Steel 8620

Aging Procedure

Not applicable to this alloy.

Annealing Procedure

AISI 8620 may be given a full anneal at 1550 F and slow cooling at not more than 50 F per hour down to 850 F. From there it may be air cooled.

Applications

In the carburized condition this alloy is used for gears, ring gears, shafts and crankshafts.

Cold Workability

The alloy may be cold worked in the annealed condition by conventional methods. Cold working, as with machining, should be done to as close a tolerance as possible before heat treatment or carburizing.

Forgeability

The alloy may be forged at 2200 F down to 1800 F prior to the hardening heat treatment or carburizing.

Formability

Forming characteristics of 8620 alloy are good in the annealed condition.

Hardening Procedure

Hardening is done by oil quench from 1675 F. See "Heat Treatment". Carburizing is accomplished at the same 1650 to 1700 F range in a carburizing "pack" or environment, followed by oil quench for thin sections or a furnace cool for heavier (over 3/4") sections. Following carburizing of heavy sections a reheat at 1575 F will enhance both case and core properties of the alloy.

Heat Treatability

This alloy may be hardened by heating to 1500 F followed by a water quench. Carburize at 1650 to 1700 F in an appropriate carburizing medium and oil quench to harden. Improved carburized case and core properties can be obtained by furnace cooling from carburizing at 1650 - 1700 F and then reheating to 1575 F.

Hot Workability

Hot working may be accomplished prior to hardening or carburizing. Consult the alloy supplier for information as to temperatures.

Machinability

Machining is done prior to carburizing to within as close a tolerance as possible. Finish machining, after heat treatment and/or carburizing, should be at a minimum so as not to impair the hardened case of the part. Machining may be done by conventional means prior to heat treatment - after carburizing machining is usually limited to grinding.

Other Comments

This alloy is typically used for carburized parts where a hardened case is desired for wear resistance.

Principle Design Features

AISI 8620 is a hardenable chromium, molybdenum, nickel low alloy steel often used for carburizing to develop a case-hardened part. This case-hardening will result in good wear characteristics.

Tempering Procedure

Tempering of carburized parts is done at 250 to 300 F and this will result in the alloy having a core strength of approximately 135 ksi minimum with Rockwell C case hardness of 90. Tempering of heat treated and water quenched parts (not carburized) is done at 400 F to 1300 F with greater hardness the lower the tempering temperature.

Weldability

The alloy may be welded by conventional methods, usually gas or arc welding. Preheating at 400 F is beneficial and subsequent heating after welding is recommended - consult the approved weld procedure for the method used.

Known Forms

Angle

Angle

Billet

Billet

Bolt

Bolt

Cee

Cee

Channel

Channel

Coil

Coil

Disc

Disc

Drill Rod

Drill Rod

Flat Bar

Flat Bar

H-Beam

H-Beam

Half Round

Half Round

Hexagon Bar

Hexagon Bar

Hollow Bar

Hollow Bar

Nut

Nut

Octagon Bar

Octagon Bar

Piling

Piling

Pipe

Pipe

Plate

Plate

Powder

Powder

Precision Ground Bar

Precision Ground Bar

Rectangle Tube

Rectangle Tube

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Screw

Screw

Sheet

Sheet

Specialty Form

Specialty Form

Square Bar

Square Bar

Square Tube

Square Tube

Standard Beam

Standard Beam

Strip

Strip

Tee

Tee

Threaded Rod

Threaded Rod

Treadplate

Treadplate

Washer

Washer

Wide Beam

Wide Beam

Wire Round

Wire Round

Zee

Zee

Additional Data

Specifications

8620,6274,6276,6277,6375,A29 (8620),A322 (8620),A331 (8620),A506 (8620),A507 (8620),A513,A519 (8620),A646 (8620-4),A752 (8620),A829,S-8690,J1397 (8620),J404 (8620),G86200

Chemical Elements

Carbon0.18 - 0.23
Chromium0.4 - 0.6
Manganese0.7 - 0.9
Molybdenum0.15 - 0.25
Nickel0.4 - 0.7
Phosphorus0.035 max
Silicon0.15 - 0.35
Sulphur0.04 max

Physical Properties

Density: 0.283lb/in³Density

Melting Point: 2600°FMelting Point

Specific Gravity: 7.8Specific Gravity

Specific Heat: 0.1BTU/lb·°FSpecific Heat

Mechanical Properties

Modulus of Elasticity – Tension: 31MSIModulus of Elasticity – Tension

Thermal Conductivity: 2.1667BTU/hr·ft·°FThermal Conductivity

Thermal Expansion: 6.6µin/in·°FThermal Expansion