Nimonic 115
Description:
Nimonic 115 is a precipitation-hardenable alloy which is available for supply in bar form and extruded sections. The material is known as a creep-resisting alloy and with initial development for high-temperature service operation up to 1010°C.
Offering superior oxidation resistance and high-temperature strength, the original intended application for this product was in the production of gas turbine blades. Heat treatment of the product is by solution treatment and then ageing.
Chemical Composition:
|
Element |
Content (%) |
|
Nickel, Ni |
54 |
|
Chromium, Cr |
14.0-16.0 |
|
Cobalt, Co |
13.0-15.5 |
|
Aluminum, Al |
4.50-5.50 |
|
Molybdenum, Mo |
3.0-5.0 |
|
Titanium, Ti |
3.50-4.50 |
|
Iron, Fe |
1.0 |
|
Manganese, Mn |
1.0 |
|
Silicon, Si |
1.0 |
|
Copper, Cu |
0.20 |
|
Zirconium, Zr |
0.15 |
|
Carbon, C |
0.12-0.20 |
|
Sulfur, S |
0.015 |
|
Boron, B |
0.010-0.025 |
Mechanical Properties: (precipitation hardened condition)
|
Properties |
Metric |
Imperial |
|
Tensile strength |
1300 MPa |
189000 psi |
|
Yield strength |
850 MPa |
123000 psi |
|
Elongation at break |
25.00% |
25.00 |
Specifications:
Equivalent materials to Nimonic 115 are:
l BSHR4
l DIN 2.4636
Applications:
Nimonic 115 is suitable for use in high temperature components in gas turbine applications.