Non-Corrosion Resisting Steel 30NCD16
Technical Data Sheet
|Chemical Composition Limits
4% Ni-Cr-Mo, Alloy Steel, Air Hardening 100 ton, Ruling Section 2.5"
|4S28||0.38 - 0.45||0.60-0.90||0.010||1.45-1.80||0.70-0.95||1.65-2||0.30-0.50||0.05-0.10|
|Chemically similar British Specifications BS.970 Pt2.|
|Other Chemically similar Specifications|
Alloy 30NCD16 is nickel-chrome-moly steel with excellent hardenability and good resistance to fatigue and repeated impact. It is used in a wide range of safety-critical parts, gears and crank shafts in both the aerospace and motorsports industries.
Typical Mechanical Properties
|Alloy||Condition||Tensile Strength N/mm²||Yield Strength N/mm²||Elongation %||Impact Strength (KCU)||Hardness HB|
|Alloy 30NCD16||Quenched & Tempered (200°C)||1750||1250||12||70 J/cm²||-|
|Alloy 30NCD16||Quenched & Tempered (625°C)||1000||900||19||140 J/cm²||-|
For all stock availability contact Sales.
835M30 / EN30B
AFNOR 30NCD16 (FDMA)
AFNOR 35NCD16 (819B)
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Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.
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