IP Library Granted Patent US 11,022,571
Granted Patent B2
US 11,022,571 · App. 16/426,070 · Granted Jun 1, 2021

X-ray scattering method and system for non-destructively inspecting bond line and porosity

Inventor: Morteza Safai (Newcastle, WA)
Assignee: The Boeing Company
G01N23/201G01N2223/054G01N2223/6462
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Quick Facts
Patent No.
US 11,022,571
App. No.
16/426,070
Granted
Jun 1, 2021
Kind
B2
Abstract

Non-destructive inspection methods, systems, and apparatuses are disclosed for non-destructively inspecting a bond line, including a bond line present in a composite substrate and in a adhesive material layers in a composite substrate, with the methods, systems, and apparatuses incorporating a small angle X-ray scattering array.

Claims (54)

1. A method comprising:

positioning a small angle X-ray scattering system proximate to a composite substrate, said composite substrate comprising an adhesive material layer interposed between a composite substrate first side and a composite substrate second side, said adhesive material layer further comprising a bond line region, with said small angle X-ray scattering system comprising first side small angle X-ray scattering system components positioned on the composite substrate first side, said first side small angle X-ray scattering system components comprising:

an X-ray source;

a first pinhole aperture and a second pinhole aperture positioned a predetermined distance from the X-ray source;

a first vacuum chamber positioned proximate to the first pinhole aperture and the composite substrate first side; and

with said small angle X-ray scattering system comprising second side small angle X-ray scattering system components positioned on the composite substrate second side, said second side small angle X-ray scattering system components comprising:

a second vacuum chamber positioned proximate to the composite substrate second side, said second vacuum chamber in communication with an X-ray scintillator;

a charged coupled device in communication with the X-ray scintillator, said X-ray scintillator comprising a scintillating layer;

activating the small angle X-ray scattering system to emit an X-ray beam from the X-ray source;

directing the X-ray beam from the X-ray source through the composite substrate first side and into the interposed adhesive material layer;

directing the X-ray beam from the interposed adhesive material layer through the composite substrate second side to the X-ray scintillator, said X-ray scintillator located proximate to the composite substrate second side;

detecting scattered X-rays on the scintillating layer;

generating imaging signals based on the scattered X-rays impacting the scintillating layer; and

assessing porosity of the bond line region of the adhesive material layer.

2. The method of claim 1 , further comprising:

sending the imaging signals of the scattered X-rays generated on the scintillating layer to imaging software;

generating a bond line image at a nano-scale level; and

displaying the bond line image on a display.

3. The method of claim 2 , wherein the bond line image is a two-dimensional image.

4. The method of claim 2 , further comprising:

non-destructively detecting anomalies present in the bond line.

5. A method for non-destructively inspecting a bond line region of an adhesive material layer of a composite substrate comprising:

positioning a small angle X-ray scattering apparatus proximate to a composite substrate, said composite substrate comprising an adhesive material layer, said adhesive material layer comprising a bond line region;

directing X-rays from the small angle X-ray scattering apparatus to the composite substrate;

detecting scattered X-rays on an X-ray scintillator;

generating imaging signals of the scattered X-rays detected on the X-ray scintillator; and

generating an image from the imaging signals; and

non-destructively inspecting the bond line region.

6. A system for non-destructively inspecting a composite substrate, said composite substrate comprising a composite substrate first side, a composite substrate second side, and at least one adhesive material layer, said adhesive material layer interposed between the composite substrate first side and the composite substrate second side, said system comprising:

first side small angle X-ray scattering system components positioned on the composite substrate first side, said first side small angle X-ray scattering system components comprising:

a monochromatic X-ray source;

a first pinhole aperture and a second pinhole aperture positioned a predetermined distance from the monochromatic X-ray source;

a first vacuum chamber positioned between the first pinhole aperture and the second pinhole aperture; and

second side small angle X-ray scattering system components positioned on the composite substrate second side, said second side small angle X-ray scattering system components comprising:

a second vacuum chamber positioned proximate to the composite substrate second side, said second vacuum chamber in communication with an X-ray scintillator;

a charged coupled device in communication with the X-ray scintillator, said scintillator comprising a scintillating layer;

imaging software in communication with the charged coupled device;

a display in communication with the imaging software; and

wherein the system is configured to display a microscopic two-dimensional image of the adhesive material layer.

7. The system of claim 6 , wherein the composite substrate comprises a bond line and the system is configured to detect nano-scale anomalies in the bond line.

8. The system of claim 6 , wherein the adhesive material layer comprises a bond line and the system is configured to detect nano-scale anomalies in the bond line.

9. The system of claim 6 , wherein the adhesive material layer comprises a bond line region and the system is configured to detect nano-scale anomalies in the bond line region.

10. The system of claim 6 , wherein at least a portion of the composite substrate comprises a composite material and the system is configured to detect nano-scale anomalies in the composite material.

11. The system of claim 6 , wherein the adhesive material layer comprises a cured adhesive material layer and the system is configured to detect nano-scale anomalies in a bond line of the cured adhesive material layer.

12. The system of claim 6 , wherein the adhesive material layer comprises an epoxy-based adhesive and the system is configured to detect nano-scale anomalies in a bond line of the epoxy-based adhesive material layer.

13. The system of claim 6 , wherein the adhesive material layer comprises at least one of: an epoxy-based adhesive; a bismaleimide-based adhesive; a cyanate ester-based adhesive; an acrylate-based adhesive; a methacrylate-based adhesive; a polyurethane-based adhesive; a silicone-based adhesive; or combinations thereof; and the system is configured to detect nano-scale anomalies in a bond line of the adhesive material layer.

14. The system of claim 6 , wherein the system is configured to detect nano-scale anomalies in a bond line of an epoxy-based adhesive material layer.

15. The system of claim 6 , wherein the system is configured to detect nano-scale anomalies in a bond line of the adhesive material layer.

16. The system of claim 6 , wherein a stationary object comprises the composite substrate, and the system is configured to detect nano-scale anomalies in a bond line in the stationary object.

17. The system of claim 16 , wherein the stationary object is a pipe, and the system is configured to detect nano-scale anomalies in a bond line in the pipe.

18. The system of claim 6 , wherein a primary structure of a vehicle comprises the composite substrate, and the system is configured to detect nano-scale anomalies in a bond line in the primary structure of the vehicle.

19. The system of claim 18 , wherein the vehicle is selected from the group consisting of:

a manned spacecraft; an unmanned spacecraft; a manned aircraft; an unmanned aircraft; a manned hovercraft; an unmanned hovercraft, a manned rotorcraft; an unmanned rotorcraft; a manned terrestrial vehicle; an unmanned terrestrial vehicle; a manned surface watercraft; an unmanned surface watercraft; a sub-surface watercraft; an unmanned sub-surface watercraft, a manned satellite; an unmanned satellite, and combinations thereof, and the system is configured to detect nano-scale anomalies in a bond line in the vehicle.

20. The system of claim 6 , wherein the composite substrate comprises a primary structure of an aircraft, and the system is configured to detect nano-scale anomalies in a bond line in the primary structure of the aircraft.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 30, 2019
From: SAFAI, MORTEZA
To: THE BOEING COMPANY
Reel/Frame 049316/0001 →
Continuity (1)
Related Publication 20200378905A1 · Dec 3, 2020