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TUTORIAL ON CLASSIFICATION NUMBERS OF VARIOUS ALLOY FAMILIES

David C. Silverman


Table of Contents

Overview of Tutorial
Carbon and Low Alloy Steels
Cast Irons
        Stainless Steels
Aluminum Alloys
Tool Steels

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
  1. austenitic stainless steels
  2. manganese-substituted austenitic stainless steels
  3. ferritic stainless steels
  4. martensitic stainless steels
  5. duplex stainless steels
  6. 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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David C. Silverman, Ph.D. - Primary Consultant
E-Mail:     dcsilverman@argentumsolutions.com
Phone:     314-576-3586
Fax:         314-754-9825
Address:   The Argentum House
                14314 Strawbridge Ct.
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