Compressor for an engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 12123419
APP PUB NO 20240003353A1
SERIAL NO

18345319

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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The invention relates to a compressor for an engine, wherein the compressor has compressor stages arranged in succession in a flow direction of the compressor and each compressor stage has a rotating blade cascade and a guide vane cascade arranged downstream of the rotating blade cascade and the rotating blade cascade and the guide vane cascade each have an aspect ratio.

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First Claim

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Patent Owner(s)

Patent OwnerAddress
MTU AERO ENGINES AGDACHAUER STRASSE 665 MUNCHEN 80995

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Elorza, Gomez Sergio Karlsfeld, DE 11 39
Humhauser, Werner Moosburg, DE 36 249
Matzgeller, Roland Hebertshausen, DE 3 0

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