Dual-Layer Coating Improves Heat Resistance for Ti-Alloy Parts

Researchers have demonstrated potential for a heat shield process to improve the performance and longevity of high-entropy materials, and thus the efficiency of jet engines.
Dec. 9, 2025
3 min read

Key Highlights

  • - The B-Si coating forms a stable, oxidation-resistant barrier on TiTaNbMoZr alloys to withstand temps exceeding 1300°C.
  • - Compared to Si-only coatings, the B-Si sequence significantly reduces oxidation and prevents cracking under extreme heat.
  • - The dual-layer coating maintains its nanostructure after prolonged high-temperature exposure, ensuring long-term durability.

A novel coating offers potential as a heat shield for high-alloy materials, to improve the performance and longevity of high-temperature aerospace components. A team of researchers at Hanbat National University in South Korea introduced a sequential boron-silicon (B-Si) coating technology that forms a highly stable, oxidation-resistant barrier on TiTaNbMoZr alloys – refractory high-entropy materials that are proposed as alternatives to nickel-based superalloys.

The alloys are comprised of titanium (Ti), tantalum (Ta), niobium (Nb), molybdenum (Mo), and zirconium (Zr), which bring a range of qualities for lightness and strength, corrosion resistance, ductility, and high melt points. Investment casting and graphite-mold casting foundries also use TiTaNbMoZr to form medical devices and surgical implants due to biocompatibility.

For decades, aerospace engineers have been seeking materials capable of enduring hotter operating conditions, where higher temperatures promote greater engine efficiency and reduced fuel burn. But even with ceramic coatings, conventional Ni-based alloys are limited by their tendency to soften above roughly 1100 °C.

High-entropy alloys (HEAs), which blend multiple metallic elements into a single robust structure, have emerged as a potential alternative to address that limitation. Now, the Hanbat researchers’ two-step pack cementation process proposes a protective dual-layer coating that will hold its nanostructure even after exposure to an intense 1300 °C.

In a research study they published earlier this year, they compared traditional Si-only coatings with the new B-Si sequence. While untreated and Si-coated alloys suffered heavy oxidation (and even cracking triggered by the transformation of Zr-rich silicides)- the B-Si coating produced a stable mix of XB, XSi, and XSiB phases that resisted degradation under extreme heat.

The performance gap was significant. After 10 hours at 1300 °C, both the uncoated alloy and the Si-coated sample registered high mass gains, a hallmark of rapid oxidation. Meanwhile, the B-Si-coated version showed dramatically reduced mass gain and a notably low parabolic oxidation rate, indicating a durable, self-protecting oxide layer.

“Currently, the Ni-based alloys used in missiles can operate at around 1100 °C, but the results of our study show that the newly developed material can withstand temperatures far exceeding that limit,” stated lead researcher Prof. Joonsik Park.

The implications are important. Components routinely exposed to searing combustion environments - jet-engine parts, missile bodies, and other defense and aerospace hardware - could achieve longer lifespans and improved performance. The new technique also may be effective in various other high-temperature uses in energy, manufacturing, and other highly engineered applications.

“Overall, our results confirm the potential of high-entropy alloys for use in high-temperature environments and emphasize the critical role of selecting suitable coating strategies tailored to the alloy composition,” Prof. Park concluded.

If adopted at scale, the dual-layer B-Si coating could be an innovation in aerospace materials science, for hotter-running, more durable, jet engines.

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