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Specification
Sheet: Alloy 800, 800H and 800AT
Nickel-Iron-Chromium Alloy 800 (UNS N08800), Alloy 800H
(UNS N08810), and
Alloy 800AT (UNS N08811) are Designed to Resist Oxidation
and Carburization |
Applications
| Standards | Corrosion
Resistance | Chemical Analysis
Mechanical Properties | Physical
Properties | Oxidation Resistance
Heat Treatment | Cold Formability
| Welding
|
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to download Alloy 800 PDF file |
| Alloy 800
(UNS N08800), Alloy 800H (UNS N08810), and Alloy 800AT
(UNS N08811) are nickel-iron-chromium alloys designed
to resist oxidation and carburization at elevated temperatures.
The nickel content, 32%, makes the alloys highly resistant
both to chloride stress-corrosion cracking and to embrittlement
from precipitation of sigma phase. The general corrosion
resistance is excellent. In the solution annealed condition,
Alloys 800H and 800AT have superior creep and stress rupture
properties. All three versions of the basic Alloy 800
have been approved as materials of construction under
ASME Boiler and Pressure Valve Code, Section I-Power Boilers,
Section III-Nuclear Vessels, and Section VIII-Unfired
Pressure Vessels.
Alloy 800, Alloy 800H and Alloy 800AT
are identical except for the higher level of carbon (0.05
to 0.10 percent) in Alloy 800H, and the addition of up
to 1.00 percent aluminum + titanium in Alloy 800AT. Alloy
800 is normally used in this service at temperatures to
approximately 1100°F (593°C). Alloy 800H and Alloy
800AT are normally used above approximately 1100°F
where resistance to creep and rupture is required.
|
| Applications
- Chemical and petrochemical processing
equipment
- Power generation
- Thermal processing fixtures
- Steel production
|
| Standards |
| ASTM........... |
B 409 |
| ASME.......... |
SB 409 |
| AMS ........... |
5871 |
|
| Corrosion
Resistance
The chromium and nickel contents of Alloys 800, 800H and
800AT are higher than those of the familiar Type 304 stainless
steel alloy. Under many conditions of service, the performance
of Alloys 800, 800H, 800AT and Type 304 are similar. For
example, comparable behavior can be expected in most rural
and industrial atmospheres and in chemical media such
as nitric acid and organic acids. Neither Alloys 800,
800H and 800AT nor Type 304 are suggested for sulfuric
acid service except at lower concentrations and temperatures.
Like the austenitic stainless steels, Alloys 800, 800H
and 800AT are subject to sensitization (precipitation
of chromium carbides at grain boundaries) if heated for
excessive time in the 1000°-1400°F (538°-760°C)
temperature range. The sensitized metal may be subject
to intergranular attack by certain corrosive agents including
pickling acids or the boiling 65% nitric acids (Huey)
test.
Alloy 800 is highly resistant, although
not totally immune, to stress-corrosion cracking. In extensive
field experience, Alloy 800 has shown excellent service
performance in many types of equipment in the petroleum,
chemical, food, and pulp and paper industries. Thus, Alloy
800 may offer a distinct advantage for use in moderately
corrosive environments where service experience has indicated
a tendency toward stress-corrosion cracking of other austenitic
stainless steels. However, the alloy is not immune to
stress-corrosion cracking as judged by the extremely severe
magnesium chloride test.
|
Chemical
Analysis
Typical
Analysis (Weight %)
| |
C |
Mn |
P |
S |
Si |
Cr |
Ni |
Ti |
Al |
Ti + Al |
Cu |
| Alloy 800 |
0.02 |
1.00 |
0.020 |
0.010 |
0.35 |
21.0 |
32.0 |
0.40 |
0.40 |
– |
0.30 |
| Alloy 800H |
0.08 |
1.00 |
0.020 |
0.010 |
0.35 |
21.0 |
32.0 |
0.40 |
0.40 |
– |
0.30 |
| Alloy 800AT |
0.08 |
1.00 |
0.020 |
0.010 |
0.35 |
21.0 |
32.0 |
– |
– |
1.00 |
0.30 |
|
| Mechanical
Properties
Typical room temperature
mechanical properties of Alloys 800, 800H and 800AT are
shown. Alloy 800 was annealed at 1800°F (928°C)
and Alloys 800H and 800AT were annealed at 2100°F
(1149°C). The different anneal temperature used contributed
to the difference in strength of the materials.
Mechanical Properties of Alloy 800
| Test
Temperature |
0.2
Offset
Yield Strength |
Ultimate
Tensile Strength |
Percent
Elongation |
| °F |
°C |
psi |
(MPa) |
psi |
(MPa) |
|
| 70 |
21 |
43,000 |
295 |
87,700 |
600 |
44 |
| 200 |
93 |
39,700 |
274 |
81,700 |
563 |
43 |
| 500 |
260 |
34,000 |
234 |
76,200 |
525 |
39 |
| 800 |
427 |
33,300 |
230 |
74,600 |
514 |
40 |
| 1000 |
538 |
31,700 |
219 |
72,000 |
496 |
39 |
| 1200 |
649 |
29,000 |
200 |
54,000 |
372 |
56 |
| 1400 |
760 |
22,600 |
156 |
32,100 |
221 |
85 |
| 1500 |
816 |
14,200 |
98 |
24,800 |
171 |
91 |
Mechanical Properties of Alloy 800H and
Alloy 800AT
| Test Temperature |
0.2 Offset
Yield Strength |
Ultimate
Tensile Strength |
Percent
Elongation |
| °F |
°C |
psi |
(MPa) |
psi |
(MPa) |
|
| 70 |
21 |
29,000 |
200 |
77,000 |
531 |
52 |
| 200 |
93 |
24,100 |
166 |
71,000 |
490 |
53 |
| 600 |
316 |
19,000 |
131 |
66,600 |
459 |
53 |
| 800 |
427 |
18,100 |
125 |
65,800 |
454 |
53 |
| 1000 |
538 |
16,500 |
114 |
63,500 |
438 |
51 |
| 1200 |
649 |
14,800 |
102 |
55,700 |
384 |
50 |
| 1400 |
780 |
14,400 |
99 |
32,300 |
223 |
78 |
| 1600 |
871 |
11,600 |
80 |
18,600 |
128 |
120 |
| 1800 |
982 |
8,900 |
61 |
10,200 |
70 |
120 |
Short Time Elevated Temperature
Properties
The above tables
illustrate the short time high-temperature tensile properties
of Alloys 800, 800H and 800AT. The strength of Alloys
800H and 800AT is lower because the heat treatment of
Alloys 800H and 800AT at 2100°F (1149°C) results
in a larger grain size to provide better creep and stress
rupture resistance. The 1800°F (982°C) anneal
of Alloy 800 results in a finer grain size to provide
better cold formability.
|
| Physical
Properties
Density
:
0.29 g/cm3 (8.03 lbs/in3)
Electrical Resistivity:
99 Microhm-cm at 70 °F (21 °C)
Magnetic Permeability
<1.02
Specific Heat
:
(32°-212 °F) 0.12
Btu/lb-°F
(0°-100 °C)
500 Joules/kg-°K
Linear Mean Coefficient
of Thermal Expansion
| Temperature Range |
µm
/ °F |
µm
/ °C |
| °F |
°C |
| 70-200 |
21-93 |
7.9 |
14.2 |
| 70-300 |
21-149 |
8.4 |
15.1 |
| 70-400 |
21-204 |
8.6 |
15.5 |
| 70-500 |
21-260 |
8.8 |
15.8 |
| 70-600 |
21-316 |
9.0 |
16.2 |
| 70-800 |
21-427 |
9.2 |
16.6 |
| 70-1000 |
21-538 |
9.4 |
16.9 |
| 70-1200 |
21-649 |
9.6 |
17.3 |
| 70-1400 |
21-760 |
9.9 |
17.8 |
Thermal Conductivity
| Temperature Range |
BTU / h-ft
°F |
W / m /
°K |
| °F |
°C |
| 70 |
21 |
6.7 |
11.6 |
| 70-800 |
21-427 |
10.6 |
18.3 |
| 70-1800 |
21-982 |
17.8 |
30.8 |
|
Oxidation
Resistance
The alloys are particularly
well suited for high temperature applications such as
furnace parts and related heating equipment, for petrochemical
reforming units and isocracker tubs, and for handling
superheated steam in nuclear and conventional power plants.
With the specified high levels of chromium and nickel,
the alloys offer superior resistance to oxidation and
scaling, and to carburization as well.
The following oxidation data for Alloy
800 was obtained by exposing samples to the indicated
temperature for 100 hours in still air and cooling. In
general, total weight gains greater than 10mg/cm2 indicate
that additional exposure at these temperatures will lead
to failure.
Since oxidation rates are greatly affected
by heating and cooling rates as well as by the atmospheres
involved, this data can only be used as approximate guidelines.
100 Hour Still Air Continuous
Oxidation Tests
| Alloy |
Sample Weight
Gain (mg / cm2 ) |
1700°F
(927°C) |
1800°F
(982°C) |
1900°F
(1038°C) |
2000°F
(1093°C) |
2100°F
(1149°C) |
| Alloy 800 |
0.77 |
1.8 |
2.09 |
2.1 |
5.06 |
| Type 309 |
0.80 |
1.2 |
2.1 |
2.5 |
4.0 |
| Type 310 |
0.80 |
1.1 |
2.6 |
3.2 |
5.2 |
|
| Heat
Treatment
The anneal
cycle conducted on Alloy 800 is typically in the 1800°-1900°F
(982°-1038°C) range. The purpose is to soften
the material after forming operations while maintaining
a relatively fine grain size.
The heat treatment conducted on Alloys
800H and 800AT is typically in the range of 2050°-2150°F
(1121°-1177°C). In addition to softening the material
after forming operations, an additional purpose of this
heat treatment is the development of larger grains for
improved resistance to creep and stress rupture.
|
Cold
Formability
Alloys
800, 800H and 800AT exhibit 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 Type 301 or Type 304
are cold worked. The alloy has a lower work hardening
rate than Types 301 or 304 and can be used in multiple
drawn forming operations where relatively large amounts
of deformations occur between anneals.
As a consequence of the anneal cycle used
on Alloys 800H and 800AT, the large grain size produces
a visibly undulated surface called “orange peel”
after forming.
|
| Welding
Alloys 800, 800H and 800AT can be joined by tungsten arc
(GTAW), gas consumable electrode (MIG), or by stick electrode
welding techniques commonly used on stainless steels.
A number of welding rods and wires are commercially available
for joining the alloys. Since these alloys form tightly
adhering scales, 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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