Patent ID: 7946811

Claim:
An assembly of sectorized fixed stators for a turbomachine compressor, made in a single piece and comprising: an inner ring; an outer ring; radial airfoils extending between the inner and outer rings and such that an inner radial end is connected to the inner ring and an outer radial end is connected to the outer ring; and a first upstream outer annular lug and a second downstream outer annular lug supported by the outer ring for mounting the assembly of stators on a casing, wherein leading edges or trailing edges of the airfoils are connected to zones of the outer ring that are less rigid than those connected to the annular mounting lugs, wherein the outer ring includes a first upstream rim that extends substantially parallel to the first upstream outer annular lug to which the leading edges of the airfoils are connected and a second downstream rim that extends substantially parallel to the second downstream outer annular lug to which the trailing edges of the airfoils are connected, and wherein the second downstream outer annular lug axially extends beyond the second downstream rim in the downstream direction.