Smart structures for vibration suppression

• US 5,525,853 A
• Filed: 06/02/1994
• Issued: 06/11/1996
• 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): Dougherty, Thomas M.
• Application Number:
  US08/253,431
• Time in Patent Office: 740 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 device for controlling strain in a foundation member comprising an assembly being a piezoelectric sensor and a piezoelectric actuator located in operative relative relationship, means for placing the assembly in operative relationship with a foundation member whereby the sensor detects a strain in the foundation member and whereby the actuator imparts a selected force to the foundation member, means for connecting local control electronics in operative relationship with the assembly, a further control means located remotely from the assembly and connected with the local control electronics, wherein said further control means provides at least one of power for the local control electronics and a central command communication for the local control electronics, means for locating the local control electronics in physical abutment with the assembly, and means for connecting the local control electronics including an interface for location between the assembly and the control electronics.

2. A device as claimed in claim 1 wherein the assembly is a pre-formed patch.

3. A foundation member comprising multiple numbers of the device as claimed in claim 1, the multiple numbers of the device each being spaced selectively about the foundation member.

4. A foundation member as claimed in claim 3 wherein the assembly is a pre-formed patch.

5. A method for controlling strain in a foundation member comprising locating a piezoelectric sensor and a piezoelectric actuator assembly in operative relative relationship, whereby when the sensor detects a strain in the foundation member the actuator imparts a force to the foundation member, connecting local control electronics in operative relationship with the assembly, connecting a further control means located remotely from the assembly with the local control electronics, wherein said further control means provides at least one of power for the local control electronics and a central command communication for the local control means, locating the local control electronics in physical abutment with the assembly, selectively embedding with or bonding the assembly with the foundation member, the sensor and actuator being spaced on the assembly and the assembly being encapsulated in graphite reinforced plastic, and providing an access in the graphite for permitting connection between the local control electronics and the assembly.

6. A control unit for controlling strain in a foundation member, the control member comprising an assembly being a piezoelectric sensor and a piezoelectric actuator locating in operative relative relationship, means for placing the assembly in operative relationship with a foundation member whereby the sensor detects a strain in the foundation member and whereby the actuator imparts a force to the foundation member, means for connecting control electronics in operative relationship with the assembly and wherein the control electronics is integrated with the assembly.

7. A control unit as claimed in claim 6 wherein the unit is a pre-formed patch.

8. A foundation member comprising multiple numbers of the control unit as claimed in claim 6, the multiple numbers of the control unit each being spaced selectively about the foundation member.

9. A foundation member as claimed in claim 8 wherein the assembly is a preformed patch.

10. A method of controlling strain in a foundation member comprising locating an assembly including a piezoelectric sensor and a piezoelectric actuator in operative relative relationship on the foundation member, whereby the sensor detects a strain in the foundation member and whereby the actuator imparts a force to the foundation member, connecting control electronics in operative relationship with the assembly, and including integrating the control electronics with the assembly.