Factory Outlet Inconel 625 N06625 Ncf625 Nickel Chromium Molybdenum Alloy Plate Sheet

Product Details
Customization: Available
Application: Aviation, Electronics, Industrial, Medical, Chemical
Standard: JIS, GB, DIN, BS, ASTM, AISI
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  • Factory Outlet Inconel 625 N06625 Ncf625 Nickel Chromium Molybdenum Alloy Plate Sheet
  • Factory Outlet Inconel 625 N06625 Ncf625 Nickel Chromium Molybdenum Alloy Plate Sheet
  • Factory Outlet Inconel 625 N06625 Ncf625 Nickel Chromium Molybdenum Alloy Plate Sheet
  • Factory Outlet Inconel 625 N06625 Ncf625 Nickel Chromium Molybdenum Alloy Plate Sheet
  • Factory Outlet Inconel 625 N06625 Ncf625 Nickel Chromium Molybdenum Alloy Plate Sheet
  • Factory Outlet Inconel 625 N06625 Ncf625 Nickel Chromium Molybdenum Alloy Plate Sheet
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Basic Info.

Model NO.
INCONEL 625 (UNS N06625/W. NR. 2.4856/JIS NCF625)
Sample
Free
Trade Terms
EXW, Fob, CIF, CFR
Surface
Mirror, Brushed, Mill Finished, Polished etc.
Transport Package
Standard Export Package
Specification
As Customer′s Request
Trademark
Mingson
Origin
China
HS Code
7506200000
Production Capacity
7000 Tons Per Year

Product Description

1.Product Name: Nickel Alloy Plate/Sheet
2.Grade: INCONEL 625 (UNS N06625/W.NR. 2.4856/JIS NCF625)
3.Thickness: 0.6mm-70mm, Length: 12000mm, Wide:≤2500mm
4.Features: Alloy 625 has excellent strength at temperatures up to 816°C. At higher temperatures, its strength is generally lower than that of other solid solution strengthened alloys. Alloy 625 has good oxidation resistance at temperatures up to 980°C and shows good resistance to aqueous corrosion, but is relatively moderate compared to other more capable corrosion resistant alloys.
5.Applications: Chemical process industry and sea water application. Alloy 625 is used in short term applications at temperatures up to 816°C. For long term service, it is best restricted to a maximum of 593°C, because long term exposure above 593°C will result in significant embrittlement.
6.Physical Properties
Density Melting Range
g/cm3 °C
8.4 1290-1350
7.The Minimum Mechanical Properties At Normal Temperature
Alloy and State Tensile Strength Yield Strength Rate of Elongation Brinell Hardness
Rm N/mm2 RP0.2N/mm2 A5% HB
Solid Solution ≥690 ≥276 ≥30 ≤220
Annealing ≥827 ≥414 ≥30 -
8.Chemical Composition
% Ni Cr Mo Nb+Ta Fe Al Ti C Mn Si Co P S
MIN 58 20 8 3.15 - - - - - - - - -
MAX - 23 10 4.15 5 0.4 0.4 0.1 0.5 0.5 1 0.015 0.015

 
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