AIR FLOW STRAIGHTENING STAGE FOR A TURBOMACHINE

A bypass turbomachine is disclosed. The turbomachine includes a longitudinal axis having an upstream blower impeller and a downstream air-flow straightening assembly of a secondary annular passage delimited radially on the inside by a radially inner shroud and radially on the outside by a radially o...

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Bibliographische Detailangaben
Hauptverfasser: RIERA, William, Henri, Joseph, PERDRIGEON, Christophe, Marcel, Lucien, ZACCARDI, Cédric
Format: Patent
Sprache:eng ; fre ; ger
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