METHOD FOR PRODUCING A ROTATING DISK FOR A TURBOMACHINE

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United States of America

APP PUB NO 20200001410A1
SERIAL NO

16453139

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Abstract

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The present invention is directed to a method for producing a rotating disk for a turbomachine, forming blade root uptakes on a plurality of circumferential positions, for which, in each case, an axially extending profile groove that is bounded circumferentially by inner wall surfaces of the rotating disk is introduced on a respective circumferential position, in which production method, initially first profile grooves are introduced in a disk on first circumferential positions, and subsequently, a second profile groove is introduced in the disk on a second circumferential position located circumferentially between the first profile grooves.

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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
BINDER, Frank Unterschleissheim, DE 3 9
HIMMELSTOSS, Waltraud Muenchen, DE 1 0
JANKO, Heinrich Dachau, DE 1 0
KREITMAIR, Florian Hirschenhausen, DE 1 0
KUEPPER, Anna Carina Muenchen, DE 2 0
ZIMMERMANN, Hans Landshut, DE 29 177

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