Nickel Alloy Bars

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Waspaloy is a precipitation hardening, nickel-based alloy which has been used in elevated temperature applications. The alloy has been used for gas turbine engine parts which require considerable strength and corrosion resistance at temperatures up to 1600°F (871°C). Waspaloy is usually vacuum-induction plus consumable electrode remelted. Waspaloy has excellent resistance to corrosion by combustion products, encountered in gas turbines and aircraft jet engines, at temperatures up to 1600°F. Intergranular oxidation occurs at temperatures above 1600°F.

Waspaloy Bar AMS 5706 – High-Performance Nickel Alloy for Demanding Applications

As trusted stockists and suppliers of premium ferrous materials, we proudly offer Waspaloy Bar AMS 5706, a high-strength, nickel-based superalloy designed for extreme environments. Known for its exceptional heat resistance, corrosion resistance, and mechanical strength, Waspaloy is ideal for aerospace, gas turbine, and industrial applications.

Our Waspaloy Bar AMS 5706 meets stringent aerospace standards, ensuring superior performance in high-temperature and high-stress conditions. With excellent creep resistance, oxidation resistance, and fatigue strength, this alloy is perfect for components like turbine blades, shafts, and fasteners.

Whether you're in aerospace, power generation, or chemical processing, our Waspaloy Bar AMS 5706 delivers unmatched reliability and durability. Contact us today for competitive pricing and fast delivery of this premium nickel alloy.

Keywords: Waspaloy Bar AMS 5706, nickel-based superalloy, high-temperature alloy, corrosion-resistant bar, aerospace-grade materials, heat-resistant alloy, turbine components, AMS 5706 specification, nickel alloy suppliers, ferrous materials stockist, high-strength nickel alloy, Waspaloy bar stock, industrial superalloy, gas turbine components, oxidation-resistant alloy.

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HAYNES® 230® (UNS N06230) alloy is a nickel-chromium-tungsten-molybdenum alloy that combines excellent high-temperature strength, outstanding resistance to oxidizing environments up to 2100°F (1149°C) for prolonged exposures, premier resistance to nitriding environments, and excellent long-term thermal stability. It is readily fabricated and formed, and is castable. Other attractive features include lower thermal expansion characteristics than most high-temperature alloys, and a pronounced resistance to grain coarsening with prolonged exposure to high temperatures.

HAYNES® 230® alloy has excellent forming and welding characteristics. It may be forged or otherwise hot-worked, providing it is held at 2150°F (1177°C) for a time sufficient to bring the entire piece to temperature. As a consequence of its good ductility, 230® alloy is also readily formed by cold-working. All hot- or cold-worked parts should be annealed and rapidly cooled in order to restore the best balance of properties. The alloy can be welded by a variety of techniques, including gas tungsten arc (GTAW), gas metal arc (GMAW), and resistance welding.

Wrought 230® alloy is furnished in the solution heat treated condition, unless otherwise specified. The alloy is solution heat-treated in the range of 2150 to 2275°F (1177 to 1246°C) and rapidly cooled or water-quenched for optimum properties.

Annealing at temperatures lower than the solution heat treating temperatures will produce some carbide precipitation in 230® alloy, which may marginally affect the alloy’s strength and ductility.

HAYNES® 230® alloy combines properties which make it ideally suited for a wide variety of component applications in the aerospace and power industries. It is used for combustion cans, transition ducts, flame holders, thermocouple sheaths, and other important gas turbine components. In the chemical process industry, 230® alloy is used for catalyst grid supports in ammonia burners, high-strength thermocouple protection tubes, high-temperature heat exchangers, ducts, high-temperature bellows, and various other key process internals.

In the industrial heating industry, applications for 230 alloy include furnace retorts, chains and fixtures, burner flame shrouds, recuperator internals, dampers, nitriding furnace internals, heat-treating baskets, grates, trays, sparger tubes, thermocouple protection tubes, cyclone internals, and many more.

Haynes 230 is a nickel-chromium-tungsten-molybdenum superalloy designed for exceptional high-temperature strength, oxidation resistance, and thermal stability. Ideal for aerospace, gas turbines, industrial heating, and chemical processing, this alloy offers superior performance in extreme environments up to 2200°F (1200°C).

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MULTIMET® alloy (UNS R30155, W73155) is recommended for use in applications involving high stress at temperatures up to 1500°F, and moderate stress up to 2000°F. It has excellent oxidation resistance, good ductility, and is readily fabricated. Its high-temperature properties are inherent and are not dependent upon age-hardening. Production and use of the alloys dates back to the late 1940s.

The alloy has been used in a number of aircraft application including tailpipes and tail cones, afterburner parts, exhaust manifolds, combustion chambers, turbine blades, buckets, and nozzles. It also gives excellent service for high-temperature bolts, and has proven to be an economical material of construction for use in heat-treating equipment where strength at high temperatures is essential.

MULTIMET® alloy has good resistance to corrosion in certain media under both oxidizing and reducing conditions. When solution heat treated, MULTIMET® alloy has about the same resistance to nitric acid as does stainless steel. It has better resistance than stainless steel to weak solutions of hydrochloric acid. It withstands all concentrations of sulfuric acid at room temperature.

MULTIMET® alloy can be machined, forged and cold-formed by conventional methods. The alloy can be welded by various arc and resistance-welding processes.

MULTIMET® alloy is available as sheet, strip, plate, wire, coated electrodes, billet stock and sane and investment castings. It is also available in the form of re-melt stock to a certified chemistry.

Most wrought forms of MULTIMET® alloy are shipped in the solution heat-treated condition to assure optimum properties. Sheet is given a solution heat-treatment of 2150°F, for a time dependent upon section thickness, followed by a rapid air cool or water quench. Bar stock and plate (1/4 in. and heavier) are usually solution heat treated at 2150°F followed by water quench.

MULTIMET® alloy suffered from mediocre oxidation resistance, a tendency for heat affected zone cracking during welding, and a relatively wide scatter band of mechanical properties.  HAYNES® 556® alloy was developed to address these concerns and as an improvement.

✔ Superior Corrosion Resistance – Resists pitting, crevice corrosion, and oxidation.
✔ High-Temperature Stability – Maintains strength in extreme heat (up to 1200°C).
✔ Excellent Weldability & Fabrication – Easy to machine and form.
✔ Durable & Long-Lasting – Ideal for harsh industrial applications.

• Chemical & Petrochemical Equipment

• Heat Exchangers & Furnace Parts

• Marine & Offshore Components

• Aerospace & Gas Turbine Parts

We supply Multimet in sheets, plates, bars, pipes, and fittings with custom sizes available. As trusted ferrous metal suppliers, we ensure high-quality material compliance with ASTM, ASME, and other international standards.

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HAYNES® Waspaloy alloy (UNS N07001) is an age-hardenable, nickel-based superalloy with very good strength at temperatures up to about 1800°F (980°C). It is widely used as a wrought material for forged and fabricated gas turbine and aerospace components. Its strength is generally comparable to HAYNES® R-41 alloy, and is superior to that of alloy 718 at temperatures above 1200-1300°F (650-705°C). Waspaloy alloy can be cold-formed in the annealed condition, and may also be hot-formed at temperatures of 1900°F (1040°C) or above. Weldability is somewhat limited by susceptibility to strain age cracking under conditions of heavy restraint. The alloy exhibits good resistance to gas turbine combustion environments at temperatures up to about 1600°F (870°C).  Waspaloy alloy is now being replaced in many applications by HAYNES® 282® alloy, due to the superior fabricability and creep-strength of 282® alloy.

Haynes Waspaloy – High-Performance Nickel-Based Superalloy for Demanding Applications

As leading stockists and suppliers of high-grade ferrous and non-ferrous metals, we proudly offer Haynes Waspaloy, a premium nickel-chromium-cobalt superalloy renowned for its exceptional high-temperature strength, oxidation resistance, and creep resistance.

✔ Excellent Heat Resistance – Performs reliably at temperatures up to 1600°F (870°C), making it ideal for aerospace, gas turbines, and industrial gas turbine components.
✔ Superior Corrosion & Oxidation Resistance – Withstands harsh environments, including chemical processing and power generation applications.
✔ High Strength & Durability – Maintains structural integrity under extreme stress, perfect for turbine blades, shafts, discs, and fasteners.
✔ Age-Hardenable Alloy – Can be heat-treated for enhanced mechanical properties.

• Aerospace & Aviation (jet engines, afterburners)

• Oil & Gas (downhole tools, valves)

• Power Generation (turbine components)

• Automotive & Defense (high-stress applications)

As trusted metal suppliers, we provide Haynes Waspaloy in various forms, including bars, sheets, plates, and forgings, customized to meet your project requirements.

Contact us today for competitive pricing, bulk availability, and global shipping!

• Haynes Waspaloy supplier

• Nickel-based superalloy stockist

• High-temperature resistant alloy

• Aerospace-grade Waspaloy

• Corrosion-resistant nickel alloy

• Waspaloy bars, sheets, and plates

• Gas turbine alloy supplier

• Heat-treated superalloy

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Nimonic C-263 (UNS N07263) - Nickel-Chromium-Cobalt Alloy - High-Temperature Superalloy

Keywords: Nimonic C-263, Nimonic C263, Nickel-Chromium-Cobalt Alloy, High-Temperature Alloy, Corrosion-Resistant Alloy, Aerospace Alloy, UNS N07263, Superalloy, Heat-Resistant Alloy, Gas Turbine Alloy, Ferrous Metals Supplier, Nimonic C-263 Stockist, Nimonic C-263 Supplier, High-Strength Alloy, Jet Engine Components, Industrial Alloy, Nickel Alloy.

Overview:
Nimonic C-263 is a high-performance nickel-chromium-cobalt superalloy renowned for its exceptional high-temperature strength, oxidation resistance, and creep resistance. It is widely used in aerospace, gas turbines, and industrial applications where extreme temperatures and stress are prevalent.

Key Properties:

• High-Temperature Performance: Retains strength and stability at temperatures up to 1500°F (815°C).

• Oxidation and Corrosion Resistance: Excellent resistance to oxidation and corrosion in harsh environments.

• High Strength: Superior mechanical properties, even under high-stress conditions.

• Weldability: Can be readily welded using conventional methods.

Chemical Composition:

• Nickel (Ni): 50-55%

• Chromium (Cr): 19-21%

• Cobalt (Co): 19-21%

• Molybdenum (Mo): 5.6-6.1%

• Titanium (Ti): 1.9-2.4%

• Aluminum (Al): 0.3-0.6%

• Iron (Fe): ≤0.7%

• Manganese (Mn): ≤0.6%

• Silicon (Si): ≤0.4%

• Carbon (C): ≤0.06%

• Boron (B): ≤0.005%

• Copper (Cu): ≤0.2%

Applications:

• Aerospace Components: Jet engine combustion chambers, turbine blades, and afterburners.

• Gas Turbines: Combustors, casings, and high-temperature fasteners.

• Industrial Gas Turbines: High-stress components in power generation.

• Chemical Processing: Equipment for high-temperature and corrosive environments.

• Automotive: Turbocharger components and exhaust systems.

Available Forms:

• Rods

• Bar

• Sheet

• Plate

• Wire

• Forgings

• Billet

• Tube/Pipe

Standards and Certifications:

• AMS 5872: Standard for Nimonic C-263 Sheet, Strip, and Plate.

• AMS 5873: Standard for Nimonic C-263 Bars and Forgings.

• ASTM B637: Standard Specification for Precipitation-Hardening Nickel Alloys.

Why Choose Us?
As trusted stockists and suppliers of ferrous metals, we provide high-quality Nimonic C-263 in various forms to meet your specific requirements. Our inventory is sourced from reputable manufacturers, ensuring compliance with international standards. Whether you need Nimonic C-263 for aerospace, industrial, or power generation applications, we offer competitive pricing and reliable delivery.

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HAYNES® HR-120® alloy (UNS N08120) alloy is a solid-solution-strengthened heat-resistant alloy that provides excellent strength at elevated temperature combined with very good resistance to carburizing and sulfidizing environments. Its oxidation resistance is comparable to other widely used Fe-Ni-Cr materials, such as alloys 330 and 800H, but its strength at temperatures up to 2000ºF (1095ºC) is significantly higher, even in comparison to Ni-Cr alloys. The alloy can be readily formed hot or cold, and is commonly welded using HAYNES® 556® filler wire.

Applications include those which require high strength combined with good resistance to carburizing and sulfidizing environments such as the following:

• Bar Frame Heat Treating Baskets                                        • Radiant Tubes

• Wire Mesh Furnace Belts and Basket Liners                       • Cast Link Belt Pins

• Muffles, Retorts                                                                    • Recuperators

• Heat Treating Fixtures                                                          • Fluidized Bed Components

• Waste Incinerators

Haynes HR-120 (UNS N08120) is a high-temperature, corrosion-resistant alloy designed for extreme environments. This nickel-iron-chromium superalloy offers exceptional oxidation resistance, carburization resistance, and thermal stability, making it ideal for industrial furnaces, heat treatment equipment, petrochemical processing, and power generation applications.

• Excellent high-temperature strength (up to 2200°F/1200°C)

• Superior resistance to oxidation, sulfidation, and carburization

• Outstanding creep resistance under prolonged stress

• Good fabricability and weldability (compatible with standard techniques)

• Resists acidic and corrosive media, including sulfur-rich environments

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MP35N (UNS R30035) - Nickel-Cobalt-Chromium-Molybdenum Alloy Rods - High-Strength, Corrosion-Resistant Alloy

Keywords: MP35N, MP35N Rods, Nickel-Cobalt-Chromium-Molybdenum Alloy, High-Strength Alloy, Corrosion-Resistant Alloy, Aerospace Alloy, Superalloy, Medical Alloy, Ferrous Metals Supplier, MP35N Stockist, MP35N Supplier, High-Performance Alloy, Non-Magnetic Alloy, Industrial Alloy, Cobalt Alloy.

Overview:
MP35N is a high-performance nickel-cobalt-chromium-molybdenum alloy known for its exceptional high strength, corrosion resistance, and fatigue resistance. It is widely used in medical devices, aerospace, oil and gas, and industrial applications where durability, reliability, and resistance to harsh environments are critical.

Key Properties:

• High Strength: Superior mechanical properties, even under high-stress conditions.

• Corrosion Resistance: Excellent resistance to oxidation, pitting, and crevice corrosion.

• Fatigue Resistance: Exceptional resistance to fatigue, making it ideal for high-stress applications.

• Non-Magnetic: Retains non-magnetic properties in all conditions.

• Biocompatibility: Suitable for medical and dental applications.

Chemical Composition:

• Nickel (Ni): 33-37%

• Cobalt (Co): 33-37%

• Chromium (Cr): 19-21%

• Molybdenum (Mo): 9-10.5%

• Iron (Fe): ≤1%

• Manganese (Mn): ≤0.15%

• Silicon (Si): ≤0.15%

• Carbon (C): ≤0.025%

• Titanium (Ti): ≤1%

Applications:

• Medical Devices: Surgical instruments, orthopedic implants, and pacemaker leads.

• Aerospace Components: Fasteners, springs, and high-stress components.

• Oil & Gas Industry: Downhole tools, valves, and wellhead components.

• Industrial Applications: High-performance springs, fasteners, and machinery parts.

• Marine Applications: Components exposed to seawater and harsh conditions.

Available Forms:

• Rods

• Bar

• Wire

• Sheet

• Plate

• Forgings

Standards and Certifications:

• ASTM F562: Standard Specification for Wrought 35Cobalt-35Nickel-20Chromium-10Molybdenum Alloy for Surgical Implant Applications.

• AMS 5844: Standard for MP35N Bars, Forgings, and Rings.

• ISO 5832-6: Implants for Surgery - Metallic Materials - Part 6: Wrought Cobalt-Nickel-Chromium-Molybdenum Alloy.

Why Choose Us?
As trusted stockists and suppliers of ferrous metals, we provide high-quality MP35N rods in various diameters and lengths to meet your specific requirements. Our inventory is sourced from reputable manufacturers, ensuring compliance with international standards. Whether you need MP35N for medical, aerospace, oil and gas, or industrial applications, we offer competitive pricing and reliable delivery.

Additional Information:

• Production Capacity: 1000
• Delivery Time: 10-15 Days
• Packaging Details: IN WOODEN BOX

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