STRAIGHTENER VANE AND STRUCTURAL SHAFT CONNECTED IN A PRIMARY FLOW PATH
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United States of America
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Jan 23, 2020
app pub date -
Aug 29, 2018
filing date -
Aug 29, 2018
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Abstract
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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