Real Time Aircraft Stress Monitoring System

• US 20180099761A1
• Filed: 10/10/2016
• Published: 04/12/2018
• Est. Priority Date: 10/10/2016
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Griffiths, Robert C., Voth, Mitchell D.
• Application Number:
  US15/289,477
• Publication Number:
  US 20180099761A1
• Time in Patent Office: Days
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: B64D 47/08 Arrangements of cameras
• CPC Class Codes: B64F 5/60 Testing or inspecting aircraft components or systems
• CPC Class Codes: G01B 21/32 for measuring the deformation in a solid
• CPC Class Codes: G01C 11/12 the pictures being supported in the same relative position as when they were taken
• CPC Class Codes: G01M 5/0016 of aircraft wings or blades
• CPC Class Codes: G01M 5/0041 by determining deflection or stress
• CPC Class Codes: G01M 5/0091 by using electromagnetic excitation or detection
• CPC Class Codes: G06T 2207/10032 Satellite or aerial image; Remote sensing
• CPC Class Codes: G06T 2207/30252 Vehicle exterior; Vicinity of vehicle
• CPC Class Codes: G06T 7/246 using feature-based methods, e.g. the tracking of corners or segments
• CPC Class Codes: G06T 7/292 Multi-camera tracking
• CPC Class Codes: H04N 7/181 for receiving images from a plurality of remote sources

Abstract

A method and apparatus for an aircraft monitoring system. The aircraft monitoring system comprises targets associated with the wing of the aircraft, a camera system and a monitor. The camera system is configured to generate images of the targets on the wing during operation of the aircraft. The monitor is configured to measure movement of the targets using images, enabling identifying wing movement.

Claims

1. An aircraft monitoring system comprising:

targets associated with a wing of an aircraft;

a camera system configured to generate images of the targets on the wing during operation of the aircraft; and

a monitor configured to measure a movement of the targets using the images, enabling identifying wing movement.

2. The aircraft monitoring system of claim 1, wherein the monitor measures the movement of the targets at a location on the wing using the images.

3. The aircraft monitoring system of claim 2, wherein the monitor is configured to identify stress in the wing at the location in real time using vibrations detected in dynamic movement of an aircraft structure.

4. The aircraft monitoring system of claim 3, wherein the monitor is configured to identify maintenance for the aircraft based on the stress in the wing at the location.

5. The aircraft monitoring system of claim 1, wherein in measuring the movement of the targets using the images, the monitor compensates for additional movement from the camera system.

6. The aircraft monitoring system of claim 1 further comprising:

an optical window in a body of the aircraft, wherein the camera system is positioned to generate the images from inside the aircraft with a view through the optical window.

7. The aircraft monitoring system of claim 1, wherein the camera system is selected from at least one of a photogrammetry camera system or a stereo photogrammetry system.

8. The aircraft monitoring system of claim 1, wherein the camera system comprises:

a fixture system; and

a plurality of cameras associated with the fixture system in which orientations for the plurality of cameras are set independently.

9. The aircraft monitoring system of claim 1, wherein the targets are elliptical targets, and wherein the elliptical targets in the images are circular based on an angle of the camera system to the elliptical targets.

10. The aircraft monitoring system of claim 1, wherein the targets are selected to be visible to the camera system in sunlight.

11. The aircraft monitoring system of claim 1, wherein the wing movement is selected from at least one of bending, deflection or a twisting.

12. The aircraft monitoring system of claim 1, wherein operation of the aircraft is selected from one of taxiing, cruising, ascending, descending, taking off, or landing.

13. A real-time aircraft stress monitoring system comprising:

elliptical targets associated with a wing of an aircraft;

a camera system configured to generate images of the elliptical targets on the wing during operation of the aircraft, wherein the elliptical targets in the images are circular based on an angle of the camera system to the elliptical targets; and

a monitor that measures a movement of the elliptical targets using the images and identifies stress in the wing based on the movement of the elliptical targets.

14. The real-time aircraft stress monitoring system of claim 13, wherein the monitor generates an alert for maintenance using the stress identified in the wing.

15. A method for monitoring movement of an aircraft structure, the method comprising:

generating images of targets on the aircraft structure using a camera system associated with an interior of an aircraft during operation of the aircraft; and

measuring movement of the targets using the images, enabling identifying the movement of the aircraft structure.

16. The method of claim 15, wherein measuring the movement of the targets using the images comprises:

measuring the movement of the targets at a location on a wing using the images.

17. The method of claim 16 further comprising:

identifying a stress in the wing at the location in real-time.

18. The method of claim 17, wherein a monitor is configured to identify maintenance for the aircraft based on the stress in the wing at the location.

19. The method of claim 15, wherein in measuring the movement of the targets using the images, a monitor compensates for additional movement from the camera system.

20. The method of claim 15, wherein an optical window is present in a body of the aircraft and wherein the camera system is positioned to generate the images from inside of the aircraft with a view through the optical window.

21. The method of claim 15, wherein the camera system is selected from at least one of a photogrammetry camera system or a stereo photogrammetry system.

22. The method of claim 15, wherein the targets are elliptical targets, and wherein the elliptical targets in the images are circular based on an angle of the camera system to the elliptical targets.

23. The method of claim 15, wherein the movement of the aircraft structure is selected from at least one of a bending, deflection, or twisting.

24. The method of claim 15, wherein the operation of the aircraft is selected from one of taxiing, cruising, ascending, descending, taking off, and landing.