# Features of the Structure of Layered Epoxy Composite Coatings Formed on a Metal-Ceramic-Coated Aluminum Base

**Authors:** Volodymyr Korzhyk, Volodymyr Kopei, Petro Stukhliak, Olena Berdnikova, Olga Kushnarova, Oleg Kolisnichenko, Oleg Totosko, Danylo Stukhliak, Liubomyr Ropyak

PMC · DOI: 10.3390/ma18153620 · Materials · 2025-08-01

## TL;DR

This paper describes the development of a multilayer epoxy composite coating for parabolic antennas that enables effective heating in harsh weather conditions.

## Contribution

The novelty lies in the creation of a layered coating with metal-ceramic and epoxy composite layers that provide high adhesion and heating performance.

## Key findings

- CDS forms metal-ceramic layers with high microhardness and a subgrain structure that enhances strength and crack resistance.
- Nanofillers like Al2O3, Cr2O3, and SiO2 improve the properties of epoxy composites, especially near the surface.
- Industrial tests confirmed the coating's effectiveness in heating parabolic antennas under extreme conditions.

## Abstract

Difficult, extreme operating conditions of parabolic antennas under precipitation and sub-zero temperatures require the creation of effective heating systems. The purpose of the research is to develop a multilayer coating containing two metal-ceramic layers, epoxy composite layers, carbon fabric, and an outer layer of basalt fabric, which allows for effective heating of the antenna, and to study the properties of this coating. The multilayer coating was formed on an aluminum base that was subjected to abrasive jet processing. The first and second metal-ceramic layers, Al2O3 + 5% Al, which were applied by high-speed multi-chamber cumulative detonation spraying (CDS), respectively, provide maximum adhesion strength to the aluminum base and high adhesion strength to the third layer of the epoxy composite containing Al2O3. On this not-yet-polymerized layer of epoxy composite containing Al2O3, a layer of carbon fabric (impregnated with epoxy resin) was formed, which serves as a resistive heating element. On top of this carbon fabric, a layer of epoxy composite containing Cr2O3 and SiO2 was applied. Next, basalt fabric was applied to this still-not-yet-polymerized layer. Then, the resulting layered coating was compacted and dried. To study this multilayer coating, X-ray analysis, light and raster scanning microscopy, and transmission electron microscopy were used. The thickness of the coating layers and microhardness were measured on transverse microsections. The adhesion strength of the metal-ceramic coating layers to the aluminum base was determined by both bending testing and peeling using the adhesive method. It was established that CDS provides the formation of metal-ceramic layers with a maximum fraction of lamellae and a microhardness of 7900–10,520 MPa. In these metal-ceramic layers, a dispersed subgrain structure, a uniform distribution of nanoparticles, and a gradient-free level of dislocation density are observed. Such a structure prevents the formation of local concentrators of internal stresses, thereby increasing the level of dispersion and substructural strengthening of the metal-ceramic layers’ material. The formation of materials with a nanostructure increases their strength and crack resistance. The effectiveness of using aluminum, chromium, and silicon oxides as nanofillers in epoxy composite layers was demonstrated. The presence of structures near the surface of these nanofillers, which differ from the properties of the epoxy matrix in the coating, was established. Such zones, specifically the outer surface layers (OSL), significantly affect the properties of the epoxy composite. The results of industrial tests showed the high performance of the multilayer coating during antenna heating.

## Linked entities

- **Chemicals:** Al2O3 (PubChem CID 9989226), SiO2 (PubChem CID 24261)

## Full-text entities

- **Chemicals:** Cr2O3 (MESH:C023600), Al2O3 (MESH:D000537), carbon (MESH:D002244), silicon (MESH:D012825), Coated Aluminum (-), Epoxy (MESH:D004853), chromium (MESH:D002857), Al (MESH:D000535), Metal (MESH:D008670), SiO2 (MESH:D012822)

## Full text

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## Figures

11 figures with captions in the complete paper: https://tomesphere.com/paper/PMC12348820/full.md

## References

111 references — full list in the complete paper: https://tomesphere.com/paper/PMC12348820/full.md

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Source: https://tomesphere.com/paper/PMC12348820