Conductive Carbon Coatings for Static-Dissipating Vehicle Surfaces

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Solution Overview

Problem

Conventional surface coatings on aircraft are not highly conductive, leading to charge buildup and lack ideal airworthiness properties such as durability, compatibility with underlying surfaces, and visibility, while also being incompatible with additional chemicals, which complicates their use in extreme conditions.

Innovation Solution

A method of forming electrically conductive materials by depositing a polymer and sulfonic acid onto a carbon allotrope material, creating a conductive layer that enhances electrical, mechanical, and thermal properties, and can be applied to vehicle components to dissipate static electricity and improve airworthiness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional surface coatings are used, then basic protective function is achieved, but compatibility with additional chemicals deteriorates

Engineering Contradiction:
Improveprotective functionVSAvoidchemical compatibility
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The patent employs parameter changes by modifying the chemical composition and structure of the coating system to enhance chemical compatibility. The conductive coating is formulated with chemically resistant materials and optimized cross-linking density to maintain stability when exposed to de-icing chemicals, fuel, and other aircraft maintenance substances, thereby improving adaptability without sacrificing protective function.

Inventive Principle:
Principle #35Parameter changes

2Area of stationary object

If conventional surface coatings are applied, then coverage is achieved, but visibility through canopy/windshield deteriorates

Engineering Contradiction:
Improvesurface coverageVSAvoidvisibility
Core Design Contradiction:
Area of stationary objectVSIllumination intensity

Solution Approach 1:

The patent applies local quality by using transparent conducting oxides (such as indium tin oxide or fluorinated tin oxide) specifically for canopy and windshield coatings, while using different conductive materials for other aircraft surfaces. This localized material selection ensures full surface coverage for protection and conductivity while maintaining optical transparency in critical visibility areas.

Inventive Principle:
Principle #3Local quality

3Reliability

If additional chemicals are mixed into conventional coatings to improve physical properties, then desired properties are enhanced, but compatibility with coating deteriorates

Engineering Contradiction:
Improvephysical propertiesVSAvoidcoating compatibility
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

The patent resolves this contradiction by carefully controlling the parameters of additive incorporation, including concentration, particle size, and distribution density. The conductive fillers are optimized to provide enhanced physical properties (conductivity, flexibility, durability) at thresholds that maintain coating integrity and compatibility, avoiding the destabilization that occurs with excessive or improperly formulated additives.

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

The resulting materials effectively dissipate static electricity, improve airworthiness by enhancing durability and visibility, and maintain compatibility with underlying surfaces, while reducing the need for excessive chemicals and improving flexibility and thermal conductivity.

Implementation Method 1

depositing a first material comprising a polymer and a sulfonic acid onto a carbon allotrope material to form a second material

Methodology Applied
Scientific EffectDeposition: Deposition (physical)

Implementation Method 2

The resulting materials effectively dissipate static electricity

Methodology Applied
Scientific EffectElectrical conduction: Conduction (electrical)

Implementation Method 3

The method comprises curing the second material

Methodology Applied
Scientific EffectCuring:

Implementation Method 4

applying a voltage to a material comprising a carbon allotrope material, a polymer, and a sulfonic acid

Methodology Applied
Scientific EffectJoule heating: Joule Heating

Data Source

PatentUS12073955B2Electrically conductive materials
Publication Date: 2024.08.27 THE BOEING CO
  • US12073955B2 patent drawing
  • US12073955B2 patent drawing
  • US12073955B2 patent drawing

AI summary

Methods of forming an electrically conductive carbon allotrope material comprise depositing a first material comprising a polymer and a sulfonic acid onto a carbon allotrope material to form a second material. The methods comprise curing the second material. Methods of heating a surface of a vehicle component comprise applying a voltage to a material comprising a carbon allotrope material, a polymer, and a sulfonic acid. The material is disposed on a surface of a vehicle component. Electrically conductive materials comprise at least one polymer, at least one sulfonic acid, and a carbon allotrope material.