Tandem blade design

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United States of America Patent

PATENT NO 8573941
APP PUB NO 20110318172A1
SERIAL NO

13145753

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Abstract

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A tandem blade design for an axial turbomachine, comprising a front blade and a rear blade disposed with an offset thereto in the circumferential direction and in the axial direction. The rear blade is profiled and positioned with respect to the front blade such that it raises the speed level at the trailing edge of the front blade in a predetermined working range in interaction with the front blade.

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Patent Owner(s)

Patent OwnerAddress
MTU AERO ENGINES GMBH A COMPANY OF GERMANYDACHAUER STRASSE 665 MUNICH 80995

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hoeger, Martin Erding, DE 15 252

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