BLADE ARRANGEMENT FOR A TURBO ENGINE

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United States of America Patent

APP PUB NO 20140072432A1
SERIAL NO

14008743

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Abstract

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A blade arrangement for a turbo engine, in particular a gas turbine, with a rotor and several blades fastened thereto, which are configured to be systematically different, wherein at least two adjacent blades have systematically different shrouds (12, 22) and/or inner blade platforms (11, 21).

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Patent Owner(s)

Patent OwnerAddress
MTU AERO ENGINES AGDACHAUER STRASSE 665 MUNICH 80995

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Schoenenborn, Harald Karsfeld, DE 7 96
Woehler, Marcus Inning am Ammersee, DE 7 21

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