MATERIAL FOR A GAS TURBINE COMPONENT, METHOD FOR PRODUCING A GAS TURBINE COMPONENT AND GAS TURBINE COMPONENT

Wilfried Smarsly; Helmut Clemens; Volker Guether; Sascha Kremmer; Andreas Otto; Harald Chladil

MATERIAL FOR A GAS TURBINE COMPONENT, METHOD FOR PRODUCING A GAS TURBINE COMPONENT AND GAS TURBINE COMPONENT

Wilfried Smarsly (Erfinder), Helmut Clemens (Erfinder), Volker Guether (Erfinder), Sascha Kremmer (Erfinder), Andreas Otto (Erfinder), Harald Chladil (Erfinder)

Publikation: Patent › Patentschrift

Abstract

A material for a gas turbine component, to be specific a titanium-aluminum-based alloy material, including at least titanium and aluminum. The material has a) in the range of room temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase with a proportion of the β/B2-Ti phase of at most 5% by volume, and b) in the range of the eutectoid temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase, with a proportion of the β/B2-Ti phase of at least 10% by volume.

Originalsprache	Englisch
Veröffentlichungsnummer	US2011189026
IPC	C22C 30/ 00 A I
Prioritätsdatum	18/10/08
Publikationsstatus	Veröffentlicht - 4 Aug. 2011

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Dieses zitieren

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abstract = "A material for a gas turbine component, to be specific a titanium-aluminum-based alloy material, including at least titanium and aluminum. The material has a) in the range of room temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase with a proportion of the β/B2-Ti phase of at most 5% by volume, and b) in the range of the eutectoid temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase, with a proportion of the β/B2-Ti phase of at least 10% by volume.",

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AU - Kremmer, Sascha

AU - Otto, Andreas

AU - Chladil, Harald

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