Nimonic 263 Forged/Forging Round Bars (UNS N07263, 2.4650, Alloy 263)

• Customization: Available
• Processing Object: Metal
• Molding Style: Forging
• Model NO.: jj521
• Application: Machinery Parts
• Material: SS
• Heat Treatment: Quenching
• Surface Treatment: Polishing
• Forging Tolerance: +/-0.5mm
• Standard: AISI
• Material of Forged Bars: Nimonic 263
• Transport Package: Wooden or Steel Frame Crate Packing
• Specification: CE
• Trademark: LY
• Origin: Jiangyin
• HS Code: 722840000
• Production Capacity: 5000 Tons/Year

Product Description

We are one leading producer of Nimonic 263 forged round bars, Nimonic 263 forging round bars, Nimonic263 forged/forging round bars, UNS N07263 forging/forged round bars, Alloy 263 forged/forging round bars, 2.4650 forging/forged round bars factory from china
We could produce Nimonic 263, UNS N07263, 2.4650 forging/forged round bars with diameters ranging from 10MM to 6000MM and with weights from 10KGS to 15000KGS
The melting method of Nimonic 263, UNS N07263, 2.4650 material is ESR+VIR or VIM+ESR+VAR
Our Nimonic 263, UNS N07263, 2.4650 forged/forging round bars are widely used in in chemical plants and heavy vessels, pump and valve producers, and industrial blades. Separators and centrifuges, Cement industry and sugar industry, drilling platform, drilling rig, pipelines and refineries, power generation and power plants, , generators, compressors, gear boxes. Oil & gas industry, concrete mills and mixers, processing units, crystalizer equipment and so on
Our Nimonic 263, UNS N07263, 2.4650 forged/forging round bars could be 100% Ultrasonic Inspection as per the forging parts UT Test standard of ASTM A 388 or EN10228.
We could supply Nimonic 263, UNS N07263, 2.4650 forged/forging round bars material certificate as per the standard of EN10204-3.1 or EN10204-3.2 of third party
Any inquiry of Nimonic 263, UNS N07263, 2.4650 forged/forging round bars, please feel free to contact us. We are glad to quote the best price for every clients

 

NIMONIC® alloy 263 (UNS N07263/W. Nr. 2.4650), an air melted nickel-base alloy, was developed by Rolls-Royce (1971) Ltd. to provide a sheet material which could be readily fabricated and would offer improved ductility in welded assemblies to replace NIMONIC alloy 80A. It was designed as sheet material to meet specific design criteria in terms of proof stress and creep strength. It is now available in all standard forms.The welding techniques for this alloy are similar to those in common use for other age-hardenable nickelbase alloys. During salvage welding operations, a preweld heat-treatment is not necessary on age-hardened
assemblies but a subsequent age-hardening treatment is desirable after all salvage welding is completed.Material will age in service if temperatures are above 750°C.

 

 

Composition, %

Carbon ........................................................................0.04-0.08
Silicon .........................................................................0.40 max.
Manganese .................................................................0.60 max.
Sulfur ........................................................................0.007 max.
Silver .......................................................................0.0005 max.
Aluminum....................................................................0.60 max.
Boron ........................................................................0.005 max.
Bismuth...................................................................0.0001 max.
Cobalt..........................................................................19.0-21.0
Chromium....................................................................19.0-21.0
Copper........................................................................0.20 max.
Iron................................................................................0.7 max.
Molybdenum ...................................................................5.6-6.1
Lead........................................................................0.0020 max.
Titanium...........................................................................1.9-2.4
Aluminum and titanium ...................................................2.4- 2.8

Nickel............................................................................Balance*

 

 

 

 Physical Properties

Density, g/cm3..............................................................................8.36
lb/in3.............................................................................0.302
Melting Range
Liquidus temperature, °C........................................................1355
Solidus temperature, °C..........................................................1300
Specific Heat, J/kg, °C.................................................................461