Rene 41 bar is a high-strength nickel-based alloy known for its toughness at high temperatures. It handles extreme heat without losing strength, making it perfect for aerospace and engine parts. Parag Metal is a trusted rene 41 bar supplier offering quality materials with reliable performance. This alloy has excellent mechanical strength, outstanding oxidation resistance and retains its shape under stress. It also shows impressive creep resistance up to 1600°F. Rene 41 has a balanced mix of nickel, chromium, cobalt, and molybdenum. These elements give it strength, stability, and corrosion resistance.
Alloy rene 41 bar stands out for its heat resistance and strength after aging. It works well in jet engines, gas turbines, and high-heat tools. It also performs well in rocket motors and exhaust parts. It resists wear, cracking, and distortion under stress. Types of rene 41 bar include hot-rolled, cold-drawn, and forged bars. This makes it useful for both structural and precision applications. Its toughness makes it a strong choice for extreme industrial uses.
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Rene 41 bar meets high-grade industry standards. Available grades include AMS 5712 and AMS 5713. We also supply UNS N07041 and UNS S66286 bar, both used in high-stress parts. These bars meet all the international standards and ensure performance and safety in every application.
Each rene 41 bar for sale comes with full test certificates. These bars include heat treatment records, hardness test results, and material test reports. Buyers looking for a rene 41 bar distributor, dealer, exporter, wholesaler, or stockist can trust our quality.
| Standards | AMS 5545, AMS 5712, AMS 5713, AMS 5800, EN 2.4973, GE B50T59, GE B50TF109, GE B50TF76, UNS N07041, Werkstoff 2.4973 |
|---|---|
| Thickness | Range from .008″ to .0125″ |
| Hardness | Soft, Hard, Half Hard, Quarter Hard, Spring Hard etc. |
| Form | Round Bar, Wire |
| Tungsten Grades | HA 190 / HA 1925 / HA 195 / HE 390 / HE 3925 / HE 395 / HE 397 |
| Standard | Werkstoff Nr. | UNS |
|---|---|---|
| Rene 41 | 2.4973 | N07041 |
| Cr | Ni | Mo | Co | Al | Ti | B | C | Fe | Mn | Si | S | Cu | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MIN | 18.00 | — | 9.00 | 10.00 | 1.40 | 3.00 | 0.003 | — | — | — | — | — | — |
| MAX | 20.00 | Balance | 10.50 | 12.00 | 1.80 | 3.30 | 0.01 | 0.12 | 5.00 | 0.10 | 0.50 | 0.015 | 0.50 |
| Mechanical & Physical Properties | 21°C | 427°C | 538°C | 649°C | 760°C | 871°C | 982°C |
|---|---|---|---|---|---|---|---|
| Ultimate Tensile Strength /MPa | 1261.7 | – | – | 1117 | 1048 | 710.2 | – |
| 0.2% Yield Strength /MPa | 820.5 | – | – | 765.3 | 751.5 | 579.2 | – |
| Elongation % | 21 | – | – | 14 | 14 | 11 | – |
| Coefficient of Thermal Expansion µm/m⁰C | – | 13.3 | 13.7 | 14.3 | 15.1 | 15.5 | 16.7 |
| Thermal Conductivity /kcal/(hr.m.°C) | – | 14.4 | 16.1 | 17.9 | 19.6 | 21.4 | – |
| Modulus of Elasticity / x105 MPa | – | 2 | 1.93 | 1.79 | 1.72 | 1.65 | 1.52 |
| Size (in.) | WT / ft |
|---|---|
| 5/16″ | 0.290 |
| 9/16″ | 0.930 |
| 7/16″ | 0.560 |
| 13/16″ | 1.950 |
| 1″ | 2.90 |
| 15/16″ | 2.625 |
| 1-1/16″ | 3.30 |
| 1-1/4″ | 4.625 |
| 1-1/8″ | 3.700 |
| 1-5/16″ | 5.100 |
| 3/16″ | 0.104 |
| 1-7/16″ | 6.100 |
| 1-3/8″ | 5.625 |
| 1-1/2″ | 6.625 |
| 1-3/4″ | 9.030 |
| 1-5/8″ | 7.800 |
| 1-7/8″ | 10.400 |
| 2-1/4″ | 14.920 |
| 2″ | 11.80 |
| 2-3/8″ | 16.920 |
| 3″ | 26.53 |
| 2-1/2″ | 18.42 |
| Size | Kgs / Mtr |
|---|---|
| 1″ | 3.0970 |
| 24 mm | 3.0543 |
| 20 mm | 2.0470 |
| 25 mm | 3.0871 |
| 27 mm | 4.0490 |
| 26 mm | 4.0170 |
| 1 to 1/8″ | 5.0033 |
| 1 to 1/4″ | 6.0349 |
| 30 mm | 5.0548 |
| 32 mm | 6.0314 |
| 1 to 3/8″ | 7.0550 |
| 35 mm | 7.0553 |
| 36 mm | 7.0999 |
| 7/8″ | 3.0038 |
| 38 mm | 8.0903 |
| 22 mm | 2.0979 |
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