Variable pitch fan
AssigneeSafran Aircraft Engines
InventorsPaul Ghislain Albert Levisse, Olivier Belmonte
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AssigneeSafran Aircraft Engines
InventorsPaul Ghislain Albert Levisse, Olivier Belmonte
Estimating the term…
The invention relates to a device comprising a fixed actuator for a control system for the orientation of fan blades of a turbomachine, comprising: at least one actuator body housed inside an annular casing of the turbomachine forming a bearing support, the annular casing being centred on a longitudinal axis of the turbomachine an inclined relative thereto, the actuator body having an internal volume in which a piston is able to slide, separating the internal volume into two chambers isolated from one another; and a plurality of actuator rods passing through the annular casing forming a bearing support and each having one end fixed to the piston and an opposite end intended to be connected to an internal ring of a movement transfer bearing in order to drive it in translation, the internal volume of the actuator body being closed downstream by a chamber bottom which forms a single part with the annular casing forming a bearing support.
A device with a fixed actuator for a system for controlling the orientation of a plurality of fan blades of a turbomachine, comprising:
A device with a fixed actuator for a system for controlling the orientation of a plurality of fan blades of a turbomachine, comprising:
Dependencies are inferred from the claim text.