Electrohydraulic pitch-control system with a valve pump in a rotating reference frame
AssigneeSafran Aircraft Engines
InventorsHuguette De Wergifosse, Jacques Auriol
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AssigneeSafran Aircraft Engines
InventorsHuguette De Wergifosse, Jacques Auriol
Estimating the term…
The present invention relates to a pitch-change mechanism for a turbine engine propeller, said turbine engine comprising a stator portion and a rotor portion, said pitch-change mechanism comprising an electrohydraulic actuator comprising: —a cylinder for actuating the propeller, comprising a first chamber and a second chamber; —a hydraulic pump suitable for selectively supplying the first chamber or the second chamber of the cylinder with pressurized hydraulic fluid; —a hydraulic fluid reservoir configured to store a pressurized hydraulic fluid; —a valve controlled between a first position in which the valve places the first chamber of the cylinder in fluid communication with the hydraulic pump, and a second position in which the valve places the first chamber of the cylinder in fluid communication with the hydraulic fluid reservoir.
A pitch change mechanism for a propeller, said pitch change mechanism comprising an electrohydraulic actuator comprising:
A pitch change mechanism for a propeller, said pitch change mechanism comprising an electrohydraulic actuator comprising:
A pitch change mechanism for a propeller, said pitch change mechanism comprising an electrohydraulic actuator comprising:
Dependencies are inferred from the claim text.