Stator of an aircraft turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10458247
APP PUB NO 20170298741A1
SERIAL NO

15517096

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Abstract

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A stator of an aircraft turbine engine, comprising an annular row of fixed vanes and an annular row of arms, wherein the trailing edges of the fixed vanes are positioned substantially in a first transverse plane that is positioned downstream of a second transverse plane that passes substantially through the leading edges of the arms.

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Patent Owner(s)

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

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Charbonnier, Simon Pierre Claude Moissy-Cramayel, FR 4 7
Perrier, Matthieu Yoann Moissy-Cramayel, FR 1 5

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