SMP Mandrel for Composite Part Fabrication

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Solution Overview

Problem

Current methods for fabricating composite parts are hindered by the difficulty and cost of removing rigid cure tools or mandrels, which often require destruction or are expensive and time-consuming, and existing solutions for reusable mandrels lack strength and rigidity.

Innovation Solution

The use of shape memory polymer (SMP) apparatuses that can change modulus from rigid to malleable states through temperature changes, allowing for the compression of composite materials against a mold during curing and easy removal by inducing a pressure differential, enabling the reuse of the SMP apparatus.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a rigid cure tool or mandrel is used to fabricate composite parts, then the composite material can be properly supported and cured, but the mandrel becomes difficult and costly to remove, often requiring destruction or segmentation

Engineering Contradiction:
Improvemandrel rigidityVSAvoidmandrel removal
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The mandrel material's mechanical properties are changed by altering its temperature. At low temperatures, the SMP mandrel is rigid to support composite layup. At high temperatures (above glass transition temperature), the mandrel becomes soft and rubbery, enabling easy removal from the cured composite part without destruction or segmentation.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The mandrel is made from shape memory polymer (SMP) material, which is a composite material that combines rigid structural properties at low temperature with flexible removable properties at high temperature. This allows the same material to provide both structural support during manufacturing and ease of removal after curing.

Inventive Principle:
Principle #40Composite materials

2Ease of operation

If a segmented mandrel is used to facilitate removal, then the mandrel can be disassembled and removed after curing, but the installation and removal process becomes time-consuming and expensive

Engineering Contradiction:
Improvemandrel removalVSAvoidmandrel installation and removal time
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

Instead of segmenting the mandrel structure, the invention changes the material's physical state through temperature. The SMP mandrel transitions from rigid to soft by heating above its glass transition temperature, allowing single-piece removal without time-consuming segmentation or complex installation procedures.

Inventive Principle:
Principle #35Parameter changes

3Ease of operation

If an inflatable mandrel is used to enable removal by deflation, then the mandrel can be removed after curing, but the mandrel lacks strength and rigidity during composite lay-up

Engineering Contradiction:
Improvemandrel removalVSAvoidmandrel rigidity during lay-up
Core Design Contradiction:
Ease of operationVSStrength

Solution Approach 1:

The SMP mandrel provides rigidity at low temperatures for proper composite support during layup, then transitions to a soft, flexible state at high temperatures for easy removal. This eliminates the need for inflatable structures while maintaining both structural integrity during manufacturing and ease of removal after curing.

Inventive Principle:
Principle #35Parameter changes

4Ease of repair

If foam tooling with silicon coating is used, then the silicon bag can be removed and reused, but the foam tooling itself is not reusable and must be machined out of new foam each cycle

Engineering Contradiction:
Improvesilicon bag reusabilityVSAvoidtooling reusability
Core Design Contradiction:
Ease of repairVSProductivity

Solution Approach 1:

The entire mandrel is made from SMP material that can be reused indefinitely. After curing, the SMP mandrel is heated above its glass transition temperature to become soft and rubbery, allowing easy removal from the composite part. The mandrel can then be cooled and reused for the next production cycle, eliminating the need to machine new foam tooling each time.

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

This method facilitates efficient fabrication and removal of composite parts with integrated stiffeners, reducing production costs and time, while allowing the SMP apparatus to be reused multiple times, maintaining structural integrity during the process.

Implementation Method 1

triggering a change in modulus of the SMP apparatus from a rigid state to a malleable state

Methodology Applied
Scientific EffectShape memory polymer phase transition: Phase Change

Implementation Method 2

systems and methods for using a reusable apparatus made of shape memory polymer (SMP)

Methodology Applied
Scientific EffectShape memory polymer effect: Shape Memory Polymer

Implementation Method 3

inducing a pressure differential that drives the SMP apparatus, in its malleable state, toward the composite material before and/or during cure to compress the composite material against a rigid mold

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Data Source

PatentEP2637838B1Methods for forming integral composite parts with a SMP apparatus
Publication Date: 2015.08.26 SPIRIT AEROSYSTEMS INC
  • EP2637838B1 patent drawingFigure 1~2
  • EP2637838B1 patent drawingFigure 3~4
  • EP2637838B1 patent drawingFigure 5~6a

AI summary

A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as a rigid lay-up tool. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. The composite material and/or nested components may be heated and compressed against the SMP apparatus. The SMP apparatus may be configured to remain rigid during the composite cure cycle. Once the composite material is cured, the SMP apparatus may be triggered to a malleable state and urged away from the cured composite material.