EP2409934B1 - Conteneur de fret aérien - Google Patents

Conteneur de fret aérien Download PDF

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Publication number
EP2409934B1
EP2409934B1 EP11154295.7A EP11154295A EP2409934B1 EP 2409934 B1 EP2409934 B1 EP 2409934B1 EP 11154295 A EP11154295 A EP 11154295A EP 2409934 B1 EP2409934 B1 EP 2409934B1
Authority
EP
European Patent Office
Prior art keywords
elements
freight container
connecting elements
wall
air freight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP11154295.7A
Other languages
German (de)
English (en)
Other versions
EP2409934A1 (fr
Inventor
Raphael Hartebrodt
Gerd Knözinger
Heidemarie Sonntag
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
KNOEZINGER, GERD
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to EP11154295.7A priority Critical patent/EP2409934B1/fr
Publication of EP2409934A1 publication Critical patent/EP2409934A1/fr
Application granted granted Critical
Publication of EP2409934B1 publication Critical patent/EP2409934B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D88/00—Large containers
    • B65D88/02—Large containers rigid
    • B65D88/12—Large containers rigid specially adapted for transport
    • B65D88/14—Large containers rigid specially adapted for transport by air
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D88/00—Large containers
    • B65D88/52—Large containers collapsible, i.e. with walls hinged together or detachably connected
    • B65D88/526—Large containers collapsible, i.e. with walls hinged together or detachably connected with detachable side walls
    • B65D88/528—Large containers collapsible, i.e. with walls hinged together or detachably connected with detachable side walls all side walls detached from each other to collapse the container
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00—Component parts, details or accessories for large containers
    • B65D90/02—Wall construction
    • B65D90/022—Laminated structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00—Component parts, details or accessories for large containers
    • B65D90/02—Wall construction
    • B65D90/08—Interconnections of wall parts; Sealing means therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D2313/00—Connecting or fastening means
    • B65D2313/02—Connecting or fastening means of hook-and-loop type

Definitions

  • Cargo containers and air freight containers of the type mentioned are well known from the prior art. These are usually formed from metallic materials, and embodiments are also known in which the metallic materials are replaced by plastics or plastic composites in order to increase the efficiency of the freight containers or to reduce their weight.
  • Air freight containers are usually formed of metallic materials and therefore - especially for the formation of sufficiently stable side walls - a high weight, which has a negative effect on fuel consumption and the possible payload.
  • known freight containers such as air freight containers have the disadvantage that they must be repaired very expensive in the event of damage to be put back into a ready state. Under certain circumstances, depending on the damage, it may even be necessary to transport the damaged freight containers / air freight containers in the unloaded state to a suitable support point where they can then be repaired. The empty transport required for this entails considerable cost disadvantages, since cargo space available in this case can not be used.
  • the AU12 650 66A discloses a freight container usable for sea, rail and road transport.
  • the freight container includes detachable connections for the walls of the container, comprising a protruding portion and a recessed portion and a type of plug receptacle.
  • the recessed portion includes means for securing a plate and a curved groove portion.
  • the male portion has means for fixing a plate and a curved tongue portion.
  • the curved tongue portion is counter-shaped to the curved groove portion and the curved tongue portion is adapted to rotate into a locking position into engagement with the curved groove portion.
  • the WO 02/02883 A1 discloses a container composed of many individual parts.
  • the plates are provided with profiles at the plate edges for coupling together, the profiles being provided with longitudinal structures intended to protect against transverse displacement in order to form a positive connection between two plates. Further, locking means are provided for locking or biasing the connection.
  • a collapsible transport container for goods having a bottom, a lid, side walls, a rear wall and a front wall comprising at least two doors.
  • the side walls, the rear wall, the front wall and the lid can be transferred from a use position to a collapsed position.
  • each hinge joints are provided which have a pivoting range of up to 270 °. Without releasing these joints, the rear wall, the lid, the side walls and the front wall should be placed in a position parallel to the ground and lying within its base surface and stacked one above the other.
  • the articulated connection is formed by two profiles arranged with a piping to each other, wherein the profiles have a U-shaped Aufsteckabêt for attachment to a wall element and the Aufsteckabrough opposite an open-edge receiving portion, wherein the piping for connecting two Profiles are used.
  • the respective piping are formed as soft parts or made of a flexible flexurally elastic plastic and further have end-side beads, which consist of a hard plastic and are inserted into the receiving portions of the profiles to be positively received therein.
  • the DE 42 185 89 A1 discloses a transport container which can be dismantled, in which locking and counter-locking elements are provided at the contour edges of the wall panels. The plates are put together.
  • a first profile strip has a circular cross-sectional area with a circular arc-shaped outer edge contour.
  • a second profile strip has a C-shaped cross-sectional area with a circular arc-shaped inner edge contour.
  • the DE 10 2006 006 511 A1 discloses a freight container, in particular an air cargo container, having a sandwiched bottom plate with a top layer laminate, an integrated frame with an enveloping composite top layer, and a supporting core material to reduce curb weight without reducing payload. Furthermore, the container comprises securing elements which are integrated in the wall elements.
  • the wall elements and the ceiling element or the wall elements and the bottom plate are fixedly or detachably connected to each other, wherein for a solid connection, a riveting or gluing is disclosed.
  • An air cargo container which has reinforced walls for protection against bomb explosions.
  • Whose walls have an at least two-layer structure, wherein a debris-catching layer and a pressure-discharging layer are provided. The individual walls are firmly connected.
  • the present invention seeks to provide an air cargo container of the type mentioned, which has a low weight and offers the possibility of easy repair.
  • the invention solves the problem by an air freight container with the features of claim 1.
  • Characteristic of the air cargo container according to the invention is the configuration of the connection of the wall elements with each other, with the base body and / or with the ceiling element such that they are detachably connected to each other.
  • the detachable connection according to which the wall elements, the ceiling element and the base body form individual modules which can be easily connected together to form an air freight container, makes it possible for the case that repair measures are required to perform this in a particularly simple manner.
  • the embodiment of the invention by the detachable connection allows easy repair at low cost by simply replacing the damaged modules. For this it is only necessary to separate the detachable connections, so that the damaged part can be replaced.
  • Air cargo container is no longer required for onward transport of air freight, but is needed at another location.
  • the detachable connection of the air cargo container according to the invention is designed such that in the mounted state interconnected wall elements, body and ceiling element allow a stable design of the air cargo container, which withstands all loads occurring during operation, but at the same time possibly allows easy disassembly, this at best the use of hand tools required is.
  • the modular design of the container also allows untrained personnel to dismantle it in the case of non-use on site without any significant technical effort and store it in a particularly space-saving manner.
  • the modular design also allows - with appropriate design of the individual modules - the formation of air cargo containers of different sizes, with several modules can be joined together according to the requirements resulting from the cargo to an individualized air cargo container.
  • the wall elements and the base body and / or the ceiling element for releasable connection form-fitting connectable connecting elements.
  • the use of form-fitting acting fasteners makes it possible to easily produce an air freight container with stable properties, at the same time the form-fitting acting fasteners possibly a simple and rapid disassembly or replacement of damaged modules allows without it complementary connecting body, such as screws, rivets, Brackets or the like required.
  • the wall elements and the base body and / or the ceiling element are connected to one another via connector elements designed as a connector, partially clipped together.
  • Such a design of the detachable connection makes it possible to mount the air freight container in a particularly simple manner, the connection by clipping or mating the individual modules in a special way a simple installation and Disassembly allows.
  • this usually has a closable loading opening on.
  • a closable loading opening is a fiber-reinforced plastic tarpaulin or the like, which, for example, can be connected via Velcro to the air freight container.
  • the loading opening can be closed by a hingedly connected to the air freight container cover, wherein the cover may be formed corresponding to the wall elements, for example.
  • connecting elements are arranged in the corner regions of the air freight container.
  • the use of such connecting elements, which may also be detachably connected to the wall elements, the ceiling element and / or the base itself, as well as the arrangement of the connecting elements in the corner of the air freight container increases its robustness in a complementary manner, in particular the exposed corner areas or connecting areas of the wall - And / or ceiling elements and the body are particularly well protected from each other damage.
  • the detachable connection is already sufficient for producing an air freight container which fulfills the required properties.
  • the air cargo container on a releasable connection arretierendes securing means.
  • the use of a securing agent which is preferred In addition to the detachable connection between the wall elements, the base body and / or the ceiling element extends, secures in a complementary manner existing between these components connection so that it can be ensured very reliable that the modules are fixed in position to each other.
  • the securing means are designed such that they can be solved in a particularly simple manner, so as to ensure a simple repair or disassembly and assembly of the air cargo container.
  • the securing elements which in principle can be configured in any desired manner, are formed by a position-secured securing pin, in particular ball locking pin, extending through the connecting elements.
  • a position-secured securing pin in particular ball locking pin
  • the use of such a security device is characterized by its low cost and high functionality.
  • the locking pin is ideally guided through aligned bores of the connected modules and is fixed in position, so that a disassembly of the interconnected modules requires a prior removal of the locking pin.
  • the use of a ball locking pin is characterized by its high position assurance in the mounted state, so that it is ensured in a particularly reliable manner that it can not come to an accidental removal of the securing means.
  • the design of the base body which serves in the mounted state of the air cargo container for receiving the goods to be transported, is basically freely selectable.
  • the base body is formed from a plastic.
  • the preparation of the base body made of plastic makes it particularly easy to train with sufficient strength and resistance, as well as inexpensive to manufacture.
  • plastic any type of plastic or composites made of plastic can be used, which meet the required uses.
  • Thermoplastic or thermosetting plastics can be used to produce the base body, which are used with suitable production processes for forming a body formed as a solid body.
  • reinforcing elements are embedded in the plastic used to form the body, which increase the strength of the body formed from a corresponding plastic and allow it due to the through the reinforcing elements achieved increase in strength with a lower material requirement to produce plastic.
  • the reinforcing elements are arbitrarily or completely or partially embedded in the plastic according to the expected load curves.
  • reinforcing elements are also freely selectable and depends primarily on the strength properties of the body to be achieved.
  • the use of wood fibers is conceivable, which are embedded in the plastic.
  • the reinforcing elements are formed by sheets, fibers, particles and / or hollow body.
  • Such reinforcing elements for example.
  • Carbon fibers or nanoparticles increase the strength properties of the body in a complementary manner and allow to reduce the total weight of the body in addition, so that the total weight of the formed with the body airfreight container can be reduced in a complementary manner.
  • the reinforcing elements can be directed or undirected embedded in the plastic, so that in a complementary manner an increase in the structural strength can be achieved, whereby a further reduction in weight can be achieved.
  • a simple embedding of the reinforcing elements in the plastic in the context of the manufacturing process makes it possible to produce the appropriately designed body particularly cost.
  • the shape of the body depends on the choice of material according to the expected load curves. In principle, although a design of the main body as a solid body is conceivable, however, a structure of the base body is preferably selected, in which this has between the base and a bottom cavities. According to a particularly advantageous embodiment of the invention, the hollow body and / or cavities are filled with foam on the base body, or are equipped with foams.
  • the resulting sandwich construction of the base body has a particularly high stability, wherein in the case of a foaming of the main body this can be made in its overall design in a complementary manner with a lower material requirement of plastic.
  • the sandwich construction is also characterized by the fact that in this way a particularly good insulation is achieved, so that sensitive to temperature influences transport goods protected against external influences, can be reliably transported with appropriately trained air cargo containers.
  • this is from the bottom to above - based on the position of use - starting with a high and / or high-strength steel sheet and then executed with wood or high pressure resistant rigid foam and can then optionally be carried out according to the above-described embodiment.
  • This embodiment of the invention makes it possible in a special way the required under the test requirements of NAS3610 loads of soil, with extreme point or line loads occur to meet.
  • the design of the base body is basically freely selectable, and in its simplest configuration it can also be formed in one piece.
  • the basic body is modular, namely formed of at least two modules.
  • the modular design of the body also makes it possible in the case of non-use on site to dismantle without any technical effort and store very space-saving.
  • the air cargo container according to the invention in particular air freight container according to this embodiment of the invention can be stored in the disassembled state in a particularly space-saving manner and / or transported.
  • the wall and / or ceiling elements are formed from at least one fiber-reinforced plastic, in particular a shear modulus of fiber-reinforced plastic, which forms a sandwich together with a foam or honeycomb core.
  • the outer layers of this sandwich structure are preferably formed of elastic material in order to minimize damage to the cargo during transport, for example.
  • transport such as the prongs of forklifts.
  • the use of selectively elastic tear-resistant material in the wall and / or ceiling elements can also serve to prevent the devastating effect on an airframe in the event of explosions within the container by the explosion pressure is reduced or deflected.
  • ceiling elements are advantageously framed by connecting elements arranged at the edge, which in turn are formed by fiber-reinforced or fiber-reinforced and / or ball-reinforced duroplastic or thermoplastic plastics.
  • the connecting elements form the supporting frame of the wall and / or ceiling elements in the form of thrust modules and, moreover, make it possible to carry the load-bearing, form-fitting connection Wall and / or ceiling elements for forming the air cargo container.
  • the connection of the wall and / or ceiling elements with the connecting elements can be done in any way, preferably a cohesive or adhesive connection is used.
  • the total weight of the air freight container can be reduced in a complementary manner compared to known air freight containers in an unrivaled manner, while maintaining or increasing the stability.
  • the wall and / or ceiling elements also have a high buckling rigidity.
  • This can basically be achieved in any way, preferably by forming the outer regions as a shear modulus.
  • a high buckling stiffness additionally increases the structural strength of the container. As a result, a particularly good shielding of the cargo arranged in the cargo container is achieved from external damage.
  • Fig. 1 is shown in a side view a freight container 1.
  • the freight container 1 has a built-up in sandwich construction base 4, which may be formed of plastic, structural foam, wood and / or sheet metal.
  • the base body 4 is adjoined by wall elements 5a-5c designed as shear modules, which form a circumferential ring in the mounted state.
  • the wall elements 5a-5c have peripheral connecting elements 2b-2c for the positive connection to the base body 4 and to each other at their edge regions.
  • the connecting elements 2b - 2e For connecting the in the position of use of the freight container 1 horizontally extending connecting elements 2b - 2e with each other or with the base body 4, the connecting elements 2b - 2e each have a cylinder-like projection 15 and a correspondingly formed recess 16, wherein the projection 15 in the mounted position within the recesses 16 is arranged.
  • This embodiment makes it possible to interlock the connecting elements 2b-2e, wherein the recess 16 surrounds the cylinder-like projection in a range of> 180 °, so that a reliable form-locking connection is formed.
  • the connecting elements 2b - 2e and the corresponding configuration of the base body 4 allow easy mounting and dismounting of the freight container 1, for example.
  • the connecting elements 2a of the ceiling elements 6a, 6b corresponding cylindrical projections 15 which are arranged in corresponding recesses 16 of the connecting elements 2b of the wall elements 5a, 5b in the mounted position.
  • the cylinder-like projections 15 are arranged in the mounted position in the recesses 16 that the Recesses 16 engage around the cylinder such that a positive structural connection is made (see. Fig. 2 ).
  • FIG. 4 is a sectional view of a designed as a shear wall module 5b with the arranged on the edge connecting elements 2a, 2e.
  • the wall element 5b has a sandwich construction and is peripherally connected in a flattened region with the connecting elements 2a, 2e in a material-locking manner.
  • a corner region of a freight container 1 with a first embodiment for securing the position of the connecting elements 2b of the wall elements 5a is shown on the connecting elements 2a of a ceiling element 6a, 6b, not shown here.
  • the wall elements 5a are positively connected to one another via their connecting elements 2b with the ceiling element 6a, 6b, not shown here, via the connecting elements 2b, the cylinder-like projections 15 engaging the connecting elements 2a, 2b in corresponding recesses 16 on the connecting elements 2a, 2b.
  • the projections 15 and the correspondingly formed receptacles 16 may have any cross-section, wherein in addition to a round or Elliptical cross-section and any other useful polygonal shape is conceivable.
  • the positive connection of the connecting elements 2a - 2g to each other can also take place in that both sides of a compound, the molded negative parts in the form of a hinge strip are mutually and with a retractable projection 15 which may be formed as described above, as explained above structurally connected. This connection can either be removed by pulling out of the projection 15 or by turning the projection 15, if this is formed appropriately meaningful.
  • the freight container 1 in the corner has a arranged inside the freight container 1 molded body 7.
  • This has two holes 11, which are arranged in the mounted position in each case in alignment with a through the connecting elements 2a, 2b extending bore 17.
  • a locking pin 8a extends.
  • a handle 9 of the locking pin 8a rests against the outside on the connecting element 2b, protrudes the free end of the molded body 7 out.
  • the securing pin 8a has a sleeve 18 embodied as a hollow body, within which a control pin 12a is arranged so as to be longitudinally displaceable.
  • a displacement of the control pin 12a which protrudes with its free end from the handle 9a, takes place against a spring force, which is applied by a helical compression spring 13 at the bottom of the sleeve 18. Due to the spring force, the locking elements 10a protrude through radial openings in the sleeve 18 to the outside, so that a withdrawal of the locking pin 8a from the holes 11, 17 is not possible.
  • FIG. 6 and 7 An alternative embodiment of an embodiment of a trained as a ball lock pin securing pin 8b is in the Fig. 6 and 7 shown.
  • the locking pin 8b shown in these figures differs from that in the Fig. 4 and 5 illustrated locking pin 8a characterized in that within the guide sleeve 8a of the control pin 12b in the backup position two balls 10b so determined in the sleeve that they protrude from the sleeve 1 * 8.
  • the unactuated state causes the helical compression spring 13 a bias of the control pin 12b in the direction of the handle 9b, so that the balls 10b protrude from the openings of the sleeve 18.
  • the longitudinally displaceably arranged in the sleeve 18 control pin 12 in the region of the balls 10b has a conical configuration.
  • the helical compression spring 13 biases the control pin 12b in the direction of the handle 9b, wherein the balls 10b are arranged in the upper portion of the conical portion in which they protrude from the sleeve 18.
  • a displacement of the control pin 12b in the direction of the helical compression spring 13 a sliding of the ball body 10b on the conical portion, whereby the balls 10b are displaced into the sleeve 18, so that a removal of the locking pin 8b is possible.
  • the locking pin 8b is secured against accidental operation.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pallets (AREA)
  • Connection Of Plates (AREA)

Claims (8)

  1. Conteneur de fret aérien comprenant un corps de base pour recevoir des articles à transporter, plusieurs éléments formant parois reliés au corps de base et un élément formant couvercle relié aux éléments formant parois, dans lequel la liaison des éléments formant parois (5a - 5c) entre eux, au corps de base (4) et/ou à l'élément formant couvercle (6a, 6b) est réalisée sous la forme d'une liaison amovible,
    caractérisé en ce que les éléments formant parois et le corps de base (4) et/ou l'élément formant couvercle (6a, 6b) présentent des éléments de liaison (2a - 2g) en une partie, pouvant être reliés par complémentarité de forme afin de créer une liaison structurelle amovible, et les éléments de liaison (2a - 2g) sont disposés dans les zones d'arête et dans les zones d'angle du conteneur de fret aérien (1), dans lequel les éléments de liaison (2a - 2e) présentent respectivement une partie faisant saillie (15) de type cylindre ou en forme de cylindre et un évidement (16) réalisé de manière correspondante, dans lequel la partie faisant saillie (15) est disposée dans la position montée à l'intérieur de l'évidement (16), dans lequel il est permis de clipser les uns dans les autres les éléments de liaison (2b - 2e) s'étendant de manière horizontale dans la position d'utilisation du conteneur, dans lequel l'évidement (16) entoure la partie faisant saillie (15) de type cylindre ou en forme de cylindre dans une zone supérieure à 180° de manière à former une liaison par complémentarité de forme fiable, et dans lequel les éléments de liaison (2f, 2g) s'étendant de manière verticale dans la position d'utilisation du conteneur présentent un angle de serrage de l'évidement (16) et de la partie faisant saillie (15) si grand qu'un assemblage par clipsage n'est plus possible et qu'un enfilement de la partie faisant saillie (15) dans l'évidement (16) est requis.
  2. Conteneur de fret aérien selon la revendication 1, caractérisé par un ou plusieurs moyens de blocage (8a - 8b) stoppant les éléments de liaison (2a - 2e) amovibles.
  3. Conteneur de fret aérien selon la revendication 2, caractérisé en ce que le moyen de blocage est formé par une cheville de blocage (8a) s'étendant à travers les éléments de liaison (2a - 2e), bloquée en position, en particulier par un boulon de verrouillage à billes (8b).
  4. Conteneur de fret aérien selon l'une quelconque des revendications précédentes, caractérisé en ce que le corps de base (4) est formé à partir d'une matière synthétique, en particulier à partir d'une matière synthétique présentant des éléments de renforcement intégrés.
  5. Conteneur de fret aérien selon la revendication 4, caractérisé en ce que les éléments de renforcement sont formés par des fibres, des particules et/ou par des corps creux.
  6. Conteneur de fret aérien selon l'une quelconque des revendications précédentes, caractérisé en ce que le corps de base (4) est formé à partir au moins de deux modules, dans lequel les modules sont reliés les uns aux autres en particulier de manière amovible, en particulier sont clipsés les uns aux autres.
  7. Conteneur de fret aérien selon l'une quelconque des revendications précédentes, caractérisé en ce que les éléments formant parois (5a - 5c) et/ou l'élément formant couvercle (6a, 6b) sont formés à partir d'une matière synthétique composite à base de fibres, d'une structure sandwich en mousse et/ou d'une structure à alvéolaire.
  8. Conteneur de fret aérien selon l'une quelconque des revendications précédentes,
    caractérisé en ce
    que les éléments formant parois et/ou les éléments formant couvercle (5a - 5c, 6a, 6b) sont réalisés sous la forme de modules de glissement composés d'une matière synthétique renforcée par des fibres, qui représentent conjointement avec une partie centrale en mousse ou alvéolaire une structure en sandwich, et sont encadrés par des éléments de liaison (2a - 2e) disposés côté bord, formés par des matières synthétiques thermodurcissables ou thermoplastiques renforcées par des fibres ou renforcées par des fibres et/ou des billes, et en ce que les éléments de liaison (2a - 2e) forment le cadre de support des éléments formant parois et/ou de l'élément formant couvercle (5a - 5c, 6a, 6b), dans lequel les éléments formant parois et/ou l'élément formant couvercle (5a - 5c, 6a, 6b) sont reliés par liaison de matière ou par une liaison par collage aux éléments de liaison (2a - 2e).
EP11154295.7A 2010-07-22 2011-02-14 Conteneur de fret aérien Not-in-force EP2409934B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP11154295.7A EP2409934B1 (fr) 2010-07-22 2011-02-14 Conteneur de fret aérien

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP10170469A EP2409933A1 (fr) 2010-07-22 2010-07-22 Support de marchandises de fret
EP11154295.7A EP2409934B1 (fr) 2010-07-22 2011-02-14 Conteneur de fret aérien

Publications (2)

Publication Number Publication Date
EP2409934A1 EP2409934A1 (fr) 2012-01-25
EP2409934B1 true EP2409934B1 (fr) 2017-03-29

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EP10170469A Withdrawn EP2409933A1 (fr) 2010-07-22 2010-07-22 Support de marchandises de fret
EP11154295.7A Not-in-force EP2409934B1 (fr) 2010-07-22 2011-02-14 Conteneur de fret aérien

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EP10170469A Withdrawn EP2409933A1 (fr) 2010-07-22 2010-07-22 Support de marchandises de fret

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