EN 10269 Grade NiCr20TiAl solution heat-treated and precipitation hardened (+AT+P)

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Description

NiCr20TiAl as a aviation material, material number 2.4631, is contained in `Werkstoff-Leistungsblättern der Deutschen Luftfahrt WL` (material data sheets) 2.4631, part 1 and 2 as well as part 100, issues 08.93. This material shows high creep strength up to 850 °C and very good scaling resistance. The nickel-chromium-alloy is hardenable due to the addition of aluminium and titanium. Its corrosion resistance is similar to NiCr20Ti. Application for maximum loaded components, such as gas turbine blades, discs, shafts, pre-combustion chambers in diesel engines, valves, hot working tools, sledge hammer, die blocks, pressing tools, shearing blades, screws and nuts. Processing properties: formability: well (annealed) weldability: possible, but unusual

Related Standards

Equivalent Materials

Diese Materialdaten wurden von WIAM zur Verfügung gestellt

Alle Daten beziehen sich auf Raumtemperatur soweit nicht anderweitig spezifiziert. SI Einheiten werden verwendt soweit nicht anderweitig spezifiziert.
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Eigenschaften

Allgemein

PropertyTemperatureValue

Dichte

20.0 °C

8.2 g/cm³

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Mechanisch

PropertyTemperatureValue

Dehnung

20.0 °C

12 %

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Elastizitätsmodul

20.0 °C

216 GPa

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100.0 °C

212 GPa

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200.0 °C

208 GPa

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300.0 °C

202 GPa

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400.0 °C

196 GPa

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500.0 °C

189 GPa

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600.0 °C

179 GPa

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700.0 °C

161 GPa

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800.0 °C

130 GPa

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Flächenreduzierung

20.0 °C

12 %

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Streckgrenze Rp 0,2

20.0 °C

600 MPa

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50.0 °C

595 MPa

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100.0 °C

586 MPa

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150.0 °C

577 MPa

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200.0 °C

568 MPa

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250.0 °C

564 MPa

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300.0 °C

560 MPa

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350.0 °C

550 MPa

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400.0 °C

540 MPa

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450.0 °C

530 MPa

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500.0 °C

520 MPa

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550.0 °C

510 MPa

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600.0 °C

500 MPa

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650.0 °C

480 MPa

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Zugfestigkeit

20.0 °C

1000 - 1300 MPa

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50.0 °C

1000 - 1070 MPa

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100.0 °C

975 - 1044 MPa

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150.0 °C

950 - 1017 MPa

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200.0 °C

900 - 990 MPa

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250.0 °C

900 - 966 MPa

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300.0 °C

900 - 942 MPa

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350.0 °C

900 - 932 MPa

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400.0 °C

900 - 922 MPa

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450.0 °C

900 - 903 MPa

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500.0 °C

590 - 883 MPa

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550.0 °C

859 - 880 MPa

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600.0 °C

834 - 850 MPa

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Thermisch

PropertyTemperatureValueComment

Koeffizient der thermischen Ausdehnung

100.0 °C

1.29E-5 1/K

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200.0 °C

1.34E-5 1/K

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300.0 °C

1.38E-5 1/K

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400.0 °C

1.43E-5 1/K

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500.0 °C

1.47E-5 1/K

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600.0 °C

1.52E-5 1/K

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Max. Betriebstemperatur, lang

0 - 1000 °C

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Schmelzpunkt

1400 °C

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Typical for Nickel Chromium Alloy

Spezifische Wärmekapazität

20.0 °C

460 J/(kg·K)

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Wärmeleitfähigkeit

20.0 °C

11.4 - 13 W/(m·K)

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Elektrisch

PropertyTemperatureValue

spezifischer Widerstand

20.0 °C

1.24E-6 Ω·m

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Chemical properties

PropertyValue

Aluminium

1 - 1.8 %

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Bor

8E-3 %

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Chrom

18 - 21 %

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Eisen

1.5 %

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Kobalt

1 %

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Kohlenstoff

0.04 - 0.1 %

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Kupfer

0.2 %

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Mangan

1 %

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Nickel

65 %

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Phosphor

0.02 %

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Schwefel

0.015 %

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Silizium

1 %

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Titan

1.8 - 2.7 %

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