Assembly for Turbine Engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20190309650A1
SERIAL NO

16379327

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An assembly for a turbine engine includes an upstream section and a downstream section, each having an annular row of semi-cylindrical radial recesses and a plurality of flanges positioned between two circumferentially adjacent recesses for holding the two sections together. The recesses form a cylindrical opening when the two sections are assembled. The openings receive pivot sections of variable stator vanes.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AERO BOOSTERS SA4041 HERSTAL

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Vyvey, Morgan Moissy-Cramayel, FR 5 1

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