TURBOMACHINE ASSEMBLY COMPRISING A HALF-SHELL CASING BEARING VARIABLE-PITCH INLET STATOR VANES

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20250116203A1
SERIAL NO

18833280

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Abstract

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The present invention relates to an assembly (12) for a turbomachine, comprising: —an outer casing (15) made of half-shells; —an inner casing (14); —a plurality of guide vanes (13) mounted between the outer casing (15) and the inner casing (14), —a structural casing comprising a flange (23) which is radially inside the inner casing (14); and—a system (24) for blocking the inner casing (14) on the structural casing, comprising a generally annular tab (25) fixed to one of the inner casing (14) and the structural casing and a complementary chute (26) fixed to the other of the inner casing (14) and the structural casing, the chute (26) being configured to receive the tab (25) and to block it along the axis (X) with respect to the structural casing.

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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
BECOULET, Julien Fabien Patrick MOISSY-CRAMAYEL, FR 39 88
BELMONTE, Olivier MOISSY-CRAMAYEL, FR 71 383

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