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Nickel alloy is formed by combining nickel with other metals, commonly titanium, copper, aluminum, iron, and chromium. Approximately 3,000 nickel-based alloys are in use, forming products for numerous industries. Roughly 90% of all new nickel sold every year is used to create alloys. The Nickel Alloy Pipe is made up of a chemical composition of nickel, manganese, carbon, silicon, sulfur, ferrous, and copper.
Nickel alloy pipes and tubes come in a range of specifications, with varying thickness and dimensions. We also carry nickel alloy bar in a variety of shapes including square, flat, and round.
Nickel : Nickel 200,201
Ni-cu alloy : alloy 400
Ni-Cr-Fe alloy: alloy 600, 690, 020,028
Ni-Cr-Mo alloy: alloy 625, C-4, C-22, C-2000, G-30, G-35
Ni-Fe-Cr alloy: alloy 800, 800H, 800HT, 825
Ni-Mo alloy: alloy B-2, B-3
Ni-Mo-Cr alloy: alloy C-276
Website results may not reflect all products and sizes, like plate, coil, sheet. Contact a sales rep for the more information.
N04400
Alloy 400 (UNS N04400) is a nickel-copper alloy with high strength (comparable to structural steel) and toughness. Alloy 400 also has excellent corrosion resistance in a range of media including seawater, hydrofluoric acid, sulphuric acid and alkalis.
Chemical Composition
|
Weight % |
C |
S |
Ni+Co |
Fe |
Mn |
Si |
Cu |
|
Nickel 400 |
0.30 max |
0.024 max |
63.0 max |
2.50 max |
2.0 max |
0.50 max |
28-34 |
Mechanical Properties
|
Material |
Form and Condition |
Tensile Strength MPa |
Yield Strength (0.2% Offset) MPa |
Elongation (%) |
Hardness Rockwell B |
|
Alloy 400 |
Annealed Rod and Bar |
517-620 |
172-345 |
60-35 |
60-80 |
|
Alloy 400 |
Hot Rolled Plate Annealed |
482-586 |
193-345 |
50-35 |
60-76 |
|
Alloy 400 |
Sheet Annealed |
482-586 |
207-310 |
45-35 |
65-80 |
|
Alloy 400 |
Tube Cold drawn Annealed Seamless |
482-586 |
172-310 |
50-35 |
75 max |
N06600
Nickel Alloy 600 (N06600) is a nickel-chromium-iron alloy with good oxidation resistance at high temperatures and resistance to chloride-ion stress corrosion cracking corrosion by high-purity water, and caustic corrosion.
Chemical Composition
|
Weight% |
C |
S |
Cr |
Cu |
Mn |
Si |
Ni |
Fe |
|
Nickel Alloy 600 |
0.15 max |
0.015 max |
14.0 - 17.0 |
0.50 max |
1.0 max |
0.50 max |
72.0 min |
6 - 10 |
Mechanical Properties
|
Temper |
Annealed |
|
|
Tensile Rm |
110 |
ksi (min) |
|
Tensile Rm |
738 |
MPa (min) |
|
R.p. 0.2% Yield |
37 |
ksi (min) |
|
R.p. 0.2% Yield |
255 |
MPa (min) |
|
Elongation (2” or 4D gl) |
45 |
% (min) |
N06625
Nickel alloy 625 is nickel-chromium-molybdenum-columbium alloy material, major content Nickel miniumum 58%, also called Inconel 625 or UNS NO6625 under standard ASTM B444 for pipes, or ASTM B443 for plates coils. Other chemical content Chromimum 20% to 23%, Columbium + tantalum 3.15% to 4.15%, Molybdenum 8.0% to 10.0%, columbium Cobalt allow 1.0% max if determined, Iron 5.0% max.
Chemical Composition
|
Weight % |
Ni |
Cr |
Mo |
Nb + Ta |
Fe |
Ti |
C |
Mn |
Si |
S |
P |
Al |
Co |
|
Alloy 625 |
58.0 min |
20 - 23 |
8 -10 |
3.15 -4.15 |
5.0 max |
0.40 max |
0.10 max |
0.50 max |
0.50 max |
0.15 max |
0.15 max |
0.40 max |
1.0 max |
Mechanical Properties
|
Temper |
Annealed |
|
|
Tensile Rm |
110 |
ksi (min) |
|
Tensile Rm |
738 |
MPa (min) |
|
R.p. 0.2% Yield |
37 |
ksi (min) |
|
R.p. 0.2% Yield |
255 |
MPa (min) |
|
Elongation (2” or 4D gl) |
45 |
% (min) |
N08800 / N08810 / N08811
Alloy 800 - The 800 series of alloy (Incoloy 800, 800H and 800HT) are nickel-iron-chromium super-alloys that have excellent properties of high temperature strength and resistance to oxidation, carburization and other types of high temperature corrosion. Alloy 800, 800H and 800HT are used in various applications from furnace components, petrochemical furnace cracker tubes to sheathing for electrical heating elements.
Chemical Composition
|
Weight % |
Ni |
Cr |
Fe |
C |
Al |
Ti |
Al+Ti |
|
Alloy 800 |
30-35 |
19-23 |
39.5 min |
0.10 max |
0.15-0.60 |
0.15-0.60 |
0.30-1.20 |
|
Alloy 800H |
30-35 |
19-23 |
39.5 |
0.05-0.10 |
0.15-0.60 |
0.15-0.60 |
0.30-1.20 |
|
Alloy 800HT |
30-35 |
19-23 |
39.5 |
0.06-0.10 |
0.25-0.60 |
0.25-0.60 |
0.85-1.20 |
|
ASTM Grain Size - Alloy 800 is not specified, Alloy 800H is 5 or coarser, Alloy 800HT is 5 or coarser. |
|||||||
Mechanical Properties
|
Temper |
800 |
800H/HT |
||
|
Tensile Rm |
77.8 |
ksi (min) |
65 |
ksi (min) |
|
Tensile Rm |
536 |
MPa (min) |
448 |
MPa (min) |
|
R.p. 0.2% Yield |
22 |
ksi (min) |
25 |
ksi (min) |
|
R.p. 0.2% Yield |
150 |
MPa (min) |
172 |
MPa (min) |
|
Elongation (2” or 4D gl) |
20 |
% (min) |
20 |
% (min) |
N08825
Alloy 825 is a nickel-iron-chromium alloy with additions of molybdenum and copper. It has excellent resistance to both reducing and oxidizing acids, to stress-corrosion cracking, and tolocalizedattack such as pitting and crevice corrosion. Alloy 825 is especially resistant to sulphuric and phosphoric acid. Alloy 825 is used for chemical processing, pollution control equipment, oil and gas well piping, nuclear fuel reprocessing, acid production and pickling equipment and handling of radioactive wastes.
Chemical Composition
|
Weight % |
Ni |
Fe |
Cr |
Mo |
Cu |
Ti |
C |
Mn |
S |
Si |
Al |
|
Alloy 825 |
38 - 46 |
22 min |
19.5 - 23.5 |
2.5 - 3.5 |
1.5 - 3 |
0.6 - 1.2 |
0.05 max |
1 max |
0.03 max |
0.5 max |
0.2 max |
Mechanical Properties
|
Temper |
Annealed |
|
|
Tensile Rm |
85 |
ksi (min) |
|
Tensile Rm |
590 |
MPa (min) |
|
R.p. 0.2% Yield |
35 |
ksi (min) |
|
R.p. 0.2% Yield |
240 |
MPa (min) |
|
Elongation (2” or 4D gl) |
30 |
% (min) |
N07718
Alloy 718 (UNS N07718, W Nr 2.4668) is an austenitic nickel-based superalloy. Alloy 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to 1300ºF and oxidation resistance to 1800ºF. Alloy 718 is used in applications that require high strength such as parts for jet engines and high speed airframe parts such as wheels, buckets, spacers and high temperature bolts and fasteners.
Chemical Composition
|
Weight % |
C |
Mn |
P |
S |
Si |
Cr |
Ni |
Mo |
Cb |
Ta |
Ti |
Al |
Co |
B |
Cu |
Fe |
|
Alloy 718
AMS 5662
|
0.08 |
0.35 |
0.015 |
0.015 |
0.35 |
17-21 |
50-55 |
2.8-3.30 |
4.75-5.50 |
0.05 |
0.65-1.15 |
0.20-0.80 |
1.00 |
0.006 |
0.30 |
Rem |
Mechanical Properties
|
Temper |
Solution-treated |
|
|
Tensile Rm |
155 |
ksi (Max) |
|
Tensile Rm |
1069 |
MPa (Max) |
|
R.p. 0.2% Yield |
95 |
ksi (Max) |
|
R.p. 0.2% Yield |
655 |
MPa (Max) |
|
Elongation (2” or 4D gl) |
30 |
% (min) |
