System for loading and unloading unit loads into a cargo...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 9/00 (2006.01) B64F 1/32 (2006.01) B65G 67/00 (2006.01) B65G 67/08 (2006.01)

Patent

CA 2484356

The invention relates to a system for loading and unloading a unit load (6), such as in particular items of luggage or similar, into a cargo hold (1) of an aircraft, comprising the transport of the unit load (6) to the inner end of the cargo hold (1) during loading and its transport away from said end during unloading and the transport of the unit load (6) between the apron area and the cargo hold opening. According to said system, the unit load (6) can be conveyed during loading in a transversal direction to the longitudinal axis of the aircraft and also conveyed into the aircraft fuselage in a longitudinal direction and stored in the cargo hold (1). During unloading, the unit load (6) that has been transported back to the plane of the cargo hold can be conveyed through and away from the cargo hold opening transversally to the longitudinal axis of the aircraft. The invention also relates to an intermediate transport device (2) for use with said system. The invention further relates to additional alternatives to the system and also to the intermediate transport device or transport unit.

L'invention concerne un système de chargement et de déchargement d'articles (6), tels que, en particulier, des bagages ou des éléments analogues, dans un espace de chargement (1) d'un avion. Les articles (6) sont transportés vers l'extrémité interne de l'espace de chargement (1) lors du chargement, et à partir de cette extrémité et dans l'autre sens lors du déchargement, ledit transport des articles (6) s'effectuant entre le plan de la piste et l'ouverture de l'espace de chargement. Selon l'invention, les articles (6) peuvent être transportés à des fins de chargement transversalement à l'axe longitudinal de l'avion ainsi que dans le sens longitudinal de l'avion dans le fuselage, et déposés dans l'espace de chargement (1). Lors du déchargement dans le plan de l'ouverture de l'espace de chargement, les articles (6) transportés dans le sens de déchargement peuvent être convoyés hors de l'espace de chargement et transversalement à l'axe longitudinal de l'avion à travers l'ouverture de l'espace de chargement. L'invention se rapporte également à un dispositif de transport intermédiaire (2) conçu pour ledit système. En outre, cette invention concerne des systèmes ainsi que des dispositifs de transport intermédiaires ou unités de transport se présentant sous d'autres formes.

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