Seamless Tube Nickel B163 Grade UNS N02200

Product info

Supplier: Tapgroup internation.,JSC
Address: Số 32 Lô N4D, đường X2A, Yên Sở, Hoàng Mai, Hà Nội
Phone: 0084 933 86 77 86
Email: info@tapgroup.vn
Website: https://supplier-pipe-tube-ongthep.com
Insurance: 12 tháng
Status: Mới 100%
Origin: China, Korea, Malaysia, Thailand, Japan, EU, G7
Name: Seamless Tube Nickel B163 Grade UNS N02200
Type Of Tubes Seamless Tubes Nickel B163 Grade UNS N02200 SMLS Tubes Nickel B163 GradeUNS N02200
Seamless Nickel and Nickel Alloy Condenser and Heat- Exchanger Tubes
Scope
This specification covers seamless tubes of nickel and nickel alloys, as shown in Table 1, for use in condenser and heat-exchanger service.
This specification covers outside diameter and average wall, or outside diameter and minimum wall tube.
The sizes covered by this specification are 3 in. (76.2 mm) and under in outside diameter with minimum wall thicknesses of 0.148 in. (3.76 mm) and under, and with average wall thicknesses of 0.165 in.
(4.19 mm) and under.
Tube shall be furnished in the alloys and conditions as shown in Table 2.
The values stated in inch-pound units are to be regarded as the standard. The values given in parentheses are for information only.
The following safety hazards caveat pertains only to the test method portion, Section 12, of this specification. This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
Workmanship, Finish, and Appearance
The material shall be uniform in quality and
temper, smooth, commercially straight, and free of
injurious imperfections.
Dimensions and Permissible Variations
Outside Diameter and Wall Thickness — The permissible variations in the outside diameter and wall thickness of tube shall not exceed those prescribed, as applicable.
Length — When tube is ordered cut-to-length, the length shall not be less than that specified, but a variation of plus 1⁄8 in. (3.2 mm) will be permitted,
except that for lengths over 30 ft (9.1 m), a variation of plus 1⁄4 in. (6.4 mm) will be permitted.
Straightness — Material shall be reasonably straight and free of bends or kinks.
Number of Tests
Chemical Analysis — One test per lot. Mechanical Properties — One test per lot.
Hardness — A representative sample consisting of 3% of each lot of tubes with annealed ends
Grain Size — One test per lot.
Flare — One end of each random length tube
Mechanical Properties and Other Requirements
Mechanical Properties — The material shall conform to the mechanical properties specified in Table 3.
Hardness — When annealed ends are specified for tubing in the stress-relieved condition, the hardness of the ends after annealing shall not exceed the values specified.
Flare — A flare test shall be made on one end of each random length tube after final heat treatment. In the case of stress-relieved tubing with annealed ends, the test shall be made prior to, or subsequent to, annealing of the ends, at the option of the manufacturer.
The flare test shall consist of flaring a test specimen with an expanding tool having an included angle of 60° until the specified outside diameter has been increased by 30%. The flared specimen shall not exhibit cracking through the wall.
Grain Size — A transverse sample representing full-wall thickness of annealed alloys UNS N08120, UNS N08810, and UNS N08811 shall conform to anaverage grain size of ASTM No. 5 or coarser.
Hydrostatic Test: Each tube with an outside diameter 1⁄8 in. (3.2 mm) and larger and tubes with wall thickness of 0.015 in. (0.38 mm) and over shall be tested by the manufacturer to an internal hydrostatic pressure of 1,000 psi (6.9 MPa) provided that the fiber stress calculated in accordance with the following equation does not exceed the allowable fiber stress, S, indicated below. The tube shall show no evidence of leakage.
                                                                                                            P = 2St/D
where:
P =  hydrostatic test pressure, psi (MPa),
S =  allowable fiber stress for material in the condition furnished, as follows:
t =  minimum wall thickness, in. (mm); equal to the specified average wall minus the permissible
“minus” wall tolerance, Table 4, or the specified minimum wall thickness, and
D =  outside diameter of the tube, in. (mm).
When so agreed upon between the manufacturer and the purchaser, tube may be tested to 11⁄2
times the above allowable fiber stress.
When stress-relieved tubes with annealed ends are to be tested hydrostatically, such pressure testing shall be done prior to annealing of the ends of the tube.
Alloy psi Mpa
Annealed low-carbon nickel UNS N02201 8 000 55.20
Stress-relieved low-carbon nickel UNS N02201 15 000 103.40
Annealed nickel UNS N02200 10 000 68.90
Stress-relieved nickel UNS N02200 16 200 111.70
Annealed nickel-copper alloy UNS N04400 17 500 120.60
Stress-relieved nickel-copper alloy UNS N04400 21 200 146.20
Annealed nickel-chromium-iron alloy UNS N06600  20 000 137.90
Annealed nickel-chromium-iron alloy UNS N06601 20 000 137.90
Annealed nickel-chromium-iron alloy UNS N06690 21 200 146.00
Annealed nickel-chromium-iron alloy UNS N06045 22 500 155.00
Annealed nickel-chromium-iron alloy UNS N06025 24 500 169.00
Solution annealed low-carbon 25 000 172
nickel-chromium-molybdenum-tungsten
alloy UNS N06686
25 000 172.00
Annealed nickel-chromium-iron-aluminum alloy UNS N06603 24 000 165.00
Annealed nickel-iron-chromium alloy UNS N08120 22  500 155.00
Annealed nickel-iron-chromium alloy UNS N08800 18 700 128.90
Annealed nickel-iron-chromium alloy UNS N08810 16 600 114.40
Annealed nickel-iron-chromium alloy UNS N08811 16 600 114.40
Annealed nickel-iron-chromium alloy UNS N08801 16 600 114.40
Annealed nickel-iron-chromium-molybdenum copper alloy UNS N08825 21 000 144.80
Cold-worked nickel-iron-chromium alloy UNS N08800 20 700 142.70
Chemical Requirements 
Composition, %
Alloy Nickel Copper Molyb-denum Iron  Manganese, Max Carbon  Silicon Sulfur, Max Chromium Aluminum Titanium Phosphorus Cerium Zirconium Yttrium Boron Cobalt Columbium (Nb) Tungsten  Nitrogen
Nickel UNS N02200 99.0 minB 0.25 max 0.40 max 0.35 0.15 max 0.35 0.01
AMaximum unless range is given
BElement shall be determined arithmetically by difference
CAlloy UNS N08811: Al + Ti, 0.85-1.20
Mechanical properties of tubes
Materials and condition Tensile strength, Min, ksi (Mpa) Yield strength (0.2% Offset), Min, psi (Mpa) Elongation in 2 in. or 50mm (or 4D) min., % Rockwell hardness (or equipvalent) for annealed endsA
Nickel UNS N02200:  
Annealed 55 (379) 15 (103) 40
Stress-relieved 65 (448) 40 (276) 15 B 65 max
Low-Carbon Nickel UNS N02201:        
Annealed 50 (345) 12 (83) 40
Stress-relieved 60 (414) 30 (207) 15 B 62 max
Nickel-Copper Alloy UNS N04400         
Annealed 70 (483) 28 (193) 35
Stress-relieved 85 (586) 55 (379) 15 B 75 max
Nickel-Chromium-Iron Alloys:        
Annealed Alloy UNS N06600 80 (552) 35 (241) 30
Annealed Alloy UNS N06601 80 (552) 30 (207) 30
Annealed Alloy UNS N06690 85 (586) 35 (241) 30
Annealed Alloy UNS N06045 90 (620) 35 (241) 35
Annealed Alloy UNS N06025 98 (680) 39 (270) 30
Annealed Alloy UNS N06603 94 (650) 43 (300) 25
Low-Carbon Nickel-Chromium- Molybdenum-Tungsten Alloy:  
Solution annealed UNS N06686 100 (690) 45 (310) 45
Nickel-Iron-Chromium Alloys:        
Annealed Alloy UNS N08120 90 (620) 40 (276) 30
Annealed Alloy UNS N08800 75 (517) 30 (207) 30
Annealed Alloy UNS N08801 65 (448) 25 (172) 30
Cold-worked Alloy UNS N08800 83 (572) 47 (324) 30
Annealed Alloy UNS N08810 65 (448) 25 (172) 30
Annealed Alloy UNS N08811 65 (448) 25 (172) 30
Nickel-Iron-Chromium-Molybdenum-Copper Alloy: Annealed UNS N08825                                      85 (586) 35 (241) 30
ARockwell or equivalent hardness values apply only to the annealed ends of stress-relieved tubing. Caution should be observed in using the Rockwell test on thin material, as the results may be affected by the thickness of specimen. For thickness under 0.050 in. (1.27 mm) the use of the Rockwell superficial or the Vickers hardness test is suggested. For hardness conversions for nickel and high-nickel alloys.
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