NiCo15Cr15MoAlTi | 2.4636 Material Datasheet

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Material Description

Material Number Material Number (single) Standard Standard Status Country Application temperature [°C] VDA 231-106 classification
2.4636 (Stahl-Eisen-Liste : 1999) 2.4636 Stahl-Eisen-Liste : 1999 Replaced Germany ≤ 1010 3.4 1)
1) Remark: The material NiCo15Cr15MoAlTi is a precipitation-hardening alloy with molybdenum additive for the solid solution solidification. Similar to NiCo20Cr15MoAlTi (aviation material, material number 2.4634), yet with a higher aluminium and titanium content for higher solidification by precipitation hardening. The alloy possesses high strength and creep strength at temperatures of up to approximately 1010 °C. Application as blade material for aeroplane gas turbines.

Chemical Composition

Al [%] B [%] C [%] Co [%] Cr [%] Cu [%] Fe [%] Mn [%] Mo [%] P [%] S [%] Si [%] Ti [%] Zr [%]
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Mechanical Properties

Semi-finished Product Condition Temperature [°C] Specimen Direction Tensile Strength [MPa] Yield Strength (0.2% offset) [MPa] Elongation A [%]
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Physical Properties

Temperature [°C] Melting Temperature [°C] Density [g/cm³] Thermal Conductivity [W/(m*K)] Specific Electrical Resistance [µΩm] Mean Specific Heat Capacity [kJ/(kg*K)]
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Cross Reference

Material Name Country Standard
HR 4 Great Britain BS HR 4

Producer/Supplier/Trade names

Tradename Supplier
Alloy 115 ROPA STAHLVERTRIEB GMBH, Bad Bergzabern
Alloy 115 Enpar Sonderwerkstoffe GmbH, Gummersbach
Dux 4636 Swiss Steel International GmbH, Düsseldorf
NiCo15Cr15MoAlTi pauly STAHLHANDEL, Essen
NIMONIC alloy 115 Special Metals Deutschland Ltd., Düsseldorf
PER 5 AUBERT & DUVAL Deutschland GmbH, München
Werkstoff 115 ZAPP AG, Ratingen

Material Compliance

REACh RoHS
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