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Stainless steels are known as high-alloy steels. These steels contain good corrosion resistance in comparison with other steels because they contain larger amounts of chromium.
Stainless steels are available in three different groups based on their crystalline structure. These groups include martensitic, austenitic and ferritic. The combination of martensitic and ferritic steels forms a fourth group of stainless steels known as precipitation-hardened steels.
Stainless steel-grade 13-8 is an age hardenable, precipitation stainless steel. This steel has good resistance to stress and general corrosion cracking, high transverse toughness and high strength obtained by a single low temperature heat treatment.
The following datasheet provides an overview of stainless steel-grade13-8.
Chemical CompositionThe chemical composition of stainless steel-grade13-8 is outlined in the following table.
Element | Content (%) |
---|---|
Iron, Fe | 76 |
Chromium, Cr | 12.25-13.25 |
Nickel, Ni | 7.50-8.50 |
Molybdenum, Mo | 2.0-2.50 |
Aluminum, Al | 0.90-1.35 |
Manganese, Mn | 0.10 |
Silicon, Si | 0.10 |
Carbon, C | 0.050 |
Nitrogen, N | 0.010 |
Phosphorous, P | 0.010 |
Sulfur, S | 0.0080 |
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Grade 630 stainless steels are martensitic stainless steels that are precipitation hardened to achieve excellent mechanical properties. These steel achieve high strength and hardness following heat treatment. The heat and corrosion resistance of grade 630 are similar to that of grade 304 steels. This grades is also commonly referred to as grade 17-4PH.
One of the key benefits of this grade is that it is available in solution treated conditions, at which they can be easily machined and age-hardened to attain high strength. The age treatment of grade 630 is carried out at low temperatures, to avoid significant distortion. Therefore, this grade is used for applications such as the manufacture of long shafts that do not require re-straightening after heat treatment.
Key PropertiesThe properties mentioned below pertain to commonly available grade 630 bar products in ASTM A564. The specifications may not be similar to other forms such as forgings and plates.
CompositionThe compositional ranges of grade 630 stainless steels are displayed below:
Table 1.Composition ranges for grade 630 stainless steels
Grade | C | Mn | Si | P | S | Cr | Ni | Cu | Nb+Ta | |
630 | min. max | - 0.07 | - 1 | - 1 | - 0.04 | - 0.030 | 15 17.5 | 3 5 | 3 5 | 0.15 0.45 |
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INCOLOY® alloy A-286 (UNS S66286/W. Nr. 1.4980) is an iron-nickel-chromium alloy with additions of molybdenum and titanium. It is agehardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The limiting chemical composition is given in Table 1. The alloy is austenitic in all metallurgical conditions. The high strength and excellent fabrication characteristics of INCOLOY alloy A-286 make the alloy useful for various components of aircraft and industrial gas turbines. It is also used for fastener applications in automotive engine and manifold components subject to high levels of heat and stress and in the offshore oil and gas industry.
Table 1 - Limiting Chemical Composition, % Nickel.........................................................................24.0-27.0
Iron .............................................................................Balance* Chromium..................................................................13.5-16.0 Titanium.....................................................................1.90-2.35 Molybdenum..................................................................1.0-1.5 Vanadium...................................................................0.10-0.50
Carbon ......................................................................0.08 max.
Manganese .................................................................2.0 max.
Silicon .........................................................................1.0 max. Aluminum..................................................................0.35 max. Sulfur.......................................................................0.030 max. Boron.......................................................................0.001-0.01
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With a high creep and rupture strength to 1400°F (760°C), Incoloy™ 901is a nickel-iron-chromium alloy ideally suited for gas turbine and aircraft applications. Because of its high nickel content, it can be joined with ferritic alloy steels without thermal expansion provisions.
CHEMICAL COMPOSITION OF INCOLOY™ 901SIZE 6MM TO 200MM DIA ROUND BAR.
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Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.
CHEMICAL COMPOSITION OF INCONEL™ 713CSIZE 6MM TO 200MM DIA ROUND BAR.
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Base Metal Price25 % rel
Density7.6 g/cm3 (470 lb/ft3)
Elastic (Young's, Tensile) Modulus220 GPa (32 x 106 psi)
Elongation at Break40 %
Poisson's Ratio0.28
PREN (Pitting Resistance)17
Specific Heat Capacity460 J/kg-K
Strength to Weight Ratio99 kN-m/kg
Tensile Strength: Ultimate (UTS)750 MPa (110 x 103 psi)
Tensile Strength: Yield (Proof)400 MPa (58 x 103 psi)
Thermal Expansion13 µm/m-K
Alloy CompositionIron (Fe)59.1 to 65.4 %
Chromium (Cr)16 to 18 %
Nickel (Ni)8.0 to 9.0 %
Manganese (Mn)7.0 to 9.0 %
Silicon (Si)3.5 to 4.5 %
Nitrogen (N)0.080 to 0.18 %
Carbon (C)0 to 0.1 %
Phosphorus (P)0 to 0.060 %
Sulfur (S)0 to 0.030 %
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Alloy Steels Maraging 300 is stocked by 8 North American distributors and produced by 8 large mills. Distributors will offer small quantity buys while mills will generally only sell large quantities, with delivery times anywhere from 10 to 50 weeks depending on size and form required
This material is stocked primarily in Bar Products by 8 distributors but is also available to a lesser extent in Flat Rolled Products, Forging Products, and Casting Products.
For distributor (small quantity) availability click here
For mill (large volume) production click here
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Specifications
The following specifications cover Alloy Steels Maraging 300
Related Metals:
Chemistry Data : [top]
Aluminum |
| |
Boron |
| |
Carbon | 0.03 max | |
Cobalt |
| |
Iron | Balance | |
Manganese | 0.1 max | |
Molybdenum |
| |
Nickel |
| |
Phosphorus | 0.01 max | |
Silicon | 0.1 max | |
Sulphur | 0.01 max | |
Titanium |
| |
Zirconium |
|
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The chemical composition of Alloy 800 is:
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.10 max | 0.15-0.60 | 0.15-0.60 | 0.30-1.20 |
The chemical composition of alloy 800H is:
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.05-0.10 | 0.15-0.60 | 0.15-0.60 | 0.30-1.20 |
The chemical composition of Alloy 800HT is :
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.06-0.10 | 0.25-0.60 | 0.25-0.60 | 0.85-1.2 |
The forms of INCOLOY 800H/800HT are:
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Stainless steels are known as high-alloy steels. These steels contain good corrosion resistance in comparison with other steels because they contain larger amounts of chromium.
Stainless steels are available in three different groups based on their crystalline structure. These groups include martensitic, austenitic and ferritic. The combination of martensitic and ferritic steels forms a fourth group of stainless steels known as precipitation-hardened steels.
Stainless steel-grade 13-8 is an age hardenable, precipitation stainless steel. This steel has good resistance to stress and general corrosion cracking, high transverse toughness and high strength obtained by a single low temperature heat treatment.
The following datasheet provides an overview of stainless steel-grade13-8.
Chemical CompositionThe chemical composition of stainless steel-grade13-8 is outlined in the following table.
Element | Content (%) |
---|---|
Iron, Fe | 76 |
Chromium, Cr | 12.25-13.25 |
Nickel, Ni | 7.50-8.50 |
Molybdenum, Mo | 2.0-2.50 |
Aluminum, Al | 0.90-1.35 |
Manganese, Mn | 0.10 |
Silicon, Si | 0.10 |
Carbon, C | 0.050 |
Nitrogen, N | 0.010 |
Phosphorous, P | 0.010 |
Sulfur, S | 0.0080 |
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Element | Min | Max |
Carbon | -- | 0.05 max |
Nickel | -- | 41.0 |
Iron | Balance | |
Silicon | -- | 0.20 |
Manganese | -- | 0.40 |
Alloy 42 is a 41% nickel-iron controlled expansion alloy which has been used in a wide variety of glass-to-metal sealing applications.
While the expansion properties of this alloy most closely match 1075 glass, it has also been used in seals for the 0120 and 0010 glasses. It may also be used with hard glasses if a thin edged tubular seal is used. For seals that are not hydrogen annealed prior to sealing, a variation of this alloy containing small additions fo titanium, Glass Sealing 42 Gas-Free, has been used to promote gas-free sealing characteristics.
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Chemical Composition, %
Ni | Mo | Cr | Fe | W | Co | Mn | C |
---|---|---|---|---|---|---|---|
Remainder | 15.0-17.0 | 14.5-16.5 | 4.0-7.0 | 3.0-4.5 | 2.5 max | 1.0 max | .01 max |
V | P | S | Si | ||||
.35 max | .04 max | .03 max | .08 max |
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Sanicro 28 is widely used, for example, in hydrogen sulphide containing environments within the oil and gas industry. This is due to the material's excellent resistance to sulphide cracking in conditions characterized by high levels of hydrogen sulphide (H2S), carbon dioxide (CO2) and chlorides (Cl-). Examples of applications are production tubing (OCTG) and heat exchangers used in the processing of sour crude.
The combination of molybdenum and nickel in Sanicro 28 helps prevent cracking caused by polythionic acid attack during equipment start up and shut down. The grade is also utilized in oil refineries to reduce the effects of naphthenic acid corrosion.
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Chemical Composition Limits | |||||||||||
Weight% | Ni | Fe | Cr | Mo | Cu | Ti | C | Mn | S | Si | Al |
Alloy 28 | 30-32 | 22 min | 26-28 | 3-4 | 0.60-1.40 | - | 0.02 max | 2 max | 0.03 max | 0.70 max | - |
Additional Information:
Custom 450® stainless is a martensitic age-hardenable stainless steel which exhibits very good corrosion resistance with moderate strength. Although the alloy a yield strength higher than 100 Ksi (689 MPa) in the annealed condition, it is easily fabricated. A single-step aging treatment develops higher strength with good ductility and toughness. Generally supplied in the annealed condition, requiring no heat treatment by the user for many applications. Because it has corrosion resistance like Type 304 stainless but three times the yield strength, it has been used in applications where Type 304 was not strong enough. On the other hand, it has also replaced Type 410 stainless directly on a strength basis where Type 410 had insufficient corrosion resistance. Mechanical properties will depend on the aging temperature selected. *
* Information supplied by Carpenter Technology Corp
Chemistry TypicalCarbon: 0.05 max
Manganese: 1.00 max
Phosphorus: 0.030 max
Sulfur: 0.030 max
Silicon: 1.00 max
Chromium: 14.00-16.00
Nickel: 5.00-7.00
Molybdenum: 0.50-1.00
Copper: 1.25-1.75
Columbium: 8 x Carbon min
Iron: Balance
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AMS 5716 INCOLOY® alloy 330 (UNS N08330/W. Nr. 1.4886) is an austenitic alloy with good high-temperature strength and corrosion resistance. It has a solid solution composition and is not hardenable by heat treatment. Its high nickel and chromium provide good resistance to oxidation and carburization. Its oxidation resistance is enhanced by the silicon content. The alloy’s strength and oxidation resistance at elevated temperatures make it a useful material for industrial heating furnaces; for muffles, retorts, conveyor systems, baskets and boxes, and various fixtures.
Chemical Composition, %
Nickel 34.0-37.0 Chromium17.0-20.0
Iron Balance* Carbon0.08 max. Silicon0.75-1.50
Manganese 2.0 max.
Phosphorus 0.030 max.
Sulfur 0.030 max.
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Whether at room or slightly higher temperatures, Jethete M152 provides sufficient ductility and high tensile strength. Jethete M152 is a new martensitic stainless steel similar to Jethete M151, and is capable of resisting heat and corrosion.
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Chemistry
Chemical Requirements | |||||||
---|---|---|---|---|---|---|---|
| Ni | Cr | Mn | C | Si | N |
|
Max | 7.50 | 21.50 | 10.0 | 0.08 | 1.00 | 0.40 | 0.030 |
Min | 5.50 | 19.00 | 8.0 |
|
| 0.15 |
|
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Chemical Composition Limits | ||||||||||||
Weight% | C | P | Si | Ni | V | Fe | Mn | S | Cr | Mo | W | Cu |
Alloy 422 | 0.20-0.25 | 0.040 max | 0.20-0.60 | 0.50-1.0 | 0.17-0.30 | Bal | 1.0 | 0.030 max | 11.0-13.5 | 0.75-1.25 | 0.75-1.25 | 0.50 |
Alloy 422 is a hardenable stainless steel designed for use at temperatures of up to 1200ºF (649ºC). Alloy 422 has good resistance to scaling and oxidation. Through heat treatment, high mechanical properties can be developed. Alloy 422 is used in applications such as compressors or steam turbines and also in aircraft parts, valves, high temperature bolting etc.
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Element | Min | Max |
Carbon | 0.06 | 0.12 |
Manganese | -- | 0.10 |
Silicon | -- | 0.20 |
Chromium | 18.0 | 20.0 |
Nickel | Balance | |
Boron | 0.003 | 0.010 |
Iron | -- | 5.00 |
Cobalt | 10.0 | 12.0 |
Titanium | 3.00 | 3.30 |
Aluminum | 1.40 | 1.60 |
Molybdenum | 9.00 | 10.50 |
Additional Information:
Additional Information:
Element | Min | Max |
---|---|---|
C | - | 0.2 |
Mn | - | 2 |
Ni | 23 | 28 |
Cr | 19 | 23 |
S | - | 0.3 |
Mo | 4 | 5 |
N | - | 0.1 |
Cu | 1 | 2 |
P | - | 0.03 |
Si | - | 0.7 |
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