Electromagnetic actuator system with a rotor oscillation
A novel electromagnetic actuator designed to operate at system resonance, used in the construction of a unique vehicle system, is presented herein. An exemplary embodiment of the vehicle system is based on an electromagnetic actuator coupled to a plurality of actuating members of a micro aerial vehicle. Attributes of this type of actuation offer several enhancements over traditional approaches. The unique use of an electromagnetic actuator lends itself to a near unlimited number of coil cross-sectional designs that can be optimized to meet performance requirements while maintaining minimal costs of fabrication.
1. An electromagnetic actuator, comprising:
an actuator frame;
a rotor disposed within the actuator frame and configured to have direct rotational oscillation about a rotation axis following a predetermined rotational arc having a middle position and operatively within a predetermined oscillation frequency range;
a stator having a coil for generating an electromagnetic force disposed within the actuator frame positioned proximate to the rotor and configured to remain stationary, combination of the stator and the rotor configured to generate a net driving torque between the rotor and the stator;
at least one restoring element configured to provide a net counter torque to the rotor to bias the rotor to rotate to the middle position without mechanical coupling, wherein the at least one restoring element is in physical contact with the stator;
at least one set of excitation terminals configured to provide potential energy to generate the net driving torque; and
at least one actuating coupling having a proximal end and a distal end, the distal end configured to couple to at least one actuating member and the proximal end configured to couple to the rotor, motion of the rotor causing motion of the at least one actuating member thereby causing motion of the electromagnetic actuator, wherein the rotor includes at least one permanent magnet, and wherein the restoring element is at least one permanent magnet, and wherein the at least one permanent magnet of the restoring element is in a polarity alignment with the at least one permanent magnet of the rotor.
2. The electromagnetic actuator of claim 1 , the potential energy is electrical.
3. The electromagnetic actuator of claim 1 , the stator includes at least one winding.
4. The electromagnetic actuator of claim 1 , the rotor includes at least one permanent magnet.
5. The electromagnetic actuator of claim 1 , the restoring element is at least one permanent magnet.
6. The electromagnetic actuator of claim 1 , the electromagnetic actuator is configured to be communicatively coupled to at least one sensor.
7. The electromagnetic actuator of claim 1 , the restoring element is at least one permanent magnet.
8. A vehicle system, comprising:
a vehicle frame;
at least one electromagnetic actuator, positioned within the vehicle frame, the at least one electromagnetic actuator comprising:
an actuator frame;
a rotor disposed within the actuator frame and configured to have direct rotational oscillation about a rotation axis following a predetermined rotational arc having a middle position and operatively within a predetermined oscillation frequency range;
a stator having a coil for generating an electromagnetic force disposed within the actuator frame positioned proximate to the rotor and configured to remain stationary, combination of the stator and the rotor configured to generate a net driving torque between the rotor and the stator;
at least one restoring element configured to provide a net counter torque to the rotor to bias the rotor to rotate to the middle position without mechanical coupling, wherein the at least one restoring element is in physical contact with the stator;
at least one set of excitation terminals configured to provide potential energy to generate the net driving torque; and
at least one actuating coupling having a proximal end and a distal end, the distal end configured to couple to at least one actuating member and the proximal end configured to couple to the rotor, motion of the rotor causing motion of the at least one actuating member thereby causing motion of the electromagnetic actuator;
at least one actuating member, the at least one actuating member configured to couple to the actuating coupling; and
a power source, the power source connected to the excitation terminals and providing potential energy to generate the net driving torque, wherein the rotor includes at least one permanent magnet, and wherein the restoring element is at least one permanent magnet, and wherein the at least one permanent magnet of the restoring element is in a polarity alignment with the at least one permanent magnet of the rotor.
9. The electromagnetic actuated vehicle system of claim 8 , the at least one actuating coupling is configured to enable at least one degree of freedom motion in the at least one actuating member.
10. The electromagnetic actuated vehicle system of claim 8 , the at least one actuating member is an element producing locomotion.
11. The electromagnetic actuated vehicle system of claim 8 , the electromagnetic actuated vehicle system is configured to be communicatively coupled to at least one sensor.
12. The electromagnetic actuated vehicle system of claim 11 , the at least one sensor comprises at least one sensor processing and coil drive circuitry unit.
13. The electromagnetic actuated aerial vehicle system of claim 12 , the at least one sensor processing and coil drive circuitry unit is powered by an electrical source, the electrical source coupled to the frame.
14. The electromagnetic actuator of claim 8 , the restoring element is at least one permanent magnet.