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Title:
OPTICALLY CONNECTING EMBEDDED OPTICAL FIBERS IN COMPOSITE PANELS
Document Type and Number:
WIPO Patent Application WO2001051974
Kind Code:
A3
Abstract:
A method of and an apparatus for coupling a first optical transmission means (10, 42), such as an optical fibre, embedded within an aircraft composite (12, 40) to a second optical transmission means (14), such as an optical fibre, external to the composite (12, 40) is described. The method comprises locating the position of the first optical means (10, 42) embedded within the composite (12, 40) using X-ray scanning for example; forming a passageway (20, 62) by laser machining or drilling within the composite (12, 40) to the first optical transmission means (10, 42); and establishing an optical connection between the first and second optical transmission means (10, 42, 14) at the intersection of the passageway (20, 62) and the first optical transmission means (10, 42).

Inventors:
ALDRIDGE NIGEL BRUCE (GB)
PROUDLEY GEOFFREY MARTLAND (GB)
FOOTE PETER DAVID (GB)
READ IAN JAMES (GB)
Application Number:
PCT/GB2001/000038
Publication Date:
December 27, 2001
Filing Date:
January 05, 2001
Export Citation:
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Assignee:
BAE SYSTEMS PLC (GB)
ALDRIDGE NIGEL BRUCE (GB)
PROUDLEY GEOFFREY MARTLAND (GB)
FOOTE PETER DAVID (GB)
READ IAN JAMES (GB)
International Classes:
B23K26/00; B64D43/00; G02B6/00; G02B6/26; G02B6/28; G02B6/36; G02B6/38; G02B26/00; G02B26/08; G02B6/42; (IPC1-7): G02B6/36; B64C1/00
Foreign References:
GB2322479A1998-08-26
EP0822430A21998-02-04
US5408568A1995-04-18
US5555330A1996-09-10
Other References:
FRIEBELE E J ET AL: "OPTICAL FIBER SENSORS FOR SPACECRAFT APPLICATIONS", SMART MATERIALS AND STRUCTURES,IOP PUBLISHING LTD., BRISTOL,GB, vol. 8, no. 6, December 1999 (1999-12-01), pages 813 - 838, XP000883621, ISSN: 0964-1726
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