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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Format: | Patent |
Sprache: | eng ; fre ; ger |
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