Integrated compliant boundary for piezoelectric bimorph actuator

Patent metadata

Field	Value
Publication number	US-9882115-B2
Application number	US-201514677138-A
Country	US
Kind code	B2
Filing date	Apr 2, 2015
Priority date	Apr 2, 2015
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

Abstract

A piezoelectric bimorph actuator with an integral compliant boundary employs a first piezoelectric element, a second piezoelectric element and a composite layer intimately engaged between the first and second piezoelectric elements to form a bimorph actuator. The composite layer extends from a peripheral edge of the piezoelectric elements and has a curved interface portion providing a mount for attachment of the bimorph actuator.

First claim

What is claimed is:

1. A piezoelectric bimorph actuator with an integral compliant boundary comprising:
a first piezoelectric element;
a second piezoelectric element;
a composite layer intimately engaged between said first and second piezoelectric elements to form a bimorph actuator, said composite layer extending from a peripheral edge of the piezoelectric elements and having a curved interface portion terminating in a peripheral attachment portion providing a mount for attachment of the bimorph actuator; and,
a ring shaped clamping element securing the peripheral attachment portion in a circular boundary.

2. The piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 1 wherein the first and second piezoelectric elements are first and second piezoelectric disks and the composite layer comprises a center section engaged between said first and second piezoelectric disks, a double radius curved interface portion extending from the center section and terminating in the peripheral attachment portion.

3. The piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 2 wherein the double radius curved interface portion is substantially S shaped.

4. The piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 1 wherein the composite layer comprises carbon fiber impregnated with an epoxy resin.

5. The piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 4 wherein the carbon fiber comprises a plain weave carbon fabric 0.003 to 0.005 inches in thickness.

6. A piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 1 wherein the first piezoelectric element comprises a first piezoelectric disk having a first diameter; the second piezoelectric elements comprises a second piezoelectric disk having a second diameter; and the composite layer has a first inflection point defining a perimeter of a center portion having a length A wherein the center portion of the composite layer is intimately engaged between the first and second piezoelectric disks to form the bimorph actuator and wherein the first and second piezoelectric disks are placed within the perimeter of the center portion length A and wherein the second diameter is less than or equal to length A.

7. A piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 1 further comprising a valve stem adapted to engage one of the piezoelectric elements.

8. A piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 1 further comprising a valve spool adapted to engage one of the piezoelectric elements.

9. The piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 1 , wherein the bimorph actuator is disposed in a recessed pocket on a wing of an aircraft to enable active flow control.

10. A piezoelectric bimorph actuator with an integral compliant boundary comprising:
a first piezoelectric element;
a second piezoelectric element;
a composite layer intimately engaged between said first and second piezoelectric elements to form a bimorph actuator, said composite layer extending from a peripheral edge of the piezoelectric elements and having a curved interface providing a mount for attachment of the bimorph actuator; and,
a first carbon veil patch adhered to the first piezoelectric element and a second carbon veil patch adhered to the second piezoelectric element each of said carbon veil patches receiving an electrical lead.

11. The piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 10 wherein each electrical lead is secured to the associated carbon veil patch with a silver epoxy.

12. A method for fabrication of a piezoelectric bimorph actuator with an integral compliant boundary comprising:
placing a piezoelectric disk as a first piezoelectric element in the center of a depression in a female mold;
pressing a composite layer comprising a saturated piece of carbon fiber on top of the piezoelectric disk urging the fiber against a filleted surface of the circumference of the depression in the mold to obtain a desired geometry of a curved section and creating an indent;
placing an upper piezoelectric disk as a second piezoelectric element in the indent on top of the saturated carbon fiber to form a bimorph actuator, said composite layer extending from a peripheral edge of the first and second piezoelectric elements and having a peripheral attachment extending from the curved section providing a mount for attachment of the bimorph actuator;
curing the bimorph actuator; and
securing a ring shaped clamping element on the peripheral attachment portion in a circular boundary.

13. The method for fabrication of a piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 12 wherein the step of curing the bimorph actuator further comprises:
aligning a male mold on top of the upper piezo electric disk to complete a mold stack;
placing the mold stack into a hot press;
heating the mold for cure.

14. The method for fabrication of a piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 13 further comprising applying force to the hot press.

15. The method for fabrication of a piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 14 further comprising:
removing the mold stack from hot press and allowing the stack to cool;
removing the cured disk bimorph from the mold.

16. The method for fabrication of a piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 15 further comprising:
cutting a substantially circular piece of carbon veil having a lesser diameter than the piezoelectric disks for placement on the upper piezoelectric disk;
applying a thin layer of epoxy to an exposed surface of the upper piezoelectric disk;
placing the carbon veil piece on the thin layer of epoxy without overlapping of carbon veil and carbon fiber;
placing a small quantity of silver epoxy on top of carbon veil piece;
placing the disk bimorph face down on the male mold;
cutting a second substantially circular piece of carbon veil having a lesser diameter than the piezoelectric disks for placement on the lower piezoelectric disk;
applying a second thin layer of epoxy to an exposed surface of the lower piezoelectric disk; and,
placing the second substantially circular carbon veil piece on the second thin layer of epoxy without overlapping of carbon veil and carbon fiber.

17. The method for fabrication of a piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 16 further comprising:
applying epoxy to fill in any holes in carbon fiber;
placing the female mold on top the disk bimorph reconstituting the mold stack;
placing the mold stack into the hot press;
applying force and heat to cure.

18. The method for fabrication of a piezoelectric bimorph actuator with an integral compliant boundary as defined in claim 17 further comprising:
removing the mold stack from the hot press and allowing the mold stack to cool;
removing the bimorph actuator from the mold;
carving a small area on the carbon fiber to attach a ground wire;
abrading the epoxy in a small area on exposed faces of the piezoelectric disks for contact exposure with the first and second carbon veil patches; and,
attaching wire leads to the bimorph actuator in the abraded areas with silver epoxy for electrical contact.

Assignees

• Boeing Co

Inventors

• Clingman Dan J
• Zidovetzki Esther S

Classifications

• H02N2/043 Primary

  Mechanical transmission means, e.g. for stroke amplification · CPC title

• B64C2230/18

  by using small jets that make the fluid flow oscillate · CPC title

• B64C23/005 Primary

  by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds · CPC title

• H01L41/0478

  Electricity · mapped topic

• H01L41/053 Primary

  Electricity · mapped topic