Turbomachine module equipped with variable pitch vanes and an annular interface shroud
AssigneeSafran Aircraft Engines
InventorsCaroline Marie Frantz, Vincent François Georges Millier, Yves Roland Crochemore
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AssigneeSafran Aircraft Engines
InventorsCaroline Marie Frantz, Vincent François Georges Millier, Yves Roland Crochemore
Estimating the term…
A turbomachine module includes a fan driven in rotation by a fan shaft and having a plurality of variable pitch vanes. The module further includes a pitch change system with a control means connected to the vanes via a connection mechanism, wherein the control means comprising a stationary body integral with the fan shaft and a movable body connected to the connection mechanism. The pitch change system comprising includes an annular part which has a segment integral with the movable body, which is bell-shaped and which extends at least partly radially outwardly from the stationary body. An annular shroud is releasably attached to the annular part and comprising has means for attaching the connection mechanism.
A turbomachine module with longitudinal axis (X), comprising:
Dependencies are inferred from the claim text.