Nickel Cobalt Alloy

GH4169 Nickel Alloy Hot Forged Round Bar for High Temperature Application A-ONE ALLOY supplies GH4169 in various of forms. We have plenty of hot forged round bar, size range diameter 20~300mm and we could make customized sizes within 3 weeks and make fast delivery. GH4169 has high strength, good toughness and has good corrosion resistance in high and low temperature environment. The supply state can be solid solution treatment or precipitation hardening state. Long term

René 41 Nickel-based Alloy Used in Jet Engine and Missile Components René 41 is an age hardening nickel base superalloy with exceptional strength from room temperature through about 1600°F. The alloy is sensitive to strain age cracking during welding. Sound welds can be made by the resistance and electron beam methods. GTAW using DC straight polarity requires good joint fit-up and cooling by means of copper backup bars or water-cooled fixtures. René 41 should be in the fully

Excellent High-Temperature Strength, Low Thermal Expansion Characteristics, and Good Oxidation Resistance HAYNES 242 is an age-hardenable nickel-molybdenum chromium alloy which derives its strength from a long-range ordering reaction upon aging. It has tensile and creep strength properties up to 1300°F (705°C) which are as much as double those for solid solution strengthened alloys, but with high ductility in the aged condition. The thermal expansion characteristics of 242®

GH4169 Nickel Alloy for High Temperature Application ranges -253°C~650°C GH4169 has high strength, good toughness and has good corrosion resistance in high and low temperature environment. The supply state can be solid solution treatment or precipitation hardening state. Long term working temperature range: -253°C~650°C. Short time working temperature up to 800°C. Chemical composition Element C Cr Ni Co Mo Al Ti Fe Weight(%) 0.08 max 17.00~21.00 50.00~55.00 1.00 max 2.80~3.30

GH4090 Nickel-chromium-Cobalt Alloy for High Temperature Application GH4090 is a nickel base precipitation hardening superalloy. The alloy is commonly used to make turbine blades, disk parts, forgings, ring parts, and thermal molds. Chemical composition Element C Cr Ni Co Al Ti Fe Zr B Si Mn S P Cu Weight(% 0.13 max 18.00~21.00 Rem 15.00~21.00 1.00~2.00 2.00~3.00 1.50 max 0.15 max 0.02 max 0.80 max 0.40 max 0.015 max 0.020 max 0.20 max Application The alloy has been used to

GH4080A Nickel Based Alloy for High Temperature Application below 800°C GH4080A is a type of Ni-Cr base precipitation hardening superalloy. It is used in temperature less than 800 ° C. The alloy in the range of 650 ° C to 850 ° C good creep resistance and oxidation resistance. The cold and hot properties of the alloy are good. The main product forms of GH4080A include hot rolled and forged bar, cold drawn bar, hot rolled plate, cold rolled plate, strip, wire and ring, etc.

REFRACTALOY 26 R26 Corrosion Resistant High Temperature Resistant Nickel Alloy REFRACTALOY 26 is a high heat resistant alloy of nickel, chromium, cobalt and iron, possessing high creep and endurance strengths along with high ductility at elevated temperatures. It responds to precipitation-hardening heat treatment. R26 has been used to produce steam turbine with fasteners on the ground, under the condition of 540 ℃ ~ 570 ℃ steam can work more than 100000 hours, use in good

Inconel X-750 Nickel Alloy Precipitation-hardened Superalloy up to 800°C Application Inconel X-750 is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures up to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. GH4145 also has excellent properties down to cryogenic termperatures.

GH3536 Nickel Based Solid Solution Reinforced Superalloy Hastelloy X GH3536 is a Nickel Based Solid Solution Reinforced Superalloy. It is equal to Hastelloy X alloy. It has good resistance to oxidation and corrosion resistance, under 900 ℃ have moderate to lasting and creep strength, cold and hot working good formability and weldability. Applicable to the manufacture of aircraft engine combustion chamber components and other high temperature parts, use for a long time under

GH4738 is a Ni-Cr-Co based precipitation hardened superalloy. GH4738 has higher yield strength and fatigue resistance during 760°C~870°C.It has good oxidation resistance and corrosion resistance in a gas turbine atmosphere at 870 degree C.It has good ductility and stable properties. It is suitable for making turbine disk, working blade, high temperature fastener, flame tube, shaft and turbine brake. Chemical composition Element C Cr Ni Co Mo Al Ti Fe Weight(%) 0.03~0.10 18.0

TRIBALOY T-800 Cobalt Alloy High Temperature Wear Abrasion resistance TRIBALOY T-800 was designed to resist high temperature wear and abrasion. It has exceptional oxidation and corrosion resistance due to its high Cr content. T-800 is harder and has better abrasive wear resistance than Tribaloy T-400. NOTE: Wear resistance of Tribaloy alloys is highly dependent on the volume percentage of Laves phase. Therefore, test results vary significantly with dilution and cooling rate

TRIBALOY T-400 Cobalt-based Alloy with Excellent Mechanical Wear Resistance TRIBALOY T-400 combines excellent mechanical wear resistance with good corrosion resistance. T-400 contains hard intermetallic phases of Mo and Si which impart excellent surface properties over a wide temperature range. Often used in similar applications to Stellite 12 or Stellite 1. T-400 exhibits outstanding resistance to galling and corrosion. CORROSION RESISTANCE T-400 shows excellent corrosion

Alloy 59 with Excellent Corrosion Resistance and High Mechanical Strength Alloy 59 is a nickel-chromium-molybdenum alloy with an extra-low carbon and silicon content. A-one Alloy is ready to supply high quality Alloy 59 products to customers from worldwide. Chemical composition (%): Cr=22.00~24.00, Fe≤1.50, C≤0.010, Mn≤0.50, Si≤0.10, Mo=15.0~16.5, Co≤0.30, Al=0.1~0.4, P≤0.015, S≤0.005 –per ASTM standard Standards: ASTM B622 seamless pipe ASTM B619/626 welded pipe ASTM B575

Alloy 31 Nicrofer 3127hMo FeNiCrMo Alloy with Addition of Nitrogen Alloy 31 is an iron-nickel-chromium-molybdenum alloy with the addition of nitrogen. The alloy closes the gap between high alloyed austenitic special stainless steels and nickel alloys. Alloy 31 has proven itself to be suitable particularly in the chemical and petrochemical industries, in ore digestion plants, in environmental and marine engineering as well as in oil and gas extraction. Chemical composition

W.Nr 2.4654 age hardenable nickel alloy very good strength up to 980°C W.Nr 2.4654 is an age hardening austenitic (face-centred cubic) nickel-based superalloy. W.Nr 2.4654 is typically used in high temperature applications, particularly in gas turbines. Formerly Grade 685 W.Nr 2.4654 is an age-hardenable, nickel-based superalloy with excellent strength properties through temperatures of roughly 980°C (1800°F). Other characteristics of Waspaloy include good corrosion

ASTM B637 N07001 Alloy with Very High Strength at Elevated Temperatures WASPALOY is an age hardening austenitic (face-centred cubic) nickel-based superalloy. Waspaloy alloy is typically used in high temperature applications, particularly in gas turbines. Waspaloy is an age-hardenable, nickel-based superalloy with excellent strength properties through temperatures of roughly 980°C (1800°F). Other characteristics of Waspaloy include good corrosion resistance, as well as being

UNS R30035 AMS5844 ASTM F562 Nickel Cobalt Alloy Surgical Implant Applications R30035 is a 35cobalt-35nickel-20chromium-10molybdenum alloy. A-ONE ALLOY supplies R30035 in the form of bar and wire. It is used for the manufacture of surgical implants. It has a unique combination of properties – ultra high strength, toughness, ductility, biocompatibility, and outstanding corrosion resistance. This alloy depends on combinations of work strengthening and aging to attain a variety

W.Nr. 2.4778 with Excellent Thermal Shock Resistance and Wear Resistance XUNSHI supplies W.Nr. 2.4778 in forms of forgings, round bar, tube and so on. UMCo50 is a heat-resistant cobalt alloy with excellent thermal shock resistance and wear resistance performance. It has great strength against sulfur-and vanadium-attacks. UmCo-50 has higher melting point compared to other cobalt based or nickel based heat-resistant alloys. For example, the alloy used for skid rails at a steel

Haynes 188 Nickel Cobalt Alloy with Excellent High-Temperature Strength HAYNES 188 is a cobalt-nickel-chromium-tungsten alloy that combines excellent high temperature strength with very good resistance to oxidizing environments up to 1095°C for prolonged exposures, and excellent resistance to sulfate deposit hot corrosion. It is readily fabricated and formed by conventional techniques, and has been used for cast component. Other attractive features include excellent

New Arrival: Super-thin R30003/R30008 Cold Rolled Foil for sensor and damper, minimum thickness 0.01mm R30003/R30008 is is an austenitic alloy strengthened by cold work and capable of additional hardening by aging at a moderate temperature (around 500°C). In the fully hardened condition, its elastic modulus is around 210 000 MPa, with UTS levels up to 2500 MPa on cold rolled strip. In addition to its very high yield strength, PHYNOX offers a range of physical, chemical and