Amorphous PEEK Molding for Tough Dielectric Aircraft Fasteners

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Solution Overview

Problem

Basic epoxy-based composite aircraft structures are susceptible to electromagnetic effects due to their limited ability to conduct electrical currents and electromagnetic forces, necessitating the development of materials with improved dielectric properties and toughness for effective electromagnetic interference protection.

Innovation Solution

The method involves molding amorphous polyether ether ketone with a crystallinity of at most 15% by cooling a mold assembly to a temperature of at most 200°F and injecting a molten mass of polyether ether ketone, which results in a tougher material suitable for forming electromagnetic effects-protective fasteners with enhanced toughness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If conventional molding processes are used for polyether ether ketone, then the material forms a protective dielectric layer, but the material exhibits limited toughness

Engineering Contradiction:
ImprovetoughnessVSAvoidelectromagnetic effects protection
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent changes the molding parameters by cooling the mold assembly to temperatures of at most 200°F before injecting the molten polyether ether ketone. This parameter change produces an amorphous material structure with enhanced toughness while maintaining the dielectric properties necessary for electromagnetic effects protection.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent utilizes phase transition by controlling the cooling process to create an amorphous phase rather than a crystalline phase. By cooling the mold to at most 200°F and injecting molten material, the process traps the polymer in an amorphous state, which provides superior toughness compared to conventional crystalline structures.

Inventive Principle:
Principle #36Phase transitions

2Strength

If the mold assembly is cooled to at most 200°F, then amorphous polyether ether ketone is produced with enhanced toughness, but the manufacturing process complexity increases

Engineering Contradiction:
ImprovetoughnessVSAvoidmolding process complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent applies preliminary action by cooling the mold assembly to at most 200°F before injecting the molten polyether ether ketone. This pre-cooling step prepares the mold in advance to achieve the desired amorphous structure and enhanced toughness, simplifying the overall process control by establishing the temperature condition beforehand.

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 resulting amorphous polyether ether ketone provides increased toughness and improved suitability for aerospace applications, effectively protecting against electromagnetic effects by forming a more robust layer on fasteners and other aircraft components.

Implementation Method 1

cooling a mold assembly to a temperature of at most about 200° F.

Methodology Applied
Scientific EffectCooling: Cooling

Implementation Method 2

injecting the molten mass into the cooled mold assembly

Methodology Applied
Scientific EffectPhase change (molten to solid): Phase Change

Data Source

PatentUS10994460B2System and method for molding amorphous polyether ether ketone
Publication Date: 2021.05.04 THE BOEING CO
  • US10994460B2 patent drawing
  • US10994460B2 patent drawing
  • US10994460B2 patent drawing

AI summary

A method for molding amorphous polyether ether ketone including steps of preparing a molten mass including polyether ether ketone, cooling a mold assembly to a temperature of at most about 200° F., and injecting the molten mass into the cooled mold assembly.