General Properties
Alloy 800 (UNS N08800), Alloy 800H (UNS N08810),
and Alloy 800HT (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 800HT 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
800HT 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 800HT. Alloy 800 is normally
used in this service at temperatures to approximately
1100°F (593°C). Alloy 800H and Alloy 800HT
are normally used above approximately 1100°F
where resistance to creep and rupture is required.
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Applications
- Chemical and petrochemical processing
equipment
- Power generation
- Thermal processing fixtures
- Steel production
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Standards
ASTM........... B 409
ASME.......... SB 409
AMS ........... 5871
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Corrosion
Resistance
The chromium and nickel contents of Alloys
800, 800H and 800HT are higher than those of the
familiar Alloy 304 stainless steel alloy. Under
many conditions of service, the performance of
Alloys 800, 800H, 800HT and Alloy 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 800HT nor
Alloy 304 are suggested for sulfuric acid service
except at lower concentrations and temperatures.
Like the austenitic stainless steels, Alloys 800,
800H and 800HT 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.
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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
800HT |
0.08 |
1.00 |
0.020 |
0.010 |
0.35 |
21.0 |
32.0 |
– |
– |
1.00 |
0.30 |
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Mechanical
Properties
Typical room temperature mechanical properties
of Alloys 800, 800H, and 800HT are shown. Alloy
800 was annealed at 1800°F (928°C), and
Alloys 800H and 800HT 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 800HT
| 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 800HT. The strength of Alloys 800H and
800HT is lower because the heat treatment of Alloys
800H and 800HT 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.
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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 |
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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 |
| Alloy 309 |
0.80 |
1.2 |
2.1 |
2.5 |
4.0 |
| Alloy 310 |
0.80 |
1.1 |
2.6 |
3.2 |
5.2 |
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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 800HT 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.
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Cold
Formability
Alloys 800, 800H, and 800HT 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 Alloy 301
or Alloy 304 are cold worked. The alloy has a
lower work hardening rate than Alloys 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 800HT, the large grain
size produces a visibly undulated surface called
“orange peel” after forming.
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Welding
Alloys 800, 800H, and 800HT 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.
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