Chromate-Free Coating for Aircraft Fasteners
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Solution Overview
Problem
Existing coatings for dissimilar metal assemblies, such as titanium and aluminum in aircraft structures, face issues with galvanic corrosion, inadequate toughness, and high production costs due to short shelf-life and toxicity concerns with chromate-based coatings, while also experiencing galling problems in threaded fasteners.
Innovation Solution
A chromate-free corrosion-resistant coating composition containing 4-8% inorganic salts and 2-15% alkaline polyamine fatty acid salt (PFAS) suspended in a phenol-formaldehyde thermosetting resin, providing both passive and active corrosion resistance and reducing galling by forming a hydrophobic layer that prevents water permeation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If chromate-based coatings are used for corrosion protection, then corrosion resistance is improved, but toxicity and environmental hazards increase
Solution Approach 1:
The patent removes chromate from the coating formulation entirely, extracting the toxic component while retaining corrosion protection functionality through alternative mechanisms using zinc phosphate, zinc molybdate, and other non-chromate corrosion inhibitors
Solution Approach 2:
The patent changes the chemical composition parameters by substituting chromate with alternative corrosion inhibitor salts (zinc phosphate, zinc molybdate, strontium aluminate) and adjusts the resin system to epoxy, polyester, or acrylic bases, achieving equivalent corrosion protection without toxic hexavalent chromium
2Reliability
If cadmium plating is applied to fasteners, then galvanic corrosion protection is improved, but embrittlement of titanium and high strength steel occurs
Solution Approach 1:
The patent eliminates cadmium from the coating system, removing the embrittling agent while maintaining galvanic corrosion protection through zinc-based inhibitors and proper coating formulation that does not induce brittleness in titanium or high strength steel substrates
Solution Approach 2:
The patent uses zinc phosphate, zinc molybdate, and other sacrificial corrosion inhibitors that provide protection through controlled corrosion of the inhibitor itself rather than the substrate, avoiding the embrittlement issues associated with cadmium
3Device complexity
If organic or inorganic coatings are applied as passive barriers, then coating simplicity is improved, but substantial corrosion protection is insufficient
Solution Approach 1:
The patent creates composite coating formulations combining organic resin matrices (epoxy, polyester, acrylic) with inorganic corrosion inhibitor salts (zinc phosphate, zinc molybdate, strontium aluminate) and pigment particles, achieving both simplicity of application and substantial active corrosion protection through the synergistic composite structure
Solution Approach 2:
The coating formulation incorporates self-healing corrosion inhibition through zinc phosphate and zinc molybdate that can actively inhibit corrosion at defect sites and provide cathodic protection, allowing the coating to protect itself and the substrate without additional external intervention
4Strength
If interference-fit fasteners are used, then assembly strength is improved, but coating toughness and adherence requirements increase
Solution Approach 1:
The composite coating structure with flexible polymer matrices and dispersed inorganic inhibitor particles provides both the toughness to withstand interference-fit forces and the adherence to maintain coating integrity, accommodating the mechanical demands of interference-fit assemblies
Solution Approach 2:
The patent adjusts coating formulation parameters including resin selection, crosslink density, and inhibitor particle size to optimize the balance between coating toughness and adherence, enabling the coating to survive the interference-fit installation process while maintaining protective functionality
5Reliability
If wet primers or elastomeric sealants are used during installation, then corrosion protection is improved, but assembly cost and production complexity increase
Solution Approach 1:
The coating formulation integrates multiple functions into a single application: corrosion inhibition through zinc phosphate and zinc molybdate, adhesion promotion, and gap filling capabilities, eliminating the need for separate wet primers or elastomeric sealants and reducing assembly complexity and cost
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 coating composition offers equivalent corrosion resistance to chromate-containing coatings, extends shelf-life, eliminates tackiness, and significantly reduces galling in fasteners, with improved frictional characteristics and lubricity, suitable for interference-fit and threaded systems.
Implementation Method 1
making the coating material hydrophobic to thus prevent water-borne corrosive materials to reach the substrate
Implementation Method 2
the chromate undergoes an oxidation reaction in the presence of water and in between two materials that are dissimilar with respect to galvanic potential. This reaction will typically result in a buildup of an oxide layer on the surface of aluminum
Implementation Method 3
The organic and inorganic type coatings typically act as a passive, physical barrier against salt, moisture and the like without providing substantial corrosion protection
Implementation Method 4
significantly reduces galling in fasteners, with improved frictional characteristics and lubricity
Data Source
AI summary
The anti-corrosion coating material contains corrosion inhibiting inorganic constituents, or a combination of inorganic and organic corrosion inhibiting constituents, suspended in a polymeric resin. The corrosion resistant composition includes a salt of inorganic constituents, and alkaline polyamine fatty acid salt (PFAS) as a corrosion inhibitor, suspended in a polymeric resin remainder. The coating material may be applied to metal parts but not limited to aircraft fasteners, such as aircraft fastener parts, including nuts and bolts, screws, rivets, and sleeved systems.


