping the lateral edges of the laminate to the tooling in a tensioned state before the male tool is bent, the laminate is pre-conditioned to resist wrinkling during the subsequent bending operation. This preliminary action of tensioning prevents the formation of wrinkles and kinks at convex curves while allowing the desired bent shape to be achieved.

Inventive Principle:
Principle #10Preliminary action

2Manufacturing precision

If portions of the laminate are cut out to remove excess material at bend areas, then wrinkles can be reduced, but the fibers of the laminate are cut which weakens the flange

Engineering Contradiction:
Improvesurface qualityVSAvoidflange strength
Core Design Contradiction:
Manufacturing precisionVSStrength

Solution Approach 1:

The method changes the stress state parameter of the laminate from compression to tension during bending. By maintaining the laminate in a tensioned state through clamping the lateral edges to the tooling, the physical condition of the fibers is altered so they remain in tension during bending. This parameter change prevents wrinkling without requiring material removal, thereby preserving the integrity and strength of the flange.

Inventive Principle:
Principle #35Parameter changes

3Shape

If the male tool is bent along a longitudinal axis to create convex curves, then the desired preform geometry is achieved, but the laminate on the outside flange surface forms wrinkles due to compression

Engineering Contradiction:
Improvepreform geometryVSAvoidwrinkles
Core Design Contradiction:
ShapeVSObject-generated harmful factors

Solution Approach 1:

The method applies a counteracting tensile force to the laminate to offset the compressive forces that would normally cause wrinkling during bending. By clamping the lateral edges of the laminate to the tooling in tension, a counterbalancing tension is introduced that opposes the compression generated at convex curves during bending. This counterweight effect prevents wrinkles from forming while allowing the male tool to be bent into the desired geometry.

Inventive Principle:
Principle #8Anti-weight (Counterweight)

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 allows for the formation of preforms with complex geometries and double curvature designs without wrinkles, enhancing the structural integrity of the preform by maintaining fibers under tension throughout the bending process.

Implementation Method 1

Clamp the lateral edges of the laminate to the tooling such that the web and the flange of the laid-up laminate are in tension

Methodology Applied
Scientific EffectTension: Tension

Implementation Method 2

The method uses the concept of neutral axis, which is an axis of a cross section of a beam (a member resisting bending) or shaft along which there are no longitudinal stresses or strains. The method of the invention displaces the neutral axis below the flanges by placing the entire preform under tension.

Methodology Applied
Scientific EffectNeutral axis displacement:

Data Source

PatentUS11518067B2Method for forming fiber composite preforms
Publication Date: 2022.12.06 AIRBUS OPERATIONS SL
  • US11518067B2 patent drawing
  • US11518067B2 patent drawing
  • US11518067B2 patent drawing

AI summary

A method for forming fiber composite preforms, the preform (1) include a web (2), a flange (3) and a bent part (2.1), and the method includes: laying-up a laminate (4) onto a tooling (5), the laminate (4) comprising lateral and transverse edges (4.1, 4.2) and the tooling (5) comprising a male part (7) comprising a surface (7.1) and a lateral wall (7.2), the web (2) being configured to be located over the surface (7.1) of the male part (7) and the flange (3) being configured to be located over the lateral wall (7.2) of the male part (7); forming the preform (1) over the male part (7); clamping the lateral edges (4.2) of the laminate (4) to the tooling (5) such that the web (2) and the flange (3) of the laid-up laminate (4) are kept under tensional loads, and bending a longitudinal portion of the male part (7).