High density structural health monitoring system and method

• US 8,447,530 B2
• Filed: 01/16/2008
• Issued: 05/21/2013
• Est. Priority Date: 01/11/2008
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Pado, Lawrence E., Dunne, James P., Belk, John H.
• Primary Examiner(s): Raymond, Edward
• Application Number:
  US12/015,289
• Publication Number:
  US 20090182515A1
• Time in Patent Office: 1,952 Days
• Field of Search: 702/36
• US Class Current: 702/36
• CPC Class Codes: G01M 5/0066 by exciting or detecting vibration or acceleration vibration testing of structures G01M7/00
• CPC Class Codes: G01M 7/025 Measuring arrangements

Abstract

A method for monitoring and diagnosing the health of a structure. The method includes providing a plurality of damage monitoring units each having at least one actuator, at least one sensor and a data collection device. The sensors are arranged and disposed to measure vibration produced by the actuator and provide a signal corresponding to the measured vibration to the data collection device. The actuator is activated and the vibration is measured with the sensor. The signal is compared to a reference signal and a damage index value is determined in response to the comparison between the signal and reference signal. The damage index value is transmitted for each vibratory path to a central processing device and the damage index values are analyzed for the plurality of damage monitoring units to determine the location of damage to the structure.

Claims

1. A method for monitoring and diagnosing the health of a structure comprising

providing a plurality of monitoring units upon a surface of the structure, the monitoring units each including at least one actuator that generates a vibration, at least one sensor a plurality of sensors and a data collection device,

wherein the plurality of damage monitoring units are separated into groups, and

wherein monitoring units of each group are spatially arranged to preclude interference,

the plurality of sensors being arranged and disposed to measure vibration produced by the at least one actuator and provide signals corresponding to the measured vibration to the data collection device, the measured vibration corresponding to a vibratory path between the at least one actuator and the plurality of sensors;

activating the at least one actuator to generate a vibration and measuring the vibration with the plurality of sensors and generating a plurality of signals corresponding to the measured vibration;

providing the plurality of signals to a data collection device;

comparing the plurality of signals to a reference signal;

determining a damage index value corresponding and limited to the vibratory path in response to the comparison between the plurality of signals and reference signal with the data collection device;

transmitting the damage index value for each vibratory path to a central processing device; and

analyzing the damage index values for the plurality of monitoring units to determine a location of damage to the structure;

wherein the at least one actuator and the plurality of sensors are printed onto the surface of the structure.

2. The method of claim 1, wherein one or both of the at least one actuator and the at least one sensor are piezoelectric transducers.

3. The method of claim 1, where the reference signal is obtained by measuring vibration with the at least one sensor on an undamaged structure.

4. The method of claim 1, where the reference signal is a signal corresponding to an undamaged structure.

5. A structural monitoring system for monitoring and diagnosing the health of a structure comprising:

a plurality of monitoring units, the monitoring units each including at least one actuator that generates a vibration, a plurality of sensors and a data collection device,

wherein the plurality of damage monitoring units are separated into groups, and

wherein monitoring units of each group are spatially arranged to preclude interference,

the plurality of sensors being arranged and disposed to measure vibration produced by the actuator and provide a plurality of signals corresponding to the measured vibration to the data collection device, the measured vibration corresponding to a vibratory path between the actuator and the plurality of sensors, the data collection device being configured to determine a damage index value from data consisting essentially of the measured vibration; and

a central processing device configured to receive and analyze damage index values from the plurality of damage monitoring units, the central processing device being capable of determining the location of damage to the structure from the damage index values determined essentially by the measure vibration;

wherein the at least one actuator and the plurality of sensors are printed onto the structure.

6. The system of claim 5, wherein the central processing device is a microprocessor that analyzes the damage index values and determines the location of damage to the structure.

7. The system of claim 5, wherein the data collection device is an integrated circuit.

8. The system of claim 5, wherein one or both of the at least one actuator and the plurality of sensors are piezoelectric transducers.

9. The system of claim 5, wherein the monitoring units include one actuator and eight sensors.

10. The system of claim 5, where the plurality of sensors and data collection device are electrically connected by printed conductive interconnections.

11. A vehicle comprising:

a structural element;

a plurality of monitoring units affixed to a surface of the structural element, the monitoring units each including at least one actuator that generates a vibration, a plurality of sensors and a data collection device,

wherein the plurality of damage monitoring units are separated into groups, and

wherein monitoring units of each group are spatially arranged to preclude interference,

the plurality of sensors being arranged and disposed to measure vibration produced by the actuator and provide a plurality of signals corresponding to the measured vibration to the data collection device, the measured vibration corresponding to a vibratory path between the actuator and the plurality of sensors, the data collection device being configured to determine a damage index value corresponding to the measured vibration; and

a central processing device configured to receive and analyze damage index values from the plurality of damage monitoring units, the central processing device determining a location of damage to the structural element by combining data damaging index values from each of the four damage monitoring groups;

wherein the at least one actuator and the plurality of sensors are printed onto the surface of the structure.

12. The vehicle of claim 11, wherein the central processing device is a microprocessor that analyzes the damage index values and determines the location of damage to the structure.

13. The vehicle of claim 11, wherein the data collection device is an integrated circuit.

14. The vehicle of claim 11, wherein one or both of the at least one actuator and the plurality of sensors are piezoelectric transducers.

15. The vehicle of claim 11, wherein the monitoring units include one actuator and eight sensors.

16. The vehicle of claim 11, wherein the sensors and data collection device are electrically connected by printed electrically conductive interconnections.

17. The vehicle of claim 11, wherein the structural element is fabricated from a material selected from the group consisting of metal, composite, polymer, ceramic and combinations thereof.