HIGH-TEMPERATURE SUPERALLOY DISTRIBUTOR
HIGH-TEMPERATURE SUPERALLOY DISTRIBUTOR
Superalloys, or High Temperature Alloys, are alloys that exhibit several key characteristics: excellent mechanical strength, resistance, thermal creep deformation, good surface stability and resistance to corrosion or oxidation. The term ‘superalloy’ was coined after World War II to describe alloys developed for use in turbine engines and turbo-superchargers that required high performance at elevated temperatures. The three major classes of superalloys are nickel-, iron-, and cobalt-based alloys. Since 1978, ASM has been supplying High Temperature Superalloys to the aerospace, and petroleum-chemical processing industries.
For more information or to receive a prompt superalloy price quote, please contact us at 800 398-4345, 954-977-0666 or submit the INSTAQUOTE Form.
SHEET & PLATE
|
Sizes: 0.010" TO 0.160" x R/W x R/L 0.188" TO 5.000" x R/W x R/L | TYPE | SPECIFICATIONS |
|---|---|---|
| A-286 | AMS-5525 | |
| HASTELLOY C-276* | ASTM-B-575 | |
| HASTELLOY C* | AMS-5530 | |
| HASTELLOY X* | AMS-5536, B50TF24, 25, PWA-1038 | |
| HAYNES 188* | AMS-5608, PWA-1042, B50TF74 | |
| INCOLOY 800² | ASTMB409 | |
| INCONEL 600² | AMS-5540 | |
| INCONEL 617² | AMS-5888, 5889, PWA-1165, B50TF181 | |
| INCONEL 625² | AMS-5599 | |
| INCONEL 718² | AMS-5596, 5597, B50TF14 | |
| INCONEL 722² | AMS-5541, B50T73 | |
| INCONEL X-750² | AMS-5542, 5598 | |
| L-605, HAYNES 25* | AMS-5537 | |
| N-155, MULTIMET* | AMS-5532 | |
| NICKEL 200 | ASTM-B162 | |
| NICKEL 201 | AMS-5553 | |
| MONEL 400² | AMS-4544, ASTM B127, QQN281 | |
| RENE 41* | AMS-5545, B50TF76, B50TF109 | |
| WASPALOY¹ | AMS-5544 |
¹ Trademark United Technologies
² Trademark Inco Alloys
* Trademark Haynes International
ROD, BAR & FORGINGS
|
Full Range of Sizes in All Shapes
Forgings: Full Range of Sizes | TYPE | SPECIFICATIONS |
|---|---|---|
| A-286 | AMS-5731, 5732, 5734, 5737 | |
| HASTELLOY C-276* | ASTM-B-574 | |
| HASTELLOY C* | AMS-5750 | |
| HASTELLOY X* | AMS-5754, B50TF31 | |
| INCOLOY 800² | AMTMB408 | |
| INCONEL 600² | AMS-5665 | |
| INCONEL 625² | AMS-5666 | |
| INCONEL 718² | AMS-5662, 5663, 5664, B50TF15, LBO170-186 | |
| INCONEL 722² | AMS-5714 | |
| INCONEL X-750² | AMS-5667, 5668, 5670, 5671 | |
| L-605, HAYES 25* | AMS-5759 | |
| N-155 | AMS-5768, 5769 | |
| NICKEL 200 | ASTMB160 | |
| MONEL 400² | ASTMB164, QQN281 | |
| MONEL² K500² | AMS4676, QQN286 | |
| WASPALOY¹ | AMS-5704, 5706, 5707, 5708, 5709 | |
| INCONEL 901² | AMS-5660, 5661 | |
| RENE 41* | AMS-5712, 5713, B50TF75 |
¹ Trademark United Technologies
² Trademark Inco Alloys
* Trademark Haynes International
TUBING
|
Sizes: 0.020" TO 12.00" OD 0.002" TO 4.000" Wall | TYPE | SPECIFICATIONS |
|---|---|---|
| A-286 | AMS-5732, 5734, 5737 | |
| HASTELLOY X* | AMS-5587, 5588, PWA-1066 | |
| HAYNES 188* | PWA-1088 | |
| INCONEL 600² | AMS-5580, PWA-1060, 1070 | |
| INCONEL 625² | AMS-5581, PWA-1069, 1072, B50TF133 | |
| INCONEL 718² | AMS-5589, 5590, PWA-1065 | |
| INCONEL X-750² | AMS-5582 | |
| WASPALOY¹ | AMS-5586 | |
| L-605 | B50T27 |
¹ Trademark United Technologies
² Trademark Inco Alloys
* Trademark Haynes International
ON-TIME DELIVERY
ALLOYS INFORMATION
Nickel-based Superalloys have been developed for very high-temperature applications where relatively high stresses are encountered and where high surface stability is frequently required. Nickel is a very versatile metal with many applications in the aerospace industry. Its ability to alloy with a wide range of metals has brought it to the forefront of metallurgy. Nickel alloys possess high strength and excellent corrosion resistance, particularly in aerospace applications where elevated temperatures are present. Cobalt is a strategic and critical metal used in many diverse commercial, industrial, and military applications. The largest use of cobalt in the aerospace industry is to make parts for gas turbine aircraft engines. Heat resistant alloys of nickel and cobalt are used where high-temperature performance, particularly creep resistance, is required. These alloys have been typically selected for gas turbine components such as blades, turbine wheels, and later stage compressor disks, which are subjected to long-term rotational stresses and high temperatures.
The commercial forms of nickel and cobalt based alloys fall into the following categories:
High Temperature
These materials are designed to provide unique strength and/or corrosion properties at elevated temperatures. Major attributes include properties such as high strength, high creep resistance, resistance to softening, or resistance to metals loss at high temperature from oxidation, sulfidation, or carburization. Nickel content ranges from approximately 25% to 60%, with critical amounts of chromium, molybdenum, columbium and titanium.
Grade | End Use |
AL 600 | Furnace parts, Heat treatment fixtures and restaurant cooking appliances |
AL 601 | Heat treat baskets, Muffles and Retorts |
AL 625 HP | Applications similar to AL 625 where extended fatigue life is desired, particularly at low cycle. |
AL 800™ | Process piping, Heat treat fixtures and Furnace parts |
ALTEMP™ 263 | Land based gas turbines |
ALTEMP™ 625 | Jet engine nacelles, Engine plumbing, Aircraft ducting, Recuperators and Trust |
Corrosion Resistant
These alloys are intended for applications in the chemical processing, petroleum refining, marine, heat treating, pollution and waste control industries where common 200, 300 and 400 Series stainlesses may not provide adequate corrosion protection. The Corrosion Resistant Materials may be grouped as follows:
Grade | End Use |
AL 200/201 | Containers and Piping |
AL 22 | Flue-gas desulphurization systems, Waste incinerators, and Sour Gas service |
AL 276 | Pipe, tube for aggressive chloride environments |
AL 400 | Pumps, Valves and Fittings |
AL 825 | Pollution control and Radioactive waste equipment, Chemical transportation and acid production equipment, Pickling equipment, Oil/Gas well piping. |
ALLCORR® | Highly aggressive acidic chloride environments |
Electric
Soft Magnetic – Controlled Expansion – The thermal expansion characteristics of this group are used in several ways. For glass-to-metal sealing applications, the thermal expansion characteristics of glass and metal are closely matched and the metal must also have an oxide which fluxes at high temperature with the glass to provide a hermetic and mechanically sound joint. The most common applications are attachment of metallic parts to the internal of TV and cathode ray tubes, and also certain lamp bulb bases.
Grade | End Use |
AL 36 | Controlled Expansion: Liquefied gas storage, Bimetallic strips for thermometers, LNG, TV Aperature masks, Composite wing molds. |
AL 42 | Controlled Expansion: Lead frames, Color TB electron guns, Glass-metal and ceramic-metal seals, Transistors. |
AL 4750 | Soft Magnetic: Magnetic relay parts, Magnetic shielding, Pole pieces, Specialty motor stators and rotors, Electric Transformers and Magnetic amplifiers |
Moly Permalloy | Soft Magnetic: Cores and relay components for high sensitivity ground fault circuit breakers, Magnetic shields and Electric transformers |
TECHNICAL DATA SHEETS
- Allegheny Ludlum Altemp® A286 Iron-Base Superalloy, UNS S66286
- Haynes® 188 alloy, 0% cold reduction, 3.2 mm thick sheet
- Haynes® 188 alloy, 10% cold reduction, 3.2 mm thick sheet
- Haynes® 188 alloy, 10% cold reduction, 3.2 mm thick sheet, 1065°C for 5 minutes
- Haynes® 188 alloy, 10% cold reduction, 3.2 mm thick sheet, 1120°C for 5 minutes
- Haynes® 188 alloy, 10% cold reduction, 3.2 mm thick sheet, 1175°C for 5 minutes
- Haynes® 188 alloy, 20% cold reduction, 3.2 mm thick sheet
- Haynes® 188 alloy, 20% cold reduction, 3.2 mm thick sheet, 1065°C for 5 minutes
- Haynes® 188 alloy, 20% cold reduction, 3.2 mm thick sheet, 1120°C for 5 minutes
- Haynes® 188 alloy, 20% cold reduction, 3.2 mm thick sheet, 1175°C for 5 minutes
- Haynes® 188 alloy, 30% cold reduction, 3.2 mm thick sheet
- Haynes® 188 alloy, 30% cold reduction, 3.2 mm thick sheet, 1065°C for 5 minutes
- Haynes® 188 alloy, 30% cold reduction, 3.2 mm thick sheet, 1120°C for 5 minutes
- Haynes® 188 alloy, 30% cold reduction, 3.2 mm thick sheet, 1175°C for 5 minutes
- Haynes® 188 alloy, 40% cold reduction, 3.2 mm thick sheet
- Haynes® 188 alloy, 40% cold reduction, 3.2 mm thick sheet, 1065°C for 5 minutes
- Haynes® 188 alloy, 40% cold reduction, 3.2 mm thick sheet, 1120°C for 5 minutes
- Haynes® 188 alloy, 40% cold reduction, 3.2 mm thick sheet, 1175°C for 5 minutes
- Haynes® 188 alloy, cold rolled and 1175°C solution annealed sheet, tested at 1095°C (2000°F)
- Haynes® 188 alloy, cold rolled and 1175°C solution annealed sheet, tested at 540°C (1000°F)
- Haynes® 188 alloy, cold rolled and 1175°C solution annealed sheet, tested at 650°C (1200°F)
- Haynes® 188 alloy, cold rolled and 1175°C solution annealed sheet, tested at 760°C (1400°F)
- Haynes® 188 alloy, cold rolled and 1175°C solution annealed sheet, tested at 870°C (1600°F)
- Haynes® 188 alloy, cold rolled and 1175°C solution annealed sheet, tested at 980°C (1800°F)
- Haynes® 188 alloy, cold rolled and 1175°C solution annealed sheet, tested at RT
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 1095°C (2000°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 1150°C (2100°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 1205°C (2200°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 540°C (1000°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 650°C (1200°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 760°C (1400°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 870°C (1600°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at 980°C (1800°F)
- Haynes® 188 alloy, hot rolled and 1175°C solution annealed plate, tested at RT
- Haynes® 188 alloy, plate at RT after 0 hours at 650°C (1200°F)
- Haynes® 188 alloy, plate at RT after 0 hours at 760°C (1400°F)
- Haynes® 188 alloy, plate at RT after 0 hours at 870°C (1600°F)
- Haynes® 188 alloy, plate at RT after 1000 hours at 870°C (1600°F)
- Haynes® 188 alloy, plate at RT after 16000 hours at 870°C (1600°F)
- Haynes® 188 alloy, plate at RT after 4000 hours at 870°C (1600°F)
- Haynes® 188 alloy, plate at RT after 8000 hours at 650°C (1200°F)
- Haynes® 188 alloy, plate at RT after 8000 hours at 760°C (1400°F)
- Haynes® 188 alloy, plate at RT after 8000 hours at 870°C (1600°F)
- Haynes® Hastelloy® X alloy, sheet, tested at 1095°C (2000°F)
- Haynes® Hastelloy® X alloy, sheet, tested at 540°C (1000°F)
- Haynes® Hastelloy® X alloy, sheet, tested at 650°C (1200°F)
- Haynes® Hastelloy® X alloy, sheet, tested at 760°C (1400°F)
- Haynes® Hastelloy® X alloy, sheet, tested at 870°C (1600°F)
- Haynes® Hastelloy® X alloy, sheet, tested at 980°C (1800°F)
- Haynes® Hastelloy® X alloy, sheet, tested at RT
- Haynes® Multimet® alloy, 1.32 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 1038°C
- Haynes® Multimet® alloy, 1.32 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 649°C (1200°F)
- Haynes® Multimet® alloy, 1.32 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 927°C
- Haynes® Multimet® alloy, 1.32 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at RT
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 1093°C
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 1149°C (2100°F)
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 1204°C (2200°F)
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 1260°C
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 1288°C
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 427°C (800°F)
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 538°C (1000°F)
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 649°C (1200°F)
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 760°C (1400°F)
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 871°C (1600°F)
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at 982°C
- Haynes® Multimet® alloy, 1.6 mm thick sheet, 1177°C heat treatment, rapid air cooled, tested at RT
- Haynes® Multimet® alloy, 12.7 mm (1/2 in.) thick plate, 1185°C heat treatment, water quenched, tested at -196°C
- Haynes® Multimet® alloy, 12.7 mm (1/2 in.) thick plate, 1185°C heat treatment, water quenched, tested at -78°C
- Haynes® Multimet® alloy, 12.7-50.8 mm hot-rolled bar, 1185°C heat treatment, water quenched, tested at RT
- Haynes® Multimet® alloy, 25.4-50.8 mm forged bar, 1185°C heat treatment, water quenched, tested at RT
- Haynes® Multimet® alloy, 533.4 by 82.55 mm forging, stress relieved at 649°C (1200°F), air cooled, tested at 649°C (1200°F)
- Haynes® Multimet® alloy, 533.4 by 82.55 mm forging, stress relieved at 649°C (1200°F), air cooled, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 10% cold reduction, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 1185°C heat treatment, rapid air cooled, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 15% cold reduction, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 20% cold reduction, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 25% cold reduction, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 30% cold reduction, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 35% cold reduction, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 40% cold reduction, tested at RT
- Haynes® Multimet® alloy, 6.15 mm hot-rolled bar, 5% cold reduction, tested at RT
- Haynes® Waspaloy™ alloy, sheet, tested at 1095°C (2000°F)
- Haynes® Waspaloy™ alloy, sheet, tested at 650°C (1200°F)
- Haynes® Waspaloy™ alloy, sheet, tested at 760°C (1400°F)
- Haynes® Waspaloy™ alloy, sheet, tested at 870°C (1600°F)
- Haynes® Waspaloy™ alloy, sheet, tested at 980°C (1800°F)
- Haynes® Waspaloy™ alloy, sheet, tested at RT
- Nickelvac® A-286 Specialty Steel, Heat Treatment: 982°C (1800°F) + Age
- Nickelvac® L-605 Nickel Superalloy, Heat Treatment: 1204°C (2200°F) Anneal
- Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age
- Special Metals INCO® A-286 Iron-Nickel-Chromium Alloy
- Special Metals INCONEL® Alloy 600
- Special Metals INCONEL® Alloy 617
- Special Metals INCONEL® Alloy 625
- Special Metals INCONEL® Alloy 718
- Special Metals INCONEL® Alloy X-750
- Special Metals NIMONIC™ Alloy 901
- Waspaloy® Nickel Superalloy, Heat Treatment: 1010°C (1850°F) + Age
Nickel-based Superalloys have been developed for very high temperature applications where relatively high stresses are encountered and where high surface stability is frequently required. Nickel is a very versatile metal with many applications in the aerospace industry. It’s ability to alloy with a wide range of metals has brought it to the forefront of metallurgy. Nickel alloys possess high strength and excellent corrosion resistance, particularly in aerospace applications where elevated temperatures are present. Cobalt is a strategic and critical metal used in many diverse commercial, industrial, and military applications. The largest use of cobalt in the aerospace industry is to make parts for gas turbine aircraft engines. Heat resistant alloys of nickel and cobalt are used where high temperature performance, particularly creep resistance, is required. These alloys have been typically selected for gas turbine components such as blades, turbine wheels and latter stage compressor disks, which are subjected to long term rotational stresses and high temperatures.
STILL HAVE ANY QUESTIONS? IS SOMETHING UNCLEAR? DO NOT SEE WHAT YOU ARE LOOKING FOR? AEROSPACE SPECIFICATION SERVICES FRIENDLY SALES TEAM IS WAITING FOR YOUR CALL AT 800-398-4345 OR SEND US AN EMAIL
