Method to monitor structural damage occurrence and progression in monolithic composite structures using fibre bragg grating sensors

Details for Australian Patent Application No. 2005244556 (hide)

Owner Airbus Operations, S.L.

Inventors Gordo, Alfredo Guemes; Martin, Jose Manuel Menendez

Agent Spruson & Ferguson

Pub. Number AU-B-2005244556

Priority 04107032.7 28.12.04 EP

Filing date 15 December 2005

Wipo publication date 13 July 2006

Acceptance publication date 26 May 2011

International Classifications

G01L 1/24 (2006.01) Measuring force or stress, in general - by measuring variations of optical properties of material when it is stressed, e.g. by photoelastic stress analysis

G01N 21/88 (2006.01) Investigating or analysing materials by the use of optical means, i.e. using infra-red, visible, or ultra-violet light - Investigating the presence of flaws, defects or contamination

Event Publications

12 January 2006 Complete Application Filed

  Priority application(s): 04107032.7 28.12.04 EP

13 July 2006 Application Open to Public Inspection

  Published as AU-B-2005244556

28 April 2011 Alteration of Name

  The name of the applicant has been altered to Airbus Operations, S.L.

26 May 2011 Application Accepted

  Published as AU-B-2005244556

22 September 2011 Standard Patent Sealed

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