Steel 4130

Aging Procedure

Not applicable to this alloy.

Annealing Procedure

4130 (and most of the other low alloy steels) may be annealed at 1550 F for a time long enough to allow thorough heating of the section size. It should then be cooled in the furnace at a rate of less than 50 F per hour down to 900 F, followed by air cooling from 900 F.

Applications

Typical applications for 4130 low alloy steel include. structural use such as aircraft engine mounts and welded tubing applications.

Cold Workability

Cold working by conventional methods is readily accomplished on this alloy.

Forgeability

Forge at 2200 F maximum down to 1750 F.

Formability

Formability is best in the annealed condition for which the ductility is very good, Bend radii of 1t on annealed sheet material may be made.

Hardening Procedure

Hardening is accomplished by heat treatment or by cold working -- see "Heat Treatment".

Heat Treatability

Heating at 1600 F followed by an oil quench will harden the 4130 alloy. For best results a normalizing pre-hardening heat treatment may be used at 1650 to 1700 F followed by the 1600 F soak and oil quench.

Hot Workability

4130 in the annealed condition has excellent ductility. Thus it is usually not necessary to do hot working to form parts. If hot working is needed it can be done in the range of 2000 F to 1500 F.

Machinability

This alloy is readily machined by conventional methods. Machinability is best with the alloy in the normalized and tempered condition. Although the alloy may be machined in the fully heat treated condition, machinability becomes more difficult with increasing strength (hardness) of the alloy.

Other Comments

The 4130 alloy is a through hardening alloy and should not be case hardened.

Principle Design Features

AISI 4130 is a low alloy steel containing molybdenum and chromium as strengthening agents. The carbon content is nominally 0.30% and with this relatively low carbon content the alloy is excellent from the fusion weldability standpoint. The alloy can be hardened by heat treatment.

Tempering Procedure

Tempering is done to restore some of the ductility that may be lost after the hardening heat treatment and quench. Alloy 4130 is tempered at between 750 F and 1050 F, depending upon the strength level desired. The lower the tempering temperature the greater the strength.

Weldability

4130 alloy is noted for its weldability by all of the commercial methods.

Known Forms

Angle

Angle

Billet

Billet

Cee

Cee

Channel

Channel

Coil

Coil

Disc

Disc

Drill Rod

Drill Rod

Fitting

Fitting

Flange

Flange

Flat Bar

Flat Bar

H-Beam

H-Beam

Half Round

Half Round

Hexagon Bar

Hexagon Bar

Hollow Bar

Hollow Bar

Octagon Bar

Octagon Bar

Piling

Piling

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

Treadplate

Treadplate

Valve

Valve

Wide Beam

Wide Beam

Wire Flat

Wire Flat

Wire Round

Wire Round

Wire Square

Wire Square

Zee

Zee

Additional Data

Specifications

4130,6348,6350,6351,6360,6361,6362,6370,6371,6373,6374,6528,7496,A108,A29,A322,A331,A506,A507,A513,A519,A646,A752,A829,S-18729,S-6758,J1397,J404,J412,G41300

Chemical Elements

Carbon0.28 - 0.33
Chromium0.8 - 1.1
Manganese0.7 - 0.9
Molybdenum0.15 - 0.25
Phosphorus0.035 max
Silicon0.15 - 0.35
Sulphur0.04 max

Physical Properties

Density: 0.283lb/in³Density

Melting Point: 2610°FMelting Point

Specific Gravity: 7.8Specific Gravity

Specific Heat: 0.114BTU/lb·°FSpecific Heat

Mechanical Properties

Modulus of Elasticity – Tension: 29MSIModulus of Elasticity – Tension

Thermal Conductivity: 1.8583BTU/hr·ft·°FThermal Conductivity

Thermal Expansion: 7µin/in·°FThermal Expansion

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Annealed68 °F700 °F2.5 μin/in·°F