| 摘要 |
An assembly of sectorized fixed compressors ( 50 ) for a turbomachine compressor, this assembly being made in a single piece and comprising two coaxial rings ( 20, 52 ) connected by radial airfoils ( 24 ), the outer ring comprising two annular mounting lugs ( 56, 66 ) on a casing of the compressor, at least one of these annular lugs being connected to the outer ring in a zone axially separate from the zone for connecting the leading edges ( 26 ) or trailing edges ( 28 ) of the airfoils to the outer ring.
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