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US 8,801,380 B2Granted
Concentric rotor control system
AssigneeSikorsky Aircraft Corporation
InventorBrandon L. Stille
Life of this patent
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Abstract
A rotor control system including a collective control rod positioned internal to a rotor shaft, the rotor shaft for imparting torque to rotor blades; and a cyclic control rod positioned internal to and concentric with the collective control rod.
Claims6
A rotor control system comprising:
- a collective control rod positioned internal to a rotor shaft, the rotor shaft for imparting torque to rotor blades;
- a cyclic control rod positioned internal to and concentric with the collective control rod;
- a first swashplate pivotally attached to the collective control rod;
- a second swashplate rotating relative to the first swashplate about a bearing;
- and
- a linkage coupling the first swashplate to the cyclic control rod, translation of the cyclic control rod relative to the collective control rod causing the first swashplate to pivot;
- the linkage is supported on a mount provided on the collective control rod.
4 more elements
A rotor control system comprising:
- a collective control rod positioned internal to a rotor shaft, the rotor shaft for imparting torque to rotor blades;
- a cyclic control rod positioned internal to and concentric with the collective control rod;
- a first swashplate pivotally attached to the collective control rod;
- a second swashplate rotating relative to the first swashplate about a bearing;
- a first servo translating the collective control rod relative to the rotor shaft;
- a second servo translating the cyclic control rod relative to the collective control rod;
- and
- a controller providing control signals to the first servo and the second servo;
- a third servo rotating the collective control rod about a longitudinal axis of the collective control rod to change the orientation of the first swashplate.
6 more elements
A method for providing collective control and cyclic control to a rotor, the method comprising:
- receiving flight inputs;
- and
- actuating at least one of a first servo and a second servo in response to the flight inputs;
- wherein,
- the first servo is coupled to a collective control rod positioned internal to a rotor shaft, the rotor shaft for imparting torque to rotor blades;
- and
- the second servo is coupled to a cyclic control rod positioned internal to and concentric with the collective control rod;
- wherein a first swashplate is pivotally attached to the collective control rod and a second swashplate rotates relative to the first swashplate about a bearing;
- the method including actuating a third servo to change the orientation of the first swashplate to provide full cyclic control to the rotor.
6 more elements
Dependencies are inferred from the claim text.