Title:
AIRCRAFT STABILISER TRAILING EDGE
Document Type and Number:
WIPO Patent Application WO/2010/070185
Kind Code:
A3
Abstract:
The invention relates to the trailing edge (3) of an aircraft stabiliser (1) which is made from a composite material and includes an outer skin (40) and an inner skin (41) which are joined to the trailing edge (3) by means of clip-type coupling element (20). The invention is characterised in that the ends of the clip-type coupling element (20) include recesses (23) intended to be coupled to the inner area of the upper and lower skins (40, 41) of the stabiliser (1), said clip-type coupling element being sufficiently flexible for it to be clipped in such a way that the ends are housed by means of the aforementioned recesses (23) between the outer and inner skins (40, 41) of the aircraft stabiliser (1), so that the outer area on the trailing edge (3) of the stabiliser (1) is formed by a continuous aerodynamic surface without any changes in slope.
Inventors:
BALSA GONZALEZ ALBERTO (ES)
BURGOS GALLEGO FRANCISCO DE PAULA (ES)
BURGOS GALLEGO FRANCISCO DE PAULA (ES)
Application Number:
PCT/ES2009/070609
Publication Date:
August 12, 2010
Filing Date:
December 18, 2009
Export Citation:
Assignee:
AIRBUS OPERATIONS SL (ES)
BALSA GONZALEZ ALBERTO (ES)
BURGOS GALLEGO FRANCISCO DE PAULA (ES)
BALSA GONZALEZ ALBERTO (ES)
BURGOS GALLEGO FRANCISCO DE PAULA (ES)
International Classes:
B64C3/28; B64C9/00
Foreign References:
| US20040000613A1 | 2004-01-01 | |||
| DE1214092B | 1966-04-07 |
Attorney, Agent or Firm:
ELZABURU, Alberto de (C/ Miguel Angel 21, Madrid, ES)
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