Aircraft surfaces endure extreme mechanical and environmental stresses, with leading edges experiencing particle impacts at velocities exceeding 800 km/h and temperature variations from -60°C at cruise altitude to +50°C on desert runways. Traditional protective coatings show significant degradation after 3,000 flight hours, particularly in high-wear areas where material loss can exceed 200 micrometers in depth.

The fundamental challenge lies in developing coating systems that can maintain both surface protection and aerodynamic performance while withstanding the combined effects of impact erosion, thermal cycling, and environmental exposure.

This page brings together solutions from recent research—including nanocomposite polyurethane systems with fluorine-modified nano-SiO2, multi-layer protective coatings with silane-coupled primers, and advanced powder coatings using nanoscale titanium dioxide formulations. These and other approaches focus on practical implementation strategies that balance durability requirements with maintenance considerations and environmental compliance.

1. Nanocomposite Polyurethane Coating with Fluorine-Modified Nano-SiO2 and Polyaspartate Resin

GUANGDONG CORROSION SCIENCE AND TECHNOLOGY INNOVATION RESEARCH INSTITUTE, 2023

Nanocomposite polyurethane coating for aircraft with enhanced durability and environmental sustainability. The coating combines a fluorine-modified nano-SiO2 surface treatment with polyaspartate resin, achieving improved impact resistance, thermal stability, and wear protection. The treatment enables the formation of a network structure that enhances crack resistance while maintaining flexibility. The coating's performance is demonstrated through accelerated aging tests, demonstrating superior durability and gloss retention compared to conventional coatings.

CN117264524A-patent-drawing

2. Aircraft Skin Finish Paint with Acrylic and Modified Polyester Resins and Graphene Dispersion

SHAANXI COAL AND CHEMICAL INDUSTRY TECHNOLOGY RESEARCH INSTITUTE CO LTD, Shaanxi Coal and Chemical Technology Institute Co., Ltd., 2023

Aircraft skin finish paint and preparation method for enhanced durability and performance in extreme environments. The paint combines a durable acrylic resin with a modified polyester resin, supplemented with graphene dispersion for superior impact resistance and thermal stability. The formulation balances performance parameters while maintaining environmental resistance, enabling aircraft surfaces to withstand harsh conditions such as high-altitude flight and landing operations.

CN114231100B-patent-drawing

3. Protective Coating for Plexiglass with Polyurethane Dispersion and Modified Aluminum Oxide Nano-Hollow Spheres

XIAN LIYUAN NEW MATERIALS TECHNOLOGY DEVELOPMENT CO LTD, 2023

A protective coating for transparent aircraft parts made from plexiglass that provides superior mechanical strength, chemical resistance, and optical clarity. The coating comprises a polyurethane dispersion, modified aluminum oxide nano-hollow spheres, fluorine-based resin, reinforcing agent, defoamer, leveling agent, film-forming agent, and silane coupling agent. The coating is prepared through a unique dispersion process that incorporates the polyurethane dispersion with the modified aluminum oxide spheres and fluorine-based resin, followed by precise formulation of the dispersion with additional agents. The coating provides exceptional mechanical properties, chemical resistance, and optical clarity, making it suitable for aircraft applications where plexiglass components are exposed to harsh environmental conditions.

CN116082946A-patent-drawing

4. Multi-Layer Protective Coatings with Silane-Coupled Primer and Organic Titanate Formulations for Aircraft Engine Components

GE AVIO SRL, 2023

Protective coatings for aircraft engine components achieve enhanced thermal and mechanical resistance through a combination of silane coupling agent and organic titanate-based formulations. The coatings combine a silane-coupled primer layer with a silicone elastomer layer, followed by an abrasion-resistant elastomeric layer. This multi-layer system provides superior thermal insulation while maintaining high abrasion resistance, enabling prolonged engine component life.

5. High-Temperature-Resistant Coating with Hollow Silica Microspheres and Nano-Oxide Mixtures for UAVs

SICHUAN UNIVERSITY, 2022

A high-temperature-resistant, anti-corrosion, lightweight coating for unmanned aerial vehicles (UAVs) that achieves both thermal insulation and radiation protection. The coating combines a hollow silica microsphere-based thermal barrier with lithium silicate and nano-oxide mixtures, specifically nano-alumina, nano-magnesia, and nano-zinc borate, to achieve superior performance in extreme temperatures (up to 1300°C) while maintaining structural integrity. The coating system demonstrates enhanced thermal insulation and radiation protection capabilities compared to conventional materials, making it suitable for UAV applications in high-temperature environments.

6. Nanoscale Titanium Dioxide-Based Powder Coating with Fluorinated Epoxy Resin for Aircraft Surfaces

SCIENTIFIC AND TECH SHARE LIMITED COMPANY OF HUAHONGQING INDUSTRY OF ANHUI, 2022

Powder coating for aircraft surfaces at the nanoscale, enabling enhanced durability and performance compared to traditional metal coatings. The coating employs a specially formulated titanium dioxide-based powder system, with additives that enhance wetting and leveling properties. The coating is cured using a fluorinated epoxy resin, which combines with the powder to create a strong, corrosion-resistant, and aerodynamically optimized finish for aircraft surfaces.

7. Multi-layer Coating for Aircraft Components with Barrier and Laminar Flow Layers Incorporating Fluoropolyether, Silicon Rubber, Polyurethane, Sol-gel Siloxane, Rare-earth Oxide, and Phosphate

ROHR INC, 2020

Multi-layer coating for aircraft components that enhances durability and performance through a barrier layer and laminar flow layer. The coating consists of a barrier layer containing fluoropolyether, silicon rubber, or polyurethane, covering the component surface. The barrier layer protects the component from environmental degradation while the laminar flow layer, comprising sol-gel siloxane, rare-earth oxide, and phosphate, forms a protective layer on top of the barrier layer. This multi-layer configuration provides enhanced mechanical properties and resistance to environmental influences, making it suitable for critical aircraft components.

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8. Aviation Coating with Polyurethane Resin and Additive for Enhanced Thermal Stability and Moisture Resistance

NANJING YOUGU INTELLECTUAL PROPERTY SERVICE CO LTD, 2019

Aviation coating for aircraft surfaces that enhances durability and performance through improved thermal management. The coating combines a polyurethane resin with a specialized additive that enhances low elongation, low reflection coefficient, and moisture resistance while maintaining thermal stability. The coating system is formulated to address existing coating limitations in aircraft surfaces, including low elongation, low reflection coefficient, and humidity intolerance. The coating provides enhanced performance characteristics through its unique combination of thermal management properties.

9. Transparent Substrate with Sputtered Zirconium-Aluminum Oxide Coating and Infrared Modulating Layer

SAINT GOBAIN, 2018

A transparent substrate coated with a stack of thin layers that provides enhanced scratch resistance, low friction, and thermal stability. The substrate is coated with a protective layer comprising a mixed oxide of zirconium and aluminum, with atomic proportions of aluminum and zirconium exceeding 99% relative to other elements. This layer is deposited by sputtering assisted by a magnetic field and forms the outermost layer of the stack. The stack comprises a base layer of mixed oxide and a functional layer that can act on infrared radiation. The substrate is preferably glass, and the stack can be applied to various substrates, including metal, ceramic, and polymer substrates. The stack provides superior performance compared to conventional coatings, particularly in applications requiring high scratch resistance and thermal stability.

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10. Rough-Surfaced ZrO2-Al2O3 Multiphase Ceramic Particles with Controlled Sintering and Rapid Cooling

GUANGDONG INST MATERIALS & PROC, 2018

Rough-surfaced ZrO2-Al2O3 multiphase ceramic particles for wear-resistant steel matrix composites, prepared through a specific processing sequence. The particles have a composition of 10-90% stabilized ZrCF and 10-90% AI2O3, with a particle size of 1-7 mm. The particles undergo a controlled sintering process in an electric furnace at temperatures below 60°C/h, followed by rapid cooling to 500-600°C. This unique processing sequence enables the formation of high wear resistance ceramic particles with a surface roughness that enhances their ability to prevent cracks and spalling during composite fabrication.

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11. Aerospace Coating with Polyurethane Matrix and Embedded Silicon Carbide Particles

AIRBUS OPERATIONS GMBH, 2017

Aerospace coating for aircraft landing flaps featuring enhanced abrasion resistance through the incorporation of polyurethane matrices with embedded silicon carbide particles. The coating provides superior wear protection in the critical landing flap contact area, particularly during high-temperature and high-velocity operations. The coating composition combines a polyurethane matrix with silicon carbide particles, which significantly improves abrasion resistance compared to conventional coatings. The coating's performance is validated through comprehensive wear testing at elevated temperatures and in extreme environments.

12. Polyurethane Coating with Low-Temperature Resistant Polyester Polyol and Organic Functional Micron Powder Modifier

Technical Institute of Physics and Chemistry, Chinese Academy of Sciences, 2017

A low-temperature resistant, wear-resistant polyurethane coating comprising a polyurethane base resin, a low-temperature resistant polyester polyol, a surface layer modifier containing organic functional micron powder, a curing agent, a solvent, and a defoamer. The coating exhibits superior low-temperature performance and abrasion resistance through the surface layer modifier, which introduces micron-sized organic powders to the surface of the polyurethane base resin.

13. Coating Composition with Inorganic-Organic Hybrid Matrix Incorporating Polysiloxane and Titanium Dioxide

GUANGXI UNIVERSITY, 广西大学, 2017

Coating composition for a helicopter landing platform that enhances its durability and resistance to environmental stressors through a novel inorganic-organic hybrid matrix. The composition incorporates a polysiloxane matrix with a silicon-oxygen bond energy of 446 kJ/mol, which significantly exceeds that of organic carbon-carbon bonds. This enables the formation of a strong interpenetrating network with the polysiloxane, providing exceptional mechanical properties. The composition combines a polysiloxane matrix with an inorganic matrix, such as titanium dioxide, to create a hybrid material with superior performance characteristics. The resulting coating exhibits enhanced weatherability, moisture resistance, and UV resistance, as well as excellent salt spray and high-temperature resistance, making it suitable for demanding helicopter landing platforms.

14. Polyurethane-Based Coating for UAVs with Enhanced Durability, Environmental Resistance, and Electrical Insulation

WENZHOU CHUYING TECHNOLOGY CO LTD, 2016

Coating for unmanned aerial vehicles (UAVs) that enhances durability and resistance to environmental stressors while maintaining electrical insulation properties. The coating comprises a specialized polyurethane-based material that provides enhanced scratch resistance and electrical insulation while maintaining the vehicle's structural integrity. The coating is applied to the UAV's surface using a controlled process that ensures uniform coverage and optimal adhesion. This coating solution enables UAVs to operate effectively in challenging environments such as high-altitude areas, remote regions, and areas with corrosive substances, while maintaining their performance characteristics.

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15. Aircraft Wing Skin Coating with Multi-Layer Zinc Yellow and Fluorocarbon Structure

溧阳市哈大成果转化中心有限公司, LIYANG HADA ACHIEVEMENTS TRANSFORMATION CENTER CO., LTD., 2016

A low-cost, environmentally friendly aircraft wing skin coating comprising a substrate and a protective zinc yellow coating comprising a layer of primer and two layers of acrylic urethane fluorocarbon finish. The coating comprises a zinc yellow primer dry film thickness of 14 microns, an intermediate fluorocarbon finish dry film thickness of 36 microns, and an outer layer of fluorocarbon finish dry film thickness of 59 microns.

16. Fluorocarbon-Based Aerospace Wing Coating with Multi-Layered Acrylic Urethane Structure

Liyang Ha Da Achievement Transformation Center Co., Ltd., LIYANG HADA ACHIEVEMENTS TRANSFORMATION CENTER CO., LTD., 2016

Aerospace wing coating for aircraft that combines superior weather resistance, chemical resistance, and thermal stability through a novel fluorocarbon-based coating system. The coating comprises a primer layer, followed by two layers of acrylic urethane fluorocarbon finish, with specific dry film thicknesses. This innovative composition enables the creation of a durable, cost-effective, and environmentally friendly coating that meets the stringent performance requirements of modern aircraft applications.

17. Two-Component Nano-Coating for Aircraft Surfaces with Integrated Multi-Property Nanoparticle Formulation

Dalian Yuxiang Technology Group Co., Ltd., DALIAN YUXIANG CO LTD, 2016

Nano-coatings for aircraft surfaces that achieve enhanced performance beyond traditional coatings. The coatings combine decorative, corrosion-resistant, self-cleaning, UV-resistant, low-friction, and high-heat resistance properties with extended service life. The coatings achieve these performance enhancements through a two-component nano-formulation that incorporates nanoparticles of specific materials. The formulation enables superior protection against environmental factors while maintaining the aircraft's aerodynamic performance.

18. Fluorocarbon Coating with Cross-Linked Matrix via Fluorine-Based Polymerization

Liyang Ha Da Achievement Transformation Center Co., Ltd., LIYANG HADA ACHIEVEMENTS TRANSFORMATION CENTER CO., LTD., 2016

A fluorocarbon protective layer for aircraft fuselage shells that enhances performance through enhanced thermal, chemical, and environmental resistance. The coating comprises a fluorocarbon body shell with a cross-linked fluorocarbon matrix, where the cross-linking is achieved through a novel fluorine-based polymerization process that incorporates high-performance fluorine-containing monomers. This process enables superior thermal stability, chemical resistance, and environmental durability compared to conventional fluorocarbon coatings. The cross-linked matrix provides enhanced mechanical strength and durability, while maintaining the inherent properties of fluorocarbon resins.

CN103640304B-patent-drawing

19. Aircraft Fuselage Skin with Fluorocarbon Coating Utilizing Fluorine-Based Crosslinking and Reduced VOC Content

溧阳市哈大成果转化中心有限公司, LIYANG HADA ACHIEVEMENTS TRANSFORMATION CENTER CO., LTD., 2016

Aerospace aircraft fuselage skin with enhanced weather resistance through advanced fluorocarbon coating. The coating combines superior chemical resistance, UV protection, and high-temperature durability with reduced VOC content and environmental impact. The coating's unique molecular structure enables strong chemical bonds through fluorine-based crosslinking, while maintaining low VOC levels and minimal environmental footprint compared to traditional fluorocarbon coatings.

CN103600557B-patent-drawing

20. Fluorinated Polymer Coating with Proprietary Crosslinking for Aircraft Fuselage Shells

LIYANG HADA ACHIEVEMENTS TRANSFORMATION CENTER CO LTD, 溧阳市哈大成果转化中心有限公司, 2015

A high-performance coating for aircraft fuselage shells that combines advanced materials science with innovative application techniques. The coating employs a novel fluorinated polymer with enhanced thermal stability and chemical resistance, achieved through a proprietary crosslinking mechanism that addresses the limitations of traditional fluorocarbon coatings. This polymer-based coating provides superior performance in extreme environmental conditions, including high-temperature resistance, UV protection, and water resistance, while maintaining low VOC emissions and reduced environmental impact.

CN103600542B-patent-drawing

21. Aircraft Fuselage Protective Layer with Zinc Yellow Acrylic Primer and Dual-Layer Fluorocarbon Finish

22. Protective Aircraft Shell Layer with Fluorocarbon Resin and Controlled Crosslinking

23. Aircraft Fuselage Coating with Zinc Yellow Acrylic Primer and Multi-Layer Fluorocarbon Finish

24. Fluorocarbon Resin-Based Coating with Proprietary Crosslinking for Aircraft Wing Shells

25. Fluorocarbon Coating for Aircraft Wings with Novel Crosslinking Using Fluorine-Containing Monomers

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