Plated Titanium Fasteners for EME Protection in Composite Assemblies

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Solution Overview

Problem

Mechanical fasteners, particularly those made of titanium, face issues with wear resistance and galvanic compatibility with aluminum alloys, and they can contribute to electromagnetic effects (EME) in aircraft structures, such as sparking and heat generation due to poor conductivity and fiber connectivity in composite materials.

Innovation Solution

A mechanical fastener system with plated components, including a base material like titanium, a conductive bonding layer, and a lubricious conductive metal plating, which enhances conductivity and galvanic compatibility, reducing the likelihood of EME by improving the conduction path and friction coefficient.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If titanium is used for mechanical fasteners, then light weight and corrosion resistance are improved, but wear resistance deteriorates and galvanic compatibility with aluminum alloys worsens

Engineering Contradiction:
Improvestrength-weight ratioVSAvoidwear resistance
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The fastener uses a composite material structure with a titanium base material providing strength and light weight, while a chromium nitride coating layer provides wear resistance. This combination allows the fastener to maintain the high strength-weight ratio of titanium while gaining the wear resistance of ceramic-like coating materials.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The chromium nitride coating acts as an intermediary layer between the titanium fastener and the aluminum alloy substrate, preventing direct galvanic contact. This intermediate layer eliminates galvanic incompatibility while allowing the titanium fastener to maintain its structural advantages.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Strength

If titanium is used for mechanical fasteners, then light weight and corrosion resistance are improved, but galvanic compatibility with aluminum alloys deteriorates

Engineering Contradiction:
Improvestrength-weight ratioVSAvoidgalvanic incompatibility
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The chromium nitride coating serves as a galvanic isolator between the titanium fastener and aluminum alloy substrate. This intermediate non-conductive or low-conductive layer prevents the formation of galvanic cells, eliminating corrosion issues while allowing the titanium fastener to maintain its high strength-weight ratio.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The fastener combines titanium base material with a chromium nitride coating to create a composite structure that provides both mechanical strength and galvanic isolation properties, making it compatible with aluminum alloy substrates.

Inventive Principle:
Principle #40Composite materials

3Ease of manufacture

If conventional fasteners are used in composite structures, then structural assembly is achieved, but electromagnetic effects worsen due to poor conductivity and current density concentration

Engineering Contradiction:
Improvestructural assemblyVSAvoidelectromagnetic effects
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The chromium nitride coating changes the electrical conductivity parameters of the fastener surface, creating a controlled conductive path that manages lightning strike current distribution. This parameter modification reduces current density concentration at the fastener-composite interface while maintaining structural assembly capabilities.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The chromium nitride coating acts as an intermediary layer that mediates the interaction between the metallic fastener and the composite structure, providing a controlled electrical interface that manages electromagnetic effects while enabling structural assembly.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 plated fastener system provides effective EME protection by reducing current density and the risk of sparking, improving conductivity, and ensuring galvanic compatibility with various substrates, thus enhancing the safety and reliability of structural assemblies.

Implementation Method 1

The bonding layer may include one or more conductive metals... improving a conduction path between the fastener and the composite structure may reduce the likelihood of sparking or other problematic EME

Methodology Applied
Scientific EffectElectrical conduction: Conduction (electrical)

Implementation Method 2

The metal plating may include one or more lubricious and conductive metals... reducing the likelihood of EME by improving the conduction path and friction coefficient

Methodology Applied
Scientific EffectLubrication: Lubrication

Data Source

PatentUS11649845B2Mechanical fastener system for electromagnetic effect (EME) protection
Publication Date: 2023.05.16 THE BOEING CO
  • US11649845B2 patent drawing
  • US11649845B2 patent drawing
  • US11649845B2 patent drawing

AI summary

A mechanical fastener system for EME protection, including at least one plated component, wherein the at least one plated component includes a base material, a bonding layer disposed over the base material, and a metal plating disposed over the bonding layer.