0.14C 17.4Ni-1.3Mo Low Alloy Steel
metalA precipitation-hardening nickel-based superalloy containing 17.4% nickel, 2.95% titanium, and 1.3% molybdenum, designed to achieve high strength at elevated temperatures through age-hardening mechanisms. This alloy is primarily used in aerospace propulsion and power generation applications where components must maintain structural integrity under sustained thermal and mechanical loading. Engineers select this material for critical rotating and stationary components when exceptional strength-to-weight ratio and creep resistance are required, particularly in environments where conventional carbon steels become inadequate.
jet engine turbine bladespower plant rotorshigh-temperature fastenersaerospace structural componentssteam turbine discsbearing races for extreme service
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.