Ti6Al16Co7
metal· JVASP-146177· Ti6Al16Co7
Ti6Al16Co7 is a titanium-based alloy containing aluminum and cobalt as primary alloying elements, designed to enhance strength and thermal stability compared to conventional titanium alloys. This material is primarily developed for high-temperature aerospace and power generation applications where superior creep resistance and elevated-temperature strength are critical, making it a candidate for turbine components and engine structures that operate beyond the capabilities of standard Ti-6Al-4V.
aerospace turbine bladeshigh-temperature engine componentspower generation systemscreep-resistant structural partsadvanced jet engine applications
Compliance & Regulations
?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.1675 | lb/in³ | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Band Gap(Eg) | 0.000 | eV | — | ||
Magnetic Moment(μB) | 0.000 | µB | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Energy Above Hull(ΔEhull) | 0.000 | eV/atom | — | ||
Formation Energy(ΔHf) | -0.5308 | eV/atom | — |
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
Export Control
RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.