Low-cost Niobium-based Alloy for Ultrahigh Temperature Applications
Tech ID: 34645 / UC Case 2026-446-0
Abstract
Researchers at the University of California, Davis have
developed a refractory niobium-based complex concentrated alloy designed for
exceptional strength and durability at ultrahigh temperatures with a
significantly reduced material’s cost.
Full Description
This technology introduces a novel
niobium-based refractory complex concentrated alloy composed primarily of
niobium, tantalum, titanium, and vanadium in specific atomic proportions,
engineered to deliver superior mechanical performance at temperatures meeting
or exceeding C-103 and conventional nickel-based superalloys. The alloy
features a body-centered cubic crystal structure and exhibits high yield and
tensile strengths at room temperature and elevated temperatures up to 1300°C,
combined with improved specific strength and structural stability.
Applications
- Gas turbine engine components, including turbine blades.
- Aerospace structural parts requiring
high-temperature durability.
- Energy sector equipment exposed to extreme
thermal and mechanical conditions.
- Advanced manufacturing of refractory alloy-based structural
components.
Features/Benefits
- Withstands ultrahigh temperatures.
- Provides superior 0.2% offset yield strength.
- Maintains outstanding ultimate tensile strength at elevated temperatures.
- Reduces costs by minimizing reliance on expensive elements such as hafnium through optimized alloy composition.
- Achieves a strong balance between strength and ductility, overcoming limitations of traditional RCCAs.
- Enhances structural integrity with a single-phase body-centered cubic crystal structure.
- Lowers component weight with reduced density.
- Surpasses temperature limitations of nickel-based superalloys in high-temperature turbine and aerospace applications.
- Resolves cost and strength issues present in niobium alloys containing hafnium.
- Improves ductility and formability compared to many other high-strength refractory complex concentrated alloys.
Patent Status
Patent Pending