Tri-axial hybrid vibration isolator

• US 7,586,236 B2
• Filed: 10/10/2006
• Issued: 09/08/2009
• Est. Priority Date: 10/07/2005
• Status: Expired due to Fees

• Current Assignee: The Government Of The United States Of America, As Represented By The Secretary Of The Navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Houston, Brian H, Klunder, Joseph D., Herdic, Peter C, Corsaro, Robert D
• Primary Examiner(s): BUDD, MARK OSBORNE
• Application Number:
  US11/539,912
• Publication Number:
  US 20070164189A1
• Time in Patent Office: 1,064 Days
• Field of Search: 310/322, 310/328, 310/329
• US Class Current: 310/322
• CPC Class Codes: F16F 15/005 using electro- or magnetostrictive actuation means generating of mechanical vibrations operating with electrostriction B06B1/06, with magnetostriction B06B1/08; vehicle suspension arrangements characterised by use of piezoelectric elements B60G17/01941; piezoelectric, electrostrictive and magnetostrictive devices per se H10N30/00
• CPC Class Codes: F16F 15/08 with rubber springs grommet- or bushing-type resilient mountings F16F1/3732, F16F1/38; with springs made of rubber and metal arrangement of internal-combustion or jet-propulsion units B60K5/12; mounting of propulsion plants on vessels B63H21/30; mounting of vehicle drivers' cabs B62D33/0604

Abstract

A tri-axial vibration isolation device having: a passive isolation assembly including a first frame, a plurality of passive lateral isolators supporting the support frame on the base, and a plurality of passive vertical isolators; and an actuator assembly including a second frame, a vertical actuator arranged between the load and the second frame, and a plurality of lateral actuators arranged between the second frame and the passive vertical isolators. The actuators can be piezoelectric elements that change their thickness in response to an electrical signal. The lateral actuators are arranged in oppositely poled pairs. An accelerometer or other sensor provides information to a controller that controls the actuators.

Claims

1. A three-axis device for reducing vibrations transmitted between a base and a load, the device comprising:

a passive isolation assembly including a first frame, a plurality of passive lateral isolators supporting the support frame on the base, and a plurality of passive vertical isolators;

an actuator assembly including a second frame, a vertical actuator arranged between the load and the second frame, and a plurality of lateral actuators arranged between the second frame and the passive vertical isolators.

2. The device according to claim 1, wherein each of the plurality of lateral actuators is adhered to one of the passive vertical isolators.

3. The device according to claim 1, wherein the vertical actuator is located on an axis collinear with applied force and displacement.

4. The device according to claim 1, wherein the lateral actuators are located in a plane that includes the center of action of the device.

5. The device according to claim 1, wherein the vertical actuator is located in the plane that includes the center of action of the device.

6. The device according to claim 1, wherein the lateral actuators are located in a common horizontal plane.

7. The device according to claim 6, wherein the vertical actuator is in the common horizontal plane or is offset vertically from the common horizontal plane.

8. The device according to claim 1, further comprising at least one sensor, the sensor being an accelerometer, a force cell, a strain sensor, a displacement sensor, a velocity sensor, or a strain sensor.

9. The device according to claim 8, further comprising a controller arranged to receive a signal from the sensor and to send electrical control signals to the vertical actuator and the lateral actuators.

10. The device according to claim 8, wherein the sensor is an accelerometer arranged to measure acceleration of the base or the load.

11. The device according to claim 1, wherein the lateral actuators are piezoelectric elements.

12. The device according to claim 1, wherein the lateral actuators are configured as two pairs of oppositely poled piezoelectric elements.

13. The device according to claim 1, wherein the frames are stiffer than the passive isolators.

14. A device for reducing vibrations transmitted from a first structure to a second structure, the device comprising:

a first support member arranged between the first structure and the second structure;

at least one actuator arranged between the first support member and the first structure;

a second support member arranged between the first support member and the second structure;

at least one passive support member arranged between the second support member and the second structure,

at least one actuator arranged between the first support member and the second support member, and

at least one passive isolation member arranged between the first support member and the second support member,

the support members being stiffer than the passive isolation members.

15. The device according to claim 14, wherein the passive isolation members are rubber.

16. The device according to claim 14, wherein the passive isolation member arranged between the first support member and the second support member is arranged between the second actuator and the first support member.

17. The device according to claim 14, wherein the actuators comprise a piezoelectric material.

18. The device according to claim 14, wherein the actuators include pairs of oppositely poled piezoelectric elements that change their thickness in response to an electrical voltage.

19. The device according to claim 14, further comprising at least one sensor, the sensor being an accelerometer, a force cell, a strain sensor, a displacement sensor, a velocity sensor, or a strain sensor.

20. The device according to claim 14, further comprising a controller arranged to receive a signal from the sensor and to send electrical control signals to the actuators.

21. The device according to claim 19, wherein the sensor is an accelerometer arranged to measure acceleration of the first structure or the second structure.