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Table of Contents
Stainless Steels
The generic term stainless steel covers a multitude of standard compositions and
variations of these compositions often bearing company trade names. Compositions vary
from fairly simple alloys containing iron with about 11 wt% chromium and little
else beyond impurities to complex alloys containing 30 wt% chromium, substantial
quantities of nickel, and a number of other elements including molybdenum, niobium
(columbium), and nitrogen specifically added to improve properties. All possess
two characteristics, the iron content is at least 50 wt% of the alloy and
the chromium content tends to be greater than 11 wt%. If the iron
content falls below 50 wt%, the alloy is often no longer considered
stainless steel but becomes classified as an alloy of the major component (e.g.
nickel-based alloy).
All of the stainless steels can be classified into six major categories. These are
- austenitic stainless steels
- manganese-substituted austenitic stainless steels
- ferritic stainless steels
- martensitic stainless steels
- duplex stainless steels
- precipitation-hardening stainless steels
Many of the common composition ranges of wrought stainless
steel are classified as standard AISI (American Iron and Steel Institute) types.
The AISI number contains three digits "XXX" and designates a specified composition.
This specification is the most common. Unfortunately, in no case does the system
offer a rational clue as to the composition. The only clues given are that in the
AISI designation system the austenitic alloys all begin with the number 3 (3XX),
the manganese-substituted austenitic stainless steels begin with a 2 (2XX),
both ferritic and martensitic classes begin with a 4 (4XX),
and the lowest numbers in the martensitic class have a lower carbon content.
Some martensitic alloys begin with a 5 (5XX) but their use is not common.
Precipitation hardening steels begin with a 6 (6XX) but are often written
as a trade designation which may appear as "XX-X PH". Sometimes, the alloys
in all of the above classes will have an AISI designation of "XM" followed by
one or two digits instead of the classification shown above. Specialty stainless
steels (for example 904L and alloy 20) which contain high alloy content
(often higher nickel, chromium, and molybdenum levels) for corrosion resistance
are not part of this tutorial.
The most comprehensive numbering system to use is the UNS (Unified Numbering System).
In this system, each stainless steels composition is uniquely described by one
letter and 5 numbers, for example SXXXXX. The relationship between the UNS and
the more common AISI system is that the first three digits of the UNS number are
the three digits of the AISI number. The second two digits usually designate
variations in composition. For example, 316 stainless steel (AISI) is S31600
(UNS). The low carbon grade of 316 stainless steel, 316L (AISI) is S31603 (UNS).
In this case the "L" in the AISI designation stands for "low carbon", not lead.
Low carbon grades of 304, 316, 317, etc. are specified as 304L, 316L, and 317L, etc.
in the AISI classification system.
Society of Automotive Engineers (SAE), military, and federal classifications also
exist that tend to standardize on mechanical properties in addition to composition.
All stainless steels have relatively high ultimate
tensile strength, high work-hardening rate (especially for the austenitic stainless
alloys), and high ductility. These factors explain the tendency for stainless
steels to be prone to form a built-up-edge on the tool. The chips exert a high
pressure on the nose of the tool at the cutting edge which when combined with
the higher temperatures at the chip-tool interface can cause pressure welding
of the chip to the tool. The low thermal conductivity contributes to heat build-up.
Cutting fluids are essential for maintaining high production. Cutting speeds lower
than for steel may be required for non-free machining stainless steel. Their general
corrosion resistance tends to be far better than carbon and low alloy steels.
Austentic Stainless Steels (3XX or S3XXXX)
Some General Machining Characteristics
The austenitic stainless steels cannot be hardened to form martensite by quenching.
Instead, cold working of the alloy can make them significantly stronger and harder.
All of the austenitic grades can be the most difficult to machine relative to other
stainless steels. They tend to have a higher work hardening rate than do other
stainless steel alloys. This attribute can make machining more difficult by creating
a hard surface region through which the cutting edge must penetrate especially as
the cutting process proceeds. Some of the problems that can occur are (1) tools
will often run hotter creating a tendency to form a built-up edge, (2) chips can be
stringier and tangle, (3) chatter will be more likely if the tool rigidity is
inadequate, and (4) cut surfaces will become work hardened and more difficult
to machine if cutting is interrupted or if the feed rate is too low.
Classification
The more common, non-specialty grades of austenitic stainless steels have a
first numeral of "3", whether AISI (XXX) or UNS number SXXXXX. The parent of
the austenitic class is AISI 302. Since these alloys can be strengthened by
work hardening, they tend to be used in structural applications where some
corrosion resistance is required. The following table shows alloy numbers
(AISI designations and UNS numbers), compositions, and the characteristics which tend
to define them in classes. Only the more common members are included.
| Alloy Designation |
Major Consituents |
Alloy Classification |
302 S30200 |
17-19 wt% chromium 8-10 wt% nickel |
Basic 18-8 grade of stainless steel 302B (S30205) has silicon for scaling resistance |
304 S30400 |
18-20 wt% chromium 8-10 wt% nickel |
Higher corrosion resistance than 302ss - more limited than 316ss |
301 S30100 |
16-18 wt% chromium 6-8 wt% nickel |
The unstable grade of stainless steel |
316 S31600 |
16-18 wt% chromium 10-14 wt% nickel 2-3 wt% molybdenum |
More highly corrosion resistant molybendum-containing stainless steel |
317 S31700 |
18-20 wt% chromium 11-15 wt% nickel 3-4 wt% molybdenum |
More highly corrosion resistant molybendum-containing stainless steel |
321 S32100 |
17-19 wt% chromium 9-12 wt% nickel titanium wt% = 5x carbon wt% |
Stabilized grade of stainless steel |
347 S34700 |
17-19 wt% chromium 9-13 wt% nickel niobium+tantalum wt% = 5x carbon wt% |
Stabilized grade of stainless steel |
304L S30403 |
18-20 wt% chromium 8-12 wt% nickel <0.03 wt% carbon |
Extra low carbon grade of stainless steel |
316L S31603 |
16-18 wt% chromium 10-14 wt% nickel 2-3 wt% molybdenum <0.03 wt% carbon |
Extra low carbon grade of stainless steel |
308 S30800 |
19-21 wt% chromium 10-12 wt% nickel
|
Oxidation resistant grade of stainless steel |
309 S30900 |
22-24 wt% chromium 12-15 wt% nickel
|
Oxidation resistant grade of stainless steel
A low carbon version (S30908) exists |
310 S31000 |
24-26 wt% chromium 19-22 wt% nickel
|
Oxidation resistant grade of stainless steel
A low carbon version (S31008) exists |
303 S30300 |
17-19 wt% chromium 8-10 wt% nickel 0.6 wt% molybdenum(?) >0.15 wt% sulfur |
Free machining grade containing increased sulfur |
303Se S30323 |
17-19 wt% chromium 8-10 wt% nickel >0.15 wt% selenium |
Free machining grade containing increased sulfur |
- Basic 18-8 alloys are used as structural materials for more mundane applications
in appliances and architecture, as materials of construction in nuclear reactors
(304), for handling less corrosive environments, and for cryogenic applications.
This grade shows some corrosion resistance. AISI 304 has better corrosion resistance
than does AISI 302.
- Metastable 301 is used in structural applications such as rapid transit and
railroad cars because of the high strength that can be achieved. This alloy tends
to have very modest corrosion resistance relative to other 3XX alloys.
It has a high rate of workability and will partially transform into martensite
upon cold working for increased strength.
- High corrosion resistant stainless steels AISI 316 and AISI 317 are used in more
severe applications as materials of construction for process and other equipment
because of their higher resistance to pitting and crevice corrosion. The presence
of molybdenum makes AISI 316 more corrosion resistant. It is a workhorse alloy.
The increase in molybdenum in AISI 317 over AISI 316 makes this alloy somewhat
more corrosion resistant than AISI 316.
- Stabilized stainless steels AISI 321 and AISI 347 are used in applications similar
to those of AISI 304. They have much less reduced susceptibility to sensitization
(chromium-carbide formation) and subsequent intergranular attack. Titanium in
AISI 321 and niobium plus tantalum in AISI 347 prevent service conditions,
welding, or other fabrication procedures from forming chromium carbides which
leads to intergranular attack.
- Extra-low-carbon stainless steels AISI 304L and AISI 316L are used in the same
applications as AISI 304 and AISI 316 respectively. The "L" designates the low carbon
content. These low carbon levels mean that the alloys have reduced susceptibility
to sensitization (chromium-carbide formation) and subsequent intergranular attack.
The low carbon limit prevents service conditions, welding or other fabrication
procedures from forming chromium carbide which leads to intergranular attack.
There are modified versions AISI 304LN and AISI 316LN which contain nitrogen (<0.18 wt%)
to overcome the decrease in yield strength created by the decrease in carbon.
- Oxidation resistant stainless steels AISI 302B, AISI 308, AISI 309, AISI 310,
and AISI 314 are used as
materials of construction in high temperature applications. Alloys AISI 302b and AISI 314
contain 2 to 3 wt% silicon and 1.5 to 3 wt% silicon respectively.
- Free-machining stainless steels AISI 303 and AISI 303Se are fabricated only in bar and
rod forms and are used primarily in mass-production operations performed on screw
machines. The selenium version is used in heavy sections. The sulfur version is
more common. Corrosion resistance is not quite as good as for AISI 304. Other
properties such as ductility, toughness, and cold workability can be degraded.
The above classifications are complicated by overlapping effects. For example, a low
carbon content alloy (the XXXL grade, e.g. 316L) to reduce sensitization also reduces
susceptibility to work hardening. The range in allowable alloy content can cause
the high end of one grade to extend into the low end of another.
Manganese Substituted Stainless Steels (2XX or S2XXXX)
The AISI 200 series of stainless steels (S2XXXX) was developed during the 1930’s.
These alloys were used during the Korean War to preserve nickel. About 4 wt% of
the nickel is replaced by manganese with small (<0.25 wt%) nitrogen for strength.
The alloys are austenitic. AISI 201 (16-18 wt% chromium, 3.5-5.5 wt% nickel,
5.5-7.5 wt% manganese) and AISI 202 (17-19 wt% chromium, 4-6 wt% nickel, and
7.5-10 wt% manganese) are common grades. These grades may be a bit easier to
machine than their 3XX counterparts because of the addition of manganese.
There are several additional alloys that carry UNS numbers such as UNS20300 but
are not listed with an AISI designation.
A number of stainless steel alloys in this classification have the trade name "Nitronic".
These alloys tend to have higher strength and good wear resistance. Some examples
are Nitronic 50 (21.2 wt% chromium, 12.5 wt% nickel, 2.5 wt% molybdenum,
and 5 wt% manganese) with corrosion resistance better than AISI 316 and
Nitronic 60 (17.0 wt% chromium, 8.5 wt% nickel, 4 wt% silicon, and 8 wt% chromium)
with excellent wear resistance.
Ferritic Stainless Steels (4XX or S4XXXX)
As a whole, ferritic alloys tend to be the easiest of the stainless steel alloys to
machine. They will not harden when heated to elevated temperatures and quenched because
ferrite and not martensite form when cooled. Carbon contents tend to be low, usually
below 0.15 wt% except for AISI 442 and AISI 446 which have nominal contents of 0.20 wt%.
The lower chromium ferritic alloys such as AISI 405 and AISI 430 are generally easier
to machine than other non free machining alloys. A number of the alloys have free
machining versions, for example AISI 430F (additional sulfur) and AISI 430FSe
(additional sulfur and selenium) are free machining versions of AISI 430.
Increasing the hardness level of any of these alloys tends to decrease their relative
machinability but not to the point that they cannot be machined relatively easily
for stainless steel.
Classification
The Ferritic stainless steels all have the number "4" as the first numeral whether
AISI (XXX) or UNS number UNS LXXXXX (L = letter, X = digit). All of these
alloys contain little to no nickel meaning that the austenite phase is not
stabilized at lower temperatures. Not all AISI 4XX stainless steels are ferritic
as martensitic stainless steels share the "4". Those alloys that are ferritic cannot,
as a rule, be strengthened by heat treatment. The three standard grades are
classified by chromium content as shown in the following table. In addition,
a number of specialized grades exist, a couple of the more common of which are included
in the table. When in doubt, the UNS number (letter followed by five digits) will
uniquely identify the alloy.
| Alloy Designation |
Major Consituents |
Alloy Classification |
405 S40500 |
11.5-14.5 wt% chromium 0.1-0.3 wt% aluminum |
11 to 14 wt% chromium |
409 S40900 |
10.5-11.75 wt% chromium Titanium wt% = 6x%Carbon wt% |
11 to 14 wt% chromium (small amount of nickel) |
430 S43000 |
16-18 wt% chromium |
17-19 wt% chromium |
430F S43020 |
16-18 wt% chromium |
17-19 wt% chromium, ≤0.6 wt% molybdenum |
430Se S43023 |
16-18 wt% chromium ≥0.15 wt% selenium |
17-19 wt% chromium |
434 S43400 |
16-18 wt% chromium 0.75-1.25 wt% molybdenum |
17-19 wt% chromium |
436 S43600 |
16-18 wt% chromium 0.75-1.25 wt% molydenum niobium wt% = 5x carbon wt% - 0.7 wt% |
17-19 wt% chromium |
442 S44200 |
18-23 wt% chromium 8-12 wt% nickel <0.03 wt% carbon |
22-27 wt% chromium |
446 S44600 |
23-27 wt% chromium 0.25 wt% nitrogen
|
22-27 wt% chromium |
29-4C S44735 |
28-30 wt% chromium 3.5-4.2 wt% molybdenum 1.0 wt% nickel |
Non-standard ferritic stainless steel |
29-4-2 S44800 |
28-30 wt% chromium 3.5-4.2 wt% molybdenum 2-2.5 wt% nickel |
Non-standard ferritic stainless steel |
- 11-14 wt% chromium ferritic stainless steels have marginal corrosion resistance
and are used primarily as structural materials. AISI 405 is used in steam turbines a
nd petroleum refineries. AISI 409 is used in light gauges in sheet and strip form.
It has found use for exhaust equipment in the automotive industry. Newer forms of
this alloy designation have small amounts of aluminum to aid in high temperature
oxidation resistance. The lower corrosion resistance afforded by these alloys means
that some care is required to make sure that carbide from tooling is not left on the
workpiece, especially in confined areas. Contact with aqueous solutions could create
a galvanic cell between the carbide and the steel causing corrosion. This corrosion
could be mistakenly attributed to the fluid.
- 17-19 wt% chromium ferritic stainless steels have better corrosion resistance
that those above. Types AISI 430, AISI 434, and AISI 436 are examples. These alloys have been
used for automotive trim, household appliances, and cookware, all of which have a
combined decorative and functional application.
- 22-27 wt% chromium ferritic stainless steels are represented by two alloys,
AISI 442 and AISI 446 but only AISI 446 is commonly encountered. The alloys have
excellent oxidation resistance and are used primarily at high temperatures.
- Newer ferritic stainless steels have been developed in the last 20 years.
Two examples of such alloys are 29-4C and 29-4-2. A number of additional alloys are
listed. All of these alloys have higher amounts of chromium, often some molybdenum, and
little or no nickel. They were developed as corrosion resistant materials of
construction for process equipment for use in applications requiring resistance
to chloride stress corrosion cracking. Many additional examples can be found in
Woldman's "Engineering Alloys"
Martensitic Stainless Steels (4XX or S4XXXX )
Martensitic stainless steels have high hardenability because of their alloy content.
That is, a greater thickness will be hardened relative to plain carbon steels
under given quenching conditions. When they are heated to high temperatures and
quenched they will form a martensite phase which is extremely hard. The carbon
content varies from about 0.15 wt% to about 1.2 wt% depending on alloy. Annealed
hardness increases with increasing carbon level. Machinability decreases as
the carbon content increases. The annealed low carbon, straight chromium grades
(for example AISI 403 and AISI 410) are generally easier to machine than other
non-free machining alloys. The alloys are often machined in the annealed condition.
Relative to other stainless steels, the machinability of martensitic alloys is
generally between ferritic (easier) and austenitic (more difficult). Within the
class, machinability difficulty increases in the order AISI 410, AISI 420, AISI 440
in which the nominal carbon level increases from 0.15 wt% in AISI 410 to about
0.20 wt% in AISI 420 to a range of 0.95 wt% to 1.2 wt% in AISI 440C. Differences
in machinability between free machining and non free machining versions become less
as the carbon level increases. The reason is that abrasive chromium carbide tends
to form at the higher carbon levels. If the alloy contains nickel, it tends to be
harder to machine than does its non-nickel counterpart.
Classification
Martensitic stainless steels can be placed into two groups which are associated
with the mechanical properties, low carbon alloys with maximum hardness of about
45 on the Rockwell C scale and higher carbon alloys which can be hardened to 60
on the Rockwell C scale. For simplicity, the alloys can be classified as falling
on one side or the other of an 0.15 wt% carbon level. One other grade classification
has been established, one that contains the nickel-bearing martensitic alloys.
All of the alloys carry the AISI 4XX designation (UNS S4XXXX) just like the ferritic alloys.
The "XX" portion of the numbers is different. The following table lists some of
the most common grades.
| Alloy Designation |
Major Consituents |
Alloy Classification |
403 S40300 |
11.5-13.5 wt% chromium 0.5 wt% silicon |
low carbon grade (0.15 wt%) |
410 S41000 |
11.5-13.5 wt% chromium 1 wt% silicon |
low carbon grade (0.15 wt%) |
416 S41600 |
12-14 wt% chromium ≥0.15 wt% sulfur |
low carbon grade (0.15 wt%) - free machining version |
416Se S41623 |
12-14 wt% chromium ≥0.15 wt% sulfur |
low carbon grade (0.15 wt%) - free machining version |
414Se S41400 |
11.5-13.5 wt% chromium 1.25-2.5 wt% nickel |
low carbon (0.15-0.25 wt%)-nickel containing grade |
422 S42200 |
11-13 wt% chromium 0.5-1.0 wt% nickel (additional constituents) |
low carbon (0.15-0.25 wt%)-nickel containing grade |
431 S43100 |
15-17 wt% chromium 1.25-2.5 wt% nickel |
low carbon (0.15-0.25 wt%)-nickel containing grade |
420 S42000 |
12-14 wt% chromium |
high carbon (≥0.15-1.2 wt%) grade (no nickel) |
420F S42020 |
12-14 wt% chromium <0.6 wt% molybdenum |
high carbon (≥0.15-1.2 wt%) grade (no nickel) |
440A S44002 |
16-18 wt% chromium 0.75 wt% molybdenum |
high carbon (0.60-0.75 wt%) grade (no nickel) |
440B S44003 |
16-18 wt% chromium 0.75 wt% molybdenum |
high carbon high carbon (0.75-0.95 wt%) grade (no nickel) |
440C S44004 |
16-18 wt% chromium 0.75 wt% molybdenum |
high carbon high carbon (0.95-1.20 wt%) grade (no nickel) |
- Low carbon grades (AISI 403, AISI 410, and AISI 416) are used in such applications as turbine
blades, valves, and fittings in which extended periods are required at elevated
temperature. They are often used at temperatures up to about 550oC
(1000oF) if adequately tempered. Having lower chromium levels, they
are only moderately resistant to corrosion.
- Nickel-bearing low carbon grades (AISI 414, AISI 422, and AISI 431) have mechanical properties
and responses to heat treatment similar to the above grade. The presence of nickel
serves to improve the toughness of AISI 414 and AISI 431 and to restore proper phase
balance to produce an austenitic phase at high temperature. AISI 422 is used
extensively in high temperature applications. The addition of nickel allows for
the lower chromium containing alloys to be used in higher temperature service.
- High carbon grades (AISI 420, AISI 420F, and AISI 440A, B, or C) are usually used in the hardened
condition. One problem with these alloys is that strength, hardness, toughness,
and corrosion resistance vary more widely with tempering temperature than those
above meaning that the history of the material plays a role in observed properties.
For example, AISI 440 is used where high hardness and wear resistance is required
but providing such properties might be done at the expense of corrosion resistance
and toughness.
Duplex Stainless Steels
Duplex stainless steels contain a mixture of ferrite and austenite crystallites.
They have good ductility and toughness along with usually good corrosion resistance.
Strength can be increased by cold working. Hardness is often comparable to austenitic
alloys containing nitrogen. Machinability is somewhat limited by their high annealed
strength level. In terms of tool life, these alloys tend to be somewhat more
machinable than stainless steel alloys hardened by the addition of nitrogen but
somewhat less machinable than austenitic alloys of normal composition. No enhanced
machining version of duplex stainless steel alloys exists.
Classification
This class of stainless steels has begun to find more widespread use as a material
of construction in various process industries because of resistance to chloride stress
corrosion cracking. Since these alloys contain a mixture of ferrite and austenite,
they tend to have features that mimic a combination of both types of alloys. Their
resistance to stress corrosion cracking is far better than that of austenitic stainless
steels but not quite as good as that of ferritic stainless steels. Their toughness
is superior to ferritic stainless steels but inferior to austenitic stainless steels.
As mentioned above, their strength is better than austenitic stainless steels.
The chromium content of these steels tends to be at three nominal levels, 18 wt%,
22 wt%, and 25 wt%. The nickel content tends to lie between 3 wt% and 6 wt%
functioning mainly to control the microstructure. All of the alloys contain
molybdenum for resistance to localized corrosion. Some of the alloys contain
nitrogen. There is no AISI numbering system for these alloys other than AISI 329.
The alloys tend to be named by their manufacturer. Some members of this class are
specified in terms of an ASTM or ASME specification. The UNS number, if available,
uniquely
designate alloys in this class and enable easier identification. The following
table shows some of these alloys and the standard to which their characteristics
must conform. More exist and still more are continually being developed. The table
is provided to show examples.
| Alloy Designation |
Major Constituents |
329 S32900 |
23-28 wt% chromium 2.5-5 wt% nickel 1-2 wt% molybdenum |
Ferralium 255 S32550 |
24-27 wt% chromium 4.5-6.5 wt% nickel 1-2 wt% molybdenum Cu,N,W present |
3RE60 S31500 |
18-19 wt% chromium 4.25-5.25 wt% nickel 2.5-3 wt% molybdenum |
2205 S31803 |
21-23 wt% chromium 4.5-6.5 wt% nickel 2.5-3.5 wt% molybdenum |
7MO PLUS S32950 |
26-29 wt% chromium 3.5-5.2 wt% nickel 1-2.5 wt% molybdenum |
Precipitation Hardening Stainless Steels (6XX)
Precipitation hardening stainless steels achieve high strength through a relatively
low temperature treatment that can be applied after fabrication. This treatment
causes precipitation of a secondary phase in the alloy that increases hardness.
Some alloys require one treatment, others two. Machining and other fabrication
is often done between the quenching step on the unfinished part and the aging step
on the final part. These alloys do not rely on cold working or conventional heat
treatments to achieve high strength. There are three groups (1) martensitic, (2)
semi-austenitic, and (3) austenitic. The machinability depends on the type of alloy
and its hardness. Many of the martensitic precipitation hardenable stainless steels
machine in a manner comparable to AISI 304. One member of this class alloy 17-4 PH
is available in a free machining version. These alloys can also be machined in an
aged condition but such machining can be more difficult requiring lower cutting speeds.
Machinability of the semi-austenitic alloys depends on the state of the alloy.
Machinability in the annealed, austenitic state can be somewhat worse than AISI 302
which work hardens. As with the martensitic precipitation hardenable alloys,
machining difficulty increases with aged hardness level. The austenitic precipitation
hardenable alloys machine poorly and can require still slower cutting speeds.
After aging, machining ability can degrade further.
Classification
Three classes of precipitation hardening stainless steels exist (1) martensitic,
(2) semi-austenitic, and (3) austenitic. Most of the alloys are incorporated
in the AISI high-temperature, high strength classification designated as 6XX
though they are usually better known by the trade names given by their manufacturers.
When a designation appears as XX-X PH, the first "XX" is the nominal chromium
concentration in weight percent. The second "X" is the nominal nickel content, both
in weight percent. Sometimes the PH ("precipitation hardening") appears in front
of the designation. If an element appears after the name, that element is present
in the alloy at a more significant (often greater than about 2 wt%) level.
Just because an element is not named, does not mean that it is not present.
The following table shows the designation and composition of several of the
more common alloys. The table is not all-inclusive but contains some
of the more commonly encountered precipitation hardening alloys.
| Alloy Designation |
Major Consituents |
Alloy Classification |
AISI 630 17-4 PH S17400 |
16 wt% chromium 4 wt% nickel 3 wt% copper P,Si,Nb,Ta present |
Martensitic precipitation hardening stainless steel |
PH 13-8 Mo S13800 |
12.5 wt% chromium 8 wt% nickel 2.5 wt% molybdenum Si,Al present |
Martensitic precipitation hardening stainless steel |
AISI 631 17-7 PH S17700 |
17 wt% chromium 7 wt% nickel Al,Si present |
Semi-austenitic precipitation hardening stainless steel |
AISI 632 PH 15-7 Mo S15700 |
15 wt% chromium 7 wt% nickel 2.2 wt% molybdenum |
Semi-austenitic precipitation hardening stainless steel |
AISI 600 A286 |
15 wt% chromium 26 wt% nickel 1.3 wt% molybdenum Si,Al,V,Ti present |
Austenitic precipitation hardening stainless steel |
| 17-10 PH |
17 wt% chromium 10 wt% nickel |
Austenitic precipitation hardening stainless steel |
Some additional characteristics of the three classes are as follows:
- Martensitic precipitation hardening stainless steels have been used extensively
for forging and fasteners in the aerospace industry. The yield strength is higher
than that for other martensitic stainless steels. Fabrication is often facilitated
by the ductility of the material after solution treating and quenching and by the
subsequent strengthening during aging. Machining is normally done before aging.
- Semi-austenitic precipitation hardening stainless steels produce an austenitic
structure after quenching. Martensite is then reformed either by cooling to sub-zero
temperatures or by using a conditioning heat treatment to remove carbon from solution.
Fabrication is done between certain steps in the heat treating cycle, often before
the sub-zero cooling or before the final aging.
- Austenitic precipitation hardening stainless steels retain their austenitic
structures at all temperatures. Fabrication is done after quenching but before
aging. The alloys tend to have lower strength levels than those above. High
temperature strength is superior. The alloys have been used in aerospace applications,
especially those requiring strength at high temperatures.
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