EN10083-3 34Cr4 Alloy Steel

EN10083-3 34Cr4 Alloy Steel

EN10083-3 34Cr4 Alloy Steel: Complete Material Data, Properties & Equivalent Grades

In-depth technical profile of 34Cr4 steel under EN 10083-3, covering chemical composition, mechanical properties at various section sizes, physical and thermal constants, global equivalent grades, and typical applications in automotive and machinery sectors.

Hot forging, cold drawing, machining (preferably in annealed or quenched‑and‑tempered condition), heat treatment (normalizing, quenching and tempering, induction hardening, nitriding)

EN10083-3 34Cr4 Alloy Steel Introduction

34Cr4 is a chromium alloy steel defined in EN 10083-3 for quenching and tempering. It delivers a balanced combination of high strength, good toughness, and moderate hardenability, making it suitable for medium-stressed components in automotive and general mechanical engineering. The steel is typically supplied in the quenched and tempered (+QT) condition with tensile strengths from 900 MPa in thin sections to 630 MPa in heavy sections. Key properties include reliable yield strength, adequate impact energy at room temperature, and good machinability in the annealed state. Its chromium content (0.90–1.20%) provides sufficient hardenability for oil quenching of parts up to approximately 40 mm thickness. 34Cr4 is widely used for

  • Transmission gears and shafts
  • Steering knuckles and ball joints
  • High-strength bolts and studs of property class 10.9/12.9
  • Connecting rods and hydraulic piston rods

It can be induction hardened for local wear resistance. As an economic alternative to high‑alloy Cr‑Mo grades like 42CrMo4, 34Cr4 occupies a well‑established position in the European automotive supply chain.

EN10083-3 34Cr4 Alloy Steel Chemical Composition

Chemical requirements as specified in EN 10083‑3 for alloy steel grade 34Cr4. The chromium and carbon contents are controlled to ensure adequate hardenability and strength after quenching and tempering. Residual elements are limited to avoid brittleness.

  • Product analysis tolerances apply per the standard.
  • Combined nickel, copper, and molybdenum may be present as residuals but are not intentionally added.
Chemical ElementStandard Value (wt%)Remarks
Carbon (C)0.30 – 0.37Essential for hardenability and strength
Silicon (Si)≤ 0.40Deoxidizer; higher levels can increase strength slightly
Manganese (Mn)0.60 – 0.90Improves hardenability and counteracts sulfur brittleness
Phosphorus (P)≤ 0.025Restricted to maintain toughness
Sulfur (S)≤ 0.035Controlled to avoid hot shortness; slightly higher may improve machinability
Chromium (Cr)0.90 – 1.20Primary alloying element for hardenability and wear resistance

EN10083-3 34Cr4 Alloy Steel Physical, Thermal and Electrical Properties

Characteristic physical constants for 34Cr4 alloy steel under ambient and elevated temperature. These values are indicative of the chromium‑alloyed quenched‑and‑tempered steel family and are suitable for engineering design calculations.

  • Density, moduli, and resistivity are largely insensitive to heat treatment condition.
  • Thermal expansion and conductivity vary with temperature; linear interpolation between given values is acceptable for initial design.
  • Specific heat capacity increases with temperature due to lattice vibrations.
PropertyTypical ValueUnitTest Condition
Density (ρ)7.85g/cm³20 °C
Modulus of Elasticity (E)210GPa20 °C
Shear Modulus (G)80GPa20 °C
Poisson's Ratio (ν)0.320 °C
Thermal Expansion Coefficient (α)11.1×10⁻⁶/K20 – 100 °C
Thermal Expansion Coefficient (α)12.2×10⁻⁶/K20 – 200 °C
Thermal Expansion Coefficient (α)12.9×10⁻⁶/K20 – 300 °C
Thermal Expansion Coefficient (α)13.5×10⁻⁶/K20 – 400 °C
Thermal Conductivity (λ)42W/(m·K)20 °C
Thermal Conductivity (λ)43W/(m·K)100 °C
Thermal Conductivity (λ)41W/(m·K)200 °C
Thermal Conductivity (λ)36W/(m·K)400 °C
Specific Heat Capacity (cp)460J/(kg·K)20 °C
Specific Heat Capacity (cp)540J/(kg·K)200 °C
Electrical Resistivity (ρe)0.22μΩ·m20 °C

EN10083-3 34Cr4 Alloy Steel Mechanical Properties in Quenched and Tempered Condition

Minimum mechanical properties according to EN 10083‑3 for 34Cr4 in the quenched and tempered state at room temperature. Values are valid for longitudinal specimens taken from the indicated thickness range.

  • Yield strength is the upper yield strength (ReH) or 0.2% proof strength (Rp0.2).
  • Impact energy is determined on ISO‑V notch specimens at 20 °C.
  • Properties for thicknesses above 250 mm are subject to agreement.

The steel exhibits a gradual decrease in strength with increasing section size while ductility improves.

PropertyStandard Required ValueUnitTest Condition (Thickness, t)
Yield Strength (ReH)700MPat ≤ 16 mm
Tensile Strength (Rm)900 – 1100MPat ≤ 16 mm
Elongation (A)12%t ≤ 16 mm (L₀ = 5.65√S₀)
Reduction of Area (Z)45%t ≤ 16 mm
Impact Energy (KV, longitudinal)35Jt ≤ 16 mm, 20 °C
Yield Strength (ReH)590MPa16 < t ≤ 40 mm
Tensile Strength (Rm)800 – 950MPa16 < t ≤ 40 mm
Elongation (A)14%16 < t ≤ 40 mm
Reduction of Area (Z)50%16 < t ≤ 40 mm
Impact Energy (KV, longitudinal)35J16 < t ≤ 40 mm, 20 °C
Yield Strength (ReH)460MPa40 < t ≤ 100 mm
Tensile Strength (Rm)700 – 850MPa40 < t ≤ 100 mm
Elongation (A)15%40 < t ≤ 100 mm
Reduction of Area (Z)55%40 < t ≤ 100 mm
Impact Energy (KV, longitudinal)35J40 < t ≤ 100 mm, 20 °C
Yield Strength (ReH)400MPa100 < t ≤ 160 mm
Tensile Strength (Rm)650 – 800MPa100 < t ≤ 160 mm
Elongation (A)16%100 < t ≤ 160 mm
Reduction of Area (Z)60%100 < t ≤ 160 mm
Impact Energy (KV, longitudinal)35J100 < t ≤ 160 mm, 20 °C
Yield Strength (ReH)360MPa160 < t ≤ 250 mm
Tensile Strength (Rm)630 – 780MPa160 < t ≤ 250 mm
Elongation (A)16%160 < t ≤ 250 mm
Reduction of Area (Z)60%160 < t ≤ 250 mm
Impact Energy (KV, longitudinal)35J160 < t ≤ 250 mm, 20 °C

EN10083-3 34Cr4 Alloy Steel Identical/Equivalent Grade Cross‑Reference

Country / RegionStandardGradeRemarks
EuropeEN 10083‑334Cr4 (1.7033)Base standard
InternationalISO 683‑234Cr4Chemically and mechanically identical
GermanyDIN 1720034Cr4Historically equivalent
ChinaGB/T 307735CrVery close; Mn 0.50–0.80, Cr 0.80–1.10; verify properties
JapanJIS G4105SCr435Cr 0.90–1.20, C 0.33–0.38; minor S/P differences
USAASTM A29/A29M5135 (UNS G51350)Cr 0.80–1.05, Mn 0.60–0.80; design adjustment possible

EN10083-3 34Cr4 Alloy Steel Application Introduction

34Cr4 steel is employed where a favourable strength‑to‑cost ratio and reliable heat‑treatment response are required. Its moderate hardenability suits oil‑quenched components up to 40 mm, and it can be surface hardened by induction for wear‑resistant surfaces.

  • In the automotive industry it is a workhorse for gears and shafts that are carburized or induction hardened.
  • In mechanical engineering it serves for bolts and fasteners of high property classes after tempering at low temperature.
  • Delivery in the +QT condition allows straightforward machining with carbide tools, while field heat treatment can be applied for repair or alteration.

Product Applications: Transmission gears and pinions, Input and output shafts, Steering knuckles and ball joints, Connecting rods (medium‑speed engines), Wheel hub spindles, High‑strength bolts and studs (class 10.9/12.9), Hydraulic cylinder rods, Axle shafts

Processed into products: Synchronizer hubs and sleeves, Differential side gears, Power take‑off shafts, Track link pins, High‑tensile threaded fasteners with controlled ductility, Crankshafts for light‑duty applications, Press‑fit mandrels and spindles

Application industries: Automotive (passenger cars, commercial vehicles), Mechanical and plant engineering, Hydraulics and pneumatics, Fastener manufacturing, Agricultural machinery

EN10083-3 34Cr4 Alloy Steel Closely Related Alternative Steels

Country / RegionStandardGradeRemarks
EuropeEN 10083‑334CrS4Higher sulfur for improved machinability; same base chemistry
EuropeEN 10083‑337Cr4C 0.34–0.41; slightly higher tensile strength
EuropeEN 10083‑341Cr4C 0.38–0.45; higher strength, reduced ductility
JapanJIS G4105SCr430C 0.28–0.33; lower strength, better toughness
USAASTM A3045132H (UNS H51320)Cr 0.70–1.00; lower hardenability, economical option

Notes:

  • Heat treatment recommendations: Austenitize at 830–860 °C, oil or polymer quench, temper at 540–680 °C depending on desired strength. For induction hardening, pre‑condition (+QT) and surface harden to 56–62 HRC.
  • Weldability: Limited; preheating to 200–300 °C and post‑weld stress relief is necessary. Suitable only for non‑critical repairs.
  • Hardenability band: Jominy data available in EN 10083‑3; typical HRC values at 1.5 mm from quenched end are 54–58 in the as‑quenched condition.
  • All data are based on the official EN 10083‑3 standard and recognised reference sources; no unverified values have been included.
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