System and method for repairing a structural component

• US 9,457,553 B2
• Filed: 12/20/2012
• Issued: 10/04/2016
• Est. Priority Date: 12/22/2011
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Operations GmbH (Airbus SE)
• Inventors: Stehmeiner, Heiner, Bockenheimer, Clemens
• Primary Examiner(s): Orlando, Michael N
• Assistant Examiner(s): Rivera, Joshel
• Application Number:
  US13/721,935
• Publication Number:
  US 20130160923A1
• Time in Patent Office: 1,384 Days
• Field of Search: 156/64, 156/350, 156/351, 156/378, 156/379, 737/67, 737/69, 737/72, 737/99, 738/626.7, 738/626.8
• US Class Current: 1/1
• CPC Class Codes: B29C 73/10 using patches sealing on the surface of the article B29C73/14 takes precedence
• CPC Class Codes: B29C 73/24 Apparatus or accessories not otherwise provided for
• CPC Class Codes: B32B 41/00 Arrangements for controlling or monitoring lamination processes; Safety arrangements
• CPC Class Codes: B64F 5/40 Maintaining or repairing aircraft

Abstract

A system for repairing a structural component, in particular an aircraft structural component, includes a repair patch which is connected to the structural component in such a manner that it covers an opening in the structural component resulting from removing a damaged region of the structural component. A sensor is fastened to the repair patch in a region of the repair patch covering the opening in the structural component and is designed to detect strains and/or stresses occurring in the repair patch. An evaluating device is adapted to evaluate the strain values and/or stress values detected by the sensor and, in dependence on the result of this evaluation, output a signal which is characteristic of the quality state of the connection between the structural component and the repair patch.

Claims

1. System for repair of a structural component, in particular an aircraft structural component, having:

a repair patch which is connected to the structural component in such a manner that it covers an opening in the structural component resulting from removing a damaged region of the structural component,

a sensor which is fastened to the repair patch in a region of the repair patch covering the opening in the structural component and is configured to detect at least one of strains and stresses occurring in the repair patch,

a bridge element which is temporarily connectable to the structural component in such a manner that it spans a section of the structural component comprising the repair patch,

a sealing system which is configured to seal a space, defined by the bridge element and the section of the structural component spanned by the bridge element, against the outside atmosphere,

a negative pressure-generating device configured to generate, in the space sealed against the outside atmosphere by the sealing system, a pressure which is reduced relative to the ambient pressure, and

an evaluating device which is configured to evaluate at least one of the strain values and the stress values detected by the sensor and, in dependence on the result of this evaluation, output a signal which is characteristic of the quality state of the connection between the structural component and the repair patch to enable immediate checking of a quality of the repair patch,

wherein the bridge element comprises a base and a carrier supported by the base, the base keeping the carrier at a distance from a surface of the repair patch and the structural component to define said space sealed by the sealing system, and

wherein the negative pressure-generating device generates in the sealed space a reduced pressure acting on the repair patch, the reduced pressure corresponding to a differential pressure acting on the repair patch when the aircraft is flying at cruising altitude.

2. System according to claim 1,

wherein the sensor is fastened to the repair patch in the region of an inner surface of the repair patch.

3. System according to claim 1,

wherein the sensor is integrated into a measuring module, which further comprises at least one of:

a data store for storing the at least one of the strain values and the stress values detected by the sensor and

a transmitter for wireless transmission of signals.

4. System according to claim 3,

wherein the evaluating device is integrated into the measuring module and the transmitter is configured to transmit the signal, outputted by the evaluating device and characteristic of the quality state of the connection between the structural component and the repair patch, to a receiving device.

5. System according to claim 3,

wherein the evaluating device is integrated into a receiving device and the transmitter is configured to transmit the at least one of the strain values and the stress values, detected by the sensor, to the receiving device.

6. System according to claim 3,

wherein the evaluating device is integrated into a receiving device and the transmitter is configured to transmit at least one of the strain values and the stress values stored in the data store, to the receiving device.

7. System according to claim 1,

wherein the sealing system comprises a vacuum film covering the bridge element and connected to the structural component, and a sealing element for sealing the vacuum film against the structural component.

15. A method of use of a system according to claim 1 comprising outputting a warning signal when the signal indicates that the quality state represents the at least one of the strain values and the stress values lie by a predetermined difference amount below at least one of strain values and stress values determined immediately after the structural component has been repaired, thereby indicating a loss of strength of the connection between the structural component and the repair patch.

17. System according to claim 1, wherein the evaluating device is structured to compare the at least one of strains and stresses detected by the sensor with a threshold value which is characteristic of a desired quality state of the connection between the structural component and the repair patch, and, in dependence on the result of this evaluation comparison, output a signal which is characteristic of the quality state of the connection between the structural component and the repair patch.

18. System according to claim 1, wherein the sensor is integrated into a measuring module which is fastened in a region of the repair patch covering the opening in the structural component, so that the sensor bears against an inner surface of a region of the repair patch covering the opening in the structural component.

20. System according to claim 1, wherein the sensor is in direct contact with a surface of the repair patch.

21. System according to claim 1, wherein the repair patch is adhesively bonded to an outer surface of the structural component.

8. Method for repair of a structural component, in particular an aircraft structural component, having the steps:

connecting a repair patch to the structural component in such a manner that the repair patch covers an opening in the structural component resulting from removing a damaged region of the structural component,

fastening a sensor, which is configured to detect at least one of strains and stresses occurring in the repair patch, to a region of the repair patch covering the opening in the structural component,

temporarily connecting a bridge element to the structural component in such a manner that the bridge element spans a section of the structural component comprising the repair patch,

sealing a space, defined by the bridge element and the section of the structural component spanned by the bridge element, against the outside atmosphere,

generating, in the space sealed against the outside atmosphere by the sealing system, a pressure which is reduced relative to the ambient pressure,

evaluating at least one of the strain values and the stress values detected by the sensor by comparing the at least one of strains and stresses detected by the sensor with a threshold value which is characteristic of a desired quality state of the connection between the structural component and the repair patch to enable immediate checking of a quality of the repair patch, and

outputting a signal which is characteristic of the quality state of the connection between the structural component and the repair patch, in dependence on the result of said comparing operation,

wherein the bridge element comprises a base and a carrier supported by the base and connecting the bridge element, so that the base keeps the carrier at a distance from a surface of the repair patch and the structural component to define said space sealed by said sealing, and

wherein generating the pressure comprises generating in the sealed space a reduced pressure acting on the repair patch, so that the reduced pressure corresponds to a differential pressure acting on the repair patch when the aircraft is flying at cruising altitude.

9. Method according to claim 8,

wherein the sensor is fastened to the repair patch in the region of an inner surface of the repair patch.

10. Method according to claim 8,

wherein the method further comprises at least one of:

storing the at least one of the strain values and the stress values detected by the sensor in a data store which is integrated into a measuring module also comprising the sensor, and

wirelessly transmitting signals by means of a transmitter which is integrated into a measuring module also comprising the sensor.

11. Method according to claim 10,

wherein the at least one of the strain values and the stress values detected by the sensor are evaluated by means of an evaluating device integrated into the measuring module, and the transmitter transmits the signal, outputted by the evaluating device and characteristic of the quality state of the connection between the structural component and the repair patch, to a receiving device.

12. Method according to claim 10,

wherein the at least one of the strain values and the stress values detected by the sensor are evaluated by means of an evaluating device integrated into a receiving device, and the transmitter transmits the at least one of the strain values and the stress values, detected by the sensor, to the receiving device.

13. Method according to claim 10,

wherein the at least one of the strain values and the stress values detected by the sensor are evaluated by an evaluating device integrated in to a receiving device, and the transmitter transmits the at least one of the strain values and the stress values stored in the data store, to the receiving device.

14. Method according to claim 8,

wherein the space defined by the bridge element and the section of the structural component spanned by the bridge element is sealed against the outside atmosphere by means of a sealing system which comprises a vacuum film covering the bridge element and connected to the structural component, and a sealing element for sealing the vacuum film against the structural component.

16. The method of claim 8 further comprising outputting a warning signal when the signal indicates that the quality state represents the at least one of the strain values and the stress values lie by a predetermined difference amount below at least one of strain values and stress values determined immediately after the structural component has been repaired, thereby indicating a loss of strength of the connection between the structural component and the repair patch.

19. Method according to claim 8, wherein the evaluating operation comprises comparing the at least one of strains and stresses detected by the sensor with a threshold value which is characteristic of a desired quality state of the connection between the structural component and the repair patch, and outputting a signal which is characteristic of the quality state of the connection between the structural component and the repair patch, in dependence on the result of said comparing operation.

22. Method according to claim 8, wherein fastening the sensor comprises fastening the sensor in direct contact with a surface of the repair patch.

23. Method according to claim 8, wherein connecting the repair patch comprises adhesively bonding the repair patch to an outer surface of the structural component.