Blade cascade for turbo machine

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United States of America Patent

PATENT NO 10190416
APP PUB NO 20140301852A1
SERIAL NO

14248058

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A blade cascade for a turbomachine, in particular a gas turbine, including multiple identical blade groups which are situated next to each other and which each include

    a first individual blade (10) having a vane (12) having a blade profile and a first side wall (11), anda second individual blade (20), which differs from the first, having a vane (22) having a blade profile and a second side wall (21),the first and second side walls (11, 21) having different contourings.

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Patent Owner(s)

  • MTU AERO ENGINES AG

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Zscherp, Carsten Groebenzell, DE 4 28

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