General Properties
Alloy 400 (UNS N04400) is a ductile nickel-copper
alloy with resistance to a variety of corrosive
conditions. The alloy is most frequently specified
in environments ranging from mildly oxidizing
through neutral and in moderately reducing conditions.
An additional application area of the material
is in marine environments and other nonoxidizing
chloride solutions.
The alloy has a long history of
use as a corrosion resistant material, dating
back to the early 20th century when it was developed
as an attempt to use a high copper content nickel
ore. The nickel and copper contents of the ore
were in the approximate ratio which is now formally
specified for the alloy.
As with commercially pure nickel,
Alloy 400 is low in strength in the annealed condition.
For this reason, a variety of tempers are used
which have the effect of increasing the strength
level of the material.
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Applications
- Marine and chemical processing
equipment
- Valves, pumps, propeller shafts
- Marine fixtures and fasteners
- Gasoline and fresh water tanks
- Process vessels and piping
- Heat exchangers
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Standards
ASTM......................... B 127
ASME......................... SB 127
AMS ........................... 4544
Federal or Military...... QQ-N-281
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Corrosion
Resistance
Alloy 400 is more corrosion resistant
than commercially pure nickel (UNS N02200) under
reducing conditions, and more resistant than refined
copper alloys under oxidizing conditions.
In moderately reducing acids, neutral
or alkaline solutions, Alloy 400 may be considered
for use. The alloy is resistant to most alkalies,
salts, organic substances, and atmospheric conditions.
Alloy 400 is a consideration for cooler alkaline
caustic conditions, although high temperature,
high stress, and high concentrations of caustic
have produced caustic stress corrosion cracking
in the material. The alloy is used in reducing
acids like sulfuric and hydrochloric, especially
in the absence of aeration and oxidizing species.
Alloy 400 is exceptionally resistant
to chloride stress corrosion cracking.
Application in waters, including
sea and brackish water, is a major use of the
material.
Alloy 400 is attacked in sulfur-bearing
gases above approximately 700°F (371°C),
and molten sulfur attacks the alloy at temperatures
over approximately 500°F (260°C).
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Chemical
Analysis
Typical Analysis (Weight %)
| C |
Mn |
P |
S |
Si |
Al |
Ni + Co |
Cu |
Fe |
| 0.10 |
0.50 |
0.005 |
0.005 |
0.25 |
0.02 |
Balance* |
32.0 |
1.0 |
*By difference - For material furnished
to QQ-N-281, lead, tin, and zinc are each typically
<0.003.
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Mechanical
Properties
The following are typical room temperature
mechanical properties of Alloy 400. The lowest
strength and most ductile condition is the annealed
condition with typical properties as shown below.
| Properties Applicable
to Plate |
| Yield
Strength |
Ultimate Tensile
Strength |
Elongation
Percent in 2" |
Elastic
Modules (E) |
| psi |
(Mpa) |
psi |
(MPa) |
(51 mm) |
psi |
(MPa) |
| 35,000 |
(240) |
75,000 |
(520) |
45 |
26 x 106 |
(180) |
Material furnished in the hot rolled
condition is somewhat stronger as indicated below.
| Properties Applicable
to Plate |
| Yield
Strength |
Ultimate Tensile
Strength |
Elongation
Percent in 2" |
Elastic Modules
(E) |
| psi |
(Mpa) |
psi |
(MPa) |
(51 mm) |
psi |
(MPa) |
| 45,000 |
(310) |
80,000 |
(550) |
30 |
26 x 106 |
(180) |
Charpy V-Notch impact values for
all of these conditions ranged from 100 to 240
ft-lbs (135 to 325 Joules) at room temperature.
Short Time Elevated Temperature
Properties
The following table illustrates the short time
high temperature tensile properties of Alloy 400
in the annealed condition. Creep resistance should
be a consideration above approximately 650°F
(343°C).
| Test
Temperature |
0.2%
Offset Yield Strength |
Ultimate
Tensile Strength |
Percent
Elongation |
| °F |
°C |
psi |
(MPa) |
psi |
(MPa) |
|
| 70 |
(21) |
31,000 |
(215) |
82,000 |
(565) |
48 |
| 200 |
(93) |
30,000 |
(205) |
80,000 |
(550) |
47 |
| 400 |
(204) |
26,000 |
(180) |
75,000 |
(520) |
45 |
| 600 |
(316) |
25,000 |
(175) |
73,000 |
(505) |
46 |
| 800 |
(427) |
23,000 |
(160) |
70,000 |
(480) |
48 |
| 1000 |
(538) |
21,000 |
(145) |
53,000 |
(370) |
40 |
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Physical
Properties
Density:
8.83 g/cm3 (.319 lbs/in3)
Specific Gravity:
8.83
Magnetic Permeability:
In the annealed condition the alloy is often moderately
to faintly magnetic at room temperature. The Curie
temperature of the material is close to room temperature.
Above the Curie temperature, the material is nonmagnetic.
The Curie temperature is influenced by minor composition
variations, so some heats of material will be
magnetic at room temperature and others will not.
Specific Heat:
Room temperature values
0.10 Btu/lb - °F
430 Joules/kg - °K
Electrical Resistivity:
51.0 Microhm - cm
Linear Coefficient of Thermal
Expansion
Average
from
70°F (21°C)
to °F (°C) |
10-6 / °F |
10-6 / °F |
| 200 |
(93) |
7.7 |
13.9 |
| 400 |
(204) |
8.6 |
15.5 |
| 600 |
(316) |
8.8 |
15.8 |
| 800 |
(427) |
8.9 |
16.0 |
| 1000 |
(538) |
9.1 |
16.4 |
Linear Coefficient of Thermal
Expansion
|
Average from
70°F (21°C) |
Btu-ft / h-ft2 - °F |
W/m - °K |
| °F |
(°C) |
| 200 |
(93) |
14.0 |
24.1 |
| 400 |
(204) |
16.1 |
27.8 |
| 600 |
(316) |
18.9 |
31.0 |
| 800 |
(427) |
19.8 |
34.3 |
| 1000 |
(538) |
22.0 |
38.1 |
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Heat
Treatment
The anneal cycle conducted on Alloy 400
is typically in the 1400° to 1800°F (760°
to 980°C) range for short times at temperature.
The purpose is to soften the material after forming
operations while maintaining a relatively fine
grain size.
Annealing should be done in an atmosphere
as free of sulfur compounds as possible since
sulfur will embrittle the material in extended
exposure time at the anneal temperature range.
A low temperature stress relief
may be conducted on cold deformed material by
heating to approximately 575°F (300°C)
for 1 to 3 hours.
A large percentage of Alloy 400
is put into service without final heat treatment.
This is done to increase the strength of the material.
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Processing
Cold Forming
Alloy 400 exhibits excellent cold forming characteristics
normally associated with chromium nickel stainless
steels. The alloy has a lower work hardening rate
than Alloys 301 or 304 stainless steel and can
be used in multiple draw forming operations where
relatively large amounts of deformation occur
between anneals.
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Welding
Alloy 400 may be joined by a variety
of processes including gas tungsten-arc, gas metal-arc
and shielded metal-arc processes. In all of these
processes, thorough cleaning of the joint area
is necessary to avoid embrittlement from such
sources as lubricants and paints. The material
must be free of scale for best welding.
Welding procedures for Alloy 400
are similar to those used for austenitic stainless
steels. Neither preheating nor post-weld heat
treatment are generally required.
Joint design is similar to that
used for austenitic stainless steels with two
exceptions. The first is the need to accommodate
the sluggish nature of the molten weld metal,
necessitating a joint design sufficiently open
to allow full filler wire access to fill the joint.
The second is the high thermal conductivity and
purity of the material which makes weld penetration
lower than in austenitic stainless steels.
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