.

42CrMo4 Alloy Structural Steel

Description:

42CrMo4 materials have been widely used in automotive driving elements. Although 42CrMo4 is more expensive than 41Cr4, it is more preferable in terms of material properties. In this study, these two materials were heat treated by austenitizing in a continuous furnace at 850°C and quenched in oil at 90°C. After they were tempered at various temperatures, mechanical properties were determined for each tempering temperature. The material properties for both materials were compared with each other. Results indicated that same mechanical properties for 41Cr4 and 42CrMo4 can be achieved by tempering 41Cr4 about 50°C lower temperature than for 42CrMo4. In addition to the mechanical tests, fatigue tests were performed for both materials. Weibull distributions were plotted. Results indicated that 42CrMo4 had a longer life than 41Cr4 material.

Chemical Composition

Properties

Metric

Imperial

Hardness, Brinell (typical)

300

33

Hardness, Rockwell C (typical)

30

30

Tensile strength, ultimate

965-1030 MPa

psi

Yield strength,

827-862 MPa

psi

Elongation at break (in 50 mm (2"))

Compressive strength

862 MPa

125000 psi

Charpy impact (V-Notch)

Poisson's ratio

Elastic modulus

190-210 GPa

ksi

Hot forming

Narmalaizing+N

Quenching+Q

Quenching+Q

Tempering+T

Stress-relieving+SR

1100-850C

870 C air

860 C oil or polymer

850 C water

540-680 C

50°C under the temperature

Soft annealing+A

Isothermal annealing+i

Spheroidizing annealing+AC

End Quench hardenability test

Pre heating welding

Stress-relieving after welding

720 C air(HP max 241)

820 C fumace cooling to 670 C, then air (HB max 200)

840 C water

300 C

550 C fumace cooling

Ac1

Ac3

Ms

Mf

745 C

790 C

335 C

120 C

Mechanical Properties((Hardened and Tempered):

Dia Scope(mm)

Tensile Strength Rm (Mpa)

Yield Strength R2 (Mpa)

Elongation (longitudinal direction) Al (%)

Reduction of area (%)

Impact Energy Joules (-20°C)

16 max

1100-1300

900 min

10 min

40 min

30 min

16-40

1000-1200

750 min

11 min

45 min

35 min

40-100

900-1100

650 min

12 min

50 min

35 min

100-160

800-950

650 min

13 min

50 min

35 min

160-250

750-900

500 min

14 min

55 min

35 min

Heat Treatment:

  • Forging: Heat to 1150°C Hold until uniform.Minimum forging temperature 850°C. Cool slowly in ashes or sand etc.
  • Annealing: Heat to 830°C – 850°C. Cool in furnace.
  • Normalising: Heat to 870°C – 900°C. Cool in still air.

Forging

Heat to 1150 °C Hold until uniform. Minimum forging temperature 850°C. Cool slowly in ashes or sand etc.

ANNEALING

Heat to 830°C – 850°C. Cool in furnace.

Normalizing

Heat to 870°C – 900°C. Cool in still air.

Stress Relieving:

• Annealed: Heat to 600°C – 650°C • Hardened: Heat to 500°C – 550°C. Cool in still air • Hardening:Heat to 830°C – 880°C. Quench in oil or polymer. • Tempering:Heat to 450°C – 700°C cool in still air. NB. Tempering within the range 200°C–420°C will result in temper brittleness and should be avoided Flame and Induction Hardening: Heat quickly to the required case depth at 860°C – 890°C and quench immediately in water or oil. Tempering at 150°C – 200°C will reduce stresses in the case with minimal effect on its hardness. All de-carburised surface material must first be removed to ensure best results. • Nitriding: Heat to 500°C – 530°C and hold for sufficient time to develop the depth of case required Parts should be pre-hardened and tempered as required and also premachined leaving a small grinding allowance only.



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