IP Library Granted Patent US 12,449,014
Granted Patent B2
US 12,449,014 · App. 18/257,602 · Granted Oct 21, 2025

Vibration control systems

Inventors: Suleiman Mahmoud Sharkh (Southampton, GB); Stephen Daley (Southampton, GB); Mehdi Hendijanizadeh (Southampton, GB)
Assignee: BAE SYSTEMS PLC
F16F7/1011F16F6/00H02K33/18F16F2222/06F16F2222/08F16F2228/063F16F2230/18
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Quick Facts
Patent No.
US 12,449,014
App. No.
18/257,602
Granted
Oct 21, 2025
Kind
B2
Abstract

According to the present invention there is provided an active vibration control system comprising: an electromagnetic actuator and a control element, the electromagnetic actuator being operable to apply a force on a base structure to which the active vibration control system is attachable such that vibrations of the base structure are actively controllable by the application of said force, wherein the electromagnetic actuator and control element are relatively moveable such that the active vibration control system has at least two modes of vibration, and wherein movement of the electromagnetic actuator causes movement of at least a part of the control element.

Claims (23)

1. An active vibration control system comprising: an electromagnetic actuator and a control element, the electromagnetic actuator being operable to apply a force on a base structure to which the active vibration control system is attachable such that vibrations of the base structure are actively controllable by the application of said force, wherein the electromagnetic actuator and the control element are relatively moveable such that the active vibration control system has at least two modes of vibration, wherein movement of the electromagnetic actuator causes movement of at least a part of the control element, wherein the electromagnetic actuator comprises a movable member, and wherein, in a first mode of vibration, the moveable member and the control element oscillate in-phase with one another, and, in a second mode of vibration, the moveable member and the control element oscillate out-of-phase with one another.

2. The active vibration control system of claim 1 , wherein the electromagnetic actuator comprises a coil and the moveable member comprising a permanent magnet, the coil being associated with the permanent magnet such that current flowing through the coil in the presence of the magnetic field causes movement of the moveable member.

3. The active vibration control system of claim 1 , comprising a control system to control flow of current to the electromagnetic actuator.

4. The active vibration control system of claim 1 , wherein the electromagnetic actuator and control element are resiliently attached so that movement of the electromagnetic actuator causes movement of the at least a part of the control element.

5. The active vibration control system of claim 4 , wherein the electromagnetic actuator and the control element are resiliently attached via a plurality of compliant material layers.

6. The active vibration control system of claim 1 , wherein the control element is resiliently attached to the base structure.

7. The active vibration control system of claim 1 , wherein the electromagnetic actuator is a first electromagnetic actuator, and the control element is an active control mechanism comprising a second electromagnetic actuator, the second electromagnetic actuator being operable to cause displacement of the at least a part of the control element relative to the first electromagnetic actuator, thereby to control movement of the first electromagnetic actuator.

8. The active vibration control system of claim 1 , wherein the control element comprises a proof-mass.

9. The active vibration control system of claim 1 , comprising a plurality of electromagnetic actuators and a common control element.

10. The active vibration control system of claim 1 , wherein the electromagnetic actuator is arranged to move parallel to an axis, and the control element is arranged to move parallel to the axis.

11. The active vibration control system of claim 9 , wherein each electromagnetic actuator is arranged to move parallel to a different axis, and the control element is arranged to move parallel to each axis.

12. An active vibration control apparatus comprising a proof-mass and a plurality of active vibration control systems as claimed in claim 1 .

13. A vehicle comprising the active vibration control system of claim 1 .

14. The vehicle of claim 13 , wherein the base structure forms part of the vehicle.

15. A method of actively controlling vibrations of a base structure, the method comprising:

providing an active vibration control system that includes an electromagnetic actuator and a control element, the electromagnetic actuator and the control element being relatively moveable such that the active vibration control system has at least two modes of vibration, wherein movement of the electromagnetic actuator causes movement of at least a part of the control element, wherein the electromagnetic actuator comprises a movable member, and wherein, in a first mode of vibration, the moveable member and the control element oscillate in-phase with one another, and, in a second mode of vibration, the moveable member and the control element oscillate out-of-phase with one another;

attaching the active vibration control system to the base structure; and

operating the electromagnetic actuator to apply a force on the base structure.

16. The method of claim 15 , wherein the control element is resiliently attachable to the base structure.

17. The vehicle of claim 13 , wherein the vehicle is one of a ground-based vehicle, an aquatic vehicle, or an airborne vehicle.

18. A vehicle comprising the active vibration control apparatus of claim 12 .

19. The active vibration control system of claim 7 , wherein the control element comprises a proof-mass.

20. An active vibration control apparatus comprising a proof-mass and a plurality of active vibration control systems as claimed in claim 7 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 10, 2023
From: SHARKH, SULEIMAN MAHMOUD; DALEY, STEPHEN; HENDIJANIZADEH, MEHDI
To: BAE SYSTEMS PLC
Reel/Frame 064553/0394 →
Priority Claims (2)
EP 20275179 · Dec 15, 2020 · regional
GB 2019754 · Dec 15, 2020 · national
Continuity (1)
Related Publication 20240035535A1 · Feb 1, 2024
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Cited By (1)
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