| Alloy
310/310S
Sandmeyer Steel Company stocks Alloy 310/310S
heat resistant stainless steel plate in thicknesses
from 3/16" through 3".
310/310S 合金( UNS S31000/S31008 ) 合金奥氏体不锈钢主要用于高温环境。其较
高的铬含量及镍含量保证了良好的抗腐蚀能力及抗氧化能力。与奥氏体304
合金相比,
它在室温下强度要高一点。
Specs:
310/310S (UNS S31000) / (UNS S31008)
General Properties
Applications
Chemical Composition
Physical Properties
Typical Short-Term Mechanical Properties
Aqueous Corrosion Resistance
Elevated Temperature Oxidation Resistance
Other Forms of Degradation
Fabrication Characteristics
Welding
Heat Treatment/Annealing
General Properties
Alloy 309/309S and Alloy 310/310S austenitic stainless
steels are typically used for elevated temperature applications.
Their high chromium and nickel contents provide comparable
corrosion resistance, superior resistance to oxidation,
and the retention of a larger fraction of room temperature
strength than the common austenitic Alloy 304.
Back to top
Applications
Higher alloyed stainless steels generally exhibit excellent
elevated temperature strength along with resistance
to creep deformation and environmental attack. As such,
they are used widely in the heat treatment industry
for furnace parts such as conveyor belts, rollers, burner
parts, refractory supports, retorts and oven linings,
fans, tube hangers, and baskets and trays to hold small
parts. These grades are also used in the chemical process
industry to contain hot concentrated acids, ammonia,
and sulfur dioxide. In the food processing industry,
they are used in contact with hot acetic and citric
acid.
Back to top
Chemical
Composition
Chemistries are taken from ASTM A167 and ASTM
A240 specifications unless otherwise noted.
| |
Alloy 309 |
Alloy 309S |
| |
(UNS S30900) |
(UNS S30908) |
| C |
0.20 |
0.08 |
| Mn |
2.00 |
2.00 |
| P |
0.045 |
0.045 |
| S |
0.030 |
0.030 |
| Si |
0.75 |
0.75 |
| Cr |
22.00 min/24.00 max |
22.00 min/24.00 max |
| Ni |
12.00 min/15.00 max |
12.00 min/15.00 max |
| Fe |
Balance |
Balance |
| |
Alloy 310 |
Alloy 310S |
| |
(UNS S31000) |
(UNS S31008) |
| C |
0.25 |
0.08 |
| Mn |
2.00 |
2.00 |
| P |
0.045 |
0.045 |
| S |
0.030 |
0.030 |
| Si |
1.75 |
1.50 |
| Cr |
24.00 min/26.00 max |
24.00 min/26.00 max |
| Ni |
19.00 min/22.00 max |
19.00 min/22.00 max |
| Fe |
Balance |
Balance |
Alloy composition – all values
in weight percent, maximum levels unless a range is
specified.
Back to top
Physical
Properties
| |
Alloy 309 |
| Density |
lbm/in3 |
g/cm3 |
| at 68°F
(20°C) |
0.29 |
8.03 |
| Coefficient of Thermal Expansion |
(min/in)•°F |
(mm/m)•°K |
at 68 - 212°F
(20 - 100°C) |
8.7 |
15.6 |
at 68 - 932°F
(20 - 500°C) |
9.8 |
17.6 |
at 68 - 1832°F
(20 - 1000°C) |
10.8 |
19.4 |
| Electrical Resistivity |
mW•in |
mW•cm |
| at 68°F
(20°C) |
30.7 |
78.0 |
| at 1200°F
(648°C) |
45.1 |
114.8 |
| Thermal Conductivity |
Btu/hr•ft•°F |
W/m•K |
at 68 - 212°F
(20 - 100°C) |
9.0 |
15.6 |
at 68 - 932°F
(20 - 500°C) |
10.8 |
18.7 |
| Specific Heat |
Btu/lbm•°F |
J/kg•K |
at 32 - 212°F
(0 - 100°C) |
0.12 |
502 |
| Magnetic Permeability (annealed)1 |
|
| at 200H |
1.02 |
| Modulus of Elasticity (annealed)2 |
psi |
GPa |
| in tension
(E) |
29 x 106 |
200 |
| in shear (G) |
11.2 x 106 |
77 |
| |
Alloy 310 |
| Density |
lbm/in3 |
g/cm3 |
| at 68°F
(20°C) |
0.29 |
8.03 |
| Coefficient of Thermal Expansion |
(min/in)•°F |
(mm/m)•°K |
at 68 - 212°F
(20 - 100°C) |
8.8 |
15.9 |
at 68 - 932°F
(20 - 500°C) |
9.5 |
17.1 |
at 68 - 1832°F
(20 - 1000°C) |
10.5 |
18.9 |
| Electrical Resistivity |
mW•in |
mW•cm |
| at 68°F
(20°C) |
30.7 |
78.0 |
| at 1200°F
(648°C) |
-- |
-- |
| Thermal Conductivity |
Btu/hr•ft•°F |
W/m•K |
at 68 - 212°F
(20 - 100°C) |
8.0 |
13.8 |
at 68 - 932°F
(20 - 500°C) |
10.8 |
18.7 |
| Specific Heat |
Btu/lbm•°F |
J/kg•K |
at 32 - 212°F
(0 - 100°C) |
0.12 |
502 |
| Magnetic Permeability (annealed)1 |
|
| at 200H |
1.02 |
| Modulus of Elasticity (annealed)2 |
psi |
GPa |
| in tension
(E) |
29 x 106 |
200 |
| in shear (G) |
11.2 x 106 |
77 |
1 Common value for both alloys,
no units
2 Common value for both alloys
General physical properties for base
Alloy 309 and Alloy 310 austenitic stainless steels
Back to top
Typical
Short-Term Mechanical Properties
All tensile testing was done in accordance with ASTM
E8. The data consists of the average results from a
minimum of two and as many as ten samples. Yield strength
was determined by the 0.2% offset method. Plastic elongation
is as measured in a two inch gauge length.
Alloy 309
| Test
Temperature |
Yield Strength |
| (°F) |
(°C) |
ksi |
MPa |
| 77 |
25 |
42.0 |
290 |
| 400 |
204 |
35.0 |
241 |
| 800 |
427 |
30.0 |
207 |
| 1000 |
538 |
24.0 |
166 |
| 1200 |
649 |
22.0 |
152 |
| 1400 |
760 |
20.0 |
138 |
| 1600 |
871 |
18.5 |
128 |
| 1800 |
982 |
-- |
-- |
| Test
Temperature |
Tensile
Strength |
Elongation |
| (°F) |
(°C) |
ksi |
MPa |
% |
| 77 |
25 |
90.0 |
621 |
49 |
| 400 |
204 |
80.0 |
552 |
46 |
| 800 |
427 |
72.0 |
497 |
40 |
| 1000 |
538 |
66.0 |
455 |
36 |
| 1200 |
649 |
55.0 |
379 |
35 |
| 1400 |
760 |
36.0 |
248 |
40 |
| 1600 |
871 |
21.0 |
145 |
50 |
| 1800 |
982 |
10.1 |
69 |
65 |
Alloy 309S
| Test
Temperature |
Yield Strength |
| (°F) |
(°C) |
ksi |
MPa |
| 77 |
25 |
50.9 |
351 |
| 200 |
93 |
44.7 |
308 |
| 400 |
204 |
37.4 |
258 |
| 600 |
316 |
33.4 |
230 |
| 800 |
427 |
29.6 |
204 |
| 900 |
482 |
30.4 |
210 |
| 1000 |
538 |
26.7 |
184 |
| 1100 |
593 |
26.5 |
182 |
| 1200 |
649 |
24.7 |
170 |
| 1300 |
704 |
23.7 |
163 |
| 1400 |
760 |
22.2 |
153 |
| 1500 |
816 |
20.1 |
138 |
| 1600 |
871 |
16.6 |
114 |
| 1700 |
927 |
13.1 |
90 |
| 1800 |
982 |
8.2 |
56 |
| 1900 |
1038 |
4.6 |
32 |
| Test
Temperature |
Tensile
Strength |
Elongation |
| (°F) |
(°C) |
ksi |
MPa |
% |
| 77 |
25 |
97.1 |
670 |
44.6 |
| 200 |
93 |
88.8 |
612 |
29.0 |
| 400 |
204 |
81.7 |
563 |
34.5 |
| 600 |
316 |
80.2 |
553 |
31.6 |
| 800 |
427 |
77.1 |
531 |
32.1 |
| 900 |
482 |
74.7 |
515 |
32.0 |
| 1000 |
538 |
71.2 |
491 |
26.6 |
| 1100 |
593 |
65.6 |
452 |
25.5 |
| 1200 |
649 |
55.9 |
386 |
28.8 |
| 1300 |
704 |
55.7 |
384 |
-- |
| 1400 |
760 |
36.0 |
248 |
22.5 |
| 1500 |
816 |
24.7 |
170 |
64.8 |
| 1600 |
871 |
20.7 |
142 |
73.3 |
| 1700 |
927 |
15.4 |
106 |
78.7 |
| 1800 |
982 |
10.8 |
74 |
-- |
| 1900 |
1038 |
6.6 |
46 |
-- |
Alloy 310
| Test
Temperature |
Yield Strength |
| (°F) |
(°C) |
ksi |
MPa |
| 77 |
25 |
42.4 |
292 |
| 400 |
204 |
31.5 |
217 |
| 800 |
427 |
27.2 |
188 |
| 1000 |
538 |
24.2 |
167 |
| 1200 |
649 |
22.6 |
156 |
| 1500 |
816 |
19.7 |
136 |
| 1800 |
982 |
-- |
-- |
| 2000 |
1093 |
-- |
-- |
| Test
Temperature |
Tensile
Strength |
Elongation |
| (°F) |
(°C) |
ksi |
MPa |
% |
| 77 |
25 |
89.5 |
617 |
45 |
| 400 |
204 |
76.6 |
528 |
37.5 |
| 800 |
427 |
74.8 |
516 |
37 |
| 1000 |
538 |
70.1 |
483 |
36 |
| 1200 |
649 |
57.2 |
394 |
41.5 |
| 1500 |
816 |
30.3 |
209 |
66 |
| 1800 |
982 |
11.0 |
76 |
65 |
| 2000 |
1093 |
7.0 |
48 |
77 |
Alloy 310S
| Test
Temperature |
Yield Strength |
| (°F) |
(°C) |
ksi |
MPa |
| 77 |
25 |
45.6 |
314 |
| 200 |
93 |
41.4 |
286 |
| 400 |
204 |
36.9 |
254 |
| 600 |
316 |
34.6 |
239 |
| 800 |
427 |
30.3 |
209 |
| 1000 |
538 |
29.4 |
203 |
| 1200 |
649 |
25.8 |
178 |
| 1400 |
760 |
21.4 |
147 |
| 1600 |
871 |
16.1 |
111 |
| 1800 |
982 |
8.2 |
56 |
| 2000 |
1093 |
4.0 |
27 |
| Test
Temperature |
Tensile
Strength |
Elongation |
| (°F) |
(°C) |
ksi |
MPa |
% |
| 77 |
25 |
90.5 |
624 |
42.6 |
| 200 |
93 |
83.4 |
575 |
41.3 |
| 400 |
204 |
77.3 |
533 |
35.8 |
| 600 |
316 |
75.2 |
519 |
35.0 |
| 800 |
427 |
73.6 |
508 |
33.5 |
| 1000 |
538 |
70.2 |
484 |
37.0 |
| 1200 |
649 |
57.0 |
393 |
32.0 |
| 1400 |
760 |
37.7 |
260 |
54.0 |
| 1600 |
871 |
22.5 |
155 |
56.5 |
| 1800 |
982 |
11.8 |
81 |
93.3 |
| 2000 |
1093 |
6.5 |
44 |
121.0 |
Back to top
Aqueous
Corrosion Resistance
Alloys 309/309S and 310/310S are primarily used at elevated
temperature to take advantage of their oxidation resistance.
However, both of these stainless grades are resistant
to aqueous corrosion due to their high chromium and
nickel contents.
Although their higher nickel content provides
marginal improvement with respect to chloride stress
corrosion cracking (SCC) compared to the 18-8 stainless
steels, Alloys 309/309S and 310/310S austenitic stainless
steels remain susceptible to this form of attack.
Certain applications specify the use of
Alloy 310/310S stainless steel where increased resistance
to aqueous corrosion is needed. An example is service
in concentrated nitric acid, where preferential attack
of grain boundaries may occur.
Back to top
Elevated
Temperature Oxidation Resistance
Metallic alloys will react with their surroundings to
some degree under most conditions. The most common reaction
is oxidation – metallic elements combining with
oxygen to form oxides. Stainless steels are resistant
to oxidation through selective oxidation of chromium,
which forms a slow-growing, very stable oxide (Cr2O3
or chromia). Given enough chromium in the underlying
alloy, a compact and adherent surface layer of chromium
oxide is established which prevents the formation of
other, faster growing oxides and serves as a barrier
to further degradation. The rate of oxidation is controlled
by transport of charged species through the external
chromia scale. As the surface scale thickens, the rate
of oxidation decreases dramatically because the charged
species have to travel farther. This process, the high
temperature analogue of passivation during corrosion
at low temperatures, is known as protective scale formation.
The oxidation resistance of austenitic
stainless steels can be approximated by the chromium
content of the alloy. True heat resistant alloys generally
contain at least 20% (by weight) chromium. Replacing
iron with nickel also generally improves an alloy's
high temperature behavior. Alloys 309/309S and 310/310S
are highly alloyed materials and are, therefore, very
resistant to oxidation.
An oxidized metal sample will increase
in weight corresponding to the amount of oxygen incorporated
into the scale and any internal oxidation. Measuring
the change in weight of a sample which has been exposed
at high temperatures for a set period of time is one
way to determine the oxidation resistance of an alloy.
Greater weight gains typically indicate more severe
oxidation.
Oxidation is more complex than simple
scale thickening. Spallation, or the detachment of the
surface oxide scale, is the most common problem encountered
during the oxidation of stainless steels. Spallation
is typically manifested by rapidly accelerating weight
loss. A number of factors can cause spallation, chief
among them thermal cycling, mechanical damage, and excessive
oxide thickness.
During oxidation, chromium is tied up
in the scale in the form of chromium oxide. When the
oxide scale spalls off, fresh metal is exposed and the
local rate of oxidation temporarily increases as new
chromium oxide forms. Given sufficient scale spallation,
enough chromium may be lost to cause the underlying
alloy to lose its heat resistant properties. The result
is the formation of rapidly growing oxides of iron and
nickel, known as breakaway oxidation.
Very high temperature oxidation can lead
to scale volatilization. The surface chromium oxide
scale formed on heat resistant stainless steels is primarily
Cr2O3. At higher temperatures, the tendency
is for further oxidation to CrO3, which has
a very high vapor pressure. The rate of oxidation is
then split into two parts – scale thickening by
formation of Cr2O3 and the thinning effect
of CrO3 evaporation. The tendency is for
eventual balance between growth and thinning with the
scale remaining at a constant thickness. The result
is continuous recession of the surface and consumption
of the metal beneath. The effect of scale volatilization
becomes a significant problem at temperatures above
approximately 2000°F (1093°C) and is exacerbated
by rapidly flowing gases.
Back to top
Other
Forms of Degradation
Species other than oxygen present in the high temperature
environment can cause accelerated degradation of stainless
steels. The presence of sulfur can lead to sulfidation
attack. Sulfidation of the stainless steels is a complex
process and depends strongly on the relative levels
of sulfur and oxygen, along with the form of sulfur
present (e.g., elemental vapor, sulfur oxides, hydrogen
sulfide). Chromium forms stable oxides and sulfides.
In the presence of both oxygen and sulfur compounds,
a stable external chromium oxide layer often forms which
can act as a barrier to sulfur ingress. However, sulfidation
attack can still occur at regions where the scale has
become damaged or detached, and under certain circumstances
sulfur can transport across a chromia scale and form
internal chromium sulfide phases. Sulfidation is enhanced
in alloys containing a significant (about 25% or more)
amount of nickel. Nickel and nickel sulfide form a low
melting point eutectic phase which can cause catastrophic
damage to the underlying alloy at elevated temperatures.
High levels of carbon-bearing species
in the environment can result in undesired carbon ingress
and the subsequent formation of internal carbides. Carburization
generally takes place at temperatures above 1470°F
(800°C) and at a carbon activity less than unity.
The formation of a zone of internally carburized metal
can cause undesired changes in mechanical and physical
properties. Generally, the presence of oxygen will prevent
carbon ingress by the formation of a protective external
scale. Higher levels of nickel and silicon are somewhat
effective in reducing the susceptibility of carburization.
Metal dusting is a specific form of carburization attack
which generally occurs at lower temperatures (660-1650°F
or 350-900°C) and at a carbon activity greater than
unity. It can result in catastrophic local attack via
the formation of deep craters through a complex mechanism
which converts solid metal to mixture of graphite and
metal particles.
Nitridation can occur in the presence
of nitrogen gas. Oxides re generally more stable than
nitrides so in an atmosphere which contains oxygen,
an oxide scale typically forms. Oxide layers are good
barriers to nitrogen ingress so nitridation is rarely
a concern in air or in gases typical of combustion products.
Nitridation can be a problem in purified nitrogen and
is of special concern in dried, cracked ammonia atmospheres
where the oxygen potential is very low. At relatively
low temperatures a surface nitride film will generally
form. At high temperatures (above about 1832°F or
1000°C) the diffusivity of nitrogen is fast enough
that nitrogen penetrates deep into the metal and causes
the formation of internal nitrides on grain boundaries
and within grains. This can lead to compromised mechanical
properties.
Metallurgical instability, or the formation
of new phases during high temperature exposures, can
adversely affect mechanical properties and reduce corrosion
resistance. Carbide particles tend to precipitate at
grain boundaries (sensitization) when austenitic stainless
steels are held in or slowly cooled through the temperature
range 800-1650°F (427-899°C). The higher levels
of chromium and nickel contained in these alloys results
in lower carbon solubility, which tends to increase
the susceptibility for sensitization. Forced quenchant
(gas or liquid) cooling is recommended through the critical
temperature range, particularly for thicker sections.
The time at temperature required to form chromium carbides
increases with decreasing carbon content. Therefore,
the low carbon versions of these alloys are more resistant
but not immune to sensitization. When heated at temperatures
between 1200-1850°F (649-1010°C) for long periods
of time, Alloys 309/309S and 310/310S can exhibit decreased
ductility at room temperature due to the precipitation
of brittle second phase particles (sigma phase and carbides).
Sigma phase often forms at grain boundaries and can
reduce ductility. This effect is reversible and full
ductility can be restored by reannealing at the suggested
temperatures.
Elevated temperature degradation is greatly
affected by the atmosphere present and other operating
conditions. General oxidation data can often be used
only in estimating the relative oxidation resistance
of different alloys. Sandmeyer Steel Company can supply
data and prior experience pertaining to specific applications
on request.
Back to top
Fabrication
Characteristics
Alloys 309/309S and 310/310S stainless steel
are widely used in the heat treatment/process industries
due to high temperature properties and corrosion resistance.
As such, they are commonly fabricated into complex structures.
Mild carbon steel is generally treated as the standard
for performance in most metal forming operations. With
respect to carbon steel, the austenitic stainless steels
exhibit a significant difference – they are tougher
and tend to work harden rapidly. While this does not
alter the general methods used for cutting, machining,
forming, etc., it does affect the specifics of those
methods.
Cutting and machining the austenitic stainless
steels is readily accomplished using standard techniques
typically employed for common mild steel, with some
modifications. Their cutting behavior can be quite different
– they are tougher and tend to harden rapidly
during working. The chips produced are stringy and tough
and retain considerable ductility. Tooling should be
kept sharp and be rigidly held. Deeper cuts and slower
speeds are generally used to cut below work hardened
zones. Due to the low thermal conductivity and high
coefficient of thermal expansion inherent to the austenitic
stainless steels, heat removal and dimensional tolerances
must be considered during cutting and machining operations.
The austenitic stainless steels are readily
cold formable by standard methods such as bending, stretch
forming, roll forming, hammer forming, flaring/flanging,
spinning, drawing, and hydroforming. They work harden
readily, which is manifested by steadily increasing
amounts of force needed to continue deformation. This
results in the need to use stronger forming machines
and eventually limits the amount of deformation possible
without cracking.
A relatively narrow range of temperatures
can be used for effective hot working of Alloys 309
and 310 due to numerous environmental and metallurgical
factors. Forging should start in the temperature range
1800-2145°F (980-1120°C) and finish no cooler
than 1800°F (980°C). Working at higher temperatures
results in a fall-off of hot ductility due to environmental
and metallurgical factors, particularly the formation
of ferrite. Working at lower temperatures can cause
the formation of brittle second phases, e.g., sigma
and/or sensitization. Following forging, the workpiece
should be cooled rapidly to a black heat.
Back to top
Welding
The austenitic grades are generally considered
to be the most weldable of the stainless steels. They
can be welded using all of the common processes. This
is generally true of Alloys 309/309S and 310/310S. When
filler metal is required, matching compositions are
generally used. The elevated alloy contents of this
grade can make the weld pool sluggish. If weld pool
fluidity is a problem, filler metal containing silicon
can help (e.g., ER309Si, ER309LSi).
Alloys 309/309S and 310/310S exhibit a
relatively high coefficient of thermal expansion and
low thermal conductivity and form low levels of ferrite
in the solidifying weld metal. These factors can lead
to hot cracking. The problem can be more severe for
restrained and/or wide joints. Filler metal with a lower
alloy content (e.g., ER308) will increase the amount
of ferrite in the weld deposit and reduce the tendency
for hot cracking. The subsequent dilution of the base
metal may decrease the corrosion/heat resistance of
the weld.
The "S" grades are relatively
low in carbon. With proper weld practices, intergranular
corrosion of the heat affected zone is unlikely. Heat
tint or scale should be removed to ensure complete restoration
of corrosion resistance near the weld. Grinding or brushing
with a stainless steel brush can be used to remove the
heat tint scale. Acid pickling will also remove heat
intent. Small pieces can be treated in a bath, and larger
pieces can be locally pickled using a special paste
consisting of a mixture of nitric acid and HF or hydrochloric
acid suspended in an inert filler. A thorough water
wash should immediately follow, taking care to completely
remove all traces of pickling paste.
Back to top
Heat
Treatment/Annealing
The primary reason for annealing these alloys
is to produce a recrystalized microstructure with a
uniform grain size and for dissolving detrimental chromium
carbide precipitates. To ensure complete annealing,
pieces should be held in the range 2050-2150°F (1120-1175°C)
for approximately 30 minutes (time at temperature) per
inch of section thickness. This is a general recommendation
only – specific cases may require further investigation.
When properly annealed, these grades are primarily austenitic
at room temperature. Some small quantities of ferrite
may be present.
Oxide scale formation is inevitable during
air annealing of Alloys 309/309S and 310/310S. The scale
that forms is generally rich in chromium and relatively
adherent. The annealing scale generally must be removed
prior to further processing or service. There are two
typical methods for removing scale – mechanical
and chemical. A combination of surface blasting prior
to chemical scale removal is generally effective at
removing all but the most tightly adherent scale. Silica
sand or glass beads are a good choice for the blasting
media. Iron or steel shot can also be used, but will
lead to embedded free iron in the surface which may
then result in surface rusting or discoloration unless
the surface is subsequently pickled.
Chemical removal of scale is generally
performed with mixed nitric-hydrofluoric acids. The
proper bath makeup and process temperature combination
depends on the situation. A typical pickling bath used
consists of 5-15% HNO3 (65% initial strength) and _-3%
HF (60% initial strength) in aqueous solution. Higher
concentrations of hydrofluoric acid lead to more aggressive
scale removal. Bath temperatures generally range from
ambient to about 140°F (50°C). Higher temperatures
result in faster descaling but may attack grain boundaries
aggressively, resulting in surface grooving. Acid pickling
must be followed with a thorough water wash to remove
all traces of pickling acids. Drying should then be
used to avoid spotting and staining.
As noted, Alloys 309/309S and 310/310S
consist solely of austenite at room temperature –
they cannot be hardened through heat treatment. Higher
mechanical strengths are attainable via cold or warm
working, but these grades are generally not available
in such conditions. The higher tensile and yield strengths
obtainable through cold working not followed by full
annealing are not stable at the higher temperatures
at which these alloys are often used. Creep properties
in particular may be adversely affected by the use of
cold worked material at elevated temperatures.
Back to top |