AMS ASME ASTM for inconel625 alloy navigators,
625 Alloy,Inconel 625 Bars ,Inconel 625 Rods,Inconel 625 sheet ,Inconel 625 plate,Inconel 625 strip,Inconel 625 coil,
Inconel Alloy 625 is a non-magnetic, corrosion and oxidation resistant, nickel-chromium alloy. The high strength of Inconel 625 is the result of the stiffening combination of molybdenum and niobium on the nickel chromium base of the alloy. Inconel 625 has tremendous resistance to a wide range of unusually severe corrosive environments including high-temperature effects such as oxidation and carburization. Its outstanding strength and toughness in temperature ranges from cryogenic temperatures to high temperature up to 2000° F (1093° C) are derived primarily from the solid solution effects of the refractory metals Columbium and molybdenum in a nickel-chromium matrix.
Inconel 625 Chemical Composition
% |
Ni |
Cr |
Fe |
Mo |
Nb+Ta |
Co |
C |
Mn |
Si |
S |
Al |
Ti |
P |
Min. |
58.0 |
20.0 |
- |
8.0 |
3.15 |
- | - | - | - | - |
- |
- | - |
Max. |
- |
23.0 |
5.0 |
10.0 |
4.15 |
1.0 |
0.1 |
0.5 |
0.5 |
0.015 |
0.4 |
0.4 |
0.015 |
Inconel 625 Physical Properties
Density | 8.4 g/cm³ |
Melting point |
1290-1350 ℃
|
Inconel 625 Typical Mechanical Properties
Status |
Tensile strength Rm N/mm² |
Yield strength Rp 0. 2N/mm² |
Elongation As % |
Brinell hardness HB |
Solution treatment | 827 | 414 | 30 | ≤220 |
AMS 5599, AMS 5666, AMS 5837, ASME SB 443 Gr 1, ASME SB 446 Gr 1, ASTM B 443 Gr 1, ASTM B 446 Gr 1, EN 2.4856, ISO 15156-3, NACE MR0175-3,
UNS N06625, Werkstoff 2.4856
Wire | Sheet | Strip | Rod | Pipe | |
AMS 5599, AMS 5666,AMS 5837, AMS 5979,ASTM B443 | ASTM B443 | AMS 5599, AMS 5979,ASTM B443 | ASTM B 446 SAE/AMS 5666,
VdTÜV 499 |
Seamless Pipe | Welded Pipe |
ASTM B 444/B 829 & ASME SB 444/SB 829SAE/AMS 5581 | ASTM B704/B751 ASME SB704/SB 751ASTM B705/B 775 , ASME SB 705/SB 775 |
Round bars/Flat bars/Hex bars, Size From 8.0mm-320mm, Used for bolts,fastners and other spare parts
Supply in welding wire and spring wire in coil form and cut length.
Widths up to 1500mm and lengths up to 6000mm,Thickness from 0.1mm to 100mm.
Standards size and customized dimension can be produced by us with small tolerance
Soft condition and hard condition with AB bright surface, width up to 1000mm
Alloy 625 we can offer bolts,Nuts and other fasteners as clients requirements
1.High creep-rupture strength
2.Oxidation resistant to 1800°F
3.Good fatigue resistance
4.Excellent weldability
5.Outstanding resistance to chloride pitting and crevice corrosion
6.Immune to chloride ion stress corrosion cracking
7.Resistant to seawater under both flowing and stagnant conditions and under fouling
• Aircraft ducting systems
• Jet engine exhaust systems
• Engine thrust-reverser systems
• Bellows and expansion joints
• Turbine shroud rings
• Flare stacks
• Seawater components
• Chemical process equipment handling mixed acids both oxidizing and reducing.
Inconel / Hastelloy/ Monel/ Haynes 25/ Titanium
Nickel/ Titanium Alloy tubes, U-bend /heat exchange tube
Inconel 601/ Hastelloy C22/Inconel x750/Inconel 625 ect
Hastelloy/Inconel/ Incoloy/ Cobalt/Tianium
Hastelloy/Inconel/ invar/ soft magnetic Alloys ect
Inconel 718/Inconel x750/ Nimonic 80A
Cobalt Alloy wire, Nickel alloy wire,Tianium Alloy wire
Monel 400/ Hastelloy C276/ Inconel 718/ Titanium
Inconel x750/ Inconel 718 /Monel 400 ect
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What material is 625 alloy made of? A nickel – based alloy with high Ni – Cr – Mo.
Chemical composition of Alloy 625: Chromium (Cr)20.0-23.0, Iron (Fe)< 5.0, (Al) & lt; 0.4, Silicon (Si)< 0.50 manganese (Mn)< 0.50, Nickel (Ni)258, sulfur (S)< 0.015, Cobalt (Co)< 1.0,(Mo)8.0-10.0, Titanium (Ti)< 0.4, Phosphorus (P)< 0.015,(Nb) 3.15-4.15, Carbon (C)< 0.01.
625 Alloy features excellent oxidation and corrosion resistance, excellent strength and toughness, excellent fatigue resistance, high formability, and excellent weldability. It can maintain its strength and toughness anywhere from low temperatures to 2000°F. Due to the rapid hardening of alloy 625, a large amount of cold forming may require annealing throughout the cold forming process. The alloy is commonly used in jet engines and other aerospace applications.