Related Tradenames :
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Inconel 622 , Nicrofer 5621 hMoW (tm)
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Chemistry Data :
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- Carbon |
0.015 max |
- Chromium |
20 - 22.5 |
- Cobalt |
2.5 min |
- Iron |
2 - 6 |
- Manganese |
0.5 max |
- Molybdenum |
12.5 - 14.5 |
- Nickel |
Balance |
- Phosphorus |
0.02 max |
- Silicon |
0.08 max |
- Sulphur |
0.02 max |
- Tungsten |
2.5 - 3.5 |
- Vanadium |
0.35 min |
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Principle Design Features :
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A wrought nickel-chromium-molybdenum alloy also
containing tungsten for improved overall corrosion resistance
than most other similar alloys. Developed to provide an alternative
to Alloys 625 and C-276. This alloy offers excellent metallurgical
stability, resistance to localized corrosion, and is not sensitized
during welding or heating.
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Applications :
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The alloy is used to manufacture a wide variety
of chemical process equipment such as: Flue gas scrubbers,
chlorination systems, acid production and pickling systems,
outlet ducting and stack liners for power plants, sulfur dioxide
scrubbers, pulp and paper bleach plants and for weld overlay
of less corrosion resistant metals.
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Machinability :
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Machining is best accomplished using high speed
steel tooling for drilling operations. Carbide tools work
well for turning or milling. Drilling (high speed steel) speeds
10-15 surface feet /minute with feeds of 0.001" (for 1/8 "
dia. hole) to 0.007" (for 1" dia. hole) per revolution. Turning
(carbide tools) at 90 to 110 surface feet per minute and feed
of 0.010" (for roughing) to 0.006" (for finishing). Machining
may be done dry or with conventional coolants.
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Forming :
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Can be readily cold or hot formed. After hot
forming, or severe cold forming, the parts should be solution
heat treated.
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Welding :
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Readily welded by conventional methods, except
that submerged arc welding should be avoided due to the high
heat input and slow cooling of that method. Clean the weld
areas thoroughly before welding and use matching filler metal
ER NiCrMo-10 and E NiCrMo-10 for GTAW and SMAC methods respectively.
This alloy may be used in the as welded form for most applications
as it resists grain boundary precipitates during welding.
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Heat Treatment :
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Solution anneal at 2050 F followed by a rapid
quench.
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Forging :
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Hot forging can be done in the temperature range
of 2100 F. A solution heat treatment should be performed after
forging.
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Hot Working :
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Hot working may be done followed by a solution
anneal heat treatment.
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Cold Working:
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The alloy has very good ductility and, although
stiffer than the austenitic stainless steels, cold working
is the preferred means of forming. Severe cold working may
cause work hardening and in this event a solution heat treatment
may be used to restore the original mechanical properties
of the alloy.
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Annealing :
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See "Heat Treatment" for solution annealing.
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Aging :
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The alloy may be aged at temperatures of 950
F to 1900 F for some increase in hardness and tensile strength
(about 3% gain). However aging (or long exposure) at temperatures
above 1400 F results in degradation of V-notch impact strength.
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Hardening :
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Not hardenable by heat treatment. The alloy does
harden due to sever cold working.
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Other Physical Props :
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V-notch impact strength is 260 ft. lbs. at 70
F and at minus 320 F.
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Mechanical Data :
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There is no Mechnical data available for this
grade.
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