Rotor blade arrangement and gas turbine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9915155
SERIAL NO

14568706

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Abstract

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A rotor blade arrangement (20), especially for a gas turbine, which can be fastened on a blade carrier (19) and includes in each case a blade aerofoil element (10) and a platform element (14), wherein the platform elements (14) of a blade row form a continuous inner shroud. With such a blade arrangement, a mechanical decoupling, which extends the service life, is achieved by the blade aerofoil element (10) and the platform element (14) being formed as separate elements and by being able to be fastened in each case separately on the blade carrier (19).

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Patent Owner(s)

Patent OwnerAddress
ANSALDO ENERGIA IP UK LIMITEDLONDON W1G 9DQ

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bossmann, Hans-Peter Lauchringen, DE 32 601
Brandl, Herbert Waldshut-Tiengen, DE 49 379
Indlekofer, Philipp Klettgau-Erzingen, DE 3 26

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