Related Tradenames:
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Nickelvac K-500(tm) , Nicorros Al(tm) , Silverin
500(tm) , CM K500(tm)
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Chemistry Data :
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- Aluminum |
2.3 - 3.15 |
- Carbon |
0.25 max |
- Copper |
27 - 33 |
- Iron |
2 max |
- Manganese |
1.5 max |
- Nickel |
Balance |
- Silicon |
0.5 max |
- Sulphur |
0.01 max |
- Titanium |
0.35 - 0.85 |
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Principal Design Features :
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This is an age-hardenable version of the nickel-copper
alloy Monel 400. As such it has increased strength with the
excellent resistance to sea water corrosion.
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Applications :
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Sea water pump shafts and impellers as well as
being used in the oil well industry for valve trim and other
components.
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Corrosion Resistance :
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Corrosion resistance is similar to that of Monel
400 -- good in sea water and many acid environments. However
in the aged-hardened condition Monel K500 is more susceptible
to stress-corrosion cracking that Monel 400.
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Machinability :
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The best machinability for this alloy is in the
annealed condition. It may be machined in the aged condition,
but the preferred practice is to rough machine as close to
finish as possible in the annealed condition. Then aging and
final machining may be done. A very slight dimensional contraction
occurs upon aging. In general this alloy, in the annealed
condition, machines in a manner similar to that of the austenitic
(300 series) stainless steels.
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Forming :
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The alloy has good ductility and is readily formed
in the annealed condition by standard means.
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Welding :
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All of the conventional welding techniques may
be used on this alloy. However it is best to weld with the
alloy in the annealed condition and the finished weldment
should then be stress-relief annealed. Exposure to temperatures
in the age-hardening range (900 F to 1100 F) should be avoided
except when the final age-hardening treatment is to be accomplished.
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Heat Treatment :
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The alloy may be annealed after cold working
and also may be precipitation-hardened by an aging heat treatment.
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Forging :
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Forging should be done in the range of 2100 F
to 1900 F. Water quench immediately after forging.
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Hot Working :
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The hot work temperature range is 2100 F to 1600
F. Water quench immediately after hot working and do not allow
to cool below 1600 F.
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Cold Working :
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The alloy has good ductility and may be cold
worked by standard means.
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Annealing :
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Anneal at 1900 F and water quench.
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Aging :
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For annealed, or slightly cold-worked, material
age-hardening is done at 1125 F for 16 hours and then furnace
cooling at a rate of 15 F to 25 F per hour down to a temperature
of 900 F. Cooling rate from 900 F to room temperature is not
critical. For severely cold-worked material aging should be
done at 1000 F for at least 6 hours and then furnace cooled
to 900 F at the 15 F to 25 F per hour rate.
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Hardening :
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See "Aging".
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Mechanical Data :
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Form |
Condition |
Temper |
Tensile Strength |
Yield Strength |
Elongation |
Rockwell |
Plate |
Hot Finished |
70 |
112 |
65 |
32 |
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Plate |
Hot Finished & Aged |
70 |
160 |
117 |
25 |
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Sheet |
Annealed |
70 |
98 |
52 |
35 |
B90 |
Strip |
Annealed |
68 |
98 |
52 |
35 |
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Strip |
Spring |
70 |
195 |
162 |
7 |
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