Alloy steel AISI 4340 (UNS G43400)

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Topics Covered

Introduction
Chemical composition
Physical properties
Mechanical properties
Thermal properties
Other designations
Manufacturing and heat treatment
Machinability
Forming
Welding
Heat treatment
To forge
Cold operation
Annealed
Hardening
Hardening
Apps


Introduction

Alloy steels are designated by four-digit AISI numbers. They include different types of steels whose composition exceeds the limits of B, C, Mn, Mo, Ni, Si, Cr and Va set for carbon steels.

AISI 4340 alloy steel is a heat treatable, low alloy steel containing chromium, nickel and molybdenum. It has high toughness and strength in the heat treated condition.


Chemical composition

The following table shows the chemical composition of AISI 4340 alloy steel.













Element Contents (%)
Iron, Fe 95.195 – 96.33
Nickel, Ni 1.65 – 2.00
Chromium, Cr 0.700 – 0.900
Manganese, Mn 0.600 – 0.800
Carbon, C 0.370 – 0.430
Molybdenum, Mo 0.200 – 0.300
Silicon, Si 0.150 – 0.300
Sulphur, S 0.0400
Phosphorus, P 0.0350


Physical properties

The physical properties of AISI 4340 alloy steel are given in the following table.






Properties Metric Imperial
Density 7.85gsm3 0.284 lb/in³
Fusion point 1427°C 2600°F


Mechanical properties

The mechanical properties of annealed AISI 4340 alloy steel are shown in the following table.


















Properties Metric Imperial
Tensile strength 745MPa 108000psi
Elasticity limit 470MPa 68200psi
Modulus of compressibility (typical for steel) 140GPa 20300 ksi
Shear modulus (typical for steel) 80GPa 11600 ksi
Elasticity module 190-210GPa 27557-30458 ksi
Poisson coefficient 0.27-0.30 0.27-0.30
Elongation at break 22% 22%
Area reduction 50% 50%
Hardness, Brinell 217 217
Hardness, Knoop (converted from Brinell hardness) 240 240
Hardness, Rockwell B (converted from Brinell hardness) 95 95
Hardness, Rockwell C (converted from Brinell hardness. Value below normal HRC range, for comparison purposes only) 17 17
Hardness, Vickers (converted from Brinell hardness) 228 228
Machinability (annealed and cold drawn. Based on a machinability of 100 for AISI 1212 steel.) 50 50


Thermal properties

The following table describes the thermal properties of AISI 4340 alloy steel.






Properties Metric Imperial
Coefficient of thermal expansion (20°C/68°F, specimen oil quenched, tempered at 600°C (1110°F) 12.3 µm/m°C 6.83 µin/in°F
Thermal conductivity (typical steel) 44.5W/mK 309 BTU in/h.ft².°F


Other designations

Other designations equivalent to AISI 4340 alloy steel include the following:








ADM 6359 ADM 6454 ASTM A331 (4340) ASTM A711 SAE J1397 (4340)
AMS 6409 ASTM A29 (4340) ASTM A506 (4340) ASTM A752 (4340) SAE J404 (4340)
ADM 6414 ASTM A320 (L43) ASTM A519 (4340) ASTM A829 SAE J412 (4340)
AMS 6415 ASTM A322 (4340) ASTM A646 (4340-7) MIL S-5000


Manufacturing and heat treatment


Machinability

AISI 4340 alloy steel can be machined using all conventional techniques. The machining process can be performed under annealed or normalized and tempered conditions.


Forming

AISI 4340 alloy steel has good ductility and formability in the annealed condition. It can be bent or formed by pressing or spinning in the annealed state.


Welding

AISI 4340 alloy steel can be fusion or resistance welded. Preheating and post-heat welding procedures are followed when welding this steel according to established methods.


Heat treatment

AISI 4340 alloy steel is heat treated at 830°C (1525°F) followed by oil quenching.


To forge

AISI 4340 alloy steel is forged at 427 to 1233°C (1800 to 2250°F).


Cold operation

AISI 4340 alloy steel can be cold worked using all conventional methods in the annealed condition. It has high ductility.


Annealed

AISI 4340 alloy steel is annealed at 844°C (1550°F) followed by furnace cooling.


Hardening

AISI 4340 alloy steel should be heat treated or normalized and heat treated before tempering. Tempering temperatures depend on the strength level desired.


Hardening

AISI 4340 alloy steel can be hardened by cold working or heat treatment.


Apps

AISI 4340 alloy steel is mainly used in gears and power transmission shafts, aircraft landing gears and other structural parts.

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