Guide device for variable pitch stator vanes of a turbine engine, and a method of assembling such a device
AssigneeSafran Aircraft Engines
InventorsClementine Charlotte Marie Mouton, Olivier Belmonte
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AssigneeSafran Aircraft Engines
InventorsClementine Charlotte Marie Mouton, Olivier Belmonte
Estimating the term…
A device for guiding variable pitch stator vanes of a turbine engine is provided. The device includes a plurality of inner ring angular sectors arranged end-to-end in order to form an inner ring, each inner ring sector having chimneys passing radially through the inner ring sector, a plurality of cylindrical bushings, each being put into place in a chimney of the inner ring from the inside and each serving to receive a guide pivot of a stator vane, a plurality of reconstitution ring angular sectors arranged end-to-end in order to form a reconstitution ring and put into place radially from the inside against the inner ring, and a plurality of blocking elements passing axially through the inner and reconstitution rings in order to assemble the rings together.
A device for guiding variable pitch stator vanes of a turbine engine, the device comprising:
Dependencies are inferred from the claim text.