Turbine engine with a flow splitter having a profile with inclined serrations

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United States of America Patent

PATENT NO 11913405
APP PUB NO 20230213000A1
SERIAL NO

18183232

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Abstract

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An airflow profile structure having a leading and/or trailing edge profiled with a serrated profile having a succession of teeth and depressions. Along the leading and/or trailing edge, from a first location to a second location, the teeth of the serrated profile are individually inclined towards the second location.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES2 BOULEVARD DU GÉNÉRAL MARTIAL VALIN PARIS 75015

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Fiack, Matthieu Moissy-Cramayel, FR 4 3
Gea, Aguilera Fernando Moissy-Cramayel, FR 10 7
Gruber, Mathieu Simon Paul Moissy-Cramayel, FR 16 50

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