IP Library Patent Application 18195816
Patent Application
App. No. 18/195,816

OPTICAL MEASUREMENT DEVICE FOR INSPECTION OF DISCONTINUITIES IN AEROSTRUCTURES

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Patent No.
US None
App. No.
18/195,816
Abstract

A handheld device for making 3D topography measurements of surface discontinuities in high performance structures, such as aerostructures (e.g., aluminum fuselages). Lights illuminate the discontinuity from multiple angles, and a camera captures images of the discontinuity. A thickness sensor generates thickness data regarding a thickness of the base material and the top protective coating. A position sensor generates position data regarding a location of the discontinuity on the structure. A processor generates geometry data regarding a geometry of the discontinuity based on the images, performs an analysis of the geometry, thickness, and position data, and communicates a result of the analysis on a display. A conforming membrane and/or a gel and an opaque lubricant may be applied over and conform to the discontinuity in order to make more uniform a reflectivity difference and a color difference between the discontinuity and an adjacent portion of the structure.

Claims (36)

1 - 20 . (canceled)

21 . A device for calculating a surface discontinuity of a structure, said structure having an outer surface and a thickness, said surface discontinuity extending from said outer surface into said thickness of said structure or above said outer surface, the device comprising:

a plurality of spaced-apart light sources for illuminating said surface discontinuity, each of said plurality of light sources providing illumination toward said surface from a different angle;

a digital camera for capturing a plurality of images of said surface discontinuity illuminated by the plurality of light sources; and

a processing component for receiving said captured images from said digital camera and calculating geometry data of said surface discontinuity using said captured images.

22 . The device of claim 21 , wherein said geometry data includes a true size of said surface discontinuity.

23 . The device of claim 22 , wherein said true size of said surface discontinuity includes at least one of a true height, depth, or volume measured from said outer surface of said structure.

24 . The device of claim 23 , wherein said true height is a calculated height of said surface discontinuity above said outer surface, said true depth is a calculated depth of said surface discontinuity from said outer surface into said thickness, and said true volume is a calculated volume of said discontinuity above or below said outer surface.

25 . The device of claim 23 , wherein said processor subtracts said calculated true depth of said surface discontinuity from said thickness of said structure to determine a criticality of said surface discontinuity.

26 . The device of claim 21 , wherein said processor generates a 3D point cloud of said surface discontinuity based upon said captured images, said 3D point cloud being used to calculate said true size of said surface discontinuity.

27 . The device of claim 21 further comprising a display operatively connected to said processing component for receiving and displaying said geometry data.

28 . The device of claim 21 further comprising a position sensor for determining a location of said surface discontinuity on said outer surface, said position sensor operatively connected to said processing component.

29 . The device of claim 28 , wherein said position sensor is a wireless 3D positional tracker for determining said location based on signals received from local transmitters.

30 . The device of claim 21 , wherein said captured images used to calculate said geometry data includes images captured through a coating applied to said outer surface.

31 . A device for calculating a surface discontinuity of a structure, said structure having an outer surface and a thickness, said surface discontinuity extending from said outer surface into said thickness of said structure or above said outer surface, the device comprising:

a plurality of spaced-apart light sources for illuminating said surface discontinuity, each of said plurality of light sources providing illumination toward said surface from a different angle;

a digital camera for capturing a plurality of images of said surface discontinuity illuminated by the plurality of light sources;

a processing component for receiving said captured images from said digital camera and calculating a true size of said surface discontinuity using said captured images; and

a display operatively connected to said processing component for receiving and displaying said calculated true size of said surface discontinuity.

32 . The device of claim 31 , wherein said calculated true size includes at least one of:

a true height that is a calculated height of said surface discontinuity above said outer surface, a true depth is a calculated depth of said surface discontinuity from said outer surface into said thickness, and a true volume is a calculated volume of said discontinuity above or below said outer surface.

33 . The device of claim 32 , wherein said processor subtracts said calculated true depth of said surface discontinuity from said thickness of said structure to determine a criticality of said surface discontinuity.

34 . The device of claim 31 , wherein said processor generates a 3D point cloud of said surface discontinuity based upon said captured images, said 3D point cloud being used to calculate said true size of said surface discontinuity.

35 . A method for calculating a surface discontinuity of a structure, said structure having an outer surface and a thickness, said surface discontinuity extending from said outer surface into said thickness of said structure or above said outer surface, the method comprising:

providing a plurality of spaced-apart light sources;

illuminating said surface discontinuity from different angles from said plurality of spaced-apart light sources;

providing a digital camera;

capturing a plurality of images of said surface discontinuity using said digital camera, said surface discontinuity being illuminated by at least one of said plurality of light sources;

transferring said plurality of captured images to a processing component;

calculating geometry data of said surface discontinuity calculated from said captured images, wherein said geometry data includes a true size of said surface discontinuity; and

displaying said calculated data on a display.

36 . The method of claim 35 , wherein said true size of said surface discontinuity is a true height, a true depth, or a true volume calculated from said outer surface of said structure.

37 . The method of claim 36 , wherein said true height is a calculated height of said surface discontinuity between said outer surface and a distance said surface discontinuity extends above said outer surface, said true depth is a calculated depth of said surface discontinuity between said outer surface and a distance said surface discontinuity extends into said thickness, and said true volume is a calculated volume of said discontinuity above or below said outer surface.

38 . The method of claim 35 , wherein said processor subtracts said true depth of said surface discontinuity from said thickness of said structure to determine a criticality of said surface discontinuity.

39 . The method of claim 38 , wherein said criticality is determined by said processing component by comparing true size of said surface discontinuity to a pre-determined maximum size of said surface discontinuity.

40 . The method of claim 38 , wherein said determination of said criticality of said surface discontinuity includes utilizes machine learning.

Assignments (7)
RELEASE OF SECURITY INTEREST Recorded Dec 10, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073888/0692 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073916/0346 →
SECURITY AGREEMENT Recorded Jul 8, 2024
From: SPIRIT AEROSYSTEMS, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 068217/0456 →
SECURITY INTEREST Recorded Nov 22, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 065650/0761 →
SECURITY AGREEMENT (SECOND LIEN NOTES) Recorded Nov 21, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 065659/0585 →
SECURITY AGREEMENT (TERM LOAN B) Recorded Nov 21, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 065658/0232 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 10, 2023
From: HAYNES, MARK DAVIS
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 063606/0254 →