Latch for joining two panels of an airplane structure

E - Fixed Constructions – 05 – C

Patent

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Details

E05C 19/14 (2006.01)

Patent

CA 2531120

The invention relates to a latch (1) provided for joining two elements to one another via, on the one hand, a hook (2) capable of coming into contact with a retaining element (18) integrally connected to the first element and, on the other, via a main pin (3) to be attached in a fixed manner to the second element. Said latch has a handle (6) that is mounted so that it can pivot about an end pin (13) and has an articulation having a pair of compression links (4) mounted in a manner that enables them to pivot about the main pin (3) and about an intermediate pin (14). The invention is characterized in that the hook is inserted between the handle and the main pin, and in that at least one compression link (4) is provided with a guiding means (21) capable of coming into contact with the surface of the hook facing the handle during the opening of the latch.

La présente invention se rapporte à un verrou (1) prévu pour relier deux éléments l'un à l'autre par l'intermédiaire, d'une part, d'un crochet (2) apte à venir en prise avec un organe de retenue (18) solidaire du premier élément, et d'autre part, d'un axe principal (3) destiné à être rattaché fixement au second élément, ledit verrou comprenant une poignée (6) montée pivotante autour d'un axe d'extrémité (13), et une articulation comprenant une paire de bielles (4) de compression montées pivotantes autour de l'axe principal (3) et d'un axe intermédiaire (14), caractérisé en ce que le crochet est intercalé entre la poignée et l'axe principal, et en ce qu'au moins une bielle (4) de compression est pourvue d'un moyen de guidage (21) apte à venir au contact de la surface du crochet située face à la poignée durant l'ouverture du verrou.

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