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 (Inventor), Helmut Clemens (Inventor), Volker Guether (Inventor), Sascha Kremmer (Inventor), Andreas Otto (Inventor), Harald Chladil (Inventor)

Research output: Patent

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.

Original language	English
Patent number	US2011189026
IPC	C22C 30/ 00 A I
Priority date	18/10/08
Publication status	Published - 4 Aug 2011

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https://worldwide.espacenet.com/publicationDetails/originalDocument?CC=US&NR=2011189026A1&KC=A1&FT=D&ND=4&date=20110804&DB=EPODOC&locale=de_EP#Licence: Other

Cite this

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title = "MATERIAL FOR A GAS TURBINE COMPONENT, METHOD FOR PRODUCING A GAS TURBINE COMPONENT AND GAS TURBINE COMPONENT",

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.",

author = "Wilfried Smarsly and Helmut Clemens and Volker Guether and Sascha Kremmer and Andreas Otto and Harald Chladil",

year = "2011",

month = aug,

day = "4",

language = "English",

type = "Patent",

note = "US2011189026; C22C 30/ 00 A I",

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T1 - MATERIAL FOR A GAS TURBINE COMPONENT, METHOD FOR PRODUCING A GAS TURBINE COMPONENT AND GAS TURBINE COMPONENT

AU - Smarsly, Wilfried

AU - Clemens, Helmut

AU - Guether, Volker

AU - Kremmer, Sascha

AU - Otto, Andreas

AU - Chladil, Harald

PY - 2011/8/4

Y1 - 2011/8/4

N2 - 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.

AB - 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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