Active vibration control systems and methods for vehicles

Patent metadata

Field	Value
Publication number	US-9623962-B2
Application number	US-201314441876-A
Country	US
Kind code	B2
Filing date	Nov 12, 2013
Priority date	Nov 12, 2012
Publication date	Apr 18, 2017
Grant date	Apr 18, 2017

Abstract

Active vibration control systems ( 100 ) and methods are provided herein. Systems ( 100 ) are expandable and include a plurality of vibration control devices ( 110 ) and at least a first controller ( 102 ) digitally linked with a second controller ( 104 ) via an interface ( 108 ). The first and the second controllers exchange information for generation of a force control command (FCC) either the first or second controller. The FCC is then executed at a first vibration control device ( 110 ) of the plurality of vibration control devices (FG) for providing active vibration control within a vehicle. A method of providing vibration control in a vehicle includes providing a plurality of active vibration control devices ( 100 ) and providing at least a first controller ( 102 ) digitally linked with a second controller ( 104 ). The method further includes generating a FCC using information exchanged between the first and the second controllers. The method further includes sending the FCC to a first vibration control device ( 110 ) of the plurality of devices (FG).

First claim

What is claimed is:

1. A vibration control system comprising:
a plurality of vibration control devices;
at least a first controller digitally linked with a second controller via a two-way electronic communication interface; and
wherein the first and the second controllers are configured to exchange information for generation of a force control command (FCC) at either one of the first or the second controllers, and wherein the FCC is executed at a first vibration control device of the plurality of vibration control devices for providing active vibration control, the second controller being slaved to the first controller.

2. The system of claim 1 , wherein the first controller is configured to generate and send a plurality of FCCs to a plurality of other controllers.

3. The system of claim 1 , wherein the first controller is configured to generate a first FCC and a wherein the second controller is configured to generate a second FCC.

4. The system of claim 1 , wherein the interface includes an Ethernet communication protocol, an RS232 communication protocol, a fiber optic cable protocol, a controller area network (CAN) bus communication protocol, an ARINC-429 communication protocol, an RS422 communication protocol, a MIL-STD-1553 communication protocol, or a wireless communication protocol.

5. The system of claim 1 , further comprising at least three controllers linked via a two-way electronic communication, wherein two of the controllers are slaved to the first controller.

6. The system of claim 1 , wherein the first and second controllers are configured to exchange information including a rotor speed.

7. The system of claim 1 , wherein the first and second controllers are configured to exchange information including at least one error code.

8. The system of claim 1 , wherein the first and second controllers are configured to exchange information including diagnostic information.

9. The system of claim 1 , wherein the first and second controllers are configured to exchange information including a software update.

10. The system of claim 1 , wherein the first and second controllers are configured to exchange information including a de-modulated accelerometer value.

11. The system of claim 1 , wherein the plurality of active vibration control devices comprises a plurality of circular force generators (CFGs).

12. The system of claim 1 , wherein the plurality of active vibration control devices comprises a plurality of linear actuators.

13. The method of claim 1 , wherein the plurality of active vibration control devices comprises a plurality of balancers.

14. A vibration control system comprising:
a plurality of active vibration control devices;
at least a first controller digitally linked with a second controller via a two-way electronic communication therebetween; and
wherein the first controller is configured to generate a force control command (FCC) for execution at a first active vibration control device of the plurality of active vibration control devices, and wherein the FCC is communicated to the first active vibration control device via the second controller, the second controller being slaved to the first controller.

15. The system of claim 13 , wherein the first controller is configured to generate the FCC using information exchanged by the first controller and the second controller.

16. The system of claim 13 , wherein the first and second controllers are configured to exchange information including a rotor speed.

17. The system of claim 13 , wherein the first and second controllers are configured to exchange information including at least one error code.

18. The system of claim 13 , wherein the first and second controllers are configured to exchange information including diagnostic information.

19. The system of claim 13 , wherein the first and second controllers are configured to exchange information including a software update.

20. The system of claim 13 , wherein the first and second controllers are configured to exchange information including a de-modulated accelerometer value.

21. The system of claim 13 , further comprising a plurality of sensors connected to the first and second controllers.

22. The system of claim 13 , wherein the plurality of vibration control devices comprises a plurality of circular force generators (CFGs), linear actuators, or balancers.

23. A method of providing vibration control in a vehicle, the method comprising:
providing a plurality of active vibration control devices;
providing at least a first controller digitally linked with a second controller, the first controller and second controller having a two-way electronic communication therebetween, wherein the second controller is slaved to the first controller;
generating a force control command (FCC) using information exchanged between the first and the second controllers; and
sending the FCC to a first vibration control device of the plurality of vibration control devices.

24. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using an Ethernet communication protocol.

25. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using a RS232 communication protocol.

26. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using a fiber optic cable communication protocol.

27. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using a controller area network (CAN) communication protocol.

28. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using an ARINC-429 communication protocol.

29. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using a RS422 communication protocol.

30. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using a MIL-STD-1553 communication protocol.

31. The method of claim 23 , wherein providing at least a first controller digitally linked with a second controller includes using a wireless communication protocol.

32. The method of claim 23 , wherein providing a plurality of active vibration control devices comprises providing a plurality of circular force generators (CFGs).

33. The method of claim 23 , wherein providing a plurality of active vibration control devices comprises providing a plurality of linear actuators.

34. The method of claim 23 , wherein providing a plurality of active vibration control devices comprises providing a plurality of balancers.

35. The method of claim 23 , wherein the information exchanged by the first controller and the second controller includes a rotor speed.

36. The method of claim 23 , wherein the information exchanged by the first controller and the second controller includes at least one error code.

37. The method of claim 23 , wherein the information exchanged by the first controller and the second controller includes diagnostic information.

Assignees

• Lord Corp
• Swanson Doug A
• Edeal David W
• Pedersen Douglas G
• Clark David

Inventors

• Swanson Doug A
• Edeal David W
• Pedersen Douglas G
• Clark David

Classifications

• F16F15/002

  characterised by the control method or circuitry (control of mechanical oscillations per se G05D19/00) · CPC title

• B64C2027/004

  using actuators, e.g. active systems · CPC title

• B64C27/001 Primary

  Vibration damping devices · CPC title

• G05D19/02

  characterised by the use of electric means · CPC title