Smart structures for vibration suppression

• US 6,191,519 B1
• Filed: 08/30/1995
• Issued: 02/20/2001
• Est. Priority Date: 01/21/1993
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: TRW Inc. (Northrop Grumman Corporation)
• Inventors: Bronowicki, Allen J., Nye, Theodore W., Wyse, Richard E., Dvorsky, George R.
• Primary Examiner(s): Doughtery, Thomas M.
• Application Number:
  US08/521,562
• Time in Patent Office: 2,001 Days
• Field of Search: 310/316, 310/317, 310/319, 310/321, 310/326, 310/328, 310/330, 310/331, 310/332
• US Class Current: 310/316.01
• 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: H10N 30/00 Piezoelectric or electrostrictive devices integrated devices or assemblies of multiple devices H10N39/00

Abstract

Modular control patches including assemblies of sensors and actuators are provided to impart or control vibration of foundation members such as struts in aerospace apparatus. Local analog electronic control means is associated with each control patch assembly. Patches are attached mechanically or by chemical bonding to the outside of the struts. The corresponding electronics can be selectively removed and replaced. The patch being the sensors and actuators may also be attached or embedded with a composite structure.

Claims

1. A pre-formed control patch for controlling strain in a foundation member, the patch comprising a base, a piezoelectric sensor and a piezoelectric actuator located in operative relative relationship, means for placing the patch in operative relationship with the foundation member whereby the sensor detects a strain in the foundation member and whereby the actuator imparts a strain-inducing force to the foundation member, and including means for connecting control electronics in operative relationship with the patch.

2. A control patch as claimed in claim 1 including means for locating control electronics in physical abutment with the patch.

3. A control patch as claimed in claim 1 wherein the means for connecting the electronic control electronics includes an interface for location between the patch and the control electronics, the interface being adapted for supporting the control electronics in strain isolation from the base.

4. A control patch as claimed in claim 1 wherein the means for placing the patch comprises the patch being bonded to the foundation member.

5. A control patch as claimed in claim 1, wherein the piezoelectric sensor is spaced laterally from the piezoelectric actuator, the patch further comprising a graphite element for at least partly encapsulating the base, the sensor and the actuator.

6. A control patch as claimed in claim 5 including access means in the graphite element for permitting connection between the electronic control means and the patch.

7. A control patch as claimed in claim 2 wherein the means for locating the control electronics in physical abutment with the assembly comprises a strain-forgiving interface connection.

8. A foundation member comprising multiple control patches as claimed in claim 1, the multiple control patches being spaced selectively about the foundation member.

9. A control patch as claimed in claim 1 wherein the means for placing the patch comprises the patch being imbedded in the foundation member.

10. A foundation member comprising a control patch as claimed in claim 1.

20. A foundation member comprising multiple numbers of the device as claimed in claim 8, the multiple numbers of the device each being spaced selectively about the foundation member.

11. A device for controlling strain in a foundation member comprising an assembly being a piezoelectric sensor and a piezoelectric actuator located in operative relative relationship, local control electronics, means for operatively connecting the local control electronics between the assembly of the sensor and the actuator, and means for placing the assembly in operative relationship with the foundation member whereby the sensor detects a strain in the foundation member and whereby the local control electronics processes a signal from the sensor and activates the actuator, and the actuator imparts a force to the foundation member.

12. A device as claimed in claim 11 wherein local control electronics comprises an input stage for amplifying an analog signal from the piezoelectric sensor, compensator means for dynamically processing the amplified signal, and a drive amplifier for receiving the processed signal and activating the piezoelectric actuator.

13. A device as claimed in claim 12 wherein the compensator means applies a frequency-dependent electric phase shift relative to a mechanical resonance of a foundation member thereby to provide a signal for suppressing vibrations of the foundation member through the actuator.

14. A device as claimed in claim 12 wherein the compensator means is an analog device including filtering means having a cutoff frequency substantially tuned to match mechanical characteristics of the foundation member.

15. A device as claimed in claim 14 wherein the filtering means includes capacitor means and resistor means, an effective capacitance and a resistance of the filtering means being selected for achieving a desired tuning frequency.

16. A device as claimed in claim 12 wherein the drive amplifier includes a lead-lag circuit, the lead-lag circuit reducing a gain of the drive amplifier at a selected frequency related to the actuator and acting to minimize oscillation at the selected frequency.

17. A device as claimed in claim 12 wherein the compensator means applies a frequency dependent electric gain relative to a mechanical resonance of a foundation member thereby to provide a signal for suppressing vibrations of the foundation member through the actuator.

18. A device as claimed in claim 12 wherein the compensator means applies a frequency dependent combination of electric gain and phase shift relative to a mechanical resonance of a foundation member thereby to provide a signal for suppressing vibrations of the foundation member through the actuator.

19. A device as claimed in claim 11 wherein the assembly is a pre-formed patch.

21. A device as claimed in claim 11 wherein the local control electronics is embedded in the means for operatively connecting.

22. A pre-formed control patch for controlling strain in a foundation member, the patch comprising a base;

a piezoelectric first sensor and a plurality of piezoelectric actuators located in operative relative relationship, the actuators being located in a string array and fixedly located on the base;

an intermediate encapsulation layer having cavities for the actuators, the intermediate encapsulation layer being fixedly located on the base and the actuators, the first sensor being fixedly located on the intermediate encapsulation layer in co-located relation with the string array of actuators;

a second piezoelectric sensor fixedly located on the intermediate encapsulation layer and spaced laterally in nearly-colocated relation with the string array;

an outer encapsulation layer having cavities for the sensors, the outer encapsulation layer being fixedly located on the intermediate encapsulation layer and the sensors;

a graphite tape overwrap affixed to the outer encapsulation layer; and

means for placing the patch in operative relationship with the foundation member whereby the sensor detects a strain in the foundation member and whereby the actuators impart a strain-inducing force to the foundation member;

means for connecting control electronics in operative relationship with the patch.

23. A method for controlling strain in a foundation member comprising the steps of providing an assembly comprising a piezoelectric sensor and a piezoelectric actuator;

locating the assembly in operative relative relationship with the foundation member; and

connecting local control electronics between the sensor and the actuator without coupling strain between the assembly and the local control electronics, whereby when the sensor detects a strain in the foundation member the control electronics processes a signal from the sensor for the actuator, the actuator imparts a force to the foundation member.

24. A method as claimed in claim 23 wherein the control electronics amplifies an analog signal from the piezoelectric sensor, dynamically compensates the amplified signal, amplifies the compensated signal, and activates the piezoelectric actuator.

25. A method of controlling strain in a foundation member comprising the steps of providing an assembly comprising a base, a piezoelectric sensor and a piezoelectric actuator coupled to the base;

locating the assembly in operative relative relationship on the foundation member; and

connecting control electronics in operative relationship with the assembly, whereby the sensor detects a strain in the foundation member and whereby the actuator imparts a force to the foundation member in response to the strain.

26. A method as claimed in claim 25 including locating the control electronics in physical abutment with the assembly.

27. A method as claimed in claim 26 including bonding the assembly to the foundation member.

28. A method as claimed in claim 26 including laterally spacing the sensor from actuator, and encapsulating the assembly in graphite reinforced plastic.

29. A method as claimed in claim 28 including providing an access in the graphite reinforced plastic for permitting connection between the control electronics and the assembly.

30. A method as claimed in claim 26 including embedding the assembly within the foundation member.