STRAIGHTENER VANE AND STRUCTURAL SHAFT CONNECTED IN A PRIMARY FLOW PATH

Number of patents in Portfolio can not be more than 2000

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)

  • SAFRAN AIRCRAFT ENGINES

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Belmon, Guillaume Claude Robert Moissy-Cramayel, FR 1 0
Bulot, Benjamin Moissy-Cramayel, FR 4 0
Lebeault, Eva Julie Moissy-Cramayel, FR 1 0

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