Fastening system for fastening a cabin fitting element to a...

H - Electricity – 01 – R

Patent

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H01R 13/631 (2006.01)

Patent

CA 2644159

The invention relates to a fastening system for fastening a cabin fitting element (1) with at least one electrical installation on a support structure (2) of an aircraft. During installation into the support structure (2), the cabin fitting element (1) is fixed in succession by at least one loose bearing (13) in at least one degree of translational freedom and then by at least one fixed bearing (3) in the at least one further degree of translational freedom. In order to ensure an improved installation and dismantling of cabin covering panels with electrical installation and to reduce the weight due to the components and also the installation space which is required, according to the invention a contact device with a bush arrangement (17, 21) and a plug arrangement (18, 23) is integrated in the at least one loose bearing (13) and/or the at least one fixed bearing (3), by which an electrical connection is produced between the support structure (2) and the electrical installation of the cabin fitting element (2) on fixing at least of one degree of translational freedom.

L'invention concerne un système de fixation servant à fixer un élément d'attache (1) de cabine avec au moins une installation électrique sur une structure de support (2) d'un aéronef. Pendant l'installation dans la structure de support (2), l'élément d'attache (1) de cabine est fixé en succession par au moins un support (13) lâche dans au moins un degré de liberté de translation puis par au moins un support (3) fixe dans au moins un autre degré de liberté de translation. Afin d'assurer une installation et un démontage améliorés des panneaux de couverture de cabine avec une installation électrique et de réduire le poids impliqué par les composants ainsi que l'espace d'installation nécessaire, un dispositif de contact avec un montage en douille (17, 21) et un montage en cheville (18, 23) est intégré selon l'invention dans ledit ou lesdits supports lâches (13) et/ou dans ledit ou lesdits supports fixes (3), ce qui permet de produire une connexion électrique entre la structure de support (2) et l'installation électrique de l'élément d'attache (2) de cabine par fixation d'au moins un degré de liberté de translation.

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