B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 11/00 (2006.01) B60R 5/00 (2006.01) B61D 37/00 (2006.01)
Patent
CA 2460590
The invention relates to an overhead luggage container (1), particularly for airlines, comprising a reinforcing structure (11) which is connected to the container (1) and which is disposed essentially in the direction of the longitudinal extension of the container (1), and at least one device (5) for suspension on a carrying structure (2) of the plane or like. In order to create a container (1) which can be subjected to relatively high static strain without running the risk that the container (1) will fall on the passengers sitting below, while at the same time reducing technical complexity in production and reducing the weight of said container, at least one respective rigid connecting element (17) is arranged to the side of the container (1) between the reinforcing structure (11) and the suspension device (5) in a substantially vertical manner with respect to the longitudinal extension of the container (1). The connecting element (17) is used to transmit forces exerted by the luggage on said container (1) and to deflect them to the suspension devices (5) and carrying structure (2) of the plane, thereby relieving the amount of strain placed on the side walls (12).
La présente invention concerne un compartiment (1) à bagages installé au-dessus de la hauteur de la tête, destiné notamment à des avions, comprenant une structure de rigidification (11) reliée au compartiment (1) qui est dirigée sensiblement dans la direction longitudinale du compartiment (1), et au moins un dispositif (5) de suspension à une structure porteuse (2) de l'avion ou analogue. L'invention a pour objet de concevoir un compartiment (1) de ce type qui peut supporter des charges statiques élevées sans que le compartiment (1) risque de s'effondrer sur les passagers ou analogue assis en-dessous, et de limiter les frais de réalisation et le poids du compartiment (1). A cet effet, entre la structure de rigidification (11) et le dispositif de suspension (5) est disposé le long du compartiment (1) au moins un élément de liaison rigide (17) respectif sensiblement verticalement par rapport à la direction longitudinale du compartiment (1). L'élément de liaison (17) sert à transmettre les forces exercées par les bagages sur le compartiment (1), aux dispositifs de suspension (5), et de cette manière à la structure porteuse (2) de l'avion, et permet ainsi de soulager les parois latérales (12).
Filsegger Hermann
Pamminger Erich
Stephan Walter A.
Facc Ag
Fischer Advanced Composite Components Ag
Macrae & Co.
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