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Home> Products> High Temperature Alloy> Nimonic 263 High-performance nickel-based alloy plate
Nimonic 263 High-performance nickel-based alloy plate
Nimonic 263 High-performance nickel-based alloy plate
Nimonic 263 High-performance nickel-based alloy plate
Nimonic 263 High-performance nickel-based alloy plate
Nimonic 263 High-performance nickel-based alloy plate
Nimonic 263 High-performance nickel-based alloy plate

Nimonic 263 High-performance nickel-based alloy plate

Min. Order:1 Kilogram

Transportation:Ocean,Land,Air,Express

Port:SHANGHAI

Product Description
Product Attributes

Model No.UNS NO7263, W.Nr.2.4650, Haynes C263, Nimonic 263

Brandhdf

Place Of OriginChina

SpeciesNickel Plate

Whether PowderNot Powder

Supply Ability & Additional Information

PackagingStandard export packaging, wooden box packaging

TransportationOcean,Land,Air,Express

Place of OriginChina

Certificateiso9001

PortSHANGHAI

Packaging & Delivery
Selling Units:
Kilogram
Package Type:
Standard export packaging, wooden box packaging
nickel alloy coil
3c9f7de7e34c944b2643735acd42806b
alloy wire cold drawing
Nimonic 263 (UNS N07263/W. No. 2.4650) is a high-performance nickel-based superalloy, which holds a significant position in the aerospace and energy sectors due to its outstanding high-temperature properties and excellent processing characteristics. Its unique chemical composition and meticulous heat treatment process enable it to exhibit remarkable performance in extreme environments, making it an ideal choice for high-temperature and high-stress applications.
 
FEATURE
1. Heat resistance: Exhibits excellent stability at high temperatures and can operate for a long time at temperatures up to 750℃. Even at higher temperatures, it maintains good performance.
2. Corrosion resistance: Performs well in acidic and alkaline media, possessing excellent corrosion resistance and oxidation resistance.
3. Mechanical properties: Demonstrates outstanding strength and toughness, maintaining high mechanical performance even at high temperatures.
 
CHEMICAL COMPONENT
Element Ni Co Mo Ti Fe Mn Al Si Cu C Cr B S
% Bal 19-21 5.6-6.1 1.9-2.4 0.7 0.6 0.6 0.4 0.2 0.4-0.8 19-21 0.005 0.007
 
PHYSICAL & MECHANICAL
Density Melting Tensile strength Yield strength Elongation
8.36 g/cm³ 1340-1380°C 940 MPa 550 MPa 39%
 
APPLICATION
1. Aviation turbine engine components
2. Ground-based turbine components
3. Various manufacturing components requiring high-temperature strength and corrosion resistance
productfactorypackagingapplicationcertificatePartner
 
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