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DIN 39NiCrMo3 1.6510 AISI 9840 Alloy Steel

Grade: DIN 39NiCrMo3 1.6510
Equivalent Steel: AISI 9840
 
39NiCrMo3/1.6510 is a widely used high-performance nickel-chromium-molybdenum alloy quenched and tempered steel. It features a medium carbon content (0.35–0.43%) and contains alloying elements such as nickel (0.70–1.00%), chromium (0.60–1.00%), and molybdenum (0.15–0.25%). After quenching and tempering, it achieves a balance of high strength, good toughness, and excellent low-temperature impact performance. It is particularly suitable for critical engineering components subjected to high loads, high impacts, and fatigue stresses, such as heavy-duty gears, drive shafts, crankshafts, and important structural fasteners.
Availability:
Quantity:
  • 9840

  • Qilu


Product Overview


39NiCrMo3 (material number 1.6510) is a high‑performance nickel‑chromium‑molybdenum alloy quenched and tempered steel defined in EN 10083‑3. It offers an outstanding balance of high strength, excellent toughness, superior low‑temperature impact resistance, and good fatigue performance, making it ideal for heavily loaded, impact‑resistant, and fatigue‑critical components across heavy machinery, automotive, aerospace, energy, and engineering structures.


Equivalent Grades


Country

USA

Europe

Standard

ASTM A29

EN10083-3

Grade

9840

39NiCrMo3/1.6510


Product Features


Chemical composition


Grade

C

Si

Mn

P

S

Cr

Mo

Ni

39NiCrMo3/1.6510

0.35-0.43

0.40Max

0.50-0.80

0.025Max

0.035Max

0.60-1.00 0.15-0.25

0.70-1.00


Mechanical Properties (Quenched + Tempered, EN 10083‑3)


Size range

Tensile strength

Yield strength

Alongation

Area of reduction

Impact value At RT/J

d≤16

t≤8

980-1180Mpa

785Mpa Min

11% Min

40% Min

/

16<d≤40

8<t≤20

930-1130Mpa

735Mpa Min

11% Min

40% Min

35J Min

40<d≤100

20<t≤60

880-1080Mpa

685Mpa Min

12% Min

45% Min

40J Min

100<d≤160

60<t≤100

830-980Mpa 635Mpa Min 12% Min 50% Min 40J Min
160<d≤250

100<t≤160

740-880Mpa 540Mpa Min 13% Min 50% Min 40J Min


Test specimens are taken 12.5 mm below the heat‑treated surface per EN 10083‑1


Hardness & Hardenability


Heat Treatment

Hardness

Soft annealed (+A)

HB240Max

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

60

60

59

58

58

57

57

56

55

52

51

49

48

46

45

min

52

51

50

49

48

46

44

43

39

36

34

33

32

31

30

Hardness

In HRC + HH

max

60

60

59

58

58

57

57

56

55

52

51

49

48

46

45

min

55

54

53

52

51

50

48

47

44

41

40

38

37

36

35

Hardness

In HRC + HL

max

57

57

56

55

55

53

53

52

50

47

45

44

43

41

40

min

52

51

50

49

48

46

44

43

39

36

34

33

32

31

30


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


39NiCrMo3


Supply Forms, Sizes & Tolerances


Product type

Size range

Length

Hot rolled bar

Φ16-Φ300mm

6000-9000mm

Hot forged bar

Φ140-Φ800mm

3000-5800mm

Hot rolled plate/sheet

T:12-120mm; W:1500-2500mm

2000-5800mm

Hot Forged block

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

2000-5800mm


Surface Finish & Tolerance


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.


To ensure optimal performance for your application, we produce 1.6510 high speed tool steel on a dedicated make-to-order basis. This approach guarantees fresh production and allows us to customize the process for your specific requirements. Tell us your needs, and let's get started.


Forging & Heat Treatment


Forging


  • Heating temperature: 1150–1200 °C

  • Cooling: Air cool after forging


Heat Treatment


1. Soft Annealing

Heat to 830–860 °C → Furnace cool


2. Normalizing

Heat to 860–900 °C → Air cool


3. Quenching + Tempering

  • Quench: 830–850 °C → Water or oil

  • Temper: 550–650 °C → Air cool

  • Note: Lower temps for water quenching; higher temps for oil quenching


Weldability

39NiCrMo3 has limited weldability due to medium carbon (0.35–0.43%) and high alloy content, leading to high hardenability and risk of hydrogen‑induced cold cracking.


  • Preheat recommended: 250–350 °C

  • Use low‑hydrogen electrodes

  • Post‑weld tempering to restore toughness and reduce residual stress


Typical Applications

39NiCrMo3 is widely used for critical components requiring high strength, toughness, and fatigue resistance:


Automotive & Heavy Vehicles

Crankshafts, connecting rods, drive shafts, heavy‑duty gears, universal joint forks


Aerospace & Defense

Aircraft landing gear parts, rotor shafts, high‑strength bolts, hinge joints


Machinery Manufacturing

Heavy‑duty spindles, turbine/compressor shafts, large pump shafts, die‑casting mold sleeves


Energy & Heavy Engineering

Wind turbine gearbox parts, oil drill pipe joints, blowout preventer components, high‑strength fasteners


FAQ


Q1: What is 39NiCrMo3 steel?

A1: 39NiCrMo3 (1.6510) is a nickel‑chromium‑molybdenum alloy quenched and tempered steel per EN 10083‑3. It delivers high strength, good toughness, excellent low‑temperature impact, and fatigue resistance for heavy‑load critical parts.


Q2: What is the equivalent grade of 1.6510?

A2: 1.6510 (39NiCrMo3) is equivalent to AISI 9840 in the US system. It is similar in performance to GB 40CrNiMo.


Q3: Is 39NiCrMo3 weldable?

A3: It has limited weldability. Preheating (250–350 °C), low‑hydrogen welding consumables, and post‑weld tempering are required to avoid cold cracking.


Q4: What heat treatment is used for 39NiCrMo3?

A4: The standard process is quenching at 830–850 °C + tempering at 550–650 °C to achieve balanced strength and toughness.


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