Chemical Composition |
Carbon |
|
0.38 - 0.43 |
Chromium |
|
0.7 - 0.9 |
Iron |
|
Balance |
Manganese |
|
0.6 - 0.8 |
Molybdenum |
|
0.2 - 0.3 |
Nickel |
|
1.65 - 2 |
Phosphorus |
|
0.035 max |
Silicon |
|
0.15 - 0.3 |
Sulphur |
|
0.04 max |
Applications |
Typical applications are for structural use, such as aircraft landing gear, power transmission gears and shafts and other structural parts. |
Machinability |
Machining is best done with this alloy in the annealed or normalized and tempered condition. It can be machined by all conventional methods. However in the high strength conditions of 200 ksi or greater the machinability is only from 25% to 10% that of the alloy in the annealed condition. |
Forming |
4340 has good ductility in the annealed condition and most forming operations are carried out in that condition. It can be bent or formed by spinning or pressing in the annealed state. Bend radii should be 3t or greater. |
Welding |
The alloy can be fusion or resistance welded. Preheat and post heat weld procedures should be followed when welding this alloy by established methods. |
Heat Treatment |
Heat treatment for strengthening is done at 1525 F followed by an oil quench. For high strength (over 200 ksi) the alloy should first be normalized at 1650 F prior to heat treatment. See "Tempering" for strength levels. |
|
Forging |
Forging may be done in the range of 2250 F max. down to 1800 F. |
|
|
Hot Working |
4340 has very good cold forming capability so that hot working should not be needed. Hot working in any but the annealed condition can affect the strength level. Consult the alloy supplier in regard to hot working. |
Cold Working |
The 4340 alloy may be cold worked, in the annealed condition, by conventional methods and tooling. It has good ductility. |
Annealing |
A full anneal may be done at 1550 F followed by controlled (furnace) cooling at a rate not faster than 50 F per hour down to 600 F. From 600 F it may be air cooled. |
|
Aging |
Not applicable to this alloy. |
|
Tempering |
The temperature for tempering depends upon the strength level desired. Before tempering the alloy should be in the heat treated or normalized & heat treated condition - see "Heat Treatment". For strength levels in the 260 - 280 ksi range temper at 450 F. For strength in the 125 - 200 ksi range temper at 950 F. Do NOT temper the alloy if it is in the 220 - 260 ksi strength range as tempering can result in degradation of impact resistance for this level of strength. |
|
Hardening |
The alloy will harden by cold working or by heat treatment -- see "Heat Treatment" and "Tempering". |
|
Other Comments |
AISI 4340 is considered to be a "through hardening" steel such that large section sizes can still be heat treated to high strength. |
|
Physical Properties |
Density (lb / cu. in.) |
|
0.28 |
Specific Gravity |
|
7.8 |
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) |
|
0.116 |
Melting Point (Deg F) |
|
2600 |
Thermal Conductivity |
|
21 |
Mean Coeff Thermal Expansion |
|
6.6 |
Modulus of Elasticity Tension |
