CONTAINER FOR AERIAL DELIVERY OF GOODS

A container for dropping from an aerial vehicle comprises a bottom section and a plurality of side walls. Wings are connected to the upper edges of the side walls to allow pivoting of the wing between a passive position, in which the wing extends along the corresponding side wall, and a deployed pos...

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Bibliographic Details
Main Authors ROSEILLER, Alexis Laurent Sebastien, KOPERBERG, Barry Willem Ferdinand, VAN DORST, Henricus Alphonsius Cornells
Format Patent
LanguageEnglish
French
Published 28.03.2019
Subjects
ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR
AIRCRAFT
AMMUNITION
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS,e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES,DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS
CONVEYING
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
FLYING SUITS
HANDLING THIN OR FILAMENTARY MATERIAL
HEATING
LIGHTING
MECHANICAL ENGINEERING
PACKAGES
PACKAGING ELEMENTS
PACKING
PARACHUTES
PERFORMING OPERATIONS
STORING
TRANSPORTING
WEAPONS
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Summary:A container for dropping from an aerial vehicle comprises a bottom section and a plurality of side walls. Wings are connected to the upper edges of the side walls to allow pivoting of the wing between a passive position, in which the wing extends along the corresponding side wall, and a deployed position, in which the wing extends substantially transversely relative to the corresponding side wall. Reinforcing units increase the bending stiffness of the wings. Retaining units limit pivoting of the wings beyond the deployed position. L'invention concerne un contenant permettant de faire tomber des objets depuis un véhicule aérien et comprenant une section inférieure et une pluralité de parois latérales. Des ailes sont reliées aux bords supérieurs des parois latérales pour permettre le pivotement de l'aile entre une position passive dans laquelle l'aile s'étend le long de la paroi latérale correspondante et une position déployée dans laquelle l'aile s'étend de manière sensiblement transversale par rapport à la paroi latérale correspondante. Des unités de renforcement augmentent la rigidité à la flexion des ailes. Des unités de retenue limitent le pivotement des ailes au-delà de la position déployée.
Bibliography:Application Number: WO2018NL50635