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Alloy
400 (UNS N04400)
A Nickel-Base Alloy with Resistance to a Variety of Corrosive
Conditions |
Applications
| Standards | Corrosion
Resistance | Chemical Analysis
Mechanical Properties | Physical
Properties | Heat Treatment
Processing | Welding
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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
twentieth 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 about 700°F (371°C) and
molten sulfur attacks the alloy at temperatures over about
500°F (260°C).
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Chemical
Analysis
Typical
values (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 about 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 Types 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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NOTE
This technical data and information represents our best
knowledge at the time of printing. However, it may be
subject to some slight variations due to our ongoing research
program on corrosion resistant grades. We, therefore,
suggest that information be verified at time of inquiry
or order. Furthermore, in service, real conditions are
specific for each application. The data presented here
is only for the purpose of description and may only be
considered as guarantees when our Company has given written
formal approval.
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