FE-PL75 F.1260 835M30 EN30B 30NiCrMo16-6 1.6747 Hardened Ste

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FE-PL75 F.1260 835M30 EN30B 30NiCrMo16-6 1.6747 Hardened Steel

FE-PL75 F.1260 835M30 EN30B 30NiCrMo16-6 DIN1.6747 Hardened Steel

FE-PL75 F.1260 835M30 EN30B 30NiCrMo16-6 DIN1.6747 Hardened Steel

1. 1.6747 Description

1.6747 Alloy special steel is nickel air/oil hardening steel. It achieves a good through hardness with high strength and toughness. It is capable of taking a good polish and is widely used as a plastic Mould-steel.  36NiCrMo16, 35NCD16, 30NCD16 are permanent chromium-nickel-molybdenum alloy construction steels for the most heavy-duty machine parts, construction and equipment, and for aviation and aerospace industries.

 

These materials (and their substitutes) are characterized by significantly higher nickel content than 36HNM, 34HNM, 38HNM, and thus better tensile strength and yield point. In addition, they exhibit very good hardenability, impact resistance, load, deformation, wear and tensions resistances.

 

30NiCrMo16 / 1.6747 as the norm itself indicates, has less carbon content. 35NiCrMo16 / 1.2766 grade is classified as a tool steel and is used for the production of special knives or molds for the production of plastics.

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2. 1.6747 Application

High Duty gears, pinions, aero engine connecting rods, differential shafts, transmission components, gudgeon pins, heavy roller bearings, breech mechanisms and small arms components , plastic die casting moulds, header dies and die rings.

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3.All Grades Comparison

DIN BS EN ANFOR UNE AECMA
1.6747 835M30 30NiCrMo16-6 35NCD16 F.1260 FE-PL75
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4.Quality Standard

EN 10083 Steels for quenching and tempering. Technical delivery conditions for alloy steels

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5. 1.6747 Chemical Composition(%)

C Mn Si P S Cr Ni Mo
0.26-0.33 0.50-0.80 0.40 max 0.025 max 0.025 max 1.20-1.50 3.30-4.30 0.30-0.60
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6.Mechanical Properties(T=20°C if not differently stated)

Process Diameter(mm) Tensile Strength Rm (Mpa) Yield Strength Rp0.2 (Mpa) Elongation A5 (%) Area Reduction Ratio C (%) Impact Value Kv (J) Room Temperature Hardness (HB)
SOFT ANNEALED / 915 max / / / / 270 max
QUENCHED AND TEMPERED 16 max 1080-1230 880 min 10 min 45 min / 318-363
QUENCHED AND TEMPERED 16-100 1080-1230 880 min 10 min 45 min 35 min 318-363
QUENCHED AND TEMPERED 100-250 900-1050 790 min 11 min 50 min 35 min 265-310
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7.HEAT TREATMENT:

Process TEMPERATURE °C Cooling Medium
Hot plastic deformation 850-1100 /
Normalization 840-870 air
Soft annealing 640-680 air
Hardening 840-860 oil
Tempering 540-630 air
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8.Mill′s test certificate:

EN 10204/3.1 with all relevant data reg. chem. composition, mech. properties and results of testing.

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In the 36NiCrMo16, 35NCD16, 30NCD16, 30NiCrMo16 grades we supply:

  • Round, square, hexagonal hot-rolled bars 36NiCrMo16
  • Forgings 36NiCrMo16
  • Drawn and peeled bars 36NiCrMo16
  • Forged square and round bars 36NiCrMo16
  • Forged flat bars 36NiCrMo16

List of equivalents and other determinations of 36NiCrMo16 – 1.6773 steel:

6773, 36 NICRMO 16, 35NCD14, 35 NCD 14, 35NICRMO14, 35 NICRMO 14, 34HN3M, 36HNM, 30NCD16, 30 NCD 16, E30NCD16, 35NCD16, 35 NCD 16, AIR 9160/C, 32HN3M, 30NICRMO16-6, 30 NICRMO 16-6, 1.6747, LW 6747, 6747, 36CH2N4MA, 36KH2N4MA, 36H2N4MA, 36Х2Н4МА, 34CHN3M, 34KHN3M, 34ХН3М, ASNA 3133, ASNA 3134, ASNA 3149, ASNA 3181, ASNA 3197, 1.6746, FE-PL75, FDMA, 30NCD16.