Al0.11Ni0.74Ti0.15

metal

· Al0.11Ni0.74Ti0.15

Al0.11Ni0.74Ti0.15 is a nickel-based superalloy with aluminum and titanium additions, designed to combine the high-temperature strength of nickel with strengthening contributions from its alloying elements. This composition falls within the family of precipitation-hardened nickel alloys, potentially developed for elevated-temperature applications where conventional nickel-base superalloys are specified. The material's specific elemental balance suggests optimization for thermal stability and creep resistance, making it relevant to aerospace, power generation, and industrial turbomachinery where sustained performance above 700°C is required.

turbine blades and vanesgas turbine engineshigh-temperature structural componentsaerospace propulsionpower generation equipmentcreep-resistant fasteners

Compliance & Regulations

?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65

Units:

si imperial

Property	Value	Unit	Conditions	Source
Formation Energy(ΔHf)	-0.4102	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.

Al0.11Ni0.74Ti0.15

Other Properties

Regulatory Screening

Environmental

Export Control