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AISI 5140 41Cr4 1.7035 SCr440 Alloy Steel

Grade: ASTM 5140
Equivalent Steel: DIN 41Cr4/1.7035, JIS SCr440, GB 40Cr

 

AISI 5140 is a medium-carbon chromium alloy steel built on a carefully balanced chemistry of carbon (0.38–0.43%), chromium (0.70–0.90%), and manganese (0.70–0.90%), with a small silicon addition (0.15–0.35%). This composition delivers good hardenability and well-rounded mechanical properties, allowing the steel to achieve an optimal balance of strength, toughness, and wear resistance after quenching and tempering—making it well suited for load-bearing parts such as gears, shafts, and high-strength fasteners.

Availability:
Quantity:
  • 5140

  • Qilu


Product Overview


AISI 5140 is a medium-carbon chromium alloy steel developed for engineering components that require a practical combination of strength, toughness, wear resistance, machinability, and heat-treatment response. It is commonly supplied as hot rolled bar, forged bar, cold drawn bar, and other customized forms depending on the application.


The grade is frequently associated with DIN 41Cr4, EN 1.7035, JIS SCr440 and GB 40Cr, although these designations should not automatically be treated as technically identical because chemical composition limits and product standards can differ. The applicable specification should always be confirmed before material substitution.


AISI 5140 / 41Cr4 is particularly suitable for shafts, gears, pins, axles, bolts, spindles, machine components, automotive parts and general engineering components that operate under moderate to high mechanical loads.


Steel Equivalent Grade


Country

USA

Europe

China

British

Japan

Standard

ASTM A29

EN10083-3

GB/T3077

BS970

JIS G4104

Grade

5140

41Cr4/1.7035

40Cr

530M40

SCr440


Product Features


Chemical Composition 


Grade

C

Si

Mn

P

S

Cr

5140

0.38-0.43

0.15-0.35

0.70-0.90

0.035Max

0.040Max

0.70-0.90

41Cr4/1.7035

0.38-0.45

0.40Max

0.60-0.90

0.035Max

0.035Max

0.90-1.20

40Cr

0.37-0.44

0.17-0.37

0.50-0.80

0.030Max

0.030Max

0.80-1.10

530M40

0.36-0.44

0.10-0.40

0.60-0.90

0.035Max

0.040Max

0.90-1.20

SCr440

0.38-0.43

0.15-0.35

0.60-0.85

0.030Max

0.030Max

0.90-1.20


Mechanical properties


Mechanical properties for 41Cr4 quenching and tempering alloy steel according to EN10083-3.


Size range

Tensile strength

Yield strength

Alongation

Area of reduction

Impact value At RT/J

d≤16

t≤8

1000-1200Mpa

800Mpa Min

11% Min

30% Min

/

16<d≤40

8<t≤20

900-1100Mpa

660Mpa Min

12% Min

35%Min

35J Min

40<d≤100

20<t≤60

800-950Mpa

560Mpa Min

14% Min

40%Min

35J Min


Sampling and preparation of test pieces for 41Cr4 quenching and tempering steel.

1): According to EN10083-1, all samples shall be taken at a distance of 12.5mm below the heat treated surface

2): As stipulated in the contract between buyer and seller.


Mechanical properties for 41Cr4 open die forgings steel according to EN10250-3


Size range

Tensile strength

Yield strength

Alongation

Impact value

At RT/J

14% Min

35J Min

d≤70

800Mpa Min

560Mpa Min


Sampling and preparation of test pieces for steel forging.

1: According to EN10250-1, all samples shall be taken at a distance of 4/T below the heat treated surface (with a minimum of 20mm and a maximum of 80mm), and t/2 from the end (where t is the equivalent thickness of the thickness of the ruling section of the forging at the time of heat treatment.

2: As stipulated in the contract between buyer and seller.


Surface hardness and hardenability


Heat Treatment

Hardness

Flame or Induction hardening

53HRC

Treated to improve shearability (+S)

HB255Max

Soft annealed (+A)

HB241Max

Quenched and tempred (+QT)

HRC28-32(Common Range)


Where the steel is ordered by using the symbols for normal (+H) or restricted (+HL, +HH) hardenability requirements, the hardenability values should apply below:


Distance in mm from quenched end

Distance

1.5

3

5

7

9

11

13

15

20

25

30

35

40

45

50

Hardness

In HRC + H

max

61

61

60

59

58

56

54

52

46

42

40

38

37

36

35

min

53

52

50

47

41

37

34

32

29

26

23

21

/

/

/

Hardness

In HRC + HH

max

61

61

60

59

58

56

54

52

46

42

40

38

37

36

35

min

56

55

53

51

47

43

41

39

35

31

29

27

26

25

24

Hardness

In HRC + HL

max

58

58

57

55

52

50

47

45

40

37

34

32

31

30

29

min

53

52

50

47

41

37

34

32

29

26

23

21

/

/

/


Scatter bands for the Rockwell - C hardness in the end quench hardenability test.


41Cr4 end‑quench hardenability curve chart +H +HH +HL grades


Supply size & Tolerance & Stock size


Product type

Size range

Length

Cold drawn bar

Φ3-Φ80mm

6000-9000mm

Hot rolled bar

Φ18-Φ300mm

6000-9000mm

Hot forged bar

Φ100-Φ1200mm

3000-5800mm

Hot rolled plate/sheet

T:3-200mm; W:1500-2500mm

2000-5800mm

Hot Forged block

T: 80-800mm; W: 100-2500mm

2000-5800mm


Surface Finish

Turned

Milled

Grinding(Best)

Polished(Best)

Peeled(Best)

Black Forged

Black Rolled

Tolerance

+0/+3mm

+0/+3mm

+0/+0.05mm

+0/+0.05mm

+0/+0.1mm

+0/+5mm

+0/+1mm

Straighness

1mm/1000mm max.

3mm/1000mm max.


Hunan Qilu Steel maintains monthly stocks of hot-rolled and cold-drawn bars (over 10,000 tons) in popular diameters (e.g., 18mm, 24mm, 50mm, 72mm, 100mm, 200mm), ensuring fast delivery for urgent orders.


Below our our stock size:


18 20 22 24 25 28 30 32 35 36 38 40 42 48
48 50 52 55 60 65 70 72 75 80 85 90 95 100
105 110 115 120 125

130

140 150 160 170 180 190 200 210
220 230 240 250 260 270 280 290 300





Optimized Heat Treatment & Forging Processes


  • Soft annealing: Heat to 670-710℃, soak at temperature, then furnace-cool. This reduces internal stress and lowers hardness for machining.

  • Normalization: Heat to 850-880℃, soak, then air-cool. Refines the microstructure, improving uniformity for subsequent QT treatment.

  • Quenching and tempering: Heat to 820-860℃ (lower end for water quenching, upper end for oil quenching), soak, quench in water or oil, then temper at 540-680℃ and air-cool. This process develops the alloy’s signature strength-toughness balance.

  • Forging: Heat ingots to 1150-1200℃, forge at a minimum temperature of 800-850℃, then sand-cool to prevent cracking. Forged components benefit from grain refinement, enhancing overall durability.


Weldability Considerations


While DIN 41Cr4 1.7035 offers exceptional performance, its weldability is classified as moderate to poor due to its carbon content (0.38-0.45%)—exceeding the 0.25% threshold where weldability begins to deteriorate. To minimize cracking during welding:


  • Preheat the base material to 200-300℃ before welding.

  • Use low-hydrogen electrodes (e.g., E7018) to reduce hydrogen-induced cracking.

  • Maintain interpass temperatures above 200℃ during multi-pass welding.

  • Post-weld heat treatment (PWHT) at 600-650℃ to relieve residual stress.


These steps ensure welded joints retain sufficient strength for non-critical applications; for high-stress components, mechanical fastening (e.g., bolts) is preferred over welding.


Applications


Automotive Industry Critical Components


  • Transmission systems: Gears, drive shafts, and camshafts—benefiting from the alloy’s 1000-1200 MPa tensile strength and wear resistance (53 HRC via induction hardening).

  • Chassis and suspension: Steering knuckles, steering shafts, and suspension arms—leveraging the alloy’s toughness (35 J impact resistance) to withstand road shocks.

  • Engine and powertrain: Cylinder piston rods, hydraulic valve cores, and connecting rods—where the QT-induced 28-32 HRC hardness balances strength and machinability for precision fitting.


Mechanical Engineering & Heavy Machinery


  • Power transmission: Gearboxes, differential parts, and torque converters—relying on the alloy’s uniform hardenability to maintain strength across thick sections.

  • Fasteners and structural parts: High-strength bolts, flanges, and brackets—benefiting from the alloy’s ≥560 MPa yield strength to resist loosening under heavy loads.

  • Hydraulic and pneumatic systems: Hydraulic cylinder rods and valve spools—where the alloy’s machinability (≤241 HB after soft annealing) enables tight tolerances and smooth surfaces.


Mold & Tooling Accessories

  • Mold bases and fixtures: Jigs, fixtures, and tooling substrates—where the alloy’s soft annealing hardness (≤241 HB) allows easy machining of complex shapes, and subsequent QT treatment (28-32 HRC) provides long-term dimensional stability.

  • Auxiliary mold components: Ejector pins and guide pillars—benefiting from the alloy’s wear resistance to withstand repeated cycles in injection molding or stamping processes.


Agricultural & Industrial Wear Parts


  • Agricultural machinery: Harvester knives, thresher shafts, and transmission chains—leveraging the alloy’s 53 HRC surface hardness (flame-hardened) to resist wear from crop residue and soil.

  • Industrial wear components: Bearing rings, rolling elements, and conveyor rollers—where the alloy’s combination of hardness (28-32 HRC) and toughness (35 J impact) prevents premature failure.

  • Mining and construction: Crusher parts and screen shafts—benefiting from the alloy’s forging capability (up to Φ1200mm) to create large, durable components for heavy-duty operations.


FAQ


Q1: Is AISI 5140 the same as 41Cr4?

A1: AISI 5140 and DIN/EN 41Cr4 are commonly compared as equivalent or closely related grades, but they are not automatically identical in every specification. Chemical composition limits and mechanical requirements can differ, so the applicable standard should be stated on the purchase order.


Q2: Is 5140 better than 4140?

A2: Not necessarily. 4140 generally provides higher hardenability and stronger performance for demanding applications, while 5140 can offer a cost-effective solution for general engineering components where the additional molybdenum in 4140 is unnecessary.


Q3: Is 5140 better than 1045?

A3: For components requiring deeper hardening, improved wear resistance and better performance under higher mechanical loads, 5140 is generally the stronger choice. 1045 remains attractive when lower cost and simpler machining are priorities.


Q4: Can 5140 be welded?

A4: 5140 is not normally selected primarily for welding because its medium-carbon content and alloying elements can increase cracking risk compared with low-carbon structural steels. If welding is unavoidable, a qualified welding procedure, preheating and appropriate post-weld treatment should be evaluated.


Q5: What is the difference between 5140 and 40Cr?

A5: 5140 and 40Cr have similar medium-carbon chromium-alloy characteristics, but their standards and chemical limits are different. They should be purchased according to the required specification rather than treated as automatically interchangeable.


Q6: What is the difference between 41Cr4 and 42CrMo4?

A6: Both are quenched-and-tempered chromium alloy steels, but 42CrMo4 contains molybdenum, which generally provides higher hardenability and improved performance in demanding sections. 41Cr4 is often selected for less demanding applications where the additional alloying of 42CrMo4 is unnecessary.


Contact us for real-time stock availability, custom quotes, or technical consultation—we deliver global-grade alloy steel to your doorstep, with flexible shipping options for all industries.


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