Hydraulic valve, a hybrid helicopter provided with such a hydraulic valve, and a method implemented by the hydraulic valve
AssigneeEurocopter
InventorJean-Pierre Jalaguier
Life of this patent
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AssigneeEurocopter
InventorJean-Pierre Jalaguier
Estimating the term…
A hydraulic valve assembly includes a hydraulic valve, a control rod configured to be moved in translation along a first longitudinal axis by flight controls of an aircraft, a servocontrol, and an outlet rod configured to be moved in translation along a second longitudinal axis and configured to transfer a hydraulic fluid between the servocontrol and the hydraulic valve. A blocker device is configured to block a movement of the control rod when a difference between a first movement of the control rod and a second movement of the outlet rod exceeds a predetermined threshold and includes at least one moveable abutment configured to block the movement of the control rod when the predetermined threshold is reached and configured to move in longitudinal translation with the outlet rod, and a differential lever configured to mechanically link the control rod to the outlet rod and to cooperate with the at least one moveable abutment.
A hydraulic valve assembly comprising:
A hybrid helicopter having a fuselage and comprising:
A method of controlling the hydraulic valve feeding a servocontrol suitable for modifying a pitch of blades of an aircraft propeller, the method comprising:
Dependencies are inferred from the claim text.