CA2490059A1 - Methods and systems for inspecting aircraft fuselage frames - Google Patents

Methods and systems for inspecting aircraft fuselage frames Download PDF

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Publication number
CA2490059A1
CA2490059A1 CA002490059A CA2490059A CA2490059A1 CA 2490059 A1 CA2490059 A1 CA 2490059A1 CA 002490059 A CA002490059 A CA 002490059A CA 2490059 A CA2490059 A CA 2490059A CA 2490059 A1 CA2490059 A1 CA 2490059A1
Authority
CA
Canada
Prior art keywords
accordance
inspection system
proximity sensor
collision avoidance
detector
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002490059A
Other languages
French (fr)
Other versions
CA2490059C (en
Inventor
Michael Robert Hopple
Elizabeth Lockenberg Dixon
Kenneth Gordon Herd
Gregory Alan Mohr
Clifford Bueno
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Company
Michael Robert Hopple
Elizabeth Lockenberg Dixon
Kenneth Gordon Herd
Gregory Alan Mohr
Clifford Bueno
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Company, Michael Robert Hopple, Elizabeth Lockenberg Dixon, Kenneth Gordon Herd, Gregory Alan Mohr, Clifford Bueno filed Critical General Electric Company
Publication of CA2490059A1 publication Critical patent/CA2490059A1/en
Application granted granted Critical
Publication of CA2490059C publication Critical patent/CA2490059C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N23/00Investigating or analysing materials by the use of wave or particle radiation, e.g. X-rays or neutrons, not covered by groups G01N3/00 – G01N17/00, G01N21/00 or G01N22/00
    • G01N23/02Investigating or analysing materials by the use of wave or particle radiation, e.g. X-rays or neutrons, not covered by groups G01N3/00 – G01N17/00, G01N21/00 or G01N22/00 by transmitting the radiation through the material
    • G01N23/04Investigating or analysing materials by the use of wave or particle radiation, e.g. X-rays or neutrons, not covered by groups G01N3/00 – G01N17/00, G01N21/00 or G01N22/00 by transmitting the radiation through the material and forming images of the material

Abstract

A method for inspecting an aircraft fuselage (10) using an inspection system (12) including a moveable detector (14), wherein the method includes coupling a collision avoidance system (20) to the inspection system detector, monitoring the collision avoidance system during operation of the inspection system, and controlling operation of the inspection system with the collision avoidance system.

Claims (16)

1. A method for inspecting an aircraft fuselage (10) using an inspection system (12) including a moveable detector (14), said method comprising:
coupling a collision avoidance system (20) to the inspection system detector;
monitoring the collision avoidance system during operation of the inspection system;
and controlling operation of the inspection system with the collision avoidance system.
2. A method in accordance with Claim 1 wherein coupling a collision avoidance system (20) comprises coupling at least one proximity sensor (22) to the inspection system detector (14).
3. A method in accordance with Claim 2 wherein coupling a collision avoidance system (20) comprises coupling the at least one proximity sensor (22) to the inspection system detector (14) such that the collision avoidance system receives signals from the proximity sensor during operation of the inspection system.
4. A method in accordance with Claim 2 wherein coupling at least one proximity sensor (22) to the inspection system (12) further comprises coupling at least one proximity sensor to the inspection system that is configured to generate an imminent collision signal.
5. A method in accordance with Claim 2 wherein controlling operation of the inspection system (12) comprises controlling operation of the inspection system based on input received by the at least one proximity sensor (22) during operation of the inspection system.
6. A method in accordance with Claim 1 wherein coupling a collision avoidance system (20) comprises coupling at least one protection device (24) to the inspection system (12) to facilitate preventing contact between the inspection system and the aircraft fuselage (10).
7. A method in accordance with Claim 1 wherein coupling a collision avoidance system (20) comprises coupling at least one of an air-filled bladder sensor and an accelerometer to the inspection system detector (14).
8. An apparatus for inspecting an aircraft fuselage (10) comprising:
a moveable detector (14); and a collision avoidance system (20) in electrical communication with said moveable detector to control said moveable detector for inspecting the aircraft fuselage.
9. An apparatus in accordance with Claim 8 wherein said apparatus further comprises at least one proximity sensor (22) electrically coupled to said moveable detector (14).
10. An apparatus in accordance with Claim 9 wherein said at least one proximity sensor (22) is electrically coupled to said collision avoidance system (20) such that said collision avoidance system receives a signal from said at least one proximity sensor (22) during operation of said moveable detector (14).
11. An apparatus in accordance with Claim 9 wherein said at least one proximity sensor (22) comprises at least one of an infrared sensor, an air-filled bladder sensor, and an accelerometer.
12. An apparatus in accordance with Claim 9 wherein said at least one proximity sensor (22) generates an imminent collision signal and transmits said signal to said collision avoidance system (20).
13. An apparatus in accordance with Claim 9 wherein said moveable detector (14) is controlled based on input received by said at least one proximity sensor (22) during the inspection of the airplane fuselage (10).
14. An apparatus in accordance with Claim 9 further comprising a stopping mechanism (28) coupled to said moveable detector (14) and configured to receive an imminent collision signals from said at least one proximity sensor (22) to facilitate preventing contact between said moveable detector and the aircraft fuselage (10) frame.
15. An apparatus in accordance with Claim 8 further comprising at least one protection device (24) electrically coupled to said moveable detector (14) to facilitate preventing contact between said moveable detector and the aircraft fuselage (10).
16. An apparatus in accordance with Claim 15 wherein said protection device (24) comprises at least one of air-filled bladder, a balloon, and an airbag system.
CA2490059A 2002-06-28 2003-06-26 Methods and systems for inspecting aircraft fuselage frames Expired - Fee Related CA2490059C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/064,291 US6662088B1 (en) 2002-06-28 2002-06-28 Methods and systems for inspecting aircraft fuselage frames
US10/064,291 2002-06-28
PCT/US2003/020953 WO2004003530A1 (en) 2002-06-28 2003-06-26 Methods and systems for inspecting aircraft fuselage frames

Publications (2)

Publication Number Publication Date
CA2490059A1 true CA2490059A1 (en) 2004-01-08
CA2490059C CA2490059C (en) 2010-12-07

Family

ID=29709240

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2490059A Expired - Fee Related CA2490059C (en) 2002-06-28 2003-06-26 Methods and systems for inspecting aircraft fuselage frames

Country Status (8)

Country Link
US (1) US6662088B1 (en)
EP (1) EP1520167B1 (en)
JP (1) JP4520850B2 (en)
AU (1) AU2003253788A1 (en)
BR (1) BR0312401A (en)
CA (1) CA2490059C (en)
SG (1) SG173935A1 (en)
WO (1) WO2004003530A1 (en)

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Also Published As

Publication number Publication date
SG173935A1 (en) 2011-09-29
US20040002797A1 (en) 2004-01-01
JP4520850B2 (en) 2010-08-11
EP1520167A1 (en) 2005-04-06
EP1520167B1 (en) 2013-09-11
JP2005531773A (en) 2005-10-20
CA2490059C (en) 2010-12-07
WO2004003530A1 (en) 2004-01-08
BR0312401A (en) 2007-06-19
AU2003253788A1 (en) 2004-01-19
US6662088B1 (en) 2003-12-09

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EEER Examination request
MKLA Lapsed

Effective date: 20170627