Mill test aisi 2205 stainless steel black bar with CE certificate 

GENERAL PROPERTIES

The AL 2205 (UNS S31803) alloy is a nitrogenenhanced duplex stainless steel alloy. The nitrogen serves to significantly improve the corrosion resistance of the alloy; especially in the welded condition. Earlier duplex alloys have had moderate resistance to general corrosion and chloride stress corrosion cracking, but suffered a substantial loss of properties when used in the as-welded condition. To impart the metallurgical benefits of nitrogen to both improved corrosion performance and as-welded properties, the AL 2205 alloy is produced to a 0.15% minimum nitrogen content compared to the ASTM range of 0.08-0.20%. The minimum Cr, Mo and Ni contents of AL 2205 alloy (22.0, 3.1 and 5.5% respectively) are all above the mid range of the ASTM composition specification. The typical high Cr, Mo and Ni contents of AL 2205 alloy give it a high PREN (Pitting Resistance Equivalent) of 35.8, further enhancing its corrosion resistance.

When heat-treated properly, the nominal 22% chromium, 5.5% nickel, 3% molybdenum, and 0.16% nitrogen in the AL 2205 alloy produces a microstructure that consists of a nearly equal mixture of austenite and ferrite phases as shown in the photomicrograph above right. The microstructure and composition of the AL 2205 alloy provides corrosion resistance to many environments that is superior to Types 316 or 317, and a yield strength that is more than double that of conventional austenitic stainless steels.

The microstructure and phase balance of AL 2205 alloy have been designed to facilitate the production of pipe and tube products. All AL 2205 alloy is metallographically examined to ensure that the as-shipped product is essentially free from the presence of detrimental precipitate phases such as sigma.

The AL 2205 alloy is the most widely used of the duplex stainless steels and is often used in the form of welded pipe or tubular components. The alloy has also been applied as a formed and welded sheet product in environments where resistance to general corrosion and chloride stress corrosion cracking is important.

CHEMICAL COMPOSITION

ASTM SPECIFICATION COVERAGE

PHYSICAL PROPERTIES

Density

0.285 Ib/in3 (7880 kg/m3)

Specific Heat at 68-212°F (20-100°C)

0.10 BTU/lb °F (0.42 kJ/kg°K)

Thermal Conductivity at 68-212°F (20-100°C)

11 BTU-ft/hr-ft2- °F (19 W/m°K)

Thermal Coefficient of Expansion at 68-212°F

(20-100°C)

7.6 x 10-6/°F (13.7 x 10-6/°C)

Modulus of Elasticity in Tension

27.5 x 106 psi (190 GPa)

Magnetic Permeability

Ferromagnetic

CORROSION RESISTANCE

Chloride Stress Corrosion Cracking

Resistance

The nickel-free ferritic steels are essentially immune to chloride stress corrosion cracking even in the extremely severe boiling 42% magnesium chloride test. Nickel-containing austenitic stainless steels, on the other hand, are highly susceptible to stress corrosion cracking. The resistance of austenitic and ferritic stainless steels to chloride stress corrosion cracking has been correlated to the nickel content of the alloys.

Duplex alloys behave in a manner that is a combination of the characteristics of the austenitic and ferritic phases that make up the alloy, as shown by the data below. Certain elements tend to partition into one of the two primary phases in duplex alloys. For example, the nickel content of the ferrite phase will be lower than that of the austenite phase relative to the bulk composition. Consequently, the ferrite phase in AL 2205 alloy will provide resistance to chloride stress corrosion cracking, making it substantially better than the standard 300 series austenitic stainless steels.

Pitting and Crevice Corrosion Resistance

A relative ranking of the resistance to chloride-ion pitting and crevice corrosion can be made by using ASTM procedure G-48 (10% FeCl3¥6H2O) and increasing the test temperature until the onset of crevice corrosion attack is observed. The temperature at which attack is first observed is called the critical crevice corrosion temperature and can be used as a relative measure of crevice corrosion resistance. The critical crevice corrosion temperature criterion is useful for ranking alloys, but does not necessarily indicate an absolute limiting temperature for the use of a particular alloy in chloride-bearing solutions. The data provided below for annealed plate indicate the superior resistance of the AL 2205 alloy to chloride- ion crevice corrosion compared to Type 316 and Type 317 stainless steels.

General Corrosion Resistance

The AL 2205 alloy is resistant to dilute reducing acids and moderate to high concentrations of oxidizing acids. The alloy is resistant to low concentrations of organic acids, but should be used with caution in higher concentrations at elevated temperatures. The following table compares the corrosion resistance of base metal and welded samples of Type 316 and AL 2205 alloy in various boiling acids. The corrosion rates that follow are given in units of mils per year (MPY) and millimeters per annum (mm/a).

Intergranular Corrosion

Tests of AL 2205 alloy in the welded condition indicate that it resists intergranular corrosion during the 16% sulfuric acid-copper sulfate test (ASTM A 262 Practice E).

MECHANICAL PROPERTIES

Mechanical Properties at Room Temperature

Typical mechanical properties for annealed AL 2205alloy material at room temperature are listed below:

Tensile Properties at Elevated Temperature

The AL 2205 alloy has been approved for use under Section Vlll, Division 1 of the ASME Boiler and Pressure Vessel Code (listed as S31803) to a maximum temperature of 600°F (316°C). The strength of the AL 2205 alloy is indicated by the maximum allowable stress values given in the ASME Boiler and Pressure Vessel Code reproduced below, and compared to values for Type 316 stainless steel. Such relatively high maximum allowable stress values can be used advantageously in process unit design. The stress values that are given below apply to plate, sheet, strip, seamless tubing and pipe products. A factor of 0.85 is applied when considering welded tubing or pipe products.

Impact Properties

Duplex AL 2205 alloy may undergo a transition from a ductile mode of fracture at higher temperatures to a brittle mode of fracture at lower temperatures when subjected to impact loading. The ductile-to-brittle transition temperature can be substantially increased by exposing the alloy for extended periods of time at temperatures in the range from 650 to 1000°F (343-538°C). Improper welding procedures, such as welding with straight chromium stainless steel filler metals, will increase the susceptibility of the weld to brittle impact behavior. The data presented below are from tests conducted on 3/8 inch (0.95 cm) thick AL 2205 unwelded plate samples in the annealed and rapidly cooled condition.

Effect of Elevated Temperature on Mechanical Properties

An upper temperature limit of 600°F (316°C) has been placed on the use of AL 2205 alloy in the ASME Boiler and Pressure Vessel Code due to what is known as Ò885°F (475°C) Embrittlement.Ó This means that the ferrite phase of AL 2205 alloy may be embrittled after exposure to temperatures from 650 to 1000°F (343-538°C). The 885°F (475°C) embrittlement is reversible by heat treating the alloy at a temperature above 1100°F (593°C). However, another embrittling range exists from about 1000°F (538°C) to 1830°F (1000°C) due to the precipitation of excess phases that are detrimental to both impact and corrosion properties. A full anneal and rapid cooling treatment is required to eliminate the latter form of embrittlement and is also the preferred manner of relieving forming stresses and 885°F (475°C) embrittlement.

Welding

The AL 2205 alloy is designed to contain approximately equal amounts of ferrite and austenite in the annealed strip or plate product. Autogenous welding will increase the amount of ferrite present in the weldment and adjacent areas of the base metal. Subsequent annealing will tend to restore the balance of phases in the base metal. However, an annealed autogenous weld mcan be expected to contain slightly more ferrite than the corresponding base metal. A fully ferritic weld should be avoided.

Matching filler metals are commercially available to weld the AL 2205 alloy. Such filler metals (AWS E2209) contain more nickel than the base metal in order to produce a phase balance within the weld that is approximately the same as the base metal. When AL 2205 alloy is welded to different metals, a filler metal should be chosen that contains a quantity of austenite forming elements that is sufficient to produce a partially or fully austenitic weld. The large, fully ferritic grains that may form in a weld made from ferritic fillers may lower impact ductility at room temperature.

Heat Treatment

The AL 2205 alloy should be annealed between 1870 and 2010°F (1020-1100°C) and cooled quickly. Annealing near 2010°F will increase the amount of ferrite present in the microstructure compared to that resulting from annealing near 1870°F. The graph below provides additional information.

Forming

The AL 2205 alloy can be successfully cold-bent and expanded. Greater loads will be required to deform the alloy because of the higher strength of this duplex alloy in comparison to conventional austenitic materials. The ferrite phase within the duplex structure of the AL 2205 alloy results in an elongation that is less than that of a comparable austenitic stainless steel. The alloy should be bent to more generous bend radii than fully austenitic materials.

Furthermore, the degree to which AL 2205 alloy tubing can be expanded into tubesheets is restricted by the lower tensile elongation of the material in comparison to conventional austenitic materials. The strength of the AL 2205 alloy is high relative to most tube sheet materials. Consequently, care must be taken to produce tight roller expanded joints between AL 2205 alloy tubing and other tube sheet materials.

Heavily cold-bent sections should be fully annealed (not just stress-relieved) after bending whenever there is the potential for stress corrosion cracking in the service environment. Stress relief heat treatments in the 600 to 1700°F (316-927°C) range adversely affect the properties of the alloy and should not be considered.

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