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DIN 35NiCr6 1.5815 Ni-Cr Alloy Steel

Grade: 35NiCr6 1.5815
 
35NiCr6/1.5815 is a widely used nickel-chromium alloy quenched and tempered steel. Its chemical composition is based on a medium carbon content (0.30-0.37%), with nickel (1.20-1.60%) and chromium (0.80-1.10%) as the core alloying elements. The addition of nickel significantly enhances the material's low-temperature toughness, hardenability, and overall toughness levels. Chromium synergistically improves hardenability, strength, and wear resistance. After quenching and tempering treatment, this material achieves an ideal combination of high strength, good plasticity, and impact toughness.
Availability:
Quantity:
  • 35NiCr6

  • Qilu


Product Overview


35NiCr6, also known by the material number 1.5815 under European standards, is a widely used nickel-chromium alloy quenched and tempered steel compliant with EN 10083-3.


Alloyed with nickel and chromium as core elements, this steel delivers an optimal balance of high tensile strength, excellent low-temperature toughness, superior hardenability, good machinability and wear resistance. After standard quenching and tempering (QT) treatment, it maintains stable comprehensive mechanical properties, making it a preferred material for heavy-load, impact-resistant and alternating-stress components in heavy machinery, automotive, mining, wind power and engineering structures.


Compared with ordinary alloy steel, the addition of nickel greatly improves the material’s cold resistance and overall toughness, while chromium further enhances hardenability, surface strength and abrasion resistance. Its uniform material structure and reliable fatigue resistance ensure long service life for critical transmission parts under harsh working conditions.


Product Features


Chemical Composition


Grade

C

Si

Mn

P

S

Cr

Ni

35NiCr6/1.5815

0.30-0.37

0.40Max

0.60-0.90

0.025Max

0.025Max

0.80-1.10

1.20-1.60


Mechanical Properties


Mechanical indicators vary slightly according to material cross-section size. All test samples are taken 12.5 mm below the heat-treated surface as required by EN 10083-1.


Size range

Tensile strength

Yield strength

Alongation

Area of reduction

Impact value At RT/J

d≤16

t≤8

880-1080Mpa

740Mpa Min

12% Min

40% Min

/

16<d≤40

8<t≤20

880-1080Mpa

740Mpa Min

14% Min

40%Min

35J Min

40<d≤100

20<t≤60

780-980Mpa

640Mpa Min

15% Min

40%Min

35J Min


Surface hardness & hardenability


Heat Treatment

Hardness

Soft annealed (+A)

HB223Max

Quenched and tempred (+QT)

HRC28-32(Common Range)


End-Quench Hardenability

Three hardenability grades (+H / +HH / +HL) are available for customized orders, applicable to parts with different hardening depth requirements:


  • +H (Normal Hardenability): Hardness range 35 ~ 58 HRC at 1.5–35 mm from quenched end;

  • +HH (High Hardenability): Higher minimum hardness (45 ~ 58 HRC), for thick-walled parts requiring full hardening;

  • +HL (Low Hardenability): Lower maximum hardness (40 ~ 54 HRC), for parts needing partial softening and easy machining.


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

58

58

58

57

57

55

55

55

53

53

50

50

/

/

/

min

49

49

49

48

48

44

44

44

40

40

35

35

/

/

/

Hardness

In HRC + HH

max

58

58

58

57

57

55

55

55

53

53

50

50

/

/

/

min

53

53

53

52

52

50

50

50

48

48

45

45

/

/

/

Hardness

In HRC + HL

max

54

54

54

53

53

49

49

49

45

45

40

40

/

/

/

min

49

49

49

48

48

44

44

44

40

40

35

35

/

/

/


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


35NiCr6 alloy steel


Forging Process


  • Heating temperature: 1150 ~ 1200 ℃ (uniform heating to avoid local overheating);

  • Cooling method: Air cooling after forging.


Heat Treatment


Soft Annealed


  • Heat to 550 ~ 650 ℃, hold for sufficient time, then furnace cooling or air cooling.

  • Purpose: Reduce hardness (≤HB 223), improve cutting performance, relieve internal stress.


Normalizing


  • Heat to 860 ~ 880 ℃, hold, then air cooling.

  • Purpose: Refine grain, homogenize structure, prepare for subsequent quenching and tempering.


Quenching & Tempering


  • Quenching: Heat to 840 ~ 860 ℃, hold, water quenching (low temperature section) or oil quenching (high temperature section);

  • Tempering: Reheat to 530 ~ 630 ℃, hold, then air cooling;

  • Final state: Comprehensive strength + toughness matched, hardness HRC 28~32.


Product Specifications, Delivery Forms & Tolerance


Supply Size Range


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.


Weldability

35NiCr6 / 1.5815 has poor weldability due to medium carbon content and high Ni-Cr alloy content. It is prone to cold cracks and hardened structures in weld seam and heat-affected zone (HAZ).


Applications

Relying on high strength, high toughness, fatigue resistance and wear resistance, 35NiCr6 / 1.5815 is widely used in core load-bearing components across multiple industries:


Heavy Machinery & General Equipment

Heavy-duty transmission gears, engine crankshafts, machine tool spindles, heavy-load connecting rods, high-strength bolts, reducer core parts.


Automotive Industry

Automotive transmission gears, drive shafts, universal joint forks, engine crankshafts, connecting rods, high-stress fastening bolts for commercial vehicles and heavy trucks.


Construction & Mining Machinery

Excavator slewing ring gears, travel mechanism shafts, crane load-bearing parts, crusher gears and drive shafts for mining equipment.


Wind Power & New Energy

Wind turbine gearbox gears and main shafts (long-term stable operation under variable loads).


Mold & Other Fields

High-toughness plastic mold bases, high-load structural parts for petrochemical and marine equipment.


Grade Comparison: 35NiCr6 VS 40Cr / 42CrMo

Customers often compare 35NiCr6 with mainstream domestic alloy steels 40Cr and 42CrMo for material selection. The detailed performance and application differences are as follows:


Comparison Item 35NiCr6 40Cr 42CrMo
Main Alloy Elements Ni + Cr (High nickel) Single Cr Cr + Mo
Low-Temperature Toughness Excellent (-20℃ impact resistance far higher than peers) General Good
Hardenability Excellent, suitable for large cross-section parts Medium (limited critical quenching diameter) Very good
Fatigue Resistance Outstanding (long life under alternating load) Medium Good
Weldability Poor Medium Poor
Typical Hardness (QT) HRC 28~32 HRC 25~35 HRC 30~40
Core Advantages Low-temperature resistance, high toughness, stable fatigue performance Cost-effective, easy processing High strength, high temperature stability, anti-creep
Preferred Application Cold-region equipment, heavy-duty crankshafts, connecting rods, impact gears Ordinary medium-load shafts, bolts, gears High-temperature parts, large-section transmission components


Selection Suggestion:


  • Choose 35NiCr6 if your parts work in low-temperature environments, bear strong impact and long-term alternating loads, or require ultra-high toughness;

  • Choose 40Cr for conventional medium-load parts with cost priority;

  • Choose 42CrMo for parts requiring high-temperature resistance and high static strength.


FAQ


Q1: What is the hardness of 35NiCr6 after quenching and tempering?

A1: The conventional QT hardness is HRC 28~32; soft annealed state ≤ HB 223. We can customize hardenability (+H/+HH/+HL) according to requirements.


Q2: Can 35NiCr6 be welded directly?

A2: Not recommended for direct welding. This steel has high cold crack sensitivity. If welding is necessary, preheat to 200~300 ℃ before welding and perform post-weld tempering for stress relief, and use special nickel-based welding materials.


Q3: What is the difference between 35NiCr6 and 42CrMo?

A3: 35NiCr6 takes nickel as the main alloy element, with better low-temperature toughness and fatigue resistance, suitable for impact and cold working conditions; 42CrMo adds molybdenum, with better high-temperature strength and anti-creep performance, suitable for high-temperature working scenarios.


Q4: What sizes of 35NiCr6 bars are in stock?

A4: We have hot-rolled bars from Φ16 mm to Φ230 mm in stock, and can provide forged bars up to Φ800 mm, steel plates and forged blocks. Support cutting, finishing and customized processing.


Inquire Now: Get the latest quotation, stock status and technical parameters.


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