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- ATI Allvac® Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age
ATI Allvac® Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age
| Category | Metal , Nonferrous Metal , Nickel Alloy , Superalloy |
| Manufacturer | ATI Allvac |
| Trade Name | |
| Port | Shanghai port,China |
| Trade Terms | FOB, CFR, CIF |
| Payment Terms | L/C, T/T, Western Union |
| Download PDF | ATI Allvac® Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age.pdf  |
| Price | EMAIL US sales@lookpolymers.com |
Material Notes:
Data provided by Allvac.Applications: Jet and rocket engines, torque rings, afterburners, and hardware; space shuttle turbo pumps seals.
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 8.24 g/cc | 0.298 lb/in³ |
| Mechanical Properties | Metric | English | Comments |
|---|---|---|---|
| Hardness, Brinell | 334 | 334 | Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball |
| Hardness, Knoop | 363 | 363 | Estimated from Rockwell C value. |
| Hardness, Rockwell C | 36 | 36 | |
| Hardness, Vickers | 349 | 349 | Estimated from Rockwell C value. |
| Tensile Strength, Ultimate | 1241 MPa | 180000 psi | |
| Tensile Strength, Yield | 793 MPa @Strain 0.200 % |
115000 psi @Strain 0.200 % |
|
| Elongation at Break | 20 % | 20 % | |
| Reduction of Area | 25 % | 25 % |
| Component Elements Properties | Metric | English | Comments |
|---|---|---|---|
| Aluminum, Al | 1.6 % | 1.6 % | |
| Boron, B | 0.0070 % | 0.0070 % | |
| Carbon, C | 0.060 % | 0.060 % | |
| Chromium, Cr | 19 % | 19 % | |
| Cobalt, Co | 11 % | 11 % | |
| Iron, Fe | 3.0 % | 3.0 % | |
| Molybdenum, Mo | 9.75 % | 9.75 % | |
| Nickel, Ni | 52 % | 52 % | as balance |
| Titanium, Ti | 3.15 % | 3.15 % |
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