0.14C Low Carbon Steel
metalThis is a precipitation-hardening nickel-based superalloy with ~0.14% carbon, significant additions of vanadium, niobium, and titanium, and a nickel-rich matrix (~16.7% Ni). The alloying strategy—particularly the V, Nb, and Ti content—suggests this material is designed to form strengthening intermetallic phases while maintaining a low carbon content to reduce brittleness and improve workability. This composition profile is characteristic of advanced high-strength alloys developed for demanding aerospace and power-generation applications where elevated-temperature strength, fatigue resistance, and controlled ductility are critical.
aerospace engine componentshigh-temperature turbine applicationspower-generation equipmentfatigue-critical structural partselevated-temperature strength applicationsresearch/development advanced alloys
Compliance & Regulations
?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | — | - | — | — | |
Ultimate Tensile Strength(σUTS) | — | ksi | — | — | |
Yield Strength (0.2% offset)(σy) | — | ksi | — | — |
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
Safety & Biocompatibility
Quality & Standards
Industry-Specific
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.