Title:
FASTENING ARRANGEMENT AND FASTENING FITTING FOR FASTENING A COMPONENT TO A STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT
Document Type and Number:
WIPO Patent Application WO/2012/080217
Kind Code:
A3
Abstract:
The present invention relates to a fastening arrangement (1) for fastening a component, in particular a cabin component, to a structural component (12) of an aircraft or spacecraft, comprising a structural component (12) which comprises a connection surface (13- 7); a fastening fitting (2) which has a geometry matched to the geometrical shape of the structural component (12), has a connection portion (3-7) associated with the connection surface (13-17) of the structural component (12) and is produced from a thermoplastic injection-moulding material; and an elastomeric adhesive joint (25) for stable fastening of the connection portion (3-7) of the fastening fitting (2) to the associated connection surface (13-17) of the structural component (12). A corresponding fastening fitting (2) and an aircraft or spacecraft comprising a fastening arrangement (1) of this type and/or a fastening fitting (2) of this type are also claimed.
Inventors:
KLAUKIEN FRANK-MICHAEL (DE)
Application Number:
PCT/EP2011/072556
Publication Date:
January 17, 2013
Filing Date:
December 13, 2011
Export Citation:
Assignee:
AIRBUS OPERATIONS GMBH (DE)
KLAUKIEN FRANK-MICHAEL (DE)
KLAUKIEN FRANK-MICHAEL (DE)
International Classes:
F16B11/00; B64C1/40
Foreign References:
| US20050284995A1 | 2005-12-29 | |||
| US4828202A | 1989-05-09 | |||
| US20070262219A1 | 2007-11-15 | |||
| US5822918A | 1998-10-20 | |||
| US4576664A | 1986-03-18 | |||
| US20050151038A1 | 2005-07-14 |
Attorney, Agent or Firm:
PECKMANN, Ralf (Friedrichstrasse 31, München, DE)
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