EN 10083-3 50CrMo4 High Tensile Alloy Steel

EN 10083-3 50CrMo4 High Tensile Alloy Steel

EN 10083-3 50CrMo4 High Tensile Alloy Steel: Composition, Properties, Equivalents, and Application Guide

Comprehensive material data for 50CrMo4 alloy steel according to EN 10083-3. Includes chemical composition, mechanical and thermal properties, international equivalent grades, and application guidance for high-strength components.

Hot forming, forging, machining, welding (with precautions), induction hardening, nitriding

EN 10083-3 50CrMo4 High Tensile Alloy Steel Introduction

50CrMo4 is a medium-carbon chromium-molybdenum alloy steel specified in EN 10083-3 for quenching and tempering. It offers high hardenability, excellent strength, and good toughness after heat treatment, making it suitable for highly stressed parts. This grade is widely used in mechanical engineering for components such as shafts, gears, and bolts. The material combines good wear resistance with the ability to withstand dynamic loads, and can be surface-hardened by induction or flame hardening. It is delivered in the quenched and tempered condition (+QT) to achieve the required mechanical properties.

EN 10083-3 50CrMo4 High Tensile Alloy Steel Chemical Composition

The chemical composition of 50CrMo4 is controlled to achieve high hardenability and uniform response to heat treatment. Chromium and molybdenum are key alloying elements that increase strength and toughness after quenching and tempering. Carbon content around 0.50% provides a balance between hardness and ductility. Maximum limits are imposed on phosphorus and sulfur to ensure cleanliness and optimal mechanical properties.

Chemical ElementStandard Value (wt%)Remarks
Carbon (C)0.46 – 0.54Based on EN 10083-3 ladle analysis
Silicon (Si)≤ 0.40Deoxidation element
Manganese (Mn)0.50 – 0.80Improves hardenability
Phosphorus (P)≤ 0.025Maximum for premium quality
Sulfur (S)≤ 0.035Control for machinability
Chromium (Cr)0.90 – 1.20Primary hardenability element
Molybdenum (Mo)0.15 – 0.30Enhances hardenability and temper resistance

EN 10083-3 50CrMo4 High Tensile Alloy Steel Physical Properties

The physical properties of 50CrMo4 are representative of chromium-molybdenum alloy steels. Thermal conductivity and expansion are average for this class of materials, allowing predictable behavior during heat treatment and in service. Electrical resistivity is typical of low-alloy steels. Values are provided for general engineering calculations and are not part of the standard's acceptance criteria.

PropertyTypical ValueUnitCondition / Note
Density (ρ)7.83 – 7.85g/cm³Room temperature, average
Modulus of elasticity (E)205 – 215GPa20 °C, dynamic method
Shear modulus (G)~ 80GPaCalculated from E and ν
Poisson's ratio (ν)0.28 – 0.30Elastic region
Thermal expansion coefficient (α)11.5 × 10⁻⁶K⁻¹20 – 100 °C
Thermal expansion coefficient12.5 × 10⁻⁶K⁻¹20 – 200 °C
Thermal expansion coefficient13.0 × 10⁻⁶K⁻¹20 – 300 °C
Thermal conductivity (λ)42 – 44W/(m·K)At 20 °C
Specific heat capacity (cp)~ 460J/(kg·K)Room temperature
Electrical resistivity (ρe)0.20 – 0.25µΩ·m20 °C

EN 10083-3 50CrMo4 High Tensile Alloy Steel Mechanical Properties

The mechanical properties of 50CrMo4 are strongly dependent on section size. Values below represent minimum requirements as specified in EN 10083-3 for different ruling sections. Tensile strength and yield strength decrease with increasing diameter, while ductility and toughness improve. Impact energy is measured on Charpy-V specimens at room temperature. For critical applications supplementary requirements may be agreed.

PropertyStandard Required ValueUnitTest Condition
Tensile strength (Rm)1100 – 1300MPaThickness ≤ 16 mm, +QT
Yield strength (ReH)≥ 900MPaThickness ≤ 16 mm, +QT
Elongation (A5)≥ 9%Thickness ≤ 16 mm, gauge length L0 = 5d
Reduction of area (Z)≥ 40%Thickness ≤ 16 mm
Impact energy (KV2)≥ 35JRoom temperature, ≤ 16 mm
Tensile strength (Rm)1000 – 1200MPa16 mm < thickness ≤ 40 mm, +QT
Yield strength (ReH)≥ 800MPa16 mm < thickness ≤ 40 mm, +QT
Elongation (A5)≥ 10%16 mm < t ≤ 40 mm
Reduction of area (Z)≥ 45%16 mm < t ≤ 40 mm
Impact energy (KV2)≥ 35JRoom temperature, 16–40 mm
Tensile strength (Rm)900 – 1100MPa40 mm < thickness ≤ 100 mm, +QT
Yield strength (ReH)≥ 700MPa40 mm < thickness ≤ 100 mm, +QT
Elongation (A5)≥ 11%40 mm < t ≤ 100 mm
Reduction of area (Z)≥ 50%40 mm < t ≤ 100 mm
Impact energy (KV2)≥ 35JRoom temperature, 40–100 mm
Tensile strength (Rm)800 – 950MPa100 mm < thickness ≤ 160 mm, +QT
Yield strength (ReH)≥ 600MPa100 mm < thickness ≤ 160 mm, +QT
Elongation (A5)≥ 12%100 mm < t ≤ 160 mm
Reduction of area (Z)≥ 55%100 mm < t ≤ 160 mm
Tensile strength (Rm)750 – 900MPa160 mm < thickness ≤ 250 mm, +QT
Yield strength (ReH)≥ 550MPa160 mm < thickness ≤ 250 mm, +QT
Elongation (A5)≥ 13%160 mm < t ≤ 250 mm
Reduction of area (Z)≥ 60%160 mm < t ≤ 250 mm

EN 10083-3 50CrMo4 High Tensile Alloy Steel Fully Equivalent Material Standards and Alternative Designations

Country / RegionStandardDesignation / GradeRemarks
EuropeEN 10083-350CrMo4Original specification
GermanyDIN EN 10083-350CrMo4Identical to EN
InternationalISO 683-250CrMo4Chemically identical
ChinaGB/T 307750CrMoEquivalent chemistry and properties
USAASTM A29 / SAE J4044150 (SAE 4150)Similar, slight variations in Mn range
JapanJIS G4053SCM445Approximate, similar composition

EN 10083-3 50CrMo4 High Tensile Alloy Steel Application Introduction

50CrMo4 is specified where high static and dynamic strength, combined with moderate toughness, are required. It is particularly suited for components that undergo heat treatment (quenching and tempering) and can benefit from surface hardening. Typical delivery condition +QT provides a ready-to-use material with guaranteed mechanical properties, reducing manufacturing steps. Machining is best performed in the pre-hardened state, and welding requires preheating and post-weld heat treatment due to its high carbon equivalent.

Product Applications: Quenched and tempered steel plates for structural components, Forged round bars and flat bars for machine parts, Seamless pipes and cylinders for hydraulic applications, Wire for high-strength fasteners and springs

Processed into products: Transmission shafts and pinion shafts, Heavy-duty gears, sprockets and gear blanks, Crankshafts and camshafts, High-tensile bolts, studs and nuts (property class 12.9), Piston rods and hydraulic cylinder rods, Steering knuckles and ball joints, Torsion bars and stabilizer links

Application industries: Automotive and heavy vehicle (axles, gears, connecting rods), General mechanical engineering (shafts, spindles, bolts), Oil and gas equipment (flanges, studs, valve bodies), Power generation (turbine shafts, generator rotors), Mining and construction machinery (pins, bushings, track links)

EN 10083-3 50CrMo4 High Tensile Alloy Steel Similar / Closely Related Grades for Alternative Selection

Country / RegionStandardDesignation / GradeComparison Notes
EuropeEN 10083-342CrMo4 (1.7225)Lower carbon (0.38–0.45%), lower core strength but better toughness; widely used substitute for slightly lower loads
EuropeEN 10083-334CrNiMo6 (1.6582)Ni-added grade with higher toughness and through-hardening capability for heavier sections
GermanyDIN 1720050CrV4Vanadium microalloyed; higher fatigue strength, often used for springs and torsion bars
USAASTM A3224140 (SAE 4140)Lower carbon and chromium; less hardenable than 50CrMo4, suitable where moderate strength is adequate
JapanJIS G4053SCM440Similar to 42CrMo4; lower strength compared to 50CrMo4

Notes:

Additional considerations:

  • For optimal properties, quenching should be carried out in oil or polymer; water quenching may cause cracking in complex shapes.
  • Stress relieving after machining is recommended at 550–600 °C.
  • Surface hardening can achieve a nitrided layer or induction-hardened case depth for improved wear resistance.
  • Welding should be performed according to approved procedures; filler metals of comparable composition (e.g., ER80S-D2) and preheating to 250–350 °C are typical.
  • This grade can be supplied in the +QT (quenched and tempered) or +A (annealed) condition as per EN 10083-3; the tensile test values shown are mandatory for the +QT condition and are guaranteed for ruling sections specified in the standard.
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