EN 10095 Grade NiCr20Ti solution annealed (+AT)

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Description

NiCr20Ti is also contained as a aviation material (mat. No 2.4630) in material-performance specifications of the German Aviation WL 2.4630-1, -2, -3,-4, -100 : 1993-08 (Werkstoff-Leistungsblätter der Deutschen Luftfahrt WL). It is non-scaling up to approx. 1150 °C (highest application temperature in air) and shows high corrosion resistance and creep rupture strength up to 750°C as well as favorable resistance to thermal shocks. Application in carburizing or sulfureous furnace athmospheres is not advisable at higher temperatures. Use for components in gas turbines (rings, casing parts), parts for industrial furnace construction, palletts and boxes for component`s heat-treatment as well as for components in aerospace. Processing properties: formability: good weldability: good

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

230 [-]

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Elongación

20.0 °C

30 %

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Límite elástico Rp 0,2

20.0 °C

240 MPa

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Módulo elástico

20.0 °C

221 GPa

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100.0 °C

217 GPa

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200.0 °C

211 GPa

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300.0 °C

204 GPa

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400.0 °C

197 GPa

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500.0 °C

190 GPa

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600.0 °C

182 GPa

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700.0 °C

174 GPa

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800.0 °C

165 GPa

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900.0 °C

154 GPa

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1000.0 °C

140 GPa

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Resistencia a la tracción

20.0 °C

650 - 850 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

1.17E-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/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/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 - 12.1 W/(m·K)

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100.0 °C

13.7 W/(m·K)

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200.0 °C

15.6 W/(m·K)

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300.0 °C

17.1 W/(m·K)

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400.0 °C

18.8 W/(m·K)

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500.0 °C

20 - 20.5 W/(m·K)

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600.0 °C

22.6 W/(m·K)

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700.0 °C

24.5 W/(m·K)

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800.0 °C

26.4 W/(m·K)

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900.0 °C

28.1 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 - 1150 °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

0.015 %

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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

0.02 %

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Hierro

5 %

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Manganeso

1 %

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Níquel

65.4 %

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Silicona

1 %

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Titanio

0.2 - 0.6 %

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