Individual blade control
AssigneeTextron Inc.
InventorsGaylord W. Carlock, Jimmy G. Garner, Charles M. Gatlin, Kenneth F. Guinn, Peter A. Reyes
Life of this patent
Estimating the term…
Loading patent…
AssigneeTextron Inc.
InventorsGaylord W. Carlock, Jimmy G. Garner, Charles M. Gatlin, Kenneth F. Guinn, Peter A. Reyes
Estimating the term…
Individual blade control of a helicopter rotor is accomplished by rotation of a mast (10) about a standpipe (12) where an individual blade (16) is coupled to the mast through a hub (18). Pilot input signals are transmitted by fly-by-optic transmission lines (14) through a fiber optic slip ring (40,42) to signal generators (134, 136, 138) for each of three sections of triplex actuators (76-79) coupled to individual rotor blades. Hydraulic fluid for positioning each of the actuators (76-79) is provided by electrohydraulic power packages (88, 90 and 92) where each package includes a pump and alternator. As each blade rotates about the mast (76) the pitch angle changes by individualizing the output of the signal generators (134-138) for each actuator.
Apparatus for individually controlling each blade of a rotor that rotates with a mast which drives the rotor through a rotating hub, the improvement comprising:
Apparatus for individually controlling each blade of a rotor that rotates with a mast which drives the rotor through a rotating hub, the improvement comprising:
Apparatus for individually controlling each blade of a rotor that rotates with a mast which drives the rotor through a rotating hub, the improvement comprising:
Apparatus for individually controlling each blade of a rotor that rotates with a mast which drives the rotor through a rotating hub, the improvement comprising:
Dependencies are inferred from the claim text.