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Alloy
600 (UNS N06600)
A Nickel-Base Alloy with Resistance to a Variety of Corrosive
Conditions |
Applications
| Standards | Corrosion
Resistance | Chemical Analysis
Mechanical Properties | Impact
Resistance | Physical Properties
Creep
and Stress Rupture Properties
| Heat Treatment | Processing
| Welding
|
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to download Alloy 600 PDF file |
| Alloy 600
(UNS Designation N06600) is a nickel-chromium alloy designed
for use from cryogenic to elevated temperatures in the
range of 2000°F (1093°C). Alloy 600 is nonmagnetic and
readily weldable.
The alloy is used in a variety of corrosion
resisting applications. The high nickel content of Alloy
600 provides a level of resistance to reducing environments,
while the chromium content of the material provides resistance
to weaker oxidizing environments. The high nickel content
of the material provides exceptional resistance to chloride
stress corrosion cracking.
|
| Applications
- Chemical and food processing equipment
- Paper mill and alkaline digesters
- Heat exchangers
- Heat treating mufflers and retorts
|
| Standards |
| ASTM.......................... |
B 168 |
| ASME......................... |
SB 168 |
| AMS ........................... |
5540 |
| Federal
or Military......... |
MIL-N-23226
MIL-T-23227 |
|
| Corrosion
Resistance
The high nickel content of Alloy 600 provides good resistance
to moderate levels of reducing conditions. The nickel
content of the alloy renders the alloy extremely resistant
to chloride stress corrosion cracking. Alloy 600 is one
alloy used in solutions of magnesium chloride. Similarly,
the chromium content of Alloy 600 provides resistance
to weak oxidizing environments. In this respect, Alloy
600 is an improvement over Alloy 200 (commercially pure
nickel). In strong oxidizing solutions
like hot, concentrated nitric acid, Alloy 600 has poor
resistance. Alloy 600 is relatively unattacked by the
majority of neutral and alkaline salt solutions. It is
used in some caustic environments. Alloy 600 resists steam
and mixtures of steam, air and carbon dioxide. The alloy
has excellent oxidation resistance to about 2100°F (1149°C).
The nickel content of the alloy renders it subject to
attack at elevated temperatures in sulfur containing atmospheres,
however.
|
Chemical
Analysis
Typical
values (Weight %)
| C |
Mn |
S |
Si |
Cr |
Ni + Co |
Fe |
Cu |
| 0.05 |
0.25 |
0.002 |
0.20 |
15.5 |
Balance |
8.0 |
0.10 |
|
| Mechanical
Properties
Room temperature
mechanical properties of Alloy 600 are shown below. The
material is in the annealed condition.
0.2%
Offeset
Yield Strength |
Ultimate
Tensile Strength |
Elongation |
| psi |
(Mpa) |
psi |
(MPa) |
%
to 2" (51 mm) |
| 37,000 |
(255) |
93,000 |
(640) |
45 |
Short Time Elevated Temperature
Tensile Properties
The following
table illustrates the short time tensile properties of
Alloy 600 at
temperatures above room temperature. Low temperature properties
are added
for comparison.
| Test
Temperature |
0.2%
Offset
Yield Strength |
Ultimate
Tensile Strength |
Elongation
percent in |
| °F |
°C |
psi |
(MPa) |
psi |
(MPa) |
2"
(1mm) |
| -110 |
(-79) |
42,400 |
(292) |
106,450 |
(734) |
64 |
| 600 |
(316) |
31,000 |
(213) |
90,500 |
(624) |
46 |
| 800 |
(427) |
29,500 |
(203) |
88,500 |
(610) |
49 |
| 1000 |
(538) |
28,500 |
(197) |
84,000 |
(579) |
47 |
| 1200 |
(649) |
26,500 |
(183) |
65,000 |
(448) |
39 |
| 1400 |
(760) |
17,000 |
(117) |
27,500 |
(190) |
46 |
| 1600 |
(871) |
9,000 |
(62) |
15,000 |
(103) |
80 |
| 1800 |
(982) |
4,000 |
(28) |
7,500 |
(52) |
118 |
|
Impact
Resistance
Alloy 600 shows excellent
toughness even at subzero temperatures. The following
are typical results for standard size Charpy V-Notch impact
specimens machined from plate.
| Test
Temperature |
Charpy
Impact Strength, ft-lb (Joules) |
| °F |
°C |
Annealed |
As
Hot Rolled |
Cold
Rolled |
| -100 |
(-73) |
180 |
(244) |
180 |
(244) |
— |
| 70 |
(21) |
180 |
(244) |
180 |
(244) |
155 |
(156) |
| 1000 |
(538) |
160 |
(217) |
160 |
(217) |
— |
|
| Physical
Properties
Density
:
8.42 g/cm3 (0.304 lbs/in3)
Specific Gravity
:
8.42
Magnetic Permeability
I<1.02
Specific Heat
:
32-212°F 0.11 Btu/lb-°F
(0-100°C) 460 Joules/kg-°K
Linear Coefficient of Thermal
Expansion
| Average
from |
| 70°F (21°C) |
to °F (°C) |
|
| Linear Coefficient
of Thermal Expansion |
| 10-6 / °F |
10-6 / °F
|
|
| 200 |
(93) |
6.9 |
12.4 |
| 400 |
(204) |
7.3 |
13.1 |
| 600 |
(316) |
7.6 |
13.7 |
| 800 |
(427) |
7.9 |
14.2 |
| 1000 |
(538) |
8.1 |
14.6 |
| 1200 |
(649) |
8.4 |
15.1 |
| 1400 |
(760) |
8.7 |
15.7 |
Thermal Conductivity
| Temperature |
Thermal
Conductivity |
| °F |
(°C) |
Btu-ft / h-ft2 - °F |
W/m - °K |
| 70 |
21 |
8.6 |
14.8 |
| 200 |
93 |
8.9 |
15.4 |
| 400 |
204 |
9.9 |
17.1 |
| 600 |
316 |
10.8 |
18.7 |
| 800 |
427 |
11.9 |
20.6 |
| 1000 |
538 |
13.0 |
22.5 |
Elastic Modulus, Modulus
of Rigidity, and Poisson's Ratio
| Temperature |
Elastic
Modulus (E) Units of |
Modulus
of Rigidity (G) Units of |
Poisson's
Ratio |
| °F |
°C |
106
psi GPa |
106
psi GPa |
(µ) |
| 70 |
21 |
30 |
207 |
11 |
76 |
0.29 |
|
Creep
and Stress Rupture Properties
Typical stress rupture
properties of Alloy 600 are presented below in comparison
to some other materials. The data indicate that Alloy
600 has modest load carrying ability in the temperature
range in which creep and stress rupture are design criteria.
| Temperature |
Stress,
psi (MPa) to Produce Rupture in |
| °F |
°C |
Alloy |
10 hr |
100 hr |
1000 hr |
| |
304 |
— |
43,000 |
(297) |
34,000 |
(234) |
| 1000 |
(538) |
600 |
74,000 |
(510) |
50,000 |
(345) |
34,000 |
(234) |
| |
A-286 |
100,000 |
(690) |
95,000 |
(655) |
88,000 |
(607) |
| |
304 |
— |
23,000 |
(159) |
16,000 |
(110) |
| 1200 |
(649) |
600 |
34,000 |
(234) |
23,000 |
(159) |
14,5000 |
(100) |
| |
800 |
40,000 |
(276) |
32,000 |
(221) |
21,000 |
(145) |
| 1350 |
(732) |
600 |
20,000 |
(138) |
13,500 |
(93) |
9,200 |
(63) |
| |
A-286 |
49,000 |
(338) |
35,000 |
(241) |
21,000 |
(145) |
|
| Heat
Treatment
Alloy 600
is not hardenable by heat treatment. The alloy can only
be strengthened by cold working. Annealing is conducted
to soften the material after cold working operations.
Softening begins at 1600°F (871°C) and can be conducted
to about 2100°F (1149°C). At temperatures of 1800°F (982°C)
or higher, grain growth will occur rapidly. However, very
short time at 1900°F (1038°C) may be used to soften the
material without producing undue grain growth. Slow cooling
or quenching produces approximately the same hardness
in Alloy 600.
|
| Processing
Cold forming
Alloy 600 exhibits the excellent cold
forming characteristics normally associated with chromium-nickel
stainless steels. The high nickel content prevents the
austenite to martensite transformation which can occur
when Types 301 or 304 stainless steels are cold formed.
The alloy has a lower work hardening rate than Types 301
or 304 and can be used in multiple draw forming operations
where relatively large amounts of deformation occur between
anneals. If a high temperature anneal is conducted on
the Alloy 600 to produce a relatively large grain size
for elevated temperature properties, extensive forming
produces a visibly undulated surface called “orange
peel.” This surface characteristic is produced by
the large grain size and is usually considered detrimental
to the properties of the material.
|
| Welding
Alloy 600 can be joined by the standard resistance and
fusion welding processes used for the stainless steels.
A number of welding rods and wires are commercially available
for joining Alloy 600 to itself and other materials. Since
the alloy forms a tightly adhering oxide, which can be
removed only by grinding, inert gas shielding is desirable.
|
| 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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