NiCr20Co18Ti | 2.4969 Material Datasheet

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Material Description

Material Number Material Name Material Number (single) Standard Standard Status Country VDA 231-106 classification Application temperature [°C]
2.4969 (Stahlschlüssel 2001) NiCr20Co18Ti 2.4969 Stahlschlüssel 2001 Replaced Germany 3.4 ≤ 1000 1)
1) Remark: The material NiCr20Co18Ti with the material number 2.4969 is, as aviation material with the material number 2.4632, also contained in the Werkstoff-Leistungsblatt der Deutschen Luftfahrt editions WL 2.4632-1 : 1993-08, WL 2.4632-2 : 1993-08, WL 2.4632-3 : 1993-08, WL 2.4632-4 : 1993-08 and WL 2.4632-100 : 1993-08. It is a precipitation-hardening nickel-chromium-cobalt alloy with high creep strength depending on time at temperatures of up to approximately 900 °C. Besides, it possesses good resistance to corrosion and oxidation at high temperatures. Vanadin-pentoxide, sodium- und sulphur compounds can lead to hot-gas corrosion, though. Application for extremely stressed construction components, such as e.g. gas turbine blades, casing parts, afterburner parts, discs, shafts, tools for hot working, forging hammers, forging saddles, pressing tools, shear blades, springs. (Werkstoff-Leistungsblatt der Deutschen Luftfahrt/WL: material specification of the German aviation)

Chemical Composition

Al [%] C [%] Co [%] Cr [%] Cu [%] Fe [%] Mn [%] P [%] S [%] Si [%] Ti [%] Remainder
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Material Compliance

REACh RoHS
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Mechanical Properties

Semi-finished Product Condition Condition Number Strength Abbrevation Area [mm²] Temperature [°C] Tensile Strength [MPa] Yield Strength (0.2% offset) [MPa] Elongation A [%] Hardness HB | HBW
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Toughness Data (Impact)

Condition Temperature [°C] Specimen Shape Specimen Direction Notch Impact Energy [J]
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Cross Reference

Material Name Country Standard
NCK20TA France AIR 9165
2 HR 2 Great Britain BS 2 HR 2
2 HR 202 Great Britain BS 2 HR 202
NA 19 Great Britain BS 3075
HR 402 Great Britain BS HR 402
N07090 USA UNS
N07090 USA AMS 5829
N07090 USA NACE MR-01-75
Nimonic 90 USA SAE J 467
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