Product Code Database
Austenitic stainless steel is one of the five families of stainless steel (along with ferritic, martensitic, duplex and precipitation hardened). Its primary crystalline structure is austenite (face-centered cubic). Such steels are not hardenable by heat treatment and are essentially non-magnetic. This structure is achieved by adding enough austenite-stabilizing elements such as nickel, manganese and nitrogen. The Incoloy family of alloys belong to the category of super austenitic stainless steels. Corrosion resistance is provided by the large percentage of alloyed chromium, the inclusion of which imparts a protective Cr2O3 layer on the exposed surface when chromium reacts with atmospheric oxygen.
300 series stainless steels are the larger subgroup. The most common austenitic stainless steel and most common of all stainless steel is Type 304, also known as 18/8 or A2. Type 304 is extensively used in such items as cookware, cutlery, and kitchen equipment. Type 316, also known as A4, is the next most common austenitic stainless steel. Some 300 series, such as Type 316, also contain some molybdenum to promote resistance to acids and increase resistance to localized attack (e.g. pitting and crevice corrosion).
The higher nitrogen addition in 200 series gives them higher mechanical strength than 300 series.
Alloy 20 (Carpenter 20) is an austenitic stainless steel possessing excellent resistance to hot sulfuric acid and many other aggressive environments which would readily attack type 316 stainless. This alloy exhibits superior resistance to stress-corrosion cracking in boiling 20–40% sulfuric acid. Alloy 20 has excellent mechanical properties and the presence of niobium in the alloy minimizes the precipitation of carbides during welding.
They must resist corrosion (usually oxidation) and retain mechanical properties, mostly strength (yield stress) and creep resistance.
Corrosion resistance is mostly provided by chromium, with additions of silicon and aluminium. Nickel does not resist well in sulphur containing environments. This is usually taken care of by adding more Si and Al which form very stable oxides. Rare earth elements such as cerium increase the stability of the oxide film.
| + Typical composition of the major grades | |||||||||
| 1.4878 | X8CrNiTi18-10 | 321H | S32109 | < 0.1 | 18 | 10.5 | - | - | Ti: ≤ 5×C |
| 1.4818 | X6CrNiSiNCe19-10 | - | S30415 | 0.06 | 19 | 10 | - | - | N: 0.16; Ce: 0.05. |
| 1.4828 | X15CrNiSi20-12 | 309 | - | < 0.2 | 20 | 12 | 2.0 | - | - |
| 1.4833 | X12CrNi23-13 | 309S | S30908 | < 0.08 | 23 | 13 | < 0.75 | - | - |
| 1.4872 | X25CrMnNiN25-9-7 | - | - | 0.25 | 25 | 7 | - | 9 | - |
| 1.4845 | X15CrNi25-21 | 310S | S31008 | < 0.1 | 25 | 20 | - | - | - |
| 1.4841 | X15CrNiSi25-21 | 314 | S31400 | < 0.15 | 25 | 20 | 1.8 | - | - |
| 1.4876 | X10NiCrAITi32-20 | "Alloy 800" | N08800 | < 0.12 | 21 | 32 | - | - | Al: 0.4; Ti: 0.4 |
| 1.4854 | X6NiCrSiNCe35-25 | "Alloy 353MA" | S35315 | 0.06 | 25 | 35 | - | - | N: 0.15; Ce: 0.06. |
| 1.4886 | X12NiCrSi35-16 | 330 | N08330 | < 0.15 | 18.5 | 35 | - | - |
Type309 and 310 are used in high temperature applications greater than .
Note: ferritic stainless steels do not retain strength at elevated temperatures and are not used when strength is required.
Austenitic stainless steel can be tested by nondestructive testing using the dye penetrant inspection method but not the magnetic particle inspection method. Eddy-current testing may also be used.
| + Typical composition | ||||||||
| 1.4980 | X6NiCrTiMoVB25-15-2 | 660 | S66286 | 0.05 | 15 | 25 | 1.25 | V: 0.3; Ti: 2.0; B: 0.006. |
| + Minimum mechanical properties | |||
| Solution treated and aged | 13 |
It is used for service temperatures up to in applications such as:
A key part of austenitic stainless steel production is decarburization, the removal of most carbon from the alloy. Due to its open FCC structure, austenite dissolves carbon very easily, causing it to accumulate within the metal during cooling. Carbon atoms readily produce carbides from alloyed chromium, forming as precipitates within the metal. While precipitates are desirable for strengthening of some steels due to their ability to obstruct (crystal latice defects) and force climb instead of glide, (1982). 9780080293370, Pergamon Press. ISBN 9780080293370 the formation of carbides can leech chromium from the Cr2O3 coating of the metal. This weakens the protective film, a process that then compounds as the reduced protection permits corrosion to cause further damage. The formation of damaging carbides can be discouraged via the addition of elements that favor carbide formation such as titanium or niobium, as these will bond with carbon rather than chromium.
The FCC structure of austenite confers ductility to stainless steel, as the slip planes permit dislocations to move easily via the glide mechanism. When worked at cold temperatures or subjected to mechanical stresses beyond the yield point, austenitic steels will Work hardening, as dislocations formed within the crystal structure compound upon one another. Additionally, misalignment of crystalline structures results in the formation of body-centered tetragonal (BCT) martensite, a significantly harder crystal structure of steel. The misalignment of the differing crystal structures will harden the metal further, as dislocations are unable to pass through the high strain area of the material. While this increases tensile strength, the material thus worked will lose much of its ductility, becoming brittle and susceptible to rapid failure if the ultimate yield strength is exceeded. The material may be returned to its original austenitic FCC structure via solution heat treatment, allowing dynamic recrystallization of the structure to release the strain present in BCT grains and the reformation of FCC structures.
Under long term stress, austenitic stainless steels are subject to creep, or slow deformation over time as dislocations move through the crystal structure. The deformation mechanisms occurring are dependent on both applied stress as well as temperature. An example of this process may be seen in the deformation map below for Alloy 316, a commonly used austenitic stainless steel. Even at low temperatures, long term application of stress can cause the movement of dislocations via diffusion. Above temperatures of approximately 480 °C (753 K), deformation becomes plastic as power-law creep occurs, with glide becoming predominant. The transition to climb-plus-glide power law creep is however not distinct, due to the temperature at which austenite forms; at this point, dynamic recrystallization of the metal begins, and creep of the material will accelerate as the steel rapidly becomes more malleable. As a result, these steels are usually not recommended for use above 700 °C for structural purposes, and 870 °C (1143 K) is usually considered the upper practical limit for high-temperature austenitic steels [1].
As the material approaches melting temperature, the crystalline structure begins to transition to a disordered liquid form. This temperature is known as the solidus/liquidus temperature, where the material is part solid, part molten. Alloy 316 has a liquidus temperature of approximately 1375 °C, and fully melts at approximately 1400 °C.
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