Customization: | Available |
---|---|
Type: | Steel Plate |
Standard: | ASTM, AISI, GB, JIS, DIN |
Still deciding? Get samples of US$ 10/Piece
Request Sample
|
Suppliers with verified business licenses
Audited by an independent third-party inspection agency
ASTM B575 alloy c-4 steel Plates
Hastelloy C4 is a versatile Ni-Cr-Mo alloy with extremely high resistance to corrosion.Hastelloy C4 also has excellent resistance to general and localized corrosion and stress corrosion.
Hastelloy C-4(UNS N06455)is very resistant to many aggressive chemicals,especially hydrochloric acid,sulfuric acid and chlorides.Hastelloy C4 is one of the best corrosion resistant alloys in nickel-chromium-molybdenum alloys. Like other nickel alloys,Hastelloy C4 is ductile,easy to weld and weld,and the stress in chloride bearing solutions has exceptional corrosion resistance.With its high chromium and molybdenum content,it can withstand both oxidizing and non-oxidizing acids and is resistant to pitting and crack attack in the presence of chlorides and other halides.
Standards: ASTM B575
Thickness: 0.5 MM TO 300 MM
Length: 2000 MM TO 6000 MM LENGTH
Width: 1000 MM TO 2500 MM
Specifications : ASTM B575
Form : Coils, Foils, Rolls, Plain Sheet, Shim Sheet, Perforated Sheet, Chequered Plate, Strip, Flats, Blank (Circle), Ring (Flange)
Finish : Hot rolled plate (HR), Cold rolled sheet (CR), 2B, 2D, BA NO(8), SATIN (Met with Plastic Coated)
EQUIVALENT GRADES:HASTELLOY C4 (ALLOY C4, 2.4610, UNS N06455)
TABLE 1 Chemical Requirements
|
|||||||||||
Element
|
Composition Limits,% | ||||||||||
Alloy | Alloy | Alloy | Alloy | Alloy | Alloy | Alloy | Alloy | Alloy | Alloy | Alloy | |
N06035 | N06044 | N10276 | N06022 | N06455(C4) | N06059 | N06058 | N06200 | N06210 | N10362 | N06686 | |
Molybdenum | 7.60-9.00 | 0.80-1.20 | 15.0-17.0 | 12.5-14.5 | 14.0-17.0 | 15.0-16.5 | 18.5-21.0 | 15.0-17.0 | 18.0-20.0 | 21.5-23.0 | 15.0-17.0 |
Chromium | 32.25-34.25 | 43.5-45.3 | 14.5-16.5 | 20.0-22.5 | 14.0-18.0 | 22.0-24.0 | 20.0-23.0 | 22.0-24.0 | 18.0-20.0 | 13.8-15.6 | 19.0-23.0 |
Iron | 2.00 max | 0.3 max | 4.0-7.0 | 2.0-6.0 | 3.0 max | 1.5, max | 1.5, max | 3.0 max | 1.0 max | 1.25 max | 5.0 max |
Tungsten | 0.60 max | ... | 3.0-4.5 | 2.5-3.5 | ... | ... | 0.3 max | ... | ... | ... | 3.0-4.4 |
Cobalt, max | 1 | ... | 2.5 | 2.5 | 2 | 0.3 | 0.3 | 2.0 max | 1 | ... | ... |
Carbon, max | 0.05 | 0.02 | 0.01 | 0.015 | 0.015 | 0.01 | 0.01 | 0.01 | 0.015 | 0.01 | 0.01 |
Silicon, max | 0.6 | 0.2 | 0.08 | 0.08 | 0.08 | 0.1 | 0.1 | 0.08 | 0.08 | 0.08 | 0.08 |
Manganese, max | 0.5 | 0.07-0.30 | 1 | 0.5 | 1 | 0.5 | 0.5 | 0.5 | 0.5 | 0.6 | 0.75 |
Vanadium, max | 0.2 | ... | 0.35 | 0.35 | ... | ... | ... | ... | 0.35 | ... | ... |
Phosphorus, max | 0.03 | 0.02 | 0.04 | 0.02 | 0.04 | 0.015 | 0.015 | 0.025 | 0.02 | 0.025 | 0.04 |
Sulfur, max | 0.015 | 0.02 | 0.03 | 0.02 | 0.03 | 0.01 | 0.01 | 0.01 | 0.02 | 0.01 | 0.02 |
Titanium | ... | 0.10-0.30 | ... | ... | 0.7 max | ... | ... | ... | ... | ... | 0.02-0.25 |
Nickel | remainderA | Bal | remainderA | remainderA | remainderA | Bal | Bal | remainderA | remainderA | remainderA | remainderA |
Aluminum | 0.40 max | 0.30 max | ... | ... | ... | 0.1-0.4 | 0.40 max | 0.50 max | ... | 0.50 max | ... |
Copper | 0.30 max | ... | ... | ... | ... | 0.50 max | 0.50 max | 1.3-1.9 | ... | ... | ... |
Tantalum | ... | ... | ... | ... | ... | ... | ... | ... | 1.5-2.2 | ... | ... |
Nitrogen | ... | ... | ... | ... | ... | ... | 0.02-0.15 | ||||
(A) Shall be determined arithmetically by difference.
|
|||||||||||
TABLE 2 Mechanical Property Requirements
|
|||||||||||
Alloy
|
Tensile Strength, min, psi (MPa) | Yield Strength (0.2% Offset), min, psi | Elongation in 2 in. | Rockwell Hardness,B | |||||||
(MPa) | (50.8 mm) or 4DA | max | |||||||||
min,% | |||||||||||
N10276 | 100 000 (690) | 41 000 (283) | 40 | 100 HRB | |||||||
N06022 | 100 000 (690) | 45 000 (310) | 45 | 100 HRB | |||||||
N06455(C4) | 100 000 (690) | 40 000 (276) | 40 | 100 HRB | |||||||
N06035 | 85 000 (586) | 35 000 (241) | 30 | 100 HRB | |||||||
N06044 | 100 000 (690) | 45 000 (310) | 30 | 100 HRB | |||||||
N06058 | 110 000 (760) | 52 000 (360) | 40 | 100 HRB | |||||||
N06059 | 100 000 (690) | 45 000 (310) | 45 | 100 HRB | |||||||
N06200 | 100 000 (690) | 45 000 (310) | 45 | 100 HRB | |||||||
N10362 | 105 000 (725) | 45 000 (310) | 40 | 100 HRB | |||||||
N06686 | 100 000 (690) | 45 000 (310) | 45 | 100 HRB | |||||||
N06210 | 100 000 (690) | 45 000 (310) | 45 | 100 HRB |
Alloy |
Tensile Strength, min, psi (MPa) |
Yield Strength (0.2% Offset), min, psi |
Elongation in 2 in. |
Rockwell Hardness,B |
N10276 |
100 000 (690) |
41 000 (283) |
40 |
100 HRB |
N06022 |
100 000 (690) |
45 000 (310) |
45 |
100 HRB |
N06455(C4) |
100 000 (690) |
40 000 (276) |
40 |
100 HRB |
N06035 |
85 000 (586) |
35 000 (241) |
30 |
100 HRB |
N06044 |
100 000 (690) |
45 000 (310) |
30 |
100 HRB |
N06058 |
110 000 (760) |
52 000 (360) |
40 |
100 HRB |
N06059 |
100 000 (690) |
45 000 (310) |
45 |
100 HRB |
N06200 |
100 000 (690) |
45 000 (310) |
45 |
100 HRB |
N10362 |
105 000 (725) |
45 000 (310) |
40 |
100 HRB |
N06686 |
100 000 (690) |
45 000 (310) |
45 |
100 HRB |
N06210 |
100 000 (690) |
45 000 (310) |
45 |
100 HRB |