Rotor or propeller blade with dynamically variable geometry and other properties
A blade for the cycloidal marine propellers or cycloidal aerial rotors operative, in response to control system commands, to dynamically; flex along its chord, vary its relative pivot point position, change its planform by extending or retracting a trailing edge extension, differentially, turn the flap along the trailing edge in either direction or allow it to be turned by the flows. For the reversal of the leading and trailing edges for operation in reverse airflow and other conditions the blades are provided with edges that can be made rigid when functioning as the leading edge and flexible if needed when functioning as the trailing edge. Also, the blades are configured to vary and reshape their cross-sectional profile thickness. Finally, the blades are given on command flow permeability along much of their surface.
1. A method for altering fluid dynamic properties of a cycloidal blade, the method comprising:
providing a cycloidal blade having:
a collective blade surface formed from a series of separately orientable, flow surfaces,
a plurality of independently operable actuators in communication with the flow surfaces, the actuators operative to orient one or more of the flow surfaces in accordance with commands received from a controlsystem; and
actuating one or more of the actuators within a revolution of the blade.
2. The method of claim 1 , wherein the flow surfaces are implemented as articulated, blade segments.
3. The method of claim 2 wherein the articulated, blade segments are implemented as foil blade segments.
4. The method of claim 3 wherein the independently operable actuators are selected from the group consisting of electro-magnetic actuators, electro-active polymer actuators, piezo electric actuators, and smart memory alloy-based actuators.
5. The method of claim 1 , further comprising a flexible core supporting the series of separately orientable, flow surfaces.
6. The method of claim 5 , wherein the flow surfaces are implemented as plates.
7. The method of claim 6 , wherein the plates are implemented as foil parts.
8. The method of claim 7 , wherein the independently operable actuators are implemented as electro-active polymer segments.