Turbine blade and aircraft engine comprising same

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 10577948
APP PUB NO 20170122256A1
SERIAL NO

14926846

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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The invention relates to a blade for use in a turbine of an aircraft engine. The blade is made of (a) a Mo-based alloy strengthened by intermetallic silicides or (b) a Ni-based single crystal superalloy. An aircraft engine and in particular, a turbofan aircraft engine including a corresponding turbine blade is also disclosed.

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Patent Owner(s)

Patent OwnerAddress
MTU AERO ENGINES AGDACHAUER STRASSE 665 MUENCHEN 80995

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Fried, Markus Valley, DE 7 22
Goehler, Thomas Dachau, DE 10 74
Smarsly, Wilfried Munich, DE 39 248

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