Gas turbine guide vane element

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 10598032
APP PUB NO 20160326895A1
SERIAL NO

15143979

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Importance

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Abstract

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A guide vane element for a gas turbine, the guide vane element having a first guide vane, a second guide vane distanced by one division in the peripheral direction, and at least one band joining these guide vanes, in particular, a radially inner band and/or a radially outer band, wherein at least one band joining these guide vanes has a vane-side surface having a contouring and a first front side in the peripheral direction having a groove, which is particularly straight in the axial direction, for the uptake of a sealing element.

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Patent Owner(s)

Patent OwnerAddress
MTU AERO ENGINES AG80995 MÜNCHEN

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Huebner, Norbert Dachau, DE 33 227
Kislinger, Bernd Reisgang, DE 11 32

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