CA2490059A1 - Methods and systems for inspecting aircraft fuselage frames - Google Patents
Methods and systems for inspecting aircraft fuselage frames Download PDFInfo
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N23/00—Investigating 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
- G01N23/02—Investigating 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
- G01N23/04—Investigating 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.
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.
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.
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) |
Families Citing this family (9)
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US7467070B2 (en) * | 2004-10-26 | 2008-12-16 | Meyer Eric S | Methods and systems for modeling stress intensity solutions for integrally stiffened panels |
JP4704735B2 (en) * | 2004-11-04 | 2011-06-22 | 株式会社島津製作所 | X-ray fluoroscope |
DE102005007094B4 (en) * | 2005-02-16 | 2007-03-29 | Siemens Ag | Digital flat detector for the detection of X-rays |
US7266174B2 (en) * | 2005-03-07 | 2007-09-04 | General Electric Company | Radiographic inspection of airframes and other large objects |
US20080061940A1 (en) * | 2006-08-03 | 2008-03-13 | Kimberly-Clark Worldwide, Inc. | Smart antenna system for reading data tags |
CN102119023B (en) * | 2008-07-03 | 2014-04-09 | 弗吉尼亚大学专利基金会 | Unit dosage of apadenoson |
US8886388B2 (en) * | 2009-06-29 | 2014-11-11 | The Boeing Company | Embedded damage detection system for composite materials of an aircraft |
US8693613B2 (en) * | 2010-01-14 | 2014-04-08 | General Electric Company | Nuclear fuel pellet inspection |
US8983172B2 (en) * | 2012-12-28 | 2015-03-17 | Modern Technology Solutions, Inc. | Visual inspection apparatus, secure one-way data transfer device and methods therefor |
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-
2002
- 2002-06-28 US US10/064,291 patent/US6662088B1/en not_active Expired - Lifetime
-
2003
- 2003-06-26 SG SG2010012854A patent/SG173935A1/en unknown
- 2003-06-26 EP EP03762327.9A patent/EP1520167B1/en not_active Expired - Fee Related
- 2003-06-26 JP JP2004518231A patent/JP4520850B2/en not_active Expired - Fee Related
- 2003-06-26 WO PCT/US2003/020953 patent/WO2004003530A1/en active Search and Examination
- 2003-06-26 AU AU2003253788A patent/AU2003253788A1/en not_active Abandoned
- 2003-06-26 BR BRPI0312401-0A patent/BR0312401A/en not_active Application Discontinuation
- 2003-06-26 CA CA2490059A patent/CA2490059C/en not_active Expired - Fee Related
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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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20170627 |