NIMONIC® alloy 115

NIMONIC-Alloy-115

Introduction to Nimonic 115™ Product

Nimonic 115™ is a high-strength nickel-based superalloy known for its exceptional performance at elevated temperatures, excellent oxidation and corrosion resistance, and superior mechanical properties. Developed for demanding applications in aerospace, gas turbine engines, and other high-temperature environments, Nimonic 115™ offers reliability and durability under extreme conditions.

Chemical Composition

ElementComposition (%)
Nickel (Ni)54.0-59.0
Chromium (Cr)15.0-19.0
Cobalt (Co)15.0-19.0
Iron (Fe)5.0 max
Molybdenum (Mo)2.5-4.0
Titanium (Ti)1.0-2.0
Aluminum (Al)0.5-1.5
Carbon (C)0.15 max
Silicon (Si)0.5 max
Manganese (Mn)0.5 max
Sulfur (S)0.015 max
Phosphorus (P)0.015 max

Mechanical Properties

PropertyValue
Tensile Strength (RT)960 MPa (139 ksi) min
Yield Strength (0.2% offset) (RT)720 MPa (105 ksi) min
Elongation (RT)20% min
Creep Rupture StrengthExcellent at high temperatures
Hardness (HV)280-320 HV

Performance at Different Temperatures

Temperature RangePerformance
Room TemperatureHigh strength and corrosion resistance
Elevated Temperatures (up to 800°C / 1470°F)Excellent creep resistance and thermal stability
Cryogenic TemperaturesRetains ductility and toughness

Industry Applications

Nimonic 115™ finds extensive use in various critical applications:

IndustryApplications
AerospaceTurbine blades, combustion chambers
Power GenerationGas turbine components, high-temperature fasteners
Oil & GasWellhead components, valve stems
AutomotiveExhaust valves, turbocharger rotors

Shapes, Sizes, and Production Standards

Shapes and Sizes
FormSize Range
SheetsThickness: 0.5 mm – 6 mm
PlatesThickness: 1 mm – 100 mm
BarsDiameter: 6 mm – 200 mm
WireDiameter: 0.1 mm – 10 mm
ForgingsVarious shapes and sizes as per standards
Production Standards and Corresponding Grades
CountryStandardCorresponding Grade
United StatesAMS 5829N07115
GermanyDIN 177522.4636
FranceAFNOR NC 20T
United KingdomBS HR 403HR403
JapanJIS HR 403
ChinaGB/T 14994

Welding, Machining, Polishing, Heat Treatment, and Cold Working

ProcessDetails
WeldingTIG and MIG methods recommended; post-weld heat treatment required
MachiningCarbide tools and lubricants for optimal results
PolishingMechanical and electrochemical methods for desired finish
Heat TreatmentSolution annealing followed by aging
Cold WorkingCold forming and shaping processes are feasible

Advantages and Disadvantages

AspectAdvantagesDisadvantages
AdvantagesHigh strength and oxidation resistanceLimited availability in certain forms
Excellent creep resistanceMachining can be challenging
Good thermal stability at high temperaturesCostlier compared to some alternatives
Versatile in high-temperature applications

Similar Products

Material GradeComparison
Nimonic 105™Similar composition with slight variations
Inconel® 718Higher nickel content, different applications

Conclusion

Nimonic 115™ stands as a robust solution for applications requiring exceptional strength, corrosion resistance, and performance at elevated temperatures. Its precise chemical composition, reliable mechanical properties, and adherence to international production standards ensure reliability across critical sectors such as aerospace, power generation, and oil & gas. Engineers and designers seeking high-performance materials for demanding environments can rely on Nimonic 115™ for optimal performance and longevity.

For detailed technical specifications and customized solutions, consulting with material suppliers and referencing specific product data sheets is recommended.