AISI 4340
AISI 4340 is a high-strength, low-alloy steel widely used in forged components due to its excellent toughness, fatigue resistance, and high tensile strength. It is part of the nickel-chromium-molybdenum family and is commonly heat-treated to achieve optimal mechanical properties.
Descriptions
1. Chemical Composition
The chemical composition of AISI 4340 steel is critical to its performance. Key alloying elements include nickel, chromium, and molybdenum, which enhance hardenability and strength.
Element | Composition Range (wt%) |
Carbon (C) | 0.38-0.43% |
Manganese (Mn) | 0.60-0.80% |
Silicon (Si) | 0.15-0.30% |
Chromium (Cr) | 0.70-0.90% |
Nickel (Ni) | 1.65-2.00% |
Molybdenum (Mo) | 0.20-0.30% |
Phosphorus (P) | ≤0.025% |
Sulfur (S) | ≤0.025% |
Iron (Fe) | Balance |
2. Mechanical Properties
AISI 4340 exhibits exceptional mechanical properties after heat treatment (e.g., quenching and tempering). Properties vary based on processing conditions.
Property | Typical Value | Heat Treatment Condition |
Tensile Strength | 930-1080 MPa (135-157 ksi) | Quenched & Tempered (Q&T) |
Yield Strength | 785-930 MPa(114-135 ksi) | Quenched & Tempered (Q&T) |
Elongation (in 50 mm) | 12-22% | Q&T |
Reduction of Area | Reduction of Area | Q&T |
Charpy Impact Energy (V-notch) | 20-40J(15-30 ft-lb) | Q&T |
Hardness (Rockwell C) | 28-35 HRC | Q&T |
Fatigue Strength | ~500 MPa(73 ksi) | Q&T (10 cycles) |
3. Key Advantages
Superior fatigue and fracture resistance.
Excellent response to heat treatment (deep hardening).
Retains strength at elevated temperatures (up to ~400°C).
Weldable with pre-/post-heat treatment.
4. Industry-specific standards
ASTM A434: Standard specification for steel bars, alloy, hot-wrought.
AMS 6414/AMS 6415: Aerospace material specifications for Q&T steel.
DIN 1.6565: European designation for equivalent alloy.
UNS G43400: Unified numbering system code.
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Applications
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