Controlling rate of rotor feather by primary blade angle control system
AssigneePratt & Whitney Canada Corp.
InventorJagoda Krzywon
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorJagoda Krzywon
Estimating the term…
A rotor blade control system includes a main control valve having an inlet for receiving liquid and an outlet for issuing liquid to a rotor pitch change actuator. The main control valve is configured to control flow of liquid from the inlet to the outlet to modify pitch angle of rotor blades. A feathering system has a first conduit in fluid communication with the outlet of the main control valve, a second conduit in fluid communication with the rotor pitch change actuator, and a drain conduit in fluid communication with a liquid return system. The feathering system has a normal operation mode for supplying liquid from the main control valve to the rotor pitch change actuator, and a feathering mode for allowing drainage from the rotor pitch change actuator to the drain conduit across a range of flow rates.
A rotor blade control system comprising:
Dependencies are inferred from the claim text.