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Model No: Multimet N155
Multimet N155
Quantity :
Multimet N155 Description:
Multimet N155 is a Nickel-Chromium-Cobalt alloy with additions of Molybdenum and Tungsten used typically in parts requiring high strength up to 1350°F and oxidation resistance up to 1800°F. Its high-temperature properties are inherent in the as-supplied condition (solution treated at 2150°F) and are not dependent on age-hardening. Multimet N155 is used in a number of aerospace applications such as tailpipes and tail cones, turbine blades, shafts and rotors, afterburner components and high-temperature bolts.
Multimet N155 Chemical Composition:
C | Carbon 0.08 – 0.16 |
Mn | Manganese 1.00 – 2.00 max |
Si | Silicon 1.00 max |
S | Sulfur 0.03 max |
P | Phosphorus 0.04 max |
Cr | Chromium 20.00 – 22.5 |
Ni | Nickel 19.00 – 21.00 |
Co | Cobalt 18.5 – 21.00 |
Mo | Molybdenum 2.5 – 3.5 |
W | Tungsten 2.0 – 3.0 |
Cb + Ta | Niobium + Tantalum 0.75 – 1.25 |
N | Nitrogen 0.1 – 0.2 |
Multimet N155 Mechanical Properties:
Material | Form | Ultimate Tensile Strength ksi | Elongation in 2"(min) | Hardness HB |
Multimet N155 | Bar (AMS 5769) |
|
| 156-217 |
Multimet N155 | Sheet / Plate (AMS 5532) | 110-140 | 40 | - |
Multimet N155 Specifications:
- AMS 5532 Sheet, Plate and Strip
- AMS 5769 Bars, Rings and Forgings
- AMS 5794 Welding Wire
- AMS 5795 Coated Electrodes
- UNS R30155
Multimet N155 Applications:
- Multimet N155 nickel alloy is used for numerous industrial applications, some of which include:
- Air & land based turbine engines
- Aircraft tail cones & tail pipes
- Aircraft exhaust manifolds
- Aircraft combustion chambers
- Afterburners
- Buckets & bolts