0.05C 16.7Ni-0.8Mo Low Alloy Steel
metalThis is a precipitation-hardened nickel-based superalloy with modest carbon content, molybdenum strengthening, and significant titanium and aluminum additions designed for age-hardening response. The composition—dominated by nickel (16.7%) with titanium (2.24%), aluminum (0.167%), and molybdenum (0.847%)—places it in the family of materials engineered for elevated-temperature service where conventional steels lose strength. It is used in aerospace turbine engines, industrial gas turbines, and other high-temperature rotating machinery where a balance of strength retention at operating temperature, fatigue resistance, and relative manufacturability is required over more exotic superalloys.
turbine blades and discsaerospace engine componentshigh-temperature fastenersgas turbine rotorsexhaust system componentsindustrial power generation
Compliance & Regulations
?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | — | - | — | — | |
Ultimate Tensile Strength(σUTS) | — | Pa | — | — | |
Yield Strength (0.2% offset)(σy) | — | Pa | — | — |
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.