AMS 4915 Grade R54810

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Description

Titanium UNS R54810 is a near Alpha Alloy that was primarily designed for use at elevated temperatures – up to 455 degrees centigrade. It offers the highest modulus and lowest density of all Titanium alloys. It has good creep strength and it’s weldable by the inert gas fusion and resistance-welding processes. Titanium UNS R54810 is used in the annealed condition for such applications as airframe and jet engine parts that demand high strength, superior creep resistance and a good stiffness-to-density ratio. The machinability of this grade is similar to that of Titanium 6Al-4V.

Related Standards

Equivalent Materials

Los datos sobre este material han sido proporcionados por VSMPO,Matmatch,RMI Titanium Co.

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

PropertyValueShapeRelated Standards

Densidad

4.37 g/cm³

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Bar, Billet

4.37 g/cm³

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Medidas

PropertyTemperatureValueShapeComment

Dimensions

15-65 mm diameter up to 6000 mm length °C

7-14.5 mm diameter up to 3000 mm length

Bar

Diámetro

7 mm

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Bar

115 mm

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Bar

130 mm

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Billet

350 mm

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Billet

Longitud

3000 mm

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Billet

4500 mm

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Billet

6000 mm

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Bar

max

Mecánica

PropertyValueShapeRelated Standards

Coeficiente de Poisson

0.35 [-]

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Bar, Billet

Dureza Rockwell C

36.0 [-]

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Bar, Billet

Elongación

10.0 %

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Bar, Billet

Límite elástico

827.0 MPa

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Módulo de cizallamiento

42.0 GPa

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Bar, Billet

Módulo elástico

117.0 GPa

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Bar, Billet

128 GPa

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Resistencia a la tracción

897.0 MPa

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Bar, Billet

931.0 MPa

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Resistencia al choque, ensayo Charpy entallado

20.0 - 34.0 kJ/m²

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Aplicaciones térmicas

PropertyTemperatureValueRelated StandardsShape

Calor específico

502 J/(kg·K)

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Coeficiente de dilatación térmica

20 °C

0.0000085 1/K

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

20 °C

0.0000090 1/K

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

100 °C

0.0000085 1/K

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

315 °C

0.0000090 1/K

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Conductividad térmica

6 W/(m·K)

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

6.5 W/(m·K)

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Bar, Billet

Temperatura de fusión

1538.0 °C

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Eléctrico

PropertyValueRelated Standards

Resistividad eléctrica

1.9699999999999998e-06 Ω·m

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Chemical properties

PropertyValueShapeRelated Standards

Aluminio

7.35 - 8.35 %

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Bar, Billet

7.5 - 8.5 %

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Carbono

0.08

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Bar, Billet

AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Hidrógeno

0.0125

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Bar, Billet

AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Hierro

0.3

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Bar, Billet

Molibdeno

0.75 - 1.25 %

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Bar, Billet

0.75 - 1.75 %

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Nitrógeno

0.05

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Bar, Billet

AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Oxígeno

0.12

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AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

Vanadio

0.75 - 1.75 %

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Bar, Billet

AMS 4915, AMS 4916, AMS 4972, AMS 4973, MIL-T 9046, MIL-T 9047

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