STRAIGHTENER VANE AND STRUCTURAL SHAFT CONNECTED IN A PRIMARY FLOW PATH

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United States of America

APP PUB NO 20200024990A1
SERIAL NO

16115879

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Abstract

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An assembly for a primary flow path of a double flow turbomachine extending along a longitudinal axis including a reduction gear, configured to drive a fan in rotation, a stator including a plurality of vanes for straightening the primary flow path, and an intermediate casing, positioned downstream of the stator, including structural arms with fairings passing through the primary flow path, wherein a fairing and one straightening vane are connected together within the primary flow path by a connecting surface, the fairing and the vane being positioned longitudinally substantially at the reduction gear.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINESPARIS FRA

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Belmon, Guillaume Claude Robert Moissy-Cramayel, FR 3 1
Bulot, Benjamin Moissy-Cramayel, FR 6 10
Lebeault, Eva Julie Moissy-Cramayel, FR 14 6

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