Electrohydraulic pitch setting with reversible pump
AssigneeSafran Aircraft Engines
InventorsHuguette De Wergifosse, Caroline Marie Frantz
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AssigneeSafran Aircraft Engines
InventorsHuguette De Wergifosse, Caroline Marie Frantz
Estimating the term…
The present invention relates to a mechanism for changing the pitch of a propeller of a turbine engine, the mechanism comprising an electrohydraulic actuator that comprises: —an electric machine comprising a rotatable actuator shaft; —a pumping assembly comprising two hydraulic axial piston pumps, each comprising: o a barrel housed in a cavity filled with hydraulic fluid; o a set of cylinders formed in the barrel, each cylinder housing a translatable piston and comprising an inlet port and a delivery port; o and an inclined plate, the plate of a first pump comprising a crescent-shaped inlet port for circulating the hydraulic fluid when the plate is rotated in a first direction, and the plate of a second pump comprising a crescent-shaped inlet port for circulating the hydraulic fluid when the plate is rotated in a second direction.
A pitch change mechanism for a propeller of a turbomachine the pitch change mechanism comprising an electrohydraulic actuator comprising:
Dependencies are inferred from the claim text.