Carrying or guiding device for aircraft components

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 9/02 (2006.01) B64C 9/16 (2006.01) F16S 3/00 (2006.01)

Patent

CA 2462517

The invention relates to a carrying or guiding device (1) for aircraft components, especially for a landing flap which is arranged on an aircraft wing. The inventive device comprises a carrier (2) having an essentially U- shaped profile and essentially parallel lateral walls (3, 4). In order to produce one such device in such a way that it weighs as little as possible, has the required mechanical properties, and is as easy to produce and to assemble as possible, the carrier (2), and preferably one covering plate (20) arranged on the open side of the carrier (2), are produced from fibre reinforced plastic, especially carbon fibre reinforced plastic (CFRP). The connection between the carrier (2) and the covering plate (20) and possible connection elements (21) is preferably carried out by means of glued joints and, if necessary, additional riveted joints or screwed joints.

L'invention concerne un dispositif de support ou de guidage (1) destiné à des composants d'avion, notamment aux volets d'atterrissage situés sur une aile portante d'avion. Ce dispositif comprend un support (2) pourvu d'un profilé sensiblement en U et de parois latérales (3, 4) sensiblement parallèles. L'invention vise à créer un tel dispositif qui soit le plus léger possible, qui ait les propriétés mécaniques requises et soit le plus facile possible à produire et à monter. A cet effet, le support (2) et, de préférence, une plaque de recouvrement (20) placée sur le côté ouvert du support (2) sont réalisés en plastique renforcé par des fibres, notamment dans un plastique renforcé par des fibres de carbone (CF). Le support (2) est raccordé à la plaque de recouvrement (20) et à d'éventuels éléments de liaison (21), de préférence, par des joints collés et éventuellement des assemblages rivés ou vissés supplémentaires.

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