Systems and methods for harvesting vibrational energy from vehicles

• US 8,860,234 B2
• Filed: 01/03/2011
• Issued: 10/14/2014
• Est. Priority Date: 01/03/2011
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hoffman, Herbert, Hofbeck, Eric, Lin, Alex
• Primary Examiner(s): GONZALEZ, JULIO CESAR
• Application Number:
  US12/983,749
• Publication Number:
  US 20120169064A1
• Time in Patent Office: 1,380 Days
• Field of Search: 290/1.R, 290/54, 310/339, 310/25, 310/29, 310/36, 310/12.12
• US Class Current: 290/1.R
• CPC Class Codes: B64D 41/00 Power installations for auxiliary purposes
• CPC Class Codes: F03G 7/08 recovering energy derived from swinging, rolling, pitching or like movements, e.g. from the vibrations of a machine
• CPC Class Codes: H02N 2/188 adapted for resonant operation
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

Disclosed are methods, systems and apparatuses for harvesting vibrational energy from vehicles, as well as methods for locating vibrational energy on a vehicle. One harvesting apparatus comprises a vibrational energy harvester coupled to a substantially maximal vibrational displacement node of the structural element of a vehicle, and tuned to a frequency of vibration of the maximal vibrational displacement node. The harvester may be one of a variety of harvesting devices, such as piezoelectric devices. Methods are also provided to locate structural elements which are appropriate for vibrational energy harvesting.

Claims

1. An apparatus for harvesting vibrational energy from structural elements of a vehicle possessing vibrational energy, said apparatus comprising:

a first vibrational energy harvester coupled to a wing-to-body fairing panel in a primary area of the vehicle, and tuned to a frequency of vibration of the wing-to-body fairing panel in the primary area, and a second vibrational energy harvester coupled to a second structural element in a secondary area of the vehicle, the secondary area structurally coupled to and receiving vibrational energy from the primary area, the second structural element comprising a wing-to-body fairing support frame.

2. The apparatus of claim 1, wherein:

the first vibrational energy harvester is coupled to a substantially maximal vibrational displacement node of the wing-to-body fairing panel.

3. The apparatus of claim 2, wherein:

the first vibrational energy harvester is a piezoelectric device.

4. The apparatus of claim 3, wherein:

the second vibrational energy harvester is a piezoelectric device.

5. The apparatus of claim 4, further comprising:

additional piezoelectric devices placed on stringers and frames located near the area of said wing-to-body fairing panel.

6. The apparatus of claim 4, further comprising:

additional piezoelectric located at points of direct attachment between said wing-to-body fairing panel and said aircraft skin.

7. The apparatus of claim 4, further comprising:

additional piezoelectric located at points of direct attachment between said wing-to-body fairing support frame and said aircraft skin.

8. The apparatus of claim 4, further comprising:

a high impedance probe for monitoring the health of said piezoelectric devices by checking for changes in voltage or vibrational frequency characteristics.

9. An apparatus for harvesting vibrational energy from structural elements of a vehicle possessing vibrational energy, said apparatus comprising:

a vibrational energy harvester coupled to a substantially maximal vibrational displacement node of the structural element, and tuned to a frequency of vibration of the maximal virbrational displacement node;

said vibrational energy harvester is located within a primary area having structural elements with vibrational energy;

wherein the vibrational energy is induced in said structural elements due to turbulent airflow caused by shape or positioning of vehicle features or airflow generated by an engine, said airflow impinging on a surface of the vehicle;

said vehicle has a secondary area structurally coupled to, and receiving vibrational energy from said primary area; and

said secondary area has a vibrational energy harvester coupled to a structural element possessing significant vibrational energy within said secondary area.

10. The apparatus of claim 9, wherein:

the vibrational energy harvester is selected from the group consisting of a piezoelectric device, an electrostatic energy harvester and an electromagnetic energy harvester.

11. The apparatus of claim 10, wherein:

the vibrational energy harvester includes a cantilever beam piezoelectric device.

12. The apparatus of claim 9, further comprising:

harvesting circuitry coupled to the vibrational energy harvester, wherein said harvesting circuitry converts a raw electrical output of the harvester to a form more appropriate for use with onboard electrical systems.

13. The apparatus of claim 9, wherein:

the vibrational energy harvester comprises a cluster of individual energy harvesting devices.

14. The apparatus of claim 9, wherein the maximal displacement node is located on a structural element within a primary area.