WL 2.4630 Grade NiCr20Ti soft annealed (+A)

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Description

The aviation material NiCr20Ti with the material number 2.4630 is contained in the Werkstoff-Leistungsblatt der Deutschen Luftfahrt editions WL 2.4630-1 : 1993-08, WL 2.4630-2 : 1993-08, WL 2.4630-3 : 1993-08, WL 2.4630-4 : 1993-08 and WL 2.4630-100 : 1993-08. DIN 17742 among other things contains the material NiCr20Ti with the material number 2.4951. The alloy is scale-resistant up to approximately 1100 °C and possesses high corrosion-resistance and creep strength depending on time up to approximately 750 °C as well as good resistance to temperature variations. The application in carbonizing or sulphur-bearing furnace atmospheres is not recommendable at higher temperatures. Application for components in aviation and space travel, for construction components in gas turbines, such as rings and casing parts, parts for the construction of industrial furnaces, pallets and baskets for the heat treatment of construction components. Processing properties: Formability: good Weldability: good (Werkstoff-Leistungsblatt der Deutschen Luftfahrt/WL: material specification of the German aviation)

Related Standards

Equivalent Materials

Los datos sobre este material han sido proporcionados por WIAM.

A menos que se indique lo contrario, todas las medidas corresponden a condiciones de temperatura ambiente. A menos que se indique lo contrario, se utilizan las unidades del SI.
Las normas armonizadas son similares a uno o varios estándares del proveedor. Es posible que algunas normas armonizadas se ajusten al estándar original, mientras que otras pueden quedar fuera de su alcance.

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Propiedades

General

PropertyTemperatureValue

Densidad

20.0 °C

8.4 g/cm³

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Mecánica

PropertyTemperatureValue

Dureza Brinell

20.0 °C

229 [-]

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Elongación

20.0 °C

25 - 30 %

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Elongación A50 transversal

20.0 °C

30 %

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Elongation A100

20.0 °C

14 - 25 %

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Límite elástico Rp 0,2

20.0 °C

230 MPa

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200.0 °C

304 MPa

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300.0 °C

304 MPa

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400.0 °C

304 MPa

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500.0 °C

294 MPa

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600.0 °C

264 MPa

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700.0 °C

225 MPa

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800.0 °C

118 MPa

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900.0 °C

59 MPa

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1000.0 °C

49 MPa

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Límite elástico transversal Rp 0,2

20.0 °C

230 MPa

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Módulo elástico

20.0 °C

221 GPa

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100.0 °C

216 - 217 GPa

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200.0 °C

210 - 211 GPa

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300.0 °C

203 - 204 GPa

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400.0 °C

196 - 197 GPa

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500.0 °C

186 - 190 GPa

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600.0 °C

181 - 182 GPa

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700.0 °C

173 - 174 GPa

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800.0 °C

165 GPa

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900.0 °C

153 - 154 GPa

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1000.0 °C

140 GPa

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Resistencia a la tracción

20.0 °C

640 - 930 MPa

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Resistencia a la tracción transversal

20.0 °C

640 - 830 MPa

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Aplicaciones térmicas

PropertyTemperatureValueComment

Calor específico

20.0 °C

445 - 460 J/(kg·K)

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100.0 °C

465 J/(kg·K)

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200.0 °C

490 J/(kg·K)

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300.0 °C

515 J/(kg·K)

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400.0 °C

540 J/(kg·K)

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500.0 °C

570 J/(kg·K)

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600.0 °C

600 J/(kg·K)

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700.0 °C

620 J/(kg·K)

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800.0 °C

650 J/(kg·K)

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900.0 °C

675 J/(kg·K)

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1000.0 °C

700 J/(kg·K)

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Coeficiente de dilatación térmica

100.0 °C

1.1E-5 - 1.17E-5 1/K

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200.0 °C

1.26E-5 - 1.27E-5 1/K

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300.0 °C

1.32E-5 - 1.34E-5 1/K

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400.0 °C

1.38E-5 - 1.39E-5 1/K

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500.0 °C

1.43E-5 1/K

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600.0 °C

1.48E-5 - 1.5E-5 1/K

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700.0 °C

1.54E-5 1/K

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800.0 °C

1.6E-5 - 1.65E-5 1/K

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900.0 °C

1.66E-5 - 1.71E-5 1/K

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1000.0 °C

1.75E-5 - 1.82E-5 1/K

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Conductividad térmica

20.0 °C

12.1 - 14 W/(m·K)

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100.0 °C

13.7 - 15 W/(m·K)

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200.0 °C

15.6 - 16 W/(m·K)

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300.0 °C

17.1 - 18 W/(m·K)

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400.0 °C

18.8 - 20 W/(m·K)

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500.0 °C

20.5 - 22 W/(m·K)

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600.0 °C

22.6 - 23 W/(m·K)

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700.0 °C

24.5 - 25 W/(m·K)

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800.0 °C

26.4 - 27 W/(m·K)

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900.0 °C

28.1 - 30 W/(m·K)

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1000.0 °C

29.9 W/(m·K)

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Temperatura de fusión

1400 °C

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Typical for Nickel Chromium Alloy

Temperatura máx. de funcionamiento, largo

0 - 750 °C

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Eléctrico

PropertyTemperatureValue

Resistividad eléctrica

20.0 °C

1.09E-6 Ω·m

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100.0 °C

1.1E-6 Ω·m

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200.0 °C

1.12E-6 Ω·m

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300.0 °C

1.15E-6 Ω·m

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400.0 °C

1.17E-6 Ω·m

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500.0 °C

1.17E-6 Ω·m

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600.0 °C

1.15E-6 Ω·m

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700.0 °C

1.15E-6 Ω·m

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800.0 °C

1.15E-6 Ω·m

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900.0 °C

1.15E-6 Ω·m

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1000.0 °C

1.16E-6 Ω·m

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Chemical properties

PropertyValue

Aluminio

0.3 %

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Azufre

0.02 - 0.15 %

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Carbono

0.08 - 0.15 %

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Cobalto

5 %

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Cobre

0.5 %

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Cromo

18 - 21 %

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Fósforo

0.2 %

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Hierro

5 %

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Manganeso

1 %

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Níquel

65.4 - 65.7 %

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Plomo

5E-3 %

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Silicona

1 %

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Titanio

0.2 - 0.6 %

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