1. Introduce
– A nickel-base superheat-resistant alloy with polycrystalline solidification
– Alloys developed for applications requiring high strength at high temperatures up to about 1000℃
* Mar M : Cast polycrystalline nickel-based super heat-resistant alloy
* Mar : Ni-based alloys with improved high temperature strength by adding alloying elements such as Co, Cr, Ta, etc.
2. Property
– High strength, low thermal conductivity, creep and oxidation resistance, corrosion resistance, excellent work hardenability
| Element | Impact |
|---|---|
| Ni | Provides excellent strength and corrosion resistance |
| Co | Precipitation strengthening element, provides strength, creep properties |
| W | Solid solution strengthening element, provides high temperature creep properties |
| Cr | Provides corrosion resistance, oxidation resistance |
| Ta | Provides high temperature strength |
[Mar-M 247 Chemical Composition (%)]
| Ni | Cr | C | Al |
|---|---|---|---|
| 66.16 ~ 68.24 | 8.00 ~ 8.50 | 0.06 ~ 0.09 | 5.40 ~ 5.70 |
| Si | Mn | Co | W |
|---|---|---|---|
| Max. 0.25 | Max. 0.10 | 9.00 ~ 9.50 | 9.30 ~ 9.70 |
[Mar-M 247 Mechanical Properties]
| Tensile Strength (Mpa) | Yield Strength (Mpa) | Elongation (%) | |
|---|---|---|---|
| Anealed | 1250 | 750 | 20 |
[Mar-M 247 Physical Properties]
| Density (g/㎤) | Melting Range (℃) |
|---|---|
| 7.80 | 1240 ~ 1330 |
3. Available Form
– Bar, Rod
– Sheet, Plate, Strip
– Wire, Coil
4. Application & Product
– Aerospace
| Application | Product |
|---|---|
| Aerospace | Combustors, Turbine engine parts, High pressure turbine blades and vanes, Rotors, Disks, Turbocharger wheels, Turbopump turbine nozzles, Turbopump impellers |

(1) Combustors / (2) Turbine engine parts / (3) Rotors
(4) Disks / (5) Turbocharger wheels / (6) Turbin blades


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