Title:
RAPID ATTACHMENT FOR A MOVABLE FLAP MODULE OF A WING OF AN AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2023/057377
Kind Code:
A9
Abstract:
The present invention relates to a method for manufacturing a connection part (10) between a wing box (20) and a leading edge module (30). The method comprises the steps of carrying out a three-dimensional digitization of a first part representative of the wing box (40) in order to obtain a first digital model (50), and of carrying out a three-dimensional digitization of a second part representative of the leading edge module (60) in order to obtain a second digital model (70). The first part comprises a first reference region (80) and a first connection region (90), and the second part comprises a second reference region (100) and a second connection region (110). A relative position (120) of the first reference region with respect to the second reference region is defined. On the basis of the first and second digital model, the connection part (10) is designed to provide a connection between the first and the second connection region such that the first and the second reference region are situated at the relative position. The connection part is then manufactured. The invention also relates to an assembly comprising a first wing of a first aircraft and a second wing of a second aircraft.
Inventors:
DE PLAEN DIDIER (BE)
ASCENZO VALERIO (BE)
GUEUNING DIMITRI (BE)
ASCENZO VALERIO (BE)
GUEUNING DIMITRI (BE)
Application Number:
PCT/EP2022/077450
Publication Date:
May 10, 2024
Filing Date:
October 03, 2022
Export Citation:
Assignee:
SONACA (BE)
International Classes:
B64C9/02; B64C9/24; B64F5/10
Attorney, Agent or Firm:
BREVALEX (Paris cedex 8, FR)
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