Stainless steels represent the most diverse and complex family of all steels. The list of their applications is endless: from the harsh environments of the chemical, oil production and power generation industries to street furniture or automotive trims without forgetting most cutlery, they are used either for decorative purposes and/or for their excellent resistance to corrosion.
Stainless steels are stainless because a protective layer
spontaneously forms on their surfaces and reduces the rate of corrosion
to almost negligible levels. Under normal conditions, this layer heals
very rapidly if scratched, so that if stainless steels only
suffered from uniform corrosion, they could survive for
literally millions of years (Nature, 2002:415, Newman, p743).
It is generally agreed that stainlessness is obtained for additions of
about 12 wt% of chromium or more, although corrosion rates
continuously reduce with increasing chromium contents from 0 to this
limit.
12% Cr-steels are resitant to atmospheric corrosion but are useless in acids such as HCl or H2SO4 where they exhibit a corrosion rate even greater than plain carbon steels. As will be discussed later, corrosion resistance can be greatly enhanced above that of a basic 12% Cr steel by further addition of Cr and/or use of other alloying elements such as Ni, Mo, N etc.
Corrosion resistance is of course not the only design criterion: materials cost considerations will typically favour basic, cheaper grades (12%Cr-0.1%C) rather than heavily alloyed steels. Mechanical properties must also be taken into account, as must fabrication difficulties (machinability, deformability, weldability, etc.). The number of grades is therefore seemingly infinite, with a large number of standard compositions to which manufacturers add their proprietary variants.
These are usually divided in four or five classes on the basis of their microstructures:
to which some add precipitation hardened stainless steels, although they are themselves divided into martensitic/ferritic/etc. so that they could be included in the above categorisation.
Iron is not stable in most of the environments in which it is used. Like most non-noble metals, it does not naturally occur in its elemental form and has to be extracted from oxides. In service, the tendency is for re-formation of these oxides. Hence the rust that can be observed on most unprotected steel components.
Materials scientists and chemists often take recourse to thermodynamics to
quantify and compare the stability of different phases, oxides, etc. In
this case however, thermodynamics alone gives an erroneous representation
of the problem: most stainless steels are used in conditions in which the
dissolution of the metal is energetically favorable.
Instead, they owe their environmental resistance to the formation of a chromium oxide
film which acts as a kinetic barrier: atomic transport through this layer is so
slow, that the steel can be considered inert.
The passive film formed at the surface of stainless steels is extremelly thin (1-2 nm). Its chromium content depends on the bulk content, and in general, increases with the latter. The overall corrosion resistance is also enhanced as the chromium content is raised.
Corrosion can nevertheless occur if the passive film breaks down, locally or uniformly. This can happen by different mechanisms depending on the conditions of use. The most common types of corrosion are:
Uniform corrosion of stainless steels can occur in acidic or hot
alkaline solutions. It results in uniform loss which can easily be predicted and
allowed for. As mentionned in the introduction, uniform corrosion is very slow
when the metal is in the passive state.
General corrosion resistance is increased with increasing chromium content, but
other elements can be detrimental. In particular, sulfur in solid solution is
believed to make passivation more difficult (M. Schütze ed., Corrosion and
Environmental Degradation, Wiley-Vch, Chap 3) and therefore is
generally undesirable for good corrosion properties.
Unfortunately, sulfur makes welding considerably easier (D. T. Llewellyn,
Steels: Metallurgy and Applications, 1992, Butterworth-Heinemann) and also
improves machinability. In the case of welding, sulfur appears to modify the
surface tension of the weld pool and therefore alters its shape
significantly. Austenitic grade 316 with sulfur content lower than 0.007 wt%
tend to have a high width-to-depth ratio while higher sulfur contents lead to a
narrower, deeper weld pool
(specifying
the sulfur content of 316L
for welding).
Some of the standard grades contain a quantity of sulfur delibarately greater
than the typical 0.003 that can otherwise routinely be achieved with modern
steel-making processes (the free machining grades).
Nickel significantly improves the general corrosion resistance of stainless
steels, by promoting passivation. The austenitic stainless steels series
therefore possesses a corrosion resistance superior to that of martensitic or
ferritic stainless steels (no nickel), particularly with mineral acids.
Pitting corrosion is the result of the local destruction of the
passive film and subsequent corrosion of the steel below. It generally occurs in
chloride, halide or bromide solutions. If a fault in the passive layer or a
surface defect results in the local destruction of the former, dissolution of
the steel underneath leads to a build up of positively charged metallic ions,
which in turn causes negatively charges (e.g. chloride ions) to migrate near the
defect. Even in a neutral solution, this can cause the pH to drop locally to 2
or 3, and can prevent regeneration of the passive layer.
In the passive condition, the current density is in the scale of nanoamperes/cm2;
in the pit, however, it may be above 1A/cm2. Similarly, the concentration in
chloride ions can be thousands of times greater than that in the solution.
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The above figure illustrates the process: the anodic dissolution of the steel leads to introduction of M+ in solution, which causes migration of Cl- ions. In turn, metal chloride reacts with water following:
M+Cl- + H2O -> MOH + H+Cl-
This causes the drop of pH mentioned earlier. The cathodic reaction, on the surface near the pit follows:
O2 + 2H2O -> MOH + 4OH-
While the propagation phenomenon is well understood, the mechanism of pit initiation is still debated. The initiation of pitting has long been associated with the presence of MnS inclusions which are difficult to avoid in the steel making process. It has recently been shown that these inclusions are surrounded by a Cr depleted region which is believed to cause the initiation (Nature, 2002:415, Ryan et al, p770).
The pitting resistance of a stainless steel is affected by its composition. Increasing the Cr content, or adding Mo or N both enhance the pitting resistance, though they are not equally potent in this respect. For comparison purposes, an index is often used to represent the combined effect of these elements:
pitting index=Cr+3.3Mo+16N
where Cr, Mo and N are given in weight percent.
One obvious environment where pitting corrosion is of concern is
marine applications. AISI type 316 (an 18Cr-12Ni austenitic stainless
steel with 2-3% Mo) is often the material of choice in this case,
although the severe conditions met in offshore platforms, for example,
call for heavily alloyed steels with up to 6% Mo (for example 254SMO,
Avesta Sheffield).
Use of stainless
steels in offshore platforms.
Street furniture is another case where pitting resistance might be
relevant, particularly in colder areas where salt de-icing is common.
Sensitisation is one of the corrosion mechanisms which causes widespread problems in austenitic stainless steels, particularly in welding. This problem can be so severe as to cause grain decohesion, as shown in the picture below.
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In normal conditions, austenitic stainless steels are given a
high-temperature heat-treatment, often called solution-treatment, which,
as its name indicates, aims at obtaining a single f.c.c. solid solution
(austenite).
At lower temperatures however (roughly, 800 C and below), this solution is not
stable: in the basic AISI 304, the carbon content exceeds the solubility limit
in austenite. This is due to the presence of chromium, which forms stable
carbides.
In austenitic steels, the chromium carbides are M23C6 (see Sourmail, Mater. Sci. Techn. 2001:17, p1 for more details about this phase), in which M stands for Cr, Fe and possibly some Mn and Mo if present in the alloy. Because the formation of these carbides involves long-range diffusion, it can be avoided by quenching the steel after the solution-treatment.
If the steel is subsequently reheated, precipitation of M23C6 may occur. Because nucleation is considerably easier on grain boundaries, there is a very strong tendency for localised precipitation. Precipitation on other defects (twin boundaries, dislocations, inclusions..) does occur, although after longer exposure at high temperatures. Depending on the composition, M23C6 may be found on grain boundaries after only a few minutes at temperatures around 750 C. The range of temperature in which sensitisation occurs is bounded in the lower temperatures by the very slow kinetics of diffusion controlled transformations, and in the higher temperatures, by the fact that chromium depletion is less pronounced at higher temperatures. As illustrated below, the conditions in which a steel is sensitised vary with temperature and time.
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When austenitic stainless steels are welded, any metal which has been melted usually cools fast enough to prevent carbide formation. However, in the metal adjacent to the fusion zone, the so-called heat-affected zone (HAZ), the temperature changes might be such that sensitisation occurs.
Various solutions can be implemented to avoid sensitisation:
The first one is obviously to reduce the carbon content of the material so as to limit the precipitation of M23C6. This approach defines the AISI L grades, such as 304L and 316L, which have lower carbon content than their standard counterparts. For both these steels, the maximum acceptable carbon content is reduced to 0.03 wt% (from 0.08 for the corresponding standard grades).
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Another `similar' solution consists in introducing carbide formers which
have an even greater affinity for carbon than chromium. These include Nb, Ti, V
or Ta. Steels containing these elements (or a combination) are said to be
stabilised (with regard to grain boundary precipitation of M23C6).
Grades 321 (Ti stabilised) and 347 (Nb stabilised) represent the most common
stabilised austenitic stainless steels. In welding applications, grade 321 is
not used as a filler metal because titanium does not transfer well accross a
high temperature arc. 347 is therefore used as a filler metal when joining
components made out of 321 or 347 (the latter being seldom used as parent
material).
To obtain stabilisation, it is not sufficient to add Nb or Ti. A stabilisation
heat-treatment must be performed to ensure formation of TiC or NbC. This is
usually performed by maintaining the steel for 1 or more hours at temperatures
around 900 C. At lower temperatures, M23C6 may form faster than TiC or NbC.
In some cases, a solution-treatment can be given to dissolve carbides which may have formed on grain boundaries, after welding for example.
A variety of other factors impact on the problem, such as grain size and the nature of the grain boundary. It has been shown that sensitisation can be avoided by grain boundary engineering (Shimada et al, Acta Mater., 2002:50, p2331), in which a thermomechanical treatment produces a microstructure with mostly low angle grain boundaries. The latters have a lower energy and are therefore less potent nucleation sites for M23C6. On the other hand, it appears that increasing the orientation randomness of the grain boundaries beyond a treshold can also lead to a reduction in sensitisation (Wasnik et al, Acta Mater. 2002:50, p4587). In this study however, it is possible that the cause is a grain size reduction rather than a change in the nature of the grain boundaries.
As explained earlier, sensitisation is caused by the formation of chromium carbides on grain boundaries. The Cr-rich precipitate draws chromium from the adjacent matrix, which results in the formation of a chromium depleted zone. If the chromium content is below 11-12% in this area, the steel is said to be sensitised.
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This short description of the problem hides most of its interesting
complexity. The first difficulty occurs if one considers the phase diagram
austenite/M23C6. This predicts that the chromium content of the austenite in
equilibrium with M23C6 is only slightly lower than the bulk composition, which
makes sense if one remembers that M23C6 seldom form more than 1% volume fraction.
The reason why the chromium content locally drops to much lower values is to be
found in the dynamics of the fluxes of elements diffusing towards the
precipitates. This problem is reviewed in details in
C. H. Too,
MPhil thesis, 2002 and
Sourmail et
al, ISIJ Int. 2003:43, p1814.
Stress corrosion cracking is an important phenomenon often related to
pitting corrosion. It is the result of a combination of corrosion
and applied stress. Under these conditions, a crack can progress alternatively through
dissolution of its tip or mechanical propagation. Stress corrosion cracking is
particularly dangerous because it may take thousands of hours for a crack to
nucleate, but considerably less for it to propagate. Dramatic examples of
catastrophic corrosion by SCC include the collapse of swimming pools ceilings in
1985 (Switzerland,
12 fatalities), and
2001,
(Netherland, no fatalities),
both attributed to SCC of type 304 or 316 austenitic stainless steels. It has
been suggested that 6%Mo austenitic stainless steels should be used in these
environments.
NPL's
guide to Stress Corrosion Cracking
As mentioned in the introduction, the designation stainless steel conventionally implies little more than a 12% Cr content. Most of the stainless steels are based on the Fe-Cr-C and Fe-Cr-Ni-C systems, but other alloying elements are also important.
Iron and its alloys can exist in two crystallographic forms (body centred or
face-centred cubic). In pure iron, the f.c.c. structure exists between 910 and
1400 C, the b.c.c. structure below and above this interval (up to the melting
temperature of 1539 C).
The importance of this phase-transformation in the metallurgy of steels cannot
be overestimated. This transformation allow for a wide range of microstructures
to be achieved by controlled heat-treatment. Mechanical properties are
essentially related to microstructure, and can therefore be obtained
in an extraordinarily large range of strength, toughness, etc..
Stainless steels are routinely produced with strengths from 100 MPa to largely
more than 1GPa.
Knowledge of the relative stability of the b.c.c. and f.c.c. structures of iron alloys is therefore of prime concern. The history of stainless steels started with a martensitic grade (12%Cr-0.1%C) in Sheffield, UK and the austenitic 18%Cr-8%Cr in Germany ( more about the history of stainless steels). For this reason, and also because they are most often the major alloying elements, Cr and Ni have long been used as reference to quantify the influence of alloying elements on the b.c.c.<->f.c.c. phase transition: chromium additions tend to stabilise the b.c.c. phase, while nickel additions stabilise the f.c.c. one.
Without carbon, the limit beyond which austenite no longer forms is
about 13.5 wt%. However, additions of carbon stabilise the austenite and
therefore increase this limit.
Other alloying elements also affect the stability of austenite/ferrite in one
direction or another. This has led to their classification as
α-stabilisers or γ-stabilisers. The concept of Cr-equivalent
(for α-stabilisers) and Ni-equivalent (for γ-stabilisers) is widely
used in conjunction with the Schaeffler diagram to quantify their roles:
Cr equivalent = (Cr) + 2(Si) + 1.5(Mo) + 5(V) + 5.5(Al) + 1.75(Nb) + 1.5(Ti) + 0.75(W)
Ni equivalent = (Ni) + (Co) + 0.5(Mn) + 0.3(Cu) + 25(N) + 30(C)
All in weight percent.
Modern thermodynamics calculation tools such as Thermocalc or MTDATA based on the CALPHAD method allow more rigourous determination of equilibrium phase diagrams in multicomponent systems.
In most grades of stainless steels, alloying elements are present in
quantities sufficient to cause precipitation of second phases. Most often the
stable carbides, nitrides or intermetallics are of little relevance as they tend
to follow a long and complex precipitation sequence.
This is because the kinetics of precipitation are largely controlled by
nucleation, and nucleation itself is not necessarily easier for the most stable
precipitates.
From the Fe-Cr diagram presented earlier, it appears that typical martensitic
steels should exhibit ferrite and M23C6 in equilibrium at 600 C (for
example). In practice, this carbide is only found after relatively long
ageing. Intermediate phases are, in order, cementite, M2X and M7C3 to finally
obtain M23C6.
These sequences are far more complex in heavily alloyed ferritic or austenitic
stainless steels such as those used in the power generation
industry. Considerable research work is being devoted to predicting
quantitatively the precipitation sequences in such alloys. This is
mainly because their life expectancy (about 30 years) vastly exceeds
the length of laboratory tests.
Most stainless steels have a high hardenability, meaning that
reconstructive austenite to (ferrite + carbides) transformation is
unlikely to happen unless the steel is cooled particularly slowly.
The most important features of these alloys are therefore the
martensite start (Ms) and finish temperatures (Mf). For martensitic
steels, the range [Mf-Ms] should be above the room temperature to
ensure fully martensitic structure. On the contrary, the [Ms-Mf] range
of austenitic stainless steels is often well below 0 C, which is why
austenitic steels are used in cryogenic applications. Cold work can
cause martensitic transformation to an extent with depends on the
deformation and on the alloying composition. Heavily alloyed
austenitic steels with up to 20% Cr and 25% Ni are fully stable.
The mechanisms of martensite nucleation are reasonably well understood and there are a number of models which predicts the Ms temperature with an acceptable accuracy.
On the basis of their main microstructural features, grades of stainless steels are typically divided into four categories:
These steels still undergo the b.c.c./f.c.c. transformation of iron, although
the range of austenite stability is reduced.
As for conventional steels, mechanical properties can be
considerably altered by heat-treatments. Typical heat-treatments consist of
austenitisation at a temperature suitable for dissolution of carbides. Stainless
steels have a high hardenability, that is to say, reconstructive transformations
are considerably slowed by the presence of Cr, so that a fully martensitic
structure can be achieved without a severe quench. Oil or water quenching are
nevertheless used with large sections so as to ensure martensite formation
throughout.
Typical compositions cover 12 to 18 Cr and 0.1 to 1.2 C (wt%). As with other martensitic steels, a balance must be sought between hardness and toughness. An untempered martensitic structure typically has high hardness/yield strength but a low toughness and ductility (although the exact values depend on the carbon content). In many conditions, these are used after a tempering treatment between 600 and 750 C, which result in a lower hardness but improved toughness.
In some applications such as cutlery, surgical intruments etc., high strength is desirable and toughness/ductility of little concern. A lower temperature tempering is then used to retain most of the strength. AISI type 420 (0.15-0.4C, 1.0Mn, 1.0Si, 0.04P, 0.03S, 12-14Cr all max wt%) is a typical composition for such applications. Its proof strength in quenched and tempered condition can be in excess of 1.2 GPa. For type 440C tempered at 300 C, the proof strength can reach about 2 GPa.
The table below shows the composition and typical use of AISI standard martensitic grades:
| AISI grade | C | Mn | Si | Cr | Ni | Mo | P | S | Comments/Applications |
|---|---|---|---|---|---|---|---|---|---|
| 410 | 0.15 | 1.0 | 0.5 | 11.5-13.0 | - | - | 0.04 | 0.03 | The basic composition. Used for cutlery, steam and gas turbine blades and buckets, bushings..More. |
| 416 | 0.15 | 1.25 | 1.0 | 12.0-14.0 | - | 0.60 | 0.04 | 0.15 | Addition of sulphur for machinability, used for screws, gears etc. 416 Se replaces suplhur by selenium. More |
| 420 | 0.15-0.40 | 1.0 | 1.0 | 12.0-14.0 | - | - | 0.04 | 0.03 | Dental and surgical instruments, cutlery.. More |
| 431 | 0.20 | 1.0 | 1.0 | 15.0-17.0 | - | 1.25-2.0 | 0.04 | 0.03 | Enhanced corrosion resistance, high strength. More |
| 440A | 0.60-0.75 | 1.0 | 1.0 | 16.0-18.0 | - | 0.75 | 0.04 | 0.03 | Ball bearings and races, gage blocks, molds and dies, cutlery, More |
| 440B | 0.75-0.95 | 1.0 | 1.0 | 16.0-18.0 | - | 0.75 | 0.04 | 0.03 | As 440A, higher hardness |
| 440C | 0.95-1.20 | 1.0 | 1.0 | 16.0-18.0 | - | 0.75 | 0.04 | 0.03 | As 440B, higher hardness |
In additions to the standard grades, a large number of alloyed martensitic
stainless steels have been developed for moderately high temperature
applications. Most common additions include Mo, V and Nb. These lead to a
complex precipitation sequence. A small amount (up to 2 wt%) of Ni is added
which improves the toughness.
The 12Cr-Mo-V-Nb steels are used in the power generation industry, for steam
turbine blades operating at temperatures around 600 C. Current research focusses
on achieving service temperatures of 630-650 C under a stress of 30 MPa.
Ferritic stainless steels: contain typically more chromium and/or less carbon than the martensitic grades. Both changes act towards stabilisation of ferrite against austenite so that ferrite is stable at all temperatures. Therefore, ferritic stainless steels cannot be hardened by heat-treatments as is the case of martensitic ones. They exhibit lower strength but higher ductility/toughness. Typical application may include appliances, automotive and architectural trim (i.e. decorative purposes), as the cheapest stainless steels are found in this family (aisi 409).
| AISI grade | C | Mn | Si | Cr | Mo | P | S | Comments/Applications |
|---|---|---|---|---|---|---|---|---|
| 405 | 0.08 | 1.0 | 1.0 | 11.5-14.5 | - | 0.04 | 0.03 | 0.1-0.3 Al |
| 409 | 0.08 | 1.0 | 1.0 | 10.5-11.75 | - | 0.045 | 0.045 | (6xC) Ti min |
| 429 | 0.12 | 1.0 | 1.0 | 14.0-16.0 | - | 0.04 | 0.03 | |
| 430 | 0.12 | 1.0 | 1.0 | 16.0-18.0 | - | 0.04 | 0.03 | |
| 446 | 0.20 | 1.5 | 1.0 | 23.0-27.0 | - | 0.04 | 0.03 | 0.25 N |
High chromium ferritic stainless steels such as 446 are sensible to the
so-called '475 C embrittlement', which is caused by the decomposition of the
Fe-Cr solid solution in two phases, Fe and Cr-rich respectively. Around 475 C and
below, and for Cr contents greater than about 25 wt%, this decomposition is
spinodal and typically exhibits wavelength below 10 nm. As the decomposition
occurs, a continuous increase of hardness is observed: for example, the hardness
of an Fe-28Cr steel can increase by more than 300 Hv over an exposure 10,000 at
450 C (Ishikawa et al., Mater. Trans. JIM, 36:1995, p16-22). This results
in a severe drop of impact toughness and ductility.
Addition of Ni appear to accelerate the spinodal decomposition and raise the
maximum temperature at which it is observed. When post-weld heat-treatment is
not possible, welding of ferritic stainless steels is usually done with a metal
filler containing Ni, and there is therefore the possibility of weld
embrittlement.
Austenitic stainless steels:
these stainless steels owe their name to their f.c.c. crystallographic
structure. Typical compositions in the early 20th century were 18Cr-8Ni. The
austenite in these alloys was only stable because of the relatively large carbon
content, and modern equivalent usually contain up to 10.5 Ni.
These steels are often in metastable conditions at room temperature or below,
and while the reconstructive formation of ferrite is not of concern, the
formation of martensite can be. Most grades have a martensite start temperature
(Ms) well below 0 C. However, cold work can result in formation of martensite at
temperatures higher than Ms (this result in the sample becoming magnetic, while
a fully austenitic structure is not). The impact of deformation on the stability
of the material is conveniently quantified by the Md,30 temperature,
the temperature at which the structure is 50% martensitic for 30% deformation.
The presence of nickel improves considerably the corrosion
resistance when compared to the martensitic and ferritic grades.
AISI type 304 is the basic 18/8 austenitic stainless steel, so widely used that
it accounts for about 50% of all stainless steel production. Other standard grades
have different preferred applications; for example, type 316 which contains up
to 3 % Mo, offers an improved corrosion resistance, in particular, improved
pitting corrosion resistance, which makes it a material of choice for many
marine applications (off-shore platforms etc..), but also for coastal
environments
(more on stainless steels in
architecture).
In severe conditions however, 316 is not sufficient and special steels such
as 254 SMO are used (example:
steels used in offshore
oil platforms), which contain up to 6% Mo.
| AISI grade | C max. | Si max. | Mn max. | Cr | Ni | Mo | Ti | Nb | Al | V |
|---|---|---|---|---|---|---|---|---|---|---|
| 301 | 0.15 | 1.00 | 2.00 | 16-18 | 6-8 | |||||
| 302 | 0.15 | 1.00 | 2.00 | 17-19 | 8-10 | |||||
| 304 | 0.08 | 1.00 | 2.00 | 17.5-20 | 8-10.5 | |||||
| 310 | 0.25 | 1.50 | 2.00 | 24-26 | 19-22 | |||||
| 316 | 0.08 | 1.00 | 2.00 | 16-18 | 10-14 | 2.0-3.0 | 321 | 0.08 | 1.00 | 2.00 | 17-19 | 9-12 | 5 x %C min. |
| 347 | 0.08 | 1.00 | 2.00 | 17-19 | 9-13 | 10 x %C min. | ||||
| E 1250 | 0.1 | 0.5 | 6.0 | 15.0 | 10.0 | 0.25 | ||||
| 20/25-Nb | 0.05 | 1.0 | 1.0 | 20.0 | 25.0 | 0.7 | ||||
| A 286 | 0.05 | 1.0 | 1.0 | 15.0 | 26.0 | 1.2 | ~1.9 | ~0.18 | ~0.25 | |
| 254SMO | 0.02 | 0.8 | 1.0 | 18.5-20.5 | 17.5-18.5 | 6-6.5 | ~1.9 | ~0.18 | ~0.25 |
Duplex stainless steels: duplex stainless steel typically contain 50% austenite and 50% ferrite. This confers them properties intermediate between the two types of steels:
a typical strength about twice that of austenitic grades, but lower than martensitic grades,
a better toughness than ferritic stainless steels, but lower than austenitics,
because of the high chromium content of the standard grades, the corrosion resistance is superior to that of the standard 304 and 316.
Only one duplex steel has an AISI designation (329) so that ASTM numbers are more currently used to reffer to different grades. The archetypal stainless steel, type 2205, contains 22-23Cr, 4.5-6.5Ni and 3-3.5Mo. This grade represents 80% of all duplex stainless steel use.
Duplex stainless steels suffer from the 475 C embrittlement described earlier for ferritic stainless steels and are therefore mostly confined to applications below 300 C.
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