Circular force generator (CFG) devices, systems, and methods having indirectly driven imbalanced rotors

Patent metadata

Field	Value
Publication number	US-10364865-B2
Application number	US-201414912820-A
Country	US
Kind code	B2
Filing date	Aug 29, 2014
Priority date	Aug 29, 2013
Publication date	Jul 30, 2019
Grant date	Jul 30, 2019

Abstract

Circular force generator (CFG) devices, systems, and methods are disclosed having indirectly driven imbalanced rotors for generating vibrations and/or imparting vibration control. A CFG device ( 10 ) includes a first set of imbalanced rotors ( 12 ) disposed about a center point and a second set of imbalanced rotors ( 12 ) disposed about the center point. The first set of imbalanced rotors is configured to co-rotate synchronously. The second set of imbalanced rotors is configured to co-rotate synchronously. The first and second sets of imbalanced rotors are configured to create a controllable rotating force vector having a controllable magnitude and phase about the center point. A CFG system includes a controller and one or more CFG devices configured to receive control commands from the controller. A method of generating a force via a CFG device includes receiving a force command and generating a force in response to receiving the force command.

First claim

What is claimed is:

1. A force generating device comprising:
an opening or keep-out zone positioned about a center point;
a first set of imbalanced rotors disposed about the center point and positioned outside of the opening or keep-out zone; and
a second set of imbalanced rotors disposed about the center point and positioned outside of the opening or keep-out zone, wherein:
the first set of imbalanced rotors is configured to co-rotate synchronously about the center point;
the second set of imbalanced rotors is configured to co-rotate synchronously about the center point; and
the first and second sets of imbalanced rotors are configured to create a controllable rotating force vector having a controllable magnitude and phase about the center point; and

wherein the first and second set of imbalanced rotors are configured to create a zero net moment.

2. The force generating device of claim 1 , wherein the first set of imbalanced rotors is configured to create a first rotating force vector having a fixed magnitude about the center point.

3. The force generating device of claim 2 , wherein the second set of imbalanced rotors is configured to create a second rotating force vector having a fixed magnitude about the center point.

4. The force generating device of claim 1 , wherein each of the first and second sets of imbalanced rotors includes two or more imbalanced rotors.

5. The force generating device of claim 1 , wherein each of the first and second sets of imbalanced rotors includes three or more imbalanced rotors.

6. The force generating device of claim 1 , wherein the first set of imbalanced rotors includes a first plurality of imbalanced rotors that are coupled together via a first mechanical coupling device.

7. The force generating device of claim 6 , wherein the second set of imbalanced rotors comprises a second plurality of imbalanced rotors that are coupled together via a second mechanical coupling device.

8. The force generating device of claim 7 , wherein the first mechanical coupling device or the second mechanical coupling device comprises a belt.

9. The force generating device of claim 7 , wherein the first mechanical coupling device or the second mechanical coupling device comprises a gear.

10. The force generating device of claim 7 , wherein the first mechanical coupling device or the second mechanical coupling device comprises a sprocket.

11. The force generating device of claim 7 , wherein a circular force generator (CFG) housing spins or rotates about a rotating center point.

12. The force generating device of claim 7 , wherein a circular force generator (CFG) housing is stationary or non-rotating about a stationary center point.

13. The force generating device of claim 1 , wherein the first and second sets of imbalanced rotors are co-planar.

14. A force generating system comprising:
a controller; and
a circular force generator (CFG) device configured to receive control commands from the controller, wherein the CFG device includes at least a first set of imbalanced rotors configured to co-rotate synchronously about different, non-coaxial axes;
an opening or keep-out zone positioned about a center point;
wherein the at least the first set of imbalanced rotors is configured to create a rotating force vector at or about the center point of the CFG device, the at least the first set of imbalanced rotors positioned outside of the opening or keep-out zone and the at least the first set of imbalanced rotors are configured to create a zero net moment.

15. The force generating system of claim 14 , wherein the first set of imbalanced rotors are disposed 180° apart about the center point of the CFG device.

16. The force generating system of claim 14 , further comprising a second set of imbalanced rotors configured to co-rotate synchronously about different, non-coaxial axes.

17. The force generating system of claim 16 , wherein the imbalanced rotors in the first and second sets of imbalanced rotors are disposed in an annular ring about the center point.

18. The force generating system of claim 16 , wherein each of the first and second sets of imbalanced rotors includes two or more imbalanced rotors.

19. The force generating system of claim 16 , wherein each of the first or second sets of imbalanced rotors is mechanically coupled via at least one belt, gear, chain, or sprocket.

20. The force generating system of claim 14 , wherein the center point is spinning or stationary.

21. The force generating device of claim 14 , wherein the step of generating the force in response to receiving the force command further comprises co-rotating the at least first set of imbalanced rotors within a same plane.

22. A method of generating a force via a circular force generator (CFG) device, the method comprising:
receiving a force command; and
generating the force in response to receiving the force command, wherein generating the force includes co-rotating one or more sets of imbalanced rotors about different, non-coaxial axes disposed about a center point of the CFG device and positioned outside of an opening or keep-out zone, the one or more sets of imbalanced rotors are configured to create a zero net moment.

23. The method of claim 22 , wherein the step of co-rotating the one or more sets of imbalanced rotors includes directly rotating a first imbalanced rotor and indirectly rotating one or more additional imbalanced rotors.

24. The method of claim 23 , wherein directly rotating the first imbalanced rotor includes rotating the first imbalanced rotor via a motor.

25. The method of claim 22 , wherein the step of co-rotating the one or more sets of imbalanced rotors further comprises co-rotating at least two sets of imbalanced rotors about the non-coaxial axes.

26. The method of claim 25 , wherein each set of imbalanced rotors includes two imbalanced rotors.

27. The method of claim 25 , wherein each set of imbalanced rotors includes three imbalanced rotors.

28. The force generating device of claim 22 , wherein co-rotating the one or more sets of imbalanced rotors further comprises rotating the one or more sets of imbalanced rotors within a same plane.

29. A force generating device comprising:
a first set of imbalanced rotors disposed about a center point;
a second set of imbalanced rotors disposed about the center point, wherein:
the first set of imbalanced rotors is configured to co-rotate synchronously about the center point;
the second set of imbalanced rotors is configured to co-rotate synchronously about the center point;
the first and second sets of imbalanced rotors are configured to create a controllable rotating force vector having a controllable magnitude and phase about the center point; and

wherein the imbalanced rotors in the first and second sets of imbalanced rotors are disposed in an annular ring about the center point.

30. A force generating system comprising:
a controller;
a circular force generating (CFG) device configured to receive control commands from the controller, wherein the CFG device includes at least a first set of imbalanced rotors configured to co-rotate synchronously about different, non-coaxial axes;
a second set of imbalanced rotors configured to co-rotate synchronously about different, non-coaxial axes;
wherein the first set of imbalanced rotors is configured to create a

Assignees

• Lord Corp

Inventors

• Hunter Anthony G
• Altieri Russell E
• Brannan Warren F
• Jolly Mark R

Classifications

• B64C27/001 Primary

  Vibration damping devices · CPC title

• F16F15/14

  using masses freely rotating with the system, {i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers (compensation of inertia forces F16F15/22; weights for balancing rotating bodies F16F15/32)} · CPC title

• B64C2027/003

  mounted on rotor hub, e.g. a rotary force generator · CPC title

• F16F15/10

  Suppression of vibrations in rotating systems by making use of members moving with the system (by balancing F16F15/22 {; yielding couplings F16D3/00} ; with flywheels acting variably or intermittently F16H {; construction providing resilience or vibration-damping for gear elements F16H55/14}) · CPC title

• F16F15/1464 Primary

  Masses connected to driveline by a kinematic mechanism or gear system (F16F15/145 takes precedence) · CPC title