CN207346451U

CN207346451U - Aircraft transportation container

Info

Publication number: CN207346451U
Application number: CN201720632566.5U
Authority: CN
Inventors: 王洪义; 李东江; 廖志生
Original assignee: Jiangsu Shenzhou Ruida Ship Technology Co Ltd
Current assignee: Jiangsu Shenzhou Ruida Ship Technology Co Ltd
Priority date: 2017-06-02
Filing date: 2017-06-02
Publication date: 2018-05-11
Anticipated expiration: 2027-06-02

Abstract

The aircraft transportation container of the utility model, integrated box lower part have the inverted trapezoidal structure being adapted with aircraft polycrystalline substance shape；Babinet front end is provided with the hinged split door of hinge, and door upper and lower ends are provided with latch；Mutually split one on the door the wherein latch of Yishanmen be Fixed latches, the latch of another Yishanmen is can be with the linkage of handle linkage；Wallboards of box body material is plastics, and beautiful, light and handy plastic container is made up of self-drilling connection inside panel, exterior panel by aluminum alloy framework, has enough support strengths, while light quality, cheap, and it is convenient to manufacture；Babinet has split door, can load bulkload, useful load is big；Aircraft polycrystalline substance shape can adapt to by inverted trapezoidal bottom, energy utilization rate is high.

Description

Aircraft transportation container

Technical field

It the utility model is related to a kind of aircraft transportation container.

Background technology

Aviation container is generally manufactured using metal material or wood materials, and volume is big and heavy, and useful load is small, is wasted The energy, cost of transportation are high；The container manufactured using composite material, manufacture are of high cost；Aircraft hold is also needed according to aircraft configuration Respective cross-section shape is set, there is the irregular shapes such as rescinded angle, fillet, thus air container is also needed according to aircraft hold shape Corresponding rescinded angle, rounded structure are set, to increase aircraft hold charging ratio, improve energy utilization rate.

The content of the invention

Technical problem to be solved in the utility model is to provide a kind of light-weight, and intensity is high, and useful load is big, Neng Goushi Aircraft hold shape is answered, saves the aircraft transportation container of the energy.

The aircraft transportation container of the utility model, including integrated box, it is characterised in that：Lower box has with flying The inverted trapezoidal structure that motor spindle planform is adapted；Babinet front end is provided with the hinged split door of hinge, door upper and lower two End is provided with latch；Split one wherein the latch of Yishanmen be Fixed latches on the door mutually, and the latch of another Yishanmen is can With the linkage of handle linkage；

The handle drives three linkages at the same time；

The wallboards of box body includes inside panel, exterior panel, and inside panel, outer wall plate material are plastics, inside panel, exterior panel it Between be provided with aluminum alloy framework, aluminum alloy framework rectangular cross-section, aluminum alloy framework is by self-drilling connection in inside panel, outer Between siding；

The door edge is provided with sealing strip, the rubber strip of sealing strip rectangular cross-section tubulose；

The aluminum alloy framework is by being welded to connect integral frame, inside panel, the plastic wall that exterior panel is rotation molding Plate.

The aircraft transportation container of the utility model, is fixedly connected with exterior panel, inside panel forms one by aluminum alloy framework Body formula babinet, is combined into beautiful, light and handy plastic container, has enough support strengths, while light quality, price are low Honest and clean, it is convenient to manufacture；Babinet has split door, can load bulkload, useful load is big；Pass through inverted trapezoidal bottom energy Aircraft polycrystalline substance shape is enough adapted to, energy utilization rate is high.

Brief description of the drawings

Fig. 1 is the aircraft transportation container dimensional structure diagram of the utility model embodiment；

Fig. 2 is the aircraft transportation container door floor map of the utility model embodiment；

Fig. 3 is the aircraft transportation container wall panel structure floor map of the utility model embodiment；

Fig. 4 is the aircraft transportation container gasket structure floor map of the utility model embodiment.

Embodiment

As shown in the figure, a kind of aircraft transportation container, including integrated box 1,1 lower part of babinet has ties with aircraft bottom The inverted trapezoidal structure 2 that configuration shape is adapted, can be adapted by inverted trapezoidal structure 2 with the planform of aircraft hold bottom, To increase aircraft cargo charging ratio, stability of the container in aircraft hold is improved；1 front end of babinet is provided with hinge hinge Split door 3 is connect, split door 3 is capable of providing wider cargo and loads passage, facilitates cargo to pass in and out container, while meet body The space requirement of the larger cargo disengaging container of product；3 upper and lower ends of door are provided with latch, and closing door can be fixed by latch 3, prevent door 3 loosens in aircraft flight from influencing flight safety；The latch of split one wherein Yishanmen on the door is mutually Fixed latches 4, the latch of another Yishanmen are the linkage 5 that can be linked with handle 6, and Yishanmen first be closed by Fixed latches 4 It is convenient after locking is fixed to close another Yishanmen, the locking of linkage 5 second fan door is driven by handle 6, easy to operate, locking is reliable It will not loosen；Second fan door upper and lower ends are provided with three linkages 5 with inserting handle position, and handle 6 drives three linkages at the same time Latch 5 locks, and interlocking is reliable.

1 siding of babinet includes inside panel 7, exterior panel 8, and inside panel 7,8 material of exterior panel are plastics, inside panel 7, exterior panel Aluminum alloy framework 9,9 rectangular cross-section of aluminum alloy framework, including aluminum alloy framework 9 is by self-drilling connection are provided between 8 Between siding 7, exterior panel 8；Aluminum alloy framework 9 is rotation molding by being welded to connect integral frame, inside panel 7, exterior panel 8 Plastic wall panels；Aluminum alloy framework 9 has enough support strengths, while light-weight, easy to assembly；The inside panel 7 of plastic material, Exterior panel 8 also has the characteristics of light-weight, intensity is good；3 edges of door are provided with sealing strip 10,10 rectangular cross-section tubulose of sealing strip Rubber strip, pass through sealing strip 10 increase door 3 sealing performance.

First using aluminium alloy extrusions welding aluminum alloy skeleton composition container general frame, the bottom plate of babinet is by 4 pieces of modelings Flitch is put together, and blending bolt is fixed on aluminum alloy framework；In the plastics that according to product technology design will be required to produce again Siding, exterior panel are fixed by screws in side wall, the head cover harden structure that babinet is formed on aluminum alloy framework, are combined into beautiful, light Skilful plastic container；Finally split door is designed in middle part before container, and split door is capable of providing larger disengaging Passage, meets the vanning requirement of bulky items；Door is hinged on wall box by hinge, easy for installation；It is a pair of split Door wherein Yishanmen is closed by Fixed latches to be locked, another Yishanmen by handle drive three linkages and wall box, Yishanmen cross-correlation locking is determined；Cost can not only be reduced using plastic material manufacture air container, and can be greatly Mitigate box weight, can ensure Strength of Container using aluminium alloy extrusions as box frame, plastics are manufactured with rotational moulding techniques Housing, is assembled into the air container of light and handy beauty.

The aircraft transportation container of the utility model, is navigated using high-density polyethylene plastics and Al-alloy metal skeleton Empty container makes, and aluminum alloy framework is used per a piece of wallboards of box body, aluminium alloy takes welding manner to form general frame, with this To ensure the intensity of container, bottom plate makes integral plastics pallet, and metallic framework is reliably connected with pallet, then by rotation molding Plastic wall panels be installed on aluminum alloy frame on, be combined into light and handy, beautiful container, the proportion of plastics only has 0.95 or so； The density of aluminium alloy is 2.75-2.8g/cm3, can mitigate Container Weight significantly；Reach saving Aviation Fuel；Reduce transport The purpose of cost.

The shape of container is designed with claimed below, and aircraft transportation container is designed according to the shape of aircraft hold, To ensure the maximum load rate of the cargo hold confined space, so it is rescinded angle or fillet design that Air Container, which has part, and aircraft Shape is determined by its air dynamic behaviour again；So air container can not possibly use same standard；Transported in aviation In defeated system, air container (Air-Mode Cargo Containers) is classified as machine for collecting load (Unit Load Device) In a kind, using the container of aircraft carrying, its specification and model are a lot of, common model have AKE, AMF, AAU, AMA, ALF etc., according to demand using the container of different size.

The utility model is adapted to the container production of various models to make, therefore selects the container figure of one of which model Shape is illustrated produces each segment type material as one embodiment, aluminum alloy materials according to design size, then uses welding side Formula is combined into aluminum alloy frame, plastic wall panels, lamina tecti and door handle etc. and is fixed using screw.

Claims

1. a kind of aircraft transportation container, including integrated box（1）, it is characterised in that：Babinet（1）Lower part has and aircraft bottom The inverted trapezoidal structure that portion's planform is adapted（2）；Babinet（1）Front end is provided with the hinged split door of hinge（3）, door （3）Upper and lower ends are provided with latch；Split one wherein the latch of Yishanmen is Fixed latches on the door mutually（4）, another Yishanmen Latch for can be with handle（6）The linkage of linkage（5）.

2. aircraft transportation container according to claim 1, it is characterised in that：The handle（6）Three connection are driven at the same time Dynamic latch.

3. aircraft transportation container according to claim 1, it is characterised in that：The babinet（1）Siding includes inside panel （7）, exterior panel（8）, inside panel（7）, exterior panel（8）Material is plastics, inside panel（7）, exterior panel（8）Between be provided with aluminium conjunction Golden skeleton（9）, aluminum alloy framework（9）Rectangular cross-section, aluminum alloy framework（9）By self-drilling connection in inside panel（7）, it is outer Siding（8）Between.

4. aircraft transportation container according to claim 1, it is characterised in that：The door（3）Edge is provided with sealing strip （10）, sealing strip（10）The rubber strip of rectangular cross-section tubulose.

5. aircraft transportation container according to claim 3, it is characterised in that：The aluminum alloy framework（9）Pass through welding Connect into general frame, inside panel（7）, exterior panel（8）For the plastic wall panels of rotation molding.