A method for the manufacture of a component by composite fibre construction

Details for Australian Patent Application No. 2003200918 (hide)

Owner Airbus Deutschland GmbH

Inventors Leeraar, Tim; Filsinger, Jurgen; Staub, Martin; Gessler, Andreas

Agent Watermark

Pub. Number AU-B-2003200918

Priority 102 10 517.0-116 09.03.02 DE

Filing date 7 March 2003

Wipo publication date 25 September 2003

Acceptance publication date 13 September 2007

International Classifications

B64C 1/00 (2006.01) Aircraft structures or fairings

B29C 39/10 (2006.01) Particular shaping techniques, e.g. moulding, joining - incorporating preformed parts or layers, e.g. casting around inserts or for coating articles

B29C 70/34 (2006.01) Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts

B29C 70/48 (2006.01) Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts

B29D 31/00 (2006.01)

B64C 9/02 (2006.01) Adjustable control surfaces or members, e.g. rudders

B29K 105/08 (2006.01)

B29L 31/30 (2006.01)

Event Publications

20 March 2003 Complete Application Filed

  Priority application(s): 102 10 517.0-116 09.03.02 DE

25 September 2003 Application Open to Public Inspection

  Published as AU-B-2003200918

13 September 2007 Application Accepted

  Published as AU-B-2003200918

17 January 2008 Standard Patent Sealed

16 June 2011 Alteration of Name

  The name of the patentee has been altered to Airbus Operations GmbH Amendments 2004

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