Stainless Alloy 20

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Annealing Procedure

Soak thoroughly at 1725-1850 F(941-1010 C), water quench.

Applications

Good availability at both the mill and distributor levels have made this a popular choice for a wide variety of applications. Included among these are: equipment for the manufacture of synthetic rubber, plastics, organic and heavy chemicals, pharmaceuticals, solvents and explosives, petroleum products, etc. Also employed in heat exchangers, mixing tanks, metal cleaning and pickling equipment and process piping.

Cold Workability

This alloy can be successfully cold formed using all common practices. Its elevated strength may require higher forming pressures.

Forgeability

Soak thoroughly at 2100-2250 F(1149-1232 C). Re-heat when temperature drops below 1800 F(982 C). After forging, reheat and soak completely at 1725-1850 F(941-1010 C) and quench rapidly in water or oil.

Formability

To obtain maximum ductility, heat material to 2100 F(1149 C). Understand, however, that this process will adversely affect the stability of the material. Without this process, the material can be satisfactorily formed albeit with a high work hardening rate.

Hardening Procedure

This material may only be hardened by cold work.

Hot Workability

This alloy can be successfully hot formed using forces similar to those required by austenitic stainless steels.

Machinability

Superior finishes may be obtained using set-up and process speeds and feeds normally employed in austenitic stainless steels such as 316 and 317. Slow speeds and heavy, constant feeds are the rules in working this alloy.

Principle Design Features

This alloy is a columbium stabilized material that combines excellent corrosion resistance with elevated mechanical properties and relatively easy fabrication. It particularly excels in resisting corrosion to hot sulfuric acids when compared to conventional stainless steels such as 316.

Weldability

Most commonly used welding methods with the exception of oxyacetylene welding have been successfully employed with this alloy. The presence of columbium tends to minimize the precipitation of carbides in the heat affected zone, so the material may, in most cases , be used in the "as welded" condition. Pre-heating is not required.

Known Forms

Angle

Angle

Channel

Channel

Coil

Coil

Disc

Disc

Flat Bar

Flat Bar

Foil

Foil

Hexagon Bar

Hexagon Bar

Hollow Bar

Hollow Bar

Pipe

Pipe

Plate

Plate

Precision Ground Bar

Precision Ground Bar

Rectangle Tube

Rectangle Tube

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Square Bar

Square Bar

Square Tube

Square Tube

Standard Beam

Standard Beam

Strip

Strip

Tee

Tee

Additional Data

Specifications

664,B366,B462,B463,B464,B468,B471,B473,B474,B475,B729,2.4660,N08020

Chemical Elements

Carbon0.07 max
Chromium19 - 21
Copper3 - 4
IronBalance
Manganese2 max
Molybdenum2 - 3
Nickel32 - 38
Phosphorus0.045 max
Silicon1 max
Sulphur0.035 max

Physical Properties

Density: 0.292lb/in³Density

Electrical Resistivity: 651µΩ·cmElectrical Resistivity

Poissons Ratio: 0.31Poissons Ratio

Specific Gravity: 8.055Specific Gravity

Specific Heat: 0.12BTU/lb·°FSpecific Heat

Mechanical Properties

Modulus of Elasticity – Tension: 28MSIModulus of Elasticity – Tension

Relative Magnetic Permeability: 1.002μᵣRelative Magnetic Permeability

Thermal Conductivity

ConditionTemperatureConductivity
Annealed120 °F8.46 BTU/hr·ft·°F

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Annealed70 °F212 °F8.16 μin/in·°F
Annealed70 °F390 °F8.37 μin/in·°F
Annealed70 °F842 °F8.83 μin/in·°F
Annealed70 °F1652 °F9.83 μin/in·°F
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