bg_image

Rene 41 Supplier and Stockist in India

Largest Rene 41 Stockist in Mumbai, India. AMS 5545 Rene 41 Sheets Supplier, Rene 41 Round Bars Stockist (AMS 5712/5713), Rene 41 Plates Dealer. Reliable Aerospace Grade Rene 41 Distributor & Exporter.

Rene 41 (UNS N07041) is a nickel-chromium alloy strengthened with cobalt, molybdenum, and titanium, engineered to deliver exceptional strength, oxidation resistance, and creep resistance at elevated temperatures. Capable of maintaining mechanical stability up to 1800°F (982°C), Rene 41 is widely used in the aerospace and defense industries for turbine engines, afterburner components, fasteners, and other critical high-temperature applications. Its outstanding resistance to thermal fatigue and corrosion ensures reliable performance in the most demanding environments.

Rene 41 Round Bars Stockist

Rene 41 Stockist in India

At Bhansali AeroAlloys, we provide premium-quality Rene 41 round bars, sheets, plates, and custom forms tailored to meet the exacting standards of aerospace and defense applications. With a strong focus on precision, durability, and timely delivery, we ensure that our materials perform flawlessly in mission-critical systems. For technical guidance, customized solutions, or pricing inquiries, reach out to our expert team today at sales@bhansaliaeroalloys.com and partner with a trusted supplier of advanced high-temperature alloys.

Type Analysis

Element Min Max
Carbon 0.06 0.12
Manganese -- 0.10
Silicon -- 0.20
Chromium 18.0 20.0
Nickel Balance --
Boron 0.003 0.010
Iron -- 5.00
Cobalt 10.0 12.0
Titanium 3.00 3.30
Aluminum 1.40 1.60
Molybdenum 9.00 10.50

Corrosion Resistance

Offers exceptional corrosion and oxidation resistance, withstanding jet engine combustion gases at temperatures up to 1800°F (982°C).

Applications

Used in afterburner components, turbine casings, wheels, buckets, bolts, and fasteners for jet engines and high-speed airframes.

Physical Properties

Property Value
Density (lb/in³) 0.298
Density (kg/m³) 8249
Melting Range (°F) 2400–2500°F
Melting Range (°C) 1316–1371°C
Specific Heat (Btu/lb-°F) 0.108 (70–600°F)
Specific Heat (kJ/kg-K) 0.452 (21–316°C)

Modulus of Elasticity

Temperature Temp (°F) Temp (°C) ksi x 10³ MPa x 10³
80 27 31.6 218
200 93 31.0 214
600 316 29.3 202
1000 538 27.3 188
1200 649 26.0 179
1400 760 24.8 171
1600 871 23.2 160

Electrical Resistivity

Condition ohms c/mf microhm-mm
Hot rolled 787.1 1310
A + 1950°F, 4 hrs, AC 751.6 1250
B + 1400°F, 16 hrs, AC 761.4 1270
A + 2150°F, 30 min, AC 803.0 1330
D + 1650°F, 4 hrs, AC 807.2 1340

Mean Coefficient of Thermal Expansion

Temperature Temperature Coefficient of Expansion
°F °C 10⁻⁶/°F 10⁻⁶/°C
200 93 6.7 12.1
600 316 7.0 12.6
1000 538 7.5 13.5
1200 649 7.8 14.0
1400 760 8.2 14.8
1600 871 8.8 15.8
1800 982 9.3 16.7
2000 1093 9.0 17.8

Thermal Conductivity

Temperature Temperature Thermal Conductivity
°F °C Btu-in/ft²-hr-°F W/m-K
300 149 80 11.5
600 316 102 14.7
1000 538 131 18.9
1200 649 146 21.1
1400 760 161 23.2
1600 871 175 25.2

Heat Treatment

Step Details
Annealing Quench from above gamma prime solvus (1950°F / 1066°C) for lowest hardness. Hardness: Rockwell B 98 / C 30.
Solution Treatment Gamma prime solvus: 1960–1980°F (1071–1082°C). Fine grain: 1900–1925°F (1038–1052°C), hold 4 hrs, air cool.
Stress Rupture Improvement Above solvus: 1975°F (1080°C), hold 1 hr, air cool.
Precipitation Hardening 1400°F (760°C) for 16 hrs, air cool. Final hardness Rockwell C 40–45.

Workability & Machining

Process Details
Hot Working / Forging Best forged between 2100°F (1149°C) and finishing at 1850–1900°F (1010–1038°C).
Cold Working Rapid work hardening; frequent annealing required. Avoid strain age cracking by heating quickly through aging range.
Machinability Difficult to machine. Use tungsten carbide tools. Typical tool geometry: 0° back rake, 6° side rake, 7° clearance, 10° end cutting edge, 45° side cutting edge, 1/16" nose radius.
Machining Conditions Feed: 0.005–0.011"/rev, Depth of cut: 1/32–1/8", Speed: 30–60 FPM. Fully treated or partially aged gives better finish. Aging causes size contraction (~0.0013" per inch).
Welding Weldable by inert gas-arc. Part should be solution treated before welding. Post-weld: solution treat and optionally age at 1650°F (899°C) for 1 hr before final aging.
Global Export Destinations for Our Rene 41
We export Rene 41 to countries across the globe, including Afghanistan, Albania, Andorra, Austria, Bahrain, Bangladesh, Bhutan, Brunei, Belarus, Belgium, Bulgaria, Cambodia, China, Cyprus, Croatia, Czech Republic, Denmark, Estonia, Egypt, Finland, France, Germany, Greece, Georgia, Hungary, Iceland, Ireland, Italy, Indonesia, Iran, Iraq, Israel, Japan, Jordan, Kazakhstan, Kuwait, Kyrgyzstan, Lebanon, Latvia, Latin America, Liechtenstein, Lithuania, Luxembourg, Malta, Moldova, Monaco, Malaysia, Maldives, Mongolia, Myanmar (Burma), Nepal, North Korea, Netherlands, Norway, Oman, Poland, Portugal, Pakistan, Palestine, Philippines, Qatar, Russia, Romania, Russia, San Marino, Serbia and Montenegro, Slovakia, Slovenia, Spain, Sweden, Switzerland, Saudi Arabia, Singapore, South Korea, South Africa, Sri Lanka, Syria, Taiwan, Tanzania, Tajikistan, Thailand, Turkey, Turkmenistan, United States, Ukraine, United Kingdom, United Arab Emirates (UAE), Uzbekistan, Vietnam, Yemen
We supply Rene 41 to cities including Mumbai, Delhi, Kolkata, Chennai, Bengaluru, Hyderabad, Ahmedabad, Pune, Surat, Jaipur, Kanpur, Lucknow, Nagpur, Ghaziabad, Indore, Coimbatore, Kochi, Patna, Kozhikode, Bhopal, Thrissur, Vadodara, Agra, Malappuram, Thiruvananthapuram, Kannur, Ludhiana, Nashik, Vijayawada, Madurai, Varanasi, Meerut, Faridabad, Rajkot, Jamshedpur, Srinagar, Jabalpur, Asansol, Vasai-Virar City, Allahabad, Dhanbad, Aurangabad, Amritsar, Jodhpur, Ranchi, Raipur, Kollam, Gwalior, Durg-Bhilainagar, Chandigarh, and Tiruchirappalli.