Denounce with righteous indignation and dislike men who are beguiled and demoralized by the charms pleasure moment so blinded desire that they cannot foresee the pain and trouble.
Read MoreAlloy 230 Supplier and Stockist in India
Largest Alloy 230 Stockist in Mumbai, India. Supplier of UNS N06230 Sheets, ASTM B435 Round Bars Supplier, DIN 2.4733 Plates Stockist. Trusted Aerospace Grade Alloy 230 Supplier & Exporter.
Alloy 230 (Haynes 230) is a high-performance nickel-chromium-tungsten-molybdenum alloy renowned for its exceptional strength, superior oxidation resistance, and excellent stability at elevated temperatures. This makes it an ideal choice for components exposed to extreme heat and corrosive environments. At Bhansali AeroAlloys, we specialize in supplying Alloy 230 in versatile forms such as round bars, sheets, plates, and custom-engineered profiles to meet the precise requirements of aerospace and defense applications. Its ability to maintain mechanical integrity under thermal stress ensures reliable performance in critical engine components, heat exchangers, and high-temperature structural applications.
Alloy 230 (Haynes 230) Stockist
Focusing on the aerospace and defense sectors, Bhansali AeroAlloys delivers Alloy 230 with unmatched quality and precision, adhering to international standards. Our experienced team ensures timely supply of standard and custom solutions, supporting manufacturers in achieving peak performance and safety. Whether you require ready-to-use round bars, sheets or custom form, we are your trusted partner in specialty alloys. Contact us today at sales@bhansaliaeroalloys.com to discuss your Alloy 230 requirements and benefit from our expert guidance and global supply network.
Alloy 230 Specifications
- UNS N06230
- WERKSTOFF 2.4733
- PLATE: AMS 5878, ASTM-B-435, ASME-SB-435, B50TF246-S2, EMS 55469 BAR AMS 5891
- SHEET: AMS 5878, ASTM-B-435, ASME-SB-435, B50TF246-S2, EMS 55469
- BAR: AMS 5891, ASTM-B-572, ASME-SB-572, EMS 55474(CHEM), PWA-1127D
Chemical Composition of Alloy 230
| Element | Min (%) | Max (%) |
|---|---|---|
| Carbon | 0.05 | 0.15 |
| Manganese | 0.30 | 1.00 |
| Silicon | 0.25 | 0.75 |
| Phosphorus | -- | 0.03 |
| Sulfur | -- | 0.015 |
| Chromium | 20.00 | 24.00 |
| Cobalt | -- | 5.00 |
| Iron | -- | 3.00 |
| Aluminum | 0.20 | 0.50 |
| Titanium | -- | 0.10 |
| Boron | -- | 0.015 |
| Copper | -- | 0.50 |
| Lanthanum | 0.005 | 0.05 |
| Tungsten | 13.00 | 15.00 |
| Molybdenum | 1.00 | 3.00 |
| Nickel | REM | |
Key Properties and Fabrication of Alloy 230
Excellent High-Temperature Strength, Thermal Stability, and Environment Resistance
Haynes 230 alloy is a nickel-chromium-tungsten-molybdenum material known for its superior high-temperature strength and outstanding oxidation resistance up to 2100°F (1149°C) during long-term exposure. It also offers excellent resistance to nitriding environments, remarkable thermal stability, and ease of fabrication. The alloy is fully castable and demonstrates lower thermal expansion compared to most other high-temperature alloys. In addition, it maintains resistance to grain coarsening even after extended service at elevated temperatures.
Easily Fabricated
Haynes 230 alloy provides excellent workability for both forming and welding. It can be hot-worked or forged when uniformly heated to around 2150°F (1177°C). Due to its high ductility, the alloy can also be shaped through cold-forming methods. All components subjected to hot or cold working should be annealed and quickly cooled to regain the best combination of strength and toughness. Welding can be performed using standard methods such as GTAW, GMAW, and resistance welding.
Heat-Treatment
Wrought 230 alloy is typically supplied in the solution heat-treated condition unless otherwise specified. The recommended treatment involves heating between 2150–2275°F (1177–1246°C), followed by rapid cooling or water quenching to optimize mechanical properties. Annealing at lower temperatures may result in carbide precipitation, which can slightly reduce ductility and mechanical strength.
Casting
Haynes 230 alloy can be manufactured using conventional air-melt sand casting or vacuum-melt investment casting techniques. For improved fluidity, silicon should be maintained at the higher end of the specification. Castings can be used either in the as-cast condition or after undergoing solution heat treatment, depending on the property requirements of the application.
Creep and Stress-Rupture Strength of Alloy 230
Alloy 230 (Haynes 230) is a solid-solution-strengthened material which combines excellent high-temperature strength with good fabricability at room temperature. It is particularly effective for very long-term applications at temperatures of 1200°F (649°C) or more, and is capable of outlasting stainless steels and nickel alloys by as much as 100 to 1 depending upon the temperature. Alternatively, the higher strength of 230 allows for the use of design section thickness as much as 75 percent thinner than lesser alloys with no loss in load-bearing capability.
Stress-Rupture Life of Alloy 230 at Fixed Test Conditions (Bar and Plate)*
| Alloy | Hours to Rupture | ||
|---|---|---|---|
| 1400°F / 15.0 Ksi (760°C / 103 MPa) |
1600°F / 4.5 Ksi (871°C / 31 MPa) |
1800°F / 2.0 Ksi (982°C / 14 MPa) |
|
| 230 alloy | 8200 | 65,000 | 5,000 |
Sheet - 2250°F (1232°C) Solution Anneal
| Test Temperature °F (°C) |
Creep, Percent | Approximate Initial Stress, Ksi (MPa) to Produce Specified Creep in: |
|||
|---|---|---|---|---|---|
| 10 Hours | 100 Hours | 1,000 Hours | 10,000 Hours* | ||
| 1200 (649) | 0.5 | 48.0 (330) | 32.0 (220) | 22.0 (150) | ----- |
| 1.0 | 51.0 (350) | 36.0 (250) | 25.0 (170) | ----- | |
| Rupture | 67.0 (460) | 48.0 (330) | 36.0 (250) | 27.0 (185) | |
| 1300 (704) | 0.5 | 31.0 (215) | 21.3 (145) | 14.5 (100) | ----- |
| 1.0 | 34.0 (235) | 24.0 (165) | 16.5 (115) | ----- | |
| Rupture | 47.0 (325) | 34.0 (235) | 25.0 (170) | 18.5 (130) | |
| 1400 (760) | 0.5 | 17.2 (120) | 13.7 (95) | 10.8 (75) | ----- |
| 1.0 | 20.0 (140) | 14.8 (100) | 11.7 (81) | ----- | |
| Rupture | 32.0 (220) | 24.5 (170) | 18.2 (125) | 13.2 (91) | |
| 1500 (816) | 0.5 | 13.1 (90) | 10.3 (71) | 7.8 (54) | ----- |
| 1.0 | 14.1 (97) | 11.2 (77) | 8.6 (59) | ----- | |
| Rupture | 23.3 (160) | 17.5 (120) | 12.5 (86) | 8.4 (58) | |
| 1600 (871) | 0.5 | 10.0 (69) | 7.6 (52) | 5.5 (38) | ----- |
| 1.0 | 11.0 (76) | 8.4 (58) | 5.8 (40) | ----- | |
| Rupture | 17.0 (115) | 12.1 (83) | 8.2 (57) | 5.6 (39) | |
| 1700 (927) | 0.5 | 7.5 (52) | 5.4 (37) | 3.4 (23) | ----- |
| 1.0 | 8.3 (57) | 5.7 (39) | 3.6 (25) | ----- | |
| Rupture | 12.0 (83) | 8.0 (55) | 4.9 (34) | 3.2 (22) | |
| 1800 (982) | 0.5 | 5.4 (37) | 3.4 (23) | 1.7 (12) | ----- |
| 1.0 | 5.7 (39) | 3.6 (25) | 1.9 (13) | ----- | |
| Rupture | 8.0 (55) | 4.9 (34) | 2.6 (18) | 1.1 (7.6) | |
| 1900 (1038) | 0.5 | ----- | ----- | ----- | ----- |
| 1.0 | ----- | ----- | ----- | ----- | |
| Rupture | 7.5 (52) | 3.5 (24) | 1.6 (11) | ----- | |
Plate and Bar - 2250°F (1232°C) Solution Anneal
| Test Temperature °F (°C) | Creep, Percent | Approximate Initial Stress, Ksi (MPa) to Produce Specified Creep in: | |||
|---|---|---|---|---|---|
| 10 Hours | 100 Hours | 1,000 Hours | 10,000 Hours* | ||
| 1200 (649) | 0.5 | 59.0 (405) | 34.0 (235) | 23.0 (160) | ---- |
| 1.0 | 60.0 (415) | 39.0 (270) | 26.4 (180) | 17.5 (120) | |
| Rupture | ---- | 42.5 (295) | 42.5 (295) | 29.0 (200) | |
| 1300 (704) | 0.5 | 30.0 (205) | 20.5 (140) | 15.0 (105) | ---- |
| 1.0 | 35.0 (240) | 23.5 (160) | 18.0 (125) | 12.3 (85) | |
| Rupture | 52.0 (360) | 39.0 (270) | 29.0 (200) | 21.0 (145) | |
| 1400 (760) | 0.5 | 19.0 (130) | 14.0 (97) | 11.0 (76) | ---- |
| 1.0 | 21.5 (150) | 15.9 (110) | 11.5 (79) | 8.0 (55) | |
| Rupture | 37.0 (255) | 27.0 (185) | 20.0 (140) | 14.2 (98) | |
| 1500 (816) | 0.5 | 13.4 (92) | 10.6 (73) | 8.2 (57) | ---- |
| 1.0 | 15.0 (105) | 12.0 (83) | 9.2 (63) | 6.5 (45) | |
| Rupture | 26.0 (180) | 19.0 (130) | 14.0 (97) | 9.8 (68) | |
| 1600 (871) | 0.5 | 10.3 (71) | 8.0 (55) | 5.6 (39) | ---- |
| 1.0 | 11.7 (81) | 9.0 (62) | 6.0 (41) | 4.4 (30) | |
| Rupture | 18.5 (130) | 13.7 (95) | 9.2 (63) | 6.2 (43) | |
| 1700 (927) | 0.5 | 7.8 (54) | 5.5 (38) | 3.4 (23) | ---- |
| 1.0 | 8.8 (61) | 6.3 (43) | 4.0 (28) | 2.6 (18) | |
| Rupture | 13.4 (92) | 9.4 (65) | 6.0 (41) | 3.5 (24) | |
| 1800 (982) | 0.5 | 5.5 (38) | 3.4 (23) | 1.6 (11) | ---- |
| 1.0 | 6.3 (43) | 3.8 (26) | 2.0 (14) | 1.1 (7.6) | |
| Rupture | 9.4 (65) | 6.0 (41) | 3.0 (21) | 1.6 (11) | |
| 1900 (1038) | 0.5 | ---- | ---- | ---- | ---- |
| 1.0 | 4.4 (30) | 2.0 (14) | 0.9 (6.2) | ---- | |
| Rupture | 7.0 (48) | 3.5 (24) | 1.8 (12) | ---- | |
| 2100 (1149)* | 0.5 | ---- | ---- | ---- | ---- |
| 1.0 | 1.1 (7.6) | 0.4 (2.8) | ---- | ---- | |
| Rupture | 2.3 (16) | 1.2 (8.3) | 0.6 (4.1) | ---- | |
ASME Vessel Code Allowance Stresses
| Metal Temperatures Not Exceeding °F (°C) |
Maximum Allowable Stress Values | |
|---|---|---|
| Standard Ksi (MPa) |
Note (1) Ksi (MPa) |
|
| 100 (37) | 27.5 (189) | 27.5 (189) |
| 200 (93) | 27.5 (189) | 27.5 (189) |
| 300 (149) | 26.2 (180) | 27.5 (189) |
| 400 (204) | 24.7 (170) | 27.0 (186) |
| 500 (260) | 23.1 (159) | 26.4 (182) |
| 600 (315) | 21.6 (148) | 26.0 (179) |
| 650 (343) | 21.1 (145) | 25.8 (177) |
| 700 (371) | 21.0 (144) | 25.7 (177) |
| 750 (398) | 21.0 (144) | 25.7 (177) |
| 800 (426) | 20.9 (144) | 25.7 (177) |
| 850 (454) | 20.9 (144) | 25.5 (175) |
| 900 (482) | 20.9 (144) | 25.4 (175) |
| 950 (510) | 20.9 (144) | 25.1 (173) |
| 1000 (537) | 20.8 (143) | 24.8 (170) |
| 1050 (565) | 20.8 (143) | 24.7 (170) |
| 1100 (593) | 20.8 (143) | 21.0 (144) |
| 1150 (621) | 17.4 (119) | 17.4 (119) |
| 1200 (648) | 14.7 (101) | 14.7 (101) |
| 1250 (676) | 12.3 (84) | 12.3 (84) |
| 1300 (704) | 10.1 (69) | 10.1 (69) |
| 1350 (732) | 8.4 (57) | 8.4 (57) |
| 1400 (760) | 7.0 (48) | 7.0 (48) |
| 1450 (787) | 5.7 (39) | 5.7 (39) |
| 1500 (815) | 4.6 (31) | 4.6 (31) |
| 1550 (843) | 3.7 (25) | 3.7 (25) |
| 1600 (871) | 2.8 (19) | 2.8 (19) |
| 1650 (898) | 2.0 (13) | 2.0 (13) |
Global Export Destinations for Our Alloy 230
We export Alloy 230 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
Domestic Cities Where We Supply Alloy 230
We supply Alloy 230 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.
