34CrNiMo6 Alloy Steel

34CrNiMo6 Alloy Steel

34CrNiMo6 Alloy Steel | Quenched & Tempered High-Strength Plate EN 10083-3

Comprehensive technical data, chemical composition, mechanical and thermal properties of 34CrNiMo6 high alloy steel according to EN 10083-3, with equivalent grades and application guidelines.

Hot rolling, forging, heat treatment (quenching + tempering), machining, welding (with precautions)

34CrNiMo6 Alloy Steel Introduction

34CrNiMo6 is a high-alloy quenched and tempered steel defined in EN 10083-3, renowned for its exceptional combination of high strength, toughness, and fatigue resistance after appropriate heat treatment. Its chemical composition features carefully balanced additions of chromium, nickel, and molybdenum, which provide deep hardenability and consistent mechanical properties even in large cross-sections.

  • Typical delivery condition is +QT (quenched and tempered), achieving tensile strengths from 750 to 1300 MPa depending on ruling section.
  • Excellent wear resistance and impact toughness allow its use in dynamically loaded components.
  • Widely employed for heavy-duty shafts, gears, crankshafts, and structural parts in automotive, mechanical, and energy industries.

34CrNiMo6 Alloy Steel Chemical Composition

Chemical composition according to EN 10083-3:2006 for 34CrNiMo6 grade. Values represent ladle analysis limits. Residual elements are controlled to ensure hardenability and mechanical properties.

ElementStandard Value (wt%)Remarks
C0.30 – 0.38Core hardenability element
Si≤ 0.40Deoxidizer, strength
Mn0.50 – 0.80Hardenability, strength
P≤ 0.025Maximum for ductility
S≤ 0.035Maximum for toughness
Cr1.30 – 1.70Hardenability, wear resistance
Mo0.15 – 0.30Hardenability, temper resistance
Ni1.30 – 1.70Toughness, hardenability
Cu≤ 0.40Residual element (not required)

34CrNiMo6 Alloy Steel Thermal & Electrical Physical Properties

Typical physical properties of 34CrNiMo6 alloy steel at room temperature unless otherwise noted. These values represent non-guaranteed reference data obtained from standard steel databases and are suitable for design calculations. Actual properties can vary slightly with heat treatment condition.

PropertyTypical ValueUnitTest Condition
Density (ρ)7.85g/cm³Room temperature
Modulus of elasticity (E)210GPaRoom temperature, tensile
Shear modulus (G)80GPaRoom temperature, calculated
Poisson's ratio (ν)0.3Room temperature
Thermal expansion coefficient (α)11.510⁻⁶/KTemperature range 20 – 100 °C
Thermal expansion coefficient (α)12.510⁻⁶/KTemperature range 20 – 200 °C
Thermal expansion coefficient (α)13.010⁻⁶/KTemperature range 20 – 300 °C
Thermal conductivity (λ)42W/(m·K)Room temperature
Specific heat capacity (c)460J/(kg·K)Room temperature
Electrical resistivity (ρ_e)0.25µΩ·mRoom temperature

34CrNiMo6 Alloy Steel Mechanical Properties

Typical mechanical properties of 34CrNiMo6 in quenched and tempered (+QT) condition according to EN 10083-3. Values depend on ruling section diameter. Minimum values are guaranteed; actual values are typically higher. Test specimens taken from a location according to the standard.

PropertyValueUnitTest Condition
Yield strength Rp0.2≥ 900MPaDiameter ≤ 16 mm, +QT, room temperature
Tensile strength Rm1100 – 1300MPaDiameter ≤ 16 mm, +QT, room temperature
Elongation A≥ 10%Diameter ≤ 16 mm, +QT, room temperature
Reduction of area Z≥ 45%Diameter ≤ 16 mm, +QT, room temperature
Impact energy KV (ISO-V)≥ 35JDiameter ≤ 16 mm, +QT, room temperature
Yield strength Rp0.2≥ 800MPa16 mm < diameter ≤ 40 mm, +QT, room temperature
Tensile strength Rm1000 – 1200MPa16 mm < diameter ≤ 40 mm, +QT, room temperature
Elongation A≥ 11%16 mm < diameter ≤ 40 mm, +QT, room temperature
Reduction of area Z≥ 50%16 mm < diameter ≤ 40 mm, +QT, room temperature
Impact energy KV (ISO-V)≥ 45J16 mm < diameter ≤ 40 mm, +QT, room temperature
Yield strength Rp0.2≥ 700MPa40 mm < diameter ≤ 100 mm, +QT, room temperature
Tensile strength Rm900 – 1100MPa40 mm < diameter ≤ 100 mm, +QT, room temperature
Elongation A≥ 12%40 mm < diameter ≤ 100 mm, +QT, room temperature
Reduction of area Z≥ 55%40 mm < diameter ≤ 100 mm, +QT, room temperature
Impact energy KV (ISO-V)≥ 45J40 mm < diameter ≤ 100 mm, +QT, room temperature
Yield strength Rp0.2≥ 600MPa100 mm < diameter ≤ 160 mm, +QT, room temperature
Tensile strength Rm800 – 950MPa100 mm < diameter ≤ 160 mm, +QT, room temperature
Elongation A≥ 13%100 mm < diameter ≤ 160 mm, +QT, room temperature
Reduction of area Z≥ 60%100 mm < diameter ≤ 160 mm, +QT, room temperature
Impact energy KV (ISO-V)≥ 45J100 mm < diameter ≤ 160 mm, +QT, room temperature
Yield strength Rp0.2≥ 550MPa160 mm < diameter ≤ 250 mm, +QT, room temperature
Tensile strength Rm750 – 900MPa160 mm < diameter ≤ 250 mm, +QT, room temperature
Elongation A≥ 14%160 mm < diameter ≤ 250 mm, +QT, room temperature
Reduction of area Z≥ 60%160 mm < diameter ≤ 250 mm, +QT, room temperature
Impact energy KV (ISO-V)≥ 45J160 mm < diameter ≤ 250 mm, +QT, room temperature

34CrNiMo6 Alloy Steel Completely Equivalent Material Standards & Substitutable Grades

Country/RegionStandardGradeRemarks
EuropeEN 10083-334CrNiMo6 (1.6582)Primary standard, identical
InternationalISO 683-234CrNiMo6Equivalent chemistry and mechanical requirements
GermanyDIN EN 10083-334CrNiMo6National adoption, identical to EN

34CrNiMo6 Alloy Steel Application Introduction

34CrNiMo6 is designed for components subjected to high dynamic loads where both strength and toughness are critical. It is typically used in the quenched and tempered (+QT) condition with surface hardening (induction, nitriding) when wear resistance is required. The alloy can be welded with special precautions and preheating.

Product Applications: High-strength gears and pinions, Drive and propeller shafts, Crankshafts and camshafts, Connecting rods and toggle levers, Axle beams and steering knuckles, Bolts, studs and fasteners with high fatigue resistance, Forged rollers, sleeves and rings

Processed into products: Transmission shafts for heavy-duty gearboxes, Wind turbine main shafts, Crankshafts for diesel engines, Forged connecting rods for compressors, Power train pinion shafts, Heavy truck axle shafts, Pump shafts for high pressure service, Induction hardened hollow spindles, High-strength structural bolts (grade 10.9/12.9)

Application industries: Heavy machinery and equipment, Automotive and commercial vehicles, Power generation (turbines, generators), Oil and gas (drilling tools, wellhead components), Mining and earthmoving, General mechanical engineering

34CrNiMo6 Alloy Steel Similar / Alternative Material Recommendations

Country/RegionStandardGradeRemarks
USAASTM A29 / A3224340Ni 1.65-2.00, Cr 0.70-0.90, Mo 0.20-0.30; very similar hardenability, widely used substitute
ChinaGB/T 307740CrNiMoAC 0.37-0.44, comparable Cr-Ni-Mo alloy, often used for similar shaft and gear applications
JapanJIS G4103SNCM439Similar quenched and tempered Cr-Ni-Mo steel, equivalent hardenability band
RussiaGOST 454340KHNMA (40ХНМА)Analogous chemical composition, used in heavy-loaded engineering components

Notes:

Heat treatment recommendation: Austenitizing at 830–870 °C, oil or polymer quenching, tempering typically at 540–660 °C depending on desired strength level. For optimal toughness, double tempering may be applied. Weldability: Limited; preheat to 200–300 °C is mandatory; post-weld heat treatment recommended. Surface hardening: Can be induction hardened or nitrided for enhanced wear resistance without loss of core toughness. Testing certification: EN 10204 type 3.1 or 3.2 certificates are standard for this grade.

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