Structural health management system and method for enhancing availability and integrity in the structural health management system

• US 7,263,446 B2
• Filed: 10/29/2004
• Issued: 08/28/2007
• Est. Priority Date: 10/29/2004
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Nutaro, Joseph J., Wilt, Nicholas J., Thompson, Steven R., Morin, Brent A.
• Primary Examiner(s): Barlow; John
• Assistant Examiner(s): KUNDU, SUJOY K
• Application Number:
  US10/976,748
• Publication Number:
  US 20060106550A1
• Time in Patent Office: 1,033 Days
• Field of Search: 702/34
• US Class Current: 702/34
• CPC Class Codes: G01N 2203/0073 Fatigue
• CPC Class Codes: G01N 2291/0258 Structural degradation, e.g. fatigue of composites, ageing of oils
• CPC Class Codes: G01N 2291/0421 Longitudinal waves
• CPC Class Codes: G01N 2291/0428 Mode conversion
• CPC Class Codes: G01N 2291/048 Transmission, i.e. analysed material between transmitter and receiver
• CPC Class Codes: G01N 2291/106 one or more transducer arrays
• CPC Class Codes: G01N 2291/2694 Wings or other aircraft parts
• CPC Class Codes: G01N 29/11 by measuring attenuation of acoustic waves

Abstract

A structural health management system is disclosed. The structural health management system comprises a zone of sensors. A first sensor data collector is coupled to a first subset of the sensors in the zone; and a second sensor data collector coupled to a second subset of the sensors in the zone. In the present invention, loss of a sensor data collector does not result in the loss of ability to perform nondestructive testing in an entire zone.

Claims

1. A method for operating a structural health management system comprising:

gathering data from a first zone of sensors and a second zone of sensors, each of the sensors mounted on a test material;

sending data from at least a first subset of sensors of the first zone of sensors to a first sensor data collector;

sending data from at least a first subset of sensors of the second zone of sensors to the first sensor data collector;

sending data from a second subset of sensors of the first zone of sensors to a second sensor data collector;

sending data from the first subset of sensors of the first zone to a processor from the first sensor data collector;

sending data from the second subset of sensors of the first zone to the processor from the second sensor data collector;

comparing the data from the first sensor data collector and the second sensor data collector; and

indicating a possible error condition indicative of a defective sensor if the data from the first sensor data collector and the data from the second sensor data collector differ by a predetermined amount.

2. The method of claim 1,

further comprising storing the data from the first and second sensor data collectors in a memory associated with the processor.

3. The method of claim 1 wherein the step of gathering data comprises:

generating elastic waves in the test material by pulsing each sensor;

receiving the elastic waves, the received elastic waves potentially altered by formations internal to the material; and

converting the received elastic waves to electrical signals representative of the structural health of the test material.

4. The method of claim 3 wherein the step of generating elastic waves in the test material comprises generating an elastic wave in an aircraft skin.

5. A method operating a structural health monitoring system comprising:

sending signals from a first subset of a zone of sensors to a first sensor data collector;

sending signals from a second subset of the zone of sensors to a second sensor data collector;

sending the signals from the first sensor data collector and the second data collector to a processor; and

evaluating the signals using the processor.

6. The method of claim 5 further comprising the steps of:

generating elastic waves in the test material by pulsing each sensor;

receiving the elastic waves, the received elastic waves altered by formations internal to the material; and

converting the received elastic waves to electrical signals representative of the structural health of the test material.

7. The method of claim 6 wherein the step of generating elastic waves in the test material comprises generating a wave in an aircraft skin.

8. The method of claim 5 further comprising:

comparing the signals from the first subset and the second subset in the processor; and

indicating a potential fault in the system if the first subset of signals and the second subset of signals differ by a predetermined threshold.

9. The method of claim 5 further comprising collecting data from the first subset in the first sensor data collector upon detection of a failure of the second sensor data collector.

30. The method of claim 5 further comprising the step of:

storing the signals from the first subset of the zone of sensors, the signals from the second subset of the zone of sensors, or the signals from both the first and second subsets of the zone of sensors in a memory.

10. A structural health management system comprising:

a plurality of sensors mounted on a structure, the plurality of sensors arranged in two or more zones;

a plurality of sensor data collectors comprising a first sensor data collector and a second sensor data collector, each sensor data collector coupled to sensors from at least two zones, wherein a first subset of sensors in a first zone is coupled to the first sensor data collector of the one or more sensor data collectors and a second subset of sensors in the first zone is coupled to the second sensor data collector of the one or more sensor data collectors; and

a processor coupled to each of the one or more sensor data collectors, the processor operable to receive data from each of the one or more sensor data collectors and perform a damage assessment.

11. The system of claim 10 wherein each of the plurality sensors is an ultrasonic transducer for use in ultrasonic testing.

12. The system of claim 10 wherein the structure is a section of an aircraft.

13. The system of claim 11 wherein the data associated with each of the sensors includes data collected in an ultrasonic test, and each of the sensors sends the data from the ultrasonic test via the sensor data collectors to the processor coupled to the sensor data collectors, the processor configured to analyze the data from the ultrasonic test to locate flaws in the structure.

14. The system of claim 13 wherein the processor is further operable to compare a first set of data from the first zone coupled to a first sensor data collector and the second set of data from the first zone coupled to the second sensor data collector and signal an error condition if the first set of data and the second set of data vary by a predetermined amount.

31. The system of claim 10 further comprising a memory coupled to processor, the memory configured to store the data from each of the sensor data collectors.

15. A structural health management system comprising:

a plurality of sensors mounted on a structure, the plurality of sensors arranged in two or more zones;

a first sensor data collector and a second sensor data collector, each coupled to sensors from at least two zones, wherein a first subset and a second subset of sensors in a first zone are coupled to the first sensor data collector and a first subset and a second subset of sensors in a second zone are coupled to the second sensor data collector; and

a processor coupled to the sensor data collector, the processor operable to receive data from the sensor data collector and perform a damage assessment.

16. The system of claim 15 wherein each of the plurality sensors is an ultrasonic transducer for use in ultrasonic testing.

17. The system of claim 15 wherein the structure is a section of an aircraft.

18. The system of claim 16 wherein the data associated with each of the plurality of sensors includes data collected in an ultrasonic test, and each of the plurality of sensors sends the data from the ultrasonic test via the sensor data collectors to the processor coupled to the sensor data collectors, the processor configured to analyze the data from the ultrasonic test to locate flaws in the structure.

32. The system of claim 15 further comprising a memory coupled to processor, the memory configured to store the data from the sensor data collector.

19. A structural health monitoring system comprising;

a plurality of sensors distributed as two or more zones of sensors mounted on a structure, the sensors configured to collect data;

a plurality of sensor data collectors, each coupled to a subset of the sensors from at least two of the two or more zones of sensors, the sensor data collectors configured to receive data from the subset of sensors to which it is coupled; and

a processor coupled to the sensor data collector, the processor configured to receive and evaluate data from the sensor data collector.

20. The system of claim 19 wherein the structural health monitoring system further comprises one or more sensors from a first zone of sensors coupled to a first sensor data collector and one or more sensors from a second zone of sensors coupled to the first sensor data collector.

21. The system of claim 19 wherein the structural health monitoring system further comprises a plurality of sensors of a first zone of sensors coupled to two or more sensor data collectors.

22. The system of claim 19 wherein the structural health monitoring system further comprises a first portion of sensors from a first zone of sensors coupled to a first sensor data collector and a second portion of sensors from the first zone of sensors coupled to a second sensor data collector.

23. The system of claim 22 wherein:

the first portion of sensors collects a first set of data regarding the structure;

the second portion of sensors collects a second set of data regarding the structure;

the first sensor data collector receives the first set of data from the first portion of sensors;

the second sensor data collector receives the second set of data from the second portion of sensors; and

the processor receives the first set of data and the second set of data, the processor analyzes the first and second data to determine if the first set of data and the second set of data match within a predetermined criteria, wherein a match verifies the integrity of the system.

24. The system of claim 19 wherein the structural health monitoring system further comprises a first portion of sensors from a first zone of sensors coupled to a first sensor data collector and a second portion from the first zone of sensors coupled to a second sensor data collector.

25. The system of claim 22 wherein the second sensor data collector sends data from the second portion of sensor from the first zone of sensors to a processor upon failure of the first sensor data collector.

26. The system of claim 19 wherein the sensors are ultrasonic transducers configured to perform ultrasonic tests upon the structure.

27. The system of claim 26 where in the structure is an aircraft skin.

28. The system of claim 19 wherein the structure is an aircraft skin.

29. The system of claim 28 wherein the sensors are ultrasonic transducers configured to produce lamb waves with in the aircraft skin and receive signals indicative of internal structures and flaws within the aircraft skin.

33. The system of claim 19 further comprising a memory coupled to processor, the memory configured to store the data from the sensor data collectors.