Contoured Composite Stiffener Fabrication via Variable Mandrel Geometry

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Solution Overview

Problem

The existing methods for fabricating composite structures, such as stiffeners, often result in wrinkling due to deformation and high friction during the lay-up process, especially when forming over contoured surfaces, leading to undesirable properties, material waste, and increased thickness and weight.

Innovation Solution

A method and apparatus that tailor the geometry of a lay-up mandrel to accommodate the material characteristics of the stiffener, allowing continuous fiber reinforcement without wrinkling by selectively widening or narrowing the mandrel to match the stiffener's curvature, thereby eliminating the need for cutting and splicing plies.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If pre-preg plies are cut into sections and spliced together to form contoured stiffeners, then the contour curvature can be achieved, but the structural properties are reduced and additional plies are required increasing thickness and weight

Engineering Contradiction:
Improvecontour curvatureVSAvoidstructural properties
Core Design Contradiction:
ShapeVSStrength

Solution Approach 1:

The mandrel is designed with variable cross-sectional geometry that dynamically adapts to the desired stiffener contour. By selectively widening or narrowing the mandrel cross-section along its length, the apparatus enables continuous fiber reinforcement to conform to complex curvatures without cutting or splicing, thereby maintaining structural integrity while achieving the required shape

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The mandrel geometry parameters (cross-sectional width, height, and contour profile) are specifically tailored to match the desired stiffener geometry. By changing the mandrel parameters along its length, the system enables continuous plies to be formed into contoured shapes without compromising fiber continuity or requiring additional corrective plies

Inventive Principle:
Principle #35Parameter changes

2Shape

If pre-preg plies are cut and spliced to achieve desired curvature, then the contour can be formed, but the manufacturing process becomes time consuming and labor intensive

Engineering Contradiction:
Improvedesired curvatureVSAvoidmanufacturing speed
Core Design Contradiction:
ShapeVSProductivity

Solution Approach 1:

The variable cross-sectional mandrel provides a continuous, pre-configured form that guides the lay-up of continuous plies directly into the final contoured shape. This eliminates the need for sequential cutting, splicing, and positioning operations, significantly reducing manufacturing time and labor requirements while maintaining the desired curvature

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The mandrel is pre-formed with the exact variable geometry required for the final stiffener contour. This preliminary preparation of the forming surface allows continuous plies to be draped and consolidated directly into the final shape in a single operation, eliminating subsequent machining or assembly steps

Inventive Principle:
Principle #10Preliminary action

3Shape

If pre-preg plies are cut and spliced to form contoured stiffeners, then the curvature can be achieved, but material waste increases

Engineering Contradiction:
ImprovecurvatureVSAvoidmaterial waste
Core Design Contradiction:
ShapeVSLoss of substance

Solution Approach 1:

The variable cross-sectional mandrel is designed to exactly match the desired stiffener geometry, allowing continuous plies to be formed to the precise final dimensions. This eliminates the need for over-material application and subsequent trimming, as well as the waste associated with cutting and splicing operations, thereby minimizing material loss

Inventive Principle:
Principle #15Dynamics

4Strength

If additional plies or doublers are added to compensate for cutting and splicing, then structural properties can be maintained, but the thickness and weight of the stiffener increase

Engineering Contradiction:
Improvestructural propertiesVSAvoidstiffener weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The variable cross-sectional mandrel enables continuous fiber reinforcement to be formed directly into the final contoured stiffener geometry without cutting or splicing. This maintains full structural properties with the minimum required ply count, eliminating the need for additional weight-bearing doublers or plies that would be required to compensate for discontinuities created by cutting and splicing

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP2433781B1Method and apparatus for fabricating highly contoured composite stiffeners with reduced wrinkling
Publication Date: 2020.08.26 THE BOEING CO
  • EP2433781B1 patent drawingFigure 1~3
  • EP2433781B1 patent drawingFigure 4~5
  • EP2433781B1 patent drawingFigure 6~7

AI summary

A mandrel having an out-of-plane curvature and a corresponding in-plane change in mandrel geometry is used to fabricate substantially wrinkle-free, fiber reinforced stiffeners having an out-of-plane curvature.