IP Library › Granted Patent US 12,392,736
Granted Patent B2
US 12,392,736 · App. 18/177,003 · Granted Aug 19, 2025

Method and system for inspecting and measuring installed one-sided fasteners in a structure

Inventor: Nicholas C. Reasoner (Seattle, WA)
Assignee: The Boeing Company
G01N23/046G01N2223/1016G01N2223/631G01N2223/646
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,392,736
App. No.
18/177,003
Granted
Aug 19, 2025
Kind
B2
Abstract

There is provided a method for inspecting and measuring one or more installed one-sided fasteners in a structure. The method includes positioning an X-ray imaging system at a first side of the structure at a location of the one or more installed one-sided fasteners. The method further includes emitting X-rays at the first side of the structure, detecting backscatter from the one or more installed one-sided fasteners, and generating image data from the X-ray imaging system in response to detecting the backscatter. The method further includes measuring and analyzing the image data, with an image processing system, to obtain one or more measurements of one or more dimensions of the one or more installed one-sided fasteners. The method further includes using the image data to inspect the one or more installed one-sided fasteners, and to detect any inconsistencies in the one or more measurements of the one or more dimensions.

Claims (46)

1. A method for inspecting and measuring one or more installed one-sided fasteners in a structure, the method comprising the steps of:

positioning an X-ray imaging system directed at a first side of the structure at a location of the one or more installed one-sided fasteners installed through one or more openings in the structure, the one or more installed one-sided fasteners each having a fastener body protruding from a second side of the structure;

emitting X-rays at the first side of the structure at the location of the one or more installed one-sided fasteners;

detecting backscatter from the one or more installed one-sided fasteners;

generating image data from the X-ray imaging system, in real time, in response to detecting the backscatter, the image data comprising one or more images of the fastener body of the one or more installed one-sided fasteners;

measuring and analyzing the image data, with an image processing system, to obtain one or more measurements of one or more dimensions of the one or more installed one-sided fasteners, the one or more measurements comprising one or more of:

a diameter of a fastener bulb of the one or more installed one-sided fasteners, wherein the fastener bulb is formed against an interior side of the structure when the fastener is installed in the structure;

a length of a pin protrusion of the one or more installed one-sided fasteners; and

a grip length of the one or more installed one-sided fasteners; and

using the image data to inspect the one or more installed one-sided fasteners, and to detect any out-of-specification parameters of the one or more measurements of the one or more dimensions of the one or more installed one-sided fasteners.

2. The method of claim 1 , wherein the step of positioning the X-ray imaging system further comprises, positioning the X-ray imaging system facing the first side of the structure comprising one of, a workpiece, a coupon, an aircraft structure, an aircraft part, a spacecraft structure, a rotorcraft structure, a watercraft structure, an automobile structure, a train structure, or an architectural structure.

3. The method of claim 1 , wherein the step of positioning the X-ray imaging system further comprises, positioning the X-ray imaging system comprising a backscatter X-ray imaging system.

4. The method of claim 1 , wherein the step of positioning the X-ray imaging system further comprises, positioning the X-ray imaging system at an end of a robot arm of a robotic system.

5. The method of claim 1 , wherein the step of positioning the X-ray imaging system further comprises, positioning the X-ray imaging system on a movable base of a mobile system.

6. The method of claim 1 , wherein the step of positioning the X-ray imaging system further comprises, positioning an X-ray device of the X-ray imaging system in a parallel position parallel to, and directly opposite, the one or more installed one-sided fasteners.

7. The method of claim 1 , wherein the step of positioning the X-ray imaging system further comprises, positioning an X-ray device of the X-ray imaging system at an angled position directed at the one or more installed one-sided fasteners.

8. The method of claim 1 , wherein the step of measuring and analyzing the image data with the image processing system further comprises, measuring and analyzing the image data with the image processing system comprising one of, an image processing software, or an artificial intelligence neural network.

9. The method of claim 1 , wherein the step of measuring and analyzing the image data further comprises, measuring and analyzing the image data to obtain the diameter of the fastener bulb to detect any out-of-specification diameter, and to detect when the fastener bulb is not properly formed.

10. The method of claim 1 , wherein the step of using the image data to inspect the one or more installed one-sided fasteners further comprises, using the image data to provide a confined space entry work reduction, by allowing for a nondestructive inspection of the one or more installed one-sided fasteners.

11. A method for inspecting and measuring one or more installed one-sided fasteners in an aircraft structure, the method comprising the steps of:

positioning an X-ray imaging system directed at a first side of the aircraft structure at a location of the one or more installed one-sided fasteners installed through one or more openings in the aircraft structure, the one or more installed one-sided fasteners each having a fastener body protruding from a second side of the aircraft structure;

emitting X-rays at the first side of the aircraft structure at the location of the one or more installed one-sided fasteners;

detecting backscatter from the one or more installed one-sided fasteners;

generating image data from the X-ray imaging system, in real time, in response to detecting the backscatter, the image data comprising one or more images of the fastener body of the one or more installed one-sided fasteners;

measuring and analyzing the image data, with an image processing system, to obtain one or more measurements of one or more dimensions of the one or more installed one-sided fasteners, wherein the one or more measurements comprise one or more of:

a diameter of a fastener bulb of the one or more installed one-sided fasteners, wherein the fastener bulb is formed against an interior side of the aircraft structure when the fastener is installed in the aircraft structure;

a length of a pin protrusion of the one or more installed one-sided fasteners; and

a grip length of the one or more installed one-sided fasteners; and

using the image data to inspect the one or more installed one-sided fasteners, and to detect any out-of-specification parameters of the one or more measurements of the one or more dimensions of the one or more installed one-sided fasteners.

12. The method of claim 11 , wherein the step of positioning the X-ray imaging system further comprises, positioning an X-ray device of the X-ray imaging system in a parallel position parallel to, and directly opposite, the one or more installed one-sided fasteners, to measure the diameter of the fastener bulb of the one or more installed one-sided fasteners.

13. The method of claim 11 , wherein the step of positioning the X-ray imaging system further comprises, positioning an X-ray device of the X-ray imaging system at an angled position directed at the one or more installed one-sided fasteners, to measure one or more of, the length of the pin protrusion of the one or more installed one-sided fasteners, and the grip length of the one or more installed one-sided fasteners.

14. The method of claim 11 , wherein the step of using the image data to inspect the one or more installed one-sided fasteners further comprises, using the image data to provide a confined space entry work reduction, by allowing for a nondestructive inspection of the one or more installed one-sided fasteners.

15. A system for inspecting and measuring one or more installed one-sided fasteners in a structure, the system comprising:

the structure having a first side and a second side;

the one or more installed one-sided fasteners installed through one or more openings in the structure, the one or more installed one-sided fasteners each having a fastener body protruding from the second side of the structure;

an X-ray imaging system configured to emit X-rays at the first side of the structure at a location of the one or more installed one-sided fasteners, and configured to detect backscatter from the one or more installed one-sided fasteners;

image data generated from the X-ray imaging system in response to detecting the backscatter, the image data comprising one or more images of the fastener body of the one or more installed one-sided fasteners; and

an image processing system to measure and analyze the image data, to obtain one or more measurements of one or more dimensions of the one or more installed one-sided fasteners, to inspect the one or more installed one-sided fasteners, and to detect any out-of-specification parameters of the one or more measurements of the one or more dimensions of the one or more installed one-sided fasteners, the one or more measurements comprising one or more of:

a diameter of a fastener bulb of the one or more installed one-sided fasteners, wherein the fastener bulb is formed against an interior side of the structure when the fastener is installed in the structure;

a length of a pin protrusion of the one or more installed one-sided fasteners; and

a grip length of the one or more installed one-sided fasteners.

16. The system of claim 15 , wherein the structure comprises one of, a workpiece, a coupon, an aircraft structure, an aircraft part, a spacecraft structure, a rotorcraft structure, a watercraft structure, an automobile structure, a train structure, or an architectural structure.

17. The system of claim 15 , wherein the X-ray imaging system is attached at an end of a robot arm of a robotic system.

18. The system of claim 15 , wherein the X-ray imaging system is attached to a movable base of a mobile system.

19. The system of claim 15 , wherein the image processing system comprises one of, an image processing software, or an artificial intelligence neural network.

20. The system of claim 15 , wherein one of the out-of-specification parameters comprises an out-of-specification diameter of the fastener bulb, when the fastener bulb is not properly formed.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 1, 2023
From: REASONER, NICHOLAS C.
To: THE BOEING COMPANY
Reel/Frame 062847/0365 →
Continuity (1)
Related Publication 20240295508A1 · Sep 5, 2024
References Cited (17)
US 8033724B2 · Edwards et al. · 2011 [cited by applicant]
US 8542876B1 · Engel et al. · 2013 [cited by applicant]
US 8879688B2 · Safai · 2014 [cited by applicant]
US 8923481B2 · Schubert et al. · 2014 [cited by applicant]
US 9123450B2 · Liesenfelt et al. · 2015 [cited by applicant]
US 9689813B2 · Lou et al. · 2017 [cited by applicant]
US 10162317B2 · Toh · 2018 [cited by applicant]
US 10859719B2 · Safai · 2020 [cited by applicant]
US 20130101090A1 · Schubert et al. · 2013 [cited by applicant]
US 20130202090A1 · Belcher · 2013 [cited by examiner]
US 20160252468A1 · Lou et al. · 2016 [cited by applicant]
US 20200200713A1 · Hafenrichter et al. · 2020 [cited by applicant]
US 20210063323A1 · Nakatani et al. · 2021 [cited by applicant]
US 20210396842A1 · Li et al. · 2021 [cited by applicant]
US 20220214290A1 · Maeder · 2022 [cited by examiner]
WO 2021130063A1 · 2021 [cited by applicant]
Extended European Search Report (EESR), European Patent Office, May 22, 2024, for Application No. EP24150280.6, Applicant the Boeing Company, 8 pages. [cited by applicant]