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1M 1.5M WIdth Monel 502 Nickel Based alloy Coil With high temperatures
Introduction
Super alloys have the capacity to function at very high temperatures and severe mechanical stress. They also have good creep and oxidation resistance. They can be formed in different shapes. They are subjected to solid-solution hardening, work hardening, and precipitation hardening for increasing their strength. There are three types of super alloys, namely cobalt-based, nickel-based, and iron-based alloys.
Monel 502 is a nickel-copper alloy. The following datasheet gives an overview of Monel 502.
| Material |
Monel/Inconel/Hastelloy/Duplex Steel/PH Steel/Nickel Alloy |
| Shape |
Round,Forging,Ring,Coil,Flange,Disc,Foil,Spherical,Ribbon,Square,Bar,Pipe,Sheet |
Grade |
Duplex: 2205(UNS S31803/S32205),2507(UNS S32750),UNS S32760(Zeron 100),2304,904L |
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Others:253Ma,254SMo,654SMo,F50(UNSS32100)F60,F61,F65,1J22,N4,N6 etc |
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Alloy : Alloy 20/28/31 |
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Hastelloy:HastelloyB/ -2/B-3/C22/C-4/S/ C276/C-2000/G-35/G-30/X/N/g |
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Hastelloy B / UNS N10001,Hastelloy B-2 / UNS N10665 / DIN W. Nr. 2.4617,Hastelloy C,
Hastelloy C-4 / UNS N06455 / DIN W. Nr. 2.4610,Hastelloy C-22 / UNS N06022 / DIN W. Nr. 2.4602,
Hastelloy C-276 / UNS N10276 / DIN W. Nr. 2.4819,Hastelloy X / UNS N06002 / DIN W. Nr. 2.4665 |
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Haynes: Haynes 230/556/188 |
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Inconel 600/601/602CA/617/625/713/718/738/X-750,Carpenter 20 |
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Inconel 718 / UNS N07718 / DIN W. Nr. 2.4668,Inconel 601 / UNS N06601 / DIN W. Nr. 2.4851,
Inconel 625 / UNS N06625 / DIN W. Nr. 2.4856,Inconel 725 / UNS N07725,Inconel X-750 / UNS N07750 / DIN W. Nr. 2.4669,Inconel 600 / UNS N06600 / DIN W. Nr. 2.4816 |
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Incoloy: Incoloy 800/800H/800HT/825/925/926; |
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GH: GH2132,GH3030,GH3039,GH3128,GH4180,GH3044 |
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Monel: Monel 400/K500/R405 |
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Nitronic: Nitronic 40/50/60; |
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Nimonic: Nimonic 75/80A/90/A263 ; |
Specification |
Wire: 0.01-10mm
Strip: 0.05*5.0-5.0*250mm
Bar: φ4-50mm;Length 2000-5000mm
Pipe: φ6-273mm;δ1-30mm;Length 1000-8000mm
Sheet: δ 0.8-36mm;Width 650-2000mm;Length 800-4500mm |
Product
Characteristics |
1.According to the preparation process can be divided into deformation superalloys,
casting superalloys and powder metallurgy superalloys.
2.According to the strengthening mode, there are solid solution strengthening type, precipitation
strengthening type, oxide dispersion strengthening type and fiber strengthening type, etc.. |
| Standard |
GB,AISI,ASTM,DIN,EN,SUS,UNS etc |
| Inspection |
ISO,SGS,BV and so on. |
Application |
High temperature components such as turbine blades, guide vanes, turbine disks,
high pressure compressor disks,machine manufacturing
and combustion chambers used in the manufacture of aviation, naval and industrial gas turbines |
Packaging |
1. cases packed in wooden cases
2. paper packaging
3. plastic packing
4. foam packaging
Packaging according to customer requirements or products |
| Delivery |
7-25days orAccording to the product |
Payment |
L/C,D/A,D/P,T/T,Western Union,MoneyGram,According to customer requirements payments
for offline orders. |
Specifications
The following specifications cover Super Alloy Monel 502
Property Results
Chemistry Data :
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Aluminum |
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2.5 - 3.5 |
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Carbon |
|
0.1 max |
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Copper |
|
Balance |
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Iron |
|
2 max |
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Manganese |
|
1.5 max |
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Nickel |
|
63 - 70 |
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Silicon |
|
0.5 max |
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Sulphur |
|
0.01 max |
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Titanium |
|
0.5 max |
| Principal Design Features |
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This nickel-copper alloy, similar to Monel K500, has better machinability. It may be precipitation hardened by heat treatment for good strength. |
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| Applications |
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The alloy is used for pump shafting, fasteners, and valve components as well as finding application for propeller shafts. |
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| Machinability |
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This alloy is similar to Monel K500, but with improved machinability. It machines much the same as the austenitic (300 Series) stainless steels. |
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| Forming |
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The alloy has good ductility and is readily formed by conventional methods. |
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| Welding |
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Weldability is good by conventional means. |
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| Heat Treatment |
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This alloy responds to a precipitation hardening heat treatment and to annealing. |
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| Forging |
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May be forged at temperatures of 2100 F to 1850 F. Water quench after forging. |
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| Hot Working |
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Hot work temperature range is 2100 F to 1600 F. Do not allow the product to slow cool in air, rather it should be cooled from 1450 F (or higher) by quenching. |
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| Cold Working |
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The alloy has good ductility and may be cold worked by conventional means. |
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| Annealing |
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Annealing is done at 1900 F and water quench. |
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| Aging |
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Aging is done at 1100 F to 1125 F for 16 hours, followed by slow furnace cooling at a rate of 25 F per hour to 900 F. Cooling rate from 900 F is not critical. |
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| Other Mechanical Props |
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Tensile data is for age hardened. |
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Physical Data :
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|
| Density (lb / cu. in.) |
0.305 |
| Specific Gravity |
8.39 |
| Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) |
0.1 |
| Electrical Resistivity (microhm-cm (at 68 Deg F)) |
370 |
| Melting Point (Deg F) |
2425 |
| Thermal Conductivity |
121 |
| Mean Coeff Thermal Expansion |
7.6 |
| Modulus of Elasticity Tension |
26 |
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