Udimet 720
VerifiedmetalUdimet 720 is a nickel-based superalloy designed for high-temperature structural applications requiring exceptional strength retention at elevated temperatures. It is widely used in jet engine components—particularly turbine blades, vanes, and casings—where it must withstand sustained thermal cycling and mechanical stress in the 700–800 °C operating range. Engineers select Udimet 720 over conventional superalloys when creep resistance, fatigue life, and damage tolerance are critical in demanding aerospace and power-generation environments.
turbine bladesjet engine componentshigh-temperature aerospacepower generationthermal fatigue resistancecreep-resistant structures
Compliance & Regulations
?ITAR?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Tensile Strength(σUTS) | — | Pa | 20°C | — | |
Yield Strength (0.2% offset)(σy) | — | Pa | 20°C | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | kg/m³ | — | — |
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
Export Control
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.