Broadband energy harvester apparatus and method

• US 7,439,657 B2
• Filed: 10/20/2006
• Issued: 10/21/2008
• Est. Priority Date: 10/20/2006
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Pena, Gerardo, Clingman, Dan J
• Primary Examiner(s): BUDD, MARK OSBORNE
• Application Number:
  US11/551,388
• Publication Number:
  US 20080100180A1
• Time in Patent Office: 732 Days
• Field of Search: 310/330, 310/332, 310/339
• US Class Current: 310/339
• CPC Class Codes: H02N 2/186 Vibration harvesters
• CPC Class Codes: H10N 30/304 Beam type

Abstract

A broadband vibration energy harvesting apparatus and method. In one embodiment, a straight piezoelectric beam and a straight biasing beam are disposed parallel to one another and axially compressed by a support structure such that both of the beams are slightly bowed. This buckles and reduces the axial stiffness of both of the beams. The piezoelectric beam is secured to an external vibrating structure and supported by the structure. The flexing motion of the piezoelectric beam generates electrical signals that can be used to power a wide variety of devices. The apparatus is especially sensitive to small amplitude vibration signals and is able to harvest vibration energy over a wide range of frequencies, and is not limited to vibrations at discrete resonant frequencies. The apparatus is especially well suited for use in powering remotely located electrical sensors and actuators employed in automotive, aircraft and aerospace applications.

Claims

1. An energy harvesting apparatus, comprising:

a beam including an electrically responsive material, and attachment structure for enabling the beam to be coupled to an external structure experiencing vibration;

a force biasing member disposed adjacent said beam;

a support structure for engaging each of said beam and said biasing member, and capable of applying compressive force to said beam and said biasing member, to soften said beam and biasing members; and

said beam adapted to flex in response to vibration from said external structure, to generate electrical signals, and said biasing member being adapted to bias said beam to promote flexing movement of said beam in response to vibration.

2. The apparatus of claim 1, wherein each of said beam and said biasing member have a lengthwise bending stiffness, and wherein the stiffnesses are substantially the same.

3. The apparatus of claim 1, wherein said beam comprises a substrate material on which said electrically responsive material is disposed.

4. The apparatus of claim 1, wherein said electrically responsive material comprises a piezoelectric material.

5. The apparatus of claim 1, wherein said beam comprises a substrate member having opposing planar surfaces, with each of said opposing planar surfaces including a layer of said electrically responsive material disposed thereon;

and

wherein said layers of electrically responsive material each comprise a piezoelectric layer of material.

6. The apparatus of claim 1, wherein said beam and said biasing member are constructed to have substantially the same coefficients of thermal expansion.

7. The apparatus of claim 1, wherein said beam comprises:

a carbon laminate substrate having first and second opposing surfaces; and

a piezoelectric material layer disposed on each of said first and second opposing surfaces.

8. The apparatus of claim 7, wherein said carbon laminate substrate comprises a fiber orientation of zero degrees.

9. The apparatus of claim 1, wherein said biasing member comprises:

a center substrate having first and second opposing surfaces; and

outer substrates formed on the first and second opposing surfaces of the center substrate.

10. The apparatus of claim 9, wherein:

said center support substrate comprises a carbon laminate having a fiber orientation of zero degrees; and

said outer substrates each comprise a carbon laminate having a fiber orientation from about 25 degrees to about 30 degrees.

11. The apparatus of claim 1, wherein:

said beam includes a carbon laminate substrate having first and second opposing surfaces, and wherein said electrically responsive material includes a piezoelectric material layer disposed on each of said first and second opposing surfaces; and

said biasing member includes a center support substrate having first and second opposing surfaces, and outer substrates formed on the first and second opposing surfaces of the center support substrate; and

wherein said outer substrates and said piezoelectric material layers all have approximately the same dimensions.

12. The apparatus of claim 11, wherein said carbon laminate substrate and said center substrate are each formed with a zero degree fiber orientation.

13. The apparatus of claim 1, wherein said support structure comprises:

a first proof mass for engaging a first end of each of said beam and said biasing member;

a second proof mass for engaging a second end of each of said beam and said biasing member;

a member communicating with said proof masses at an intermediate position on each said proof mass, and between areas where said ends of said beam and said biasing member are engaging said proof masses, to urge said proof masses towards one another and thus axially compress said beam and said biasing member; and

said member being operatively engaged with said proof masses to enable pivoting movement of both of said proof masses about areas where said ends of said beam and said biasing member are engaging said proof masses.

14. The apparatus of claim 13, wherein at least one of said proof masses includes an opening for receiving an end portion of said member, said opening being shaped to prevent rotational movement of said end portion of said member as said member is used to axially compress said beams.

15. The apparatus of claim 13, wherein at least one end of said beam comprises at least one protrusion, and wherein one of said proof masses includes a recess for engaging said protrusion, and wherein engagement of said protrusion within said recess forms a bearing arrangement that promotes pivoting movement of said one proof mass relative to said beam.

16. An energy harvesting apparatus, comprising:

a first beam including;

a support substrate

piezoelectric material layer secured to said support substrate for generating electrical output signals in response to flexing motion of the first beam; and

attachment structure for enabling the first beam to be coupled to an external structure experiencing vibration;

a second beam being flexible and disposed generally adjacent said first beam; and

a support structure for axially compressing both of said beams to soften said beams, and such that both of said beams assume a bowed shape, said softening of said first beam enabling said first beam to readily flex in response to vibration.

17. The apparatus of claim 16, wherein said first beam and said second beam have approximately the same axial stiffness.

18. The apparatus of claim 16, wherein said first beam comprises a pair of piezoelectric material layers on opposing surfaces of said support substrate.

19. The apparatus of claim 18, wherein said piezoelectric material layers are approximately equal in length, width and thickness to said outer carbon laminate layers.

20. The apparatus of claim 16, wherein said second beam comprises a center carbon laminate substrate with opposing surfaces, and outer carbon laminate layers secured to said opposing surfaces.

21. A method for harvesting vibration energy, comprising:

disposing a beam having an electrically responsive material adjacent a biasing member, each of said beam and biasing member being compressible;

supporting said beam and said biasing member under compression, and such that said compression softens said electrically responsive material of said beam;

securing said beam to a vibrating structure such that vibration generated by said vibrating structure causes flexing of said beam, with said electrically responsive material generating electrical signals in response to said vibration; and

using said biasing member to promote flexing movement of said beam.

22. The method of claim 21, wherein supporting said beams under compression comprises supporting said beam and said biasing member generally parallel to one another, and between a pair of proof mass members;

and

coupling said proof mass members to one another with a coupling member that compresses both said beam and said biasing member while enabling said proof mass members to both move pivotally relative to said coupling member as said beam flexes.