Super Alloy Nitronic 33(tm) is stocked by 0 North American distributors and produced by 9 large mills. Distributors will offer small quantity buys while mills will generally only sell large quantities, with delivery times anywhere from 10 to 50 weeks depending on size and form required
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Specifications
The following specifications cover Super Alloy Nitronic 33(tm)
- ASTM A240 (XM-29)
- ASTM A249 (XM-29)
- ASTM A269 (XM-29)
- ASTM A276
- ASTM A312 (XM-29)
- ASTM A412 (XM-29)
- ASTM A479 (XM-29)
- ASTM A580 (XM-29)
- ASTM A688 (XM-29)
- ASTM A813 (TP XM-29)
- ASTM A814 (TP XM-29)
- UNS S24000
Property Results
Chemistry Data : [top]
Carbon
|
|
0.08 max |
Chromium
|
|
17 - 19 |
Iron
|
|
Balance |
Manganese
|
|
11.5 - 14.5 |
Nickel
|
|
2.25 - 3.75 |
Nitrogen
|
|
0.2 - 0.4 |
Phosphorus
|
|
0.06 max |
Silicon
|
|
1 max |
Sulphur
|
|
0.03 max |
Principal Design Features
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Designed primarily for low magnetic permeability, high yield strength and strong cryogenic properties.
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Applications
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A wide variety of cryogenic equipment including pipe and tube assemblies, valves, tanks and cable typify the applications of this alloy. It has also found use in a number of rotating parts such as fans and containment rings.
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Machinability
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Slow speeds, positive feeds and abundant resulphurized lubricant are essential to success in machining this alloy. Speeds and feeds similar to those employed with 316 or 317 stainless are appropriate here. All common machining practices can be used on this material. Chips will be tough and stringy and it is recommended that curlers or breakers are used.
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Forming
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All common forming techniques can be used with this alloy. Springback will be greater than with standard austenitics and should be taken into consideration when choosing the appropriate forming forces. Process annealing is recommended to remove stresses resulting from this alloys' high work hardening rate. Heat to 1950 F(1065 C) for intermediate anneal.
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Welding
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Pre-heating is not required with this material and all common welding methods including gas tungsten arc, gas metal arc and submerged arc are acceptable. Filler metal selection should be of similar chemistry for maximum strength and resistance to intergranular attack.
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Forging
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Heat to 2000 F, soak to equalize, then heat to 2150 and equalize prior to forging.
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Annealing
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Soak at 1900-2050 F, quench quickly in air or water.
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Hardening
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Hardening this alloy requires cold working. It will not harden with exposure to thermal treatment.
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Physical Data : [top]
|
|
Density (lb / cu. in.)
|
0.28
|
Specific Heat (Btu/lb/Deg F - [32-212 Deg F])
|
0.11
|
Poissons Ratio
|
0.298
|
Modulus of Elasticity Tension
|
29
|
Mechanical Data : [top]
Form |
|
Sheet |
Condition |
|
Annealed |
Temper |
|
70 |
Tensile Strength |
|
115 |
Yield Strength |
|
66 |
Elongation |
|
49 |
Rockwell |
|
B95 |
|
Form |
|
Sheet |
Condition |
|
Cold Reduced 10% |
Temper |
|
132 |
Tensile Strength |
|
100 |
Yield Strength |
|
32 |
Rockwell |
|
C29 |
|
Form |
|
Sheet |
Condition |
|
Cold Reduced 20% |
Temper |
|
159 |
Tensile Strength |
|
135 |
Yield Strength |
|
19 |
Rockwell |
|
C35 |
|
Form |
|
Sheet |
Condition |
|
Cold Reduced 30% |
Temper |
|
185 |
Tensile Strength |
|
168 |
Yield Strength |
|
11 |
Rockwell |
|
C40 |
|
Form |
|
Sheet |
Condition |
|
Cold Reduced 40% |
Temper |
|
202 |
Tensile Strength |
|
180 |
Yield Strength |
|
7 |
Rockwell |
|
C43 |
|
Form |
|
Sheet |
Condition |
|
Cold Reduced 50% |
Temper |
|
210 |
Tensile Strength |
|
190 |
Yield Strength |
|
6 |
Rockwell |
|
C45 |
|
Form |
|
Sheet |
Condition |
|
Cold Reduced 60% |
Temper |
|
223 |
Tensile Strength |
|
200 |
Yield Strength |
|
5 |
Rockwell |
|
C46 |
Videos :
MSO currently has no videos available for this grade.
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