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

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MATERIAL FOR A GAS TURBINE COMPONENT, METHOD FOR PRODUCING A GAS TURBINE COMPONENT AND GAS TURBINE COMPONENT. / Smarsly, Wilfried (Inventor); Clemens, Helmut (Inventor); Guether, Volker (Inventor) et al.
Patent No.: US2011189026. Aug 04, 2011.

Research output: Patent

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Smarsly, Wilfried (Inventor) ; Clemens, Helmut (Inventor) ; Guether, Volker (Inventor) et al. / MATERIAL FOR A GAS TURBINE COMPONENT, METHOD FOR PRODUCING A GAS TURBINE COMPONENT AND GAS TURBINE COMPONENT. Patent No.: US2011189026. Aug 04, 2011.

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@misc{db3e14bc7f6a4c36bd9177df5f5cf83d,
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",

}

RIS (suitable for import to EndNote) - Download

TY - PAT

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.

M3 - Patent

M1 - US2011189026

ER -