Preformed Dielectric Inserts for Composite Lightning Protection

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current methods for lightning strike protection in aircraft composite structures are labor-intensive, interfere with aerodynamic dimensional tolerances, and generate waste due to the in-place curing and shaving of dielectric sealants, which are not suitable for all production environments and can damage the surface.

Innovation Solution

The use of preformed dielectric inserts with a complimentary shape to recessed fasteners, coated with adhesive, which are inserted and secured to provide a smooth surface, reducing installation and inspection time, and improving precision in meeting dimensional tolerances.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If in-place curing and shaving of dielectric sealant is used, then lightning strike protection is provided, but labor intensity increases and aerodynamic dimensional tolerances are affected

Engineering Contradiction:
Improvelightning strike protectionVSAvoidinstallation efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The dielectric insert is pre-formed with a contour that matches the recess geometry before installation. This preliminary preparation eliminates the need for on-site curing and shaving operations, reducing labor intensity while maintaining aerodynamic dimensional tolerances. The insert is ready for direct installation into the recessed fastener.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If in-place curing and shaving of dielectric sealant is used, then lightning strike protection is provided, but surface damage may occur

Engineering Contradiction:
Improvelightning strike protectionVSAvoidsurface damage
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The dielectric insert is pre-formed with the correct contour and surface finish before installation. This eliminates the need for on-site shaving operations that could damage the composite aircraft surface. The insert is designed to fit precisely into the recess without requiring destructive removal of material.

Inventive Principle:
Principle #10Preliminary action

3Manufacturing precision

If mechanical devices with reciprocating metal blades are used for shaving, then dielectric sealant can be flushed with surface, but the devices cannot be utilized in certain production environments

Engineering Contradiction:
Improvesurface flushnessVSAvoidproduction environment compatibility
Core Design Contradiction:
Manufacturing precisionVSAdaptability or versatility

Solution Approach 1:

The dielectric insert is pre-formed with a contour that matches the recess geometry, eliminating the need for on-site shaving operations. This approach is compatible with all production environments including automated assembly lines, whereas mechanical shaving devices require specific manual operation conditions and cannot be used in automated or constrained production settings.

Inventive Principle:
Principle #10Preliminary action

4Reliability

If sealant application is made integral to assembly process, then lightning strike protection is achieved, but labor and time increase

Engineering Contradiction:
Improvelightning strike protectionVSAvoidassembly time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The dielectric insert is pre-formed and prepared before assembly, allowing it to be installed as a discrete component rather than requiring integral sealant application during the assembly process. This separation of operations reduces the time and labor required for assembly while maintaining the lightning strike protection function.

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

This method reduces installation and inspection time, minimizes waste, and enhances precision in meeting aerodynamic dimensional tolerances, providing better lightning strike protection while avoiding surface damage and allowing for automation and easier integration into production processes.

Implementation Method 1

coating at least one of a head of the fastener and a preformed dielectric insert with an adhesive, inserting the preformed dielectric insert into the recess such that the adhesive engages both contours of the recess and the preformed dielectric insert

Methodology Applied
Scientific EffectAdhesive bonding: Adhesive

Data Source

PatentUS8999097B2Fabrication and installation of preformed dielectric inserts for lightning strike protection
Publication Date: 2015.04.07 THE BOEING CO
  • US8999097B2 patent drawing
  • US8999097B2 patent drawing
  • US8999097B2 patent drawing

AI summary

A fabrication method for providing a relatively smooth surface associated with lightning strike protection for composite materials joined with fasteners recessed below the surface is described. The method includes coating at least one of a head of the fastener and a preformed dielectric insert with an adhesive, inserting the preformed dielectric insert into the recess such that the adhesive engages both contours of the recess and the preformed dielectric insert, and removing any excess adhesive from the surface area of the composite material and a top surface of the insert.