CN207191659U - Aircraft box - Google Patents
Aircraft box Download PDFInfo
- Publication number
- CN207191659U CN207191659U CN201721078490.2U CN201721078490U CN207191659U CN 207191659 U CN207191659 U CN 207191659U CN 201721078490 U CN201721078490 U CN 201721078490U CN 207191659 U CN207191659 U CN 207191659U
- Authority
- CN
- China
- Prior art keywords
- plate
- side plate
- aircraft box
- hanger
- vertical folding
- 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.)
- Expired - Fee Related
Links
Abstract
The embodiment of the utility model one provides a kind of aircraft box, the aircraft box includes bottom plate and is connected to first side plate, the second side plate, the 3rd side plate and the 4th side plate of four sides of bottom plate, the both ends of first side plate and second side are further connected with hanger plate, in the first side plate and the second side plate opposed bottom vertical folding and hanger plate the first side plate and the second side plate vertical folding relatively, non-overlapped splicing is chimeric each other for hanger plate.The aircraft box structure that the utility model embodiment provides is novel, by hanger plate non-overlapped splicing is chimeric each other may be such that aircraft box is molded when structure it is well-balanced attractive in appearance.
Description
Technical field
It the utility model is related to packing appliance technical field, and in particular to a kind of aircraft box
Background technology
Aircraft box, gained the name because its expansion exactly likes aircraft, turn into various productions due to simple and practical and cheap
Product packaging, the preferred carton of express delivery packing.
Common aircraft box mainly has two kinds, one kind be tongue position without coupling type, be usually used in thicker cell type, box is overall
It is very loose；Another kind is that have tongue position to have coupling type, after aircraft box shaping, because hook has lap, shaping rear side
Face easily forms the narrow big tripe shape in thick middle both sides, occupies more spaces and influences attractive in appearance.
Utility model content
The utility model provides a kind of aircraft box, with meeting when solving that the hook of aircraft box in the prior art is overlapping to cause shaping
The problem of forming the narrow big tripe shape in thick middle both sides.
In order to solve the above technical problems, the technical scheme that the utility model embodiment uses is：A kind of aircraft is provided
Box, aircraft box include bottom plate and be connected to first side plate of described four sides of bottom plate, the second side plate, the 3rd side plate and
The both ends of 4th side plate, first side plate and second side plate are further connected with hanger plate, in first side plate and
The relatively described bottom plate vertical folding of second side plate and relatively described first side plate of the hanger plate and second side plate hang down
During straight folding, non-overlapped splicing is chimeric each other for the hanger plate.
According to the specific embodiment of the utility model one, the bottom plate is close to the 3rd side plate and the 4th side plate
Marginal position is provided with cutting wire casing.
According to the specific embodiment of the utility model one, the 3rd side plate and the 4th side plate are included from the bottom plate
The external plate and interior buckle that side stretches out successively, the length and the hanger plate that the external plate extends from the bottom plate
Identical with length that second side plate extends from first side plate, the external plate is used in first side plate and institute
State the relatively described bottom plate vertical folding of the second side plate and relatively described first side plate of the hanger plate and second side plate are vertical
Relatively described bottom plate vertical folding is with the hanger plate that reclines during folding.
According to the specific embodiment of the utility model one, length that the interior buckle extends from the external plate with it is described outer
It is identical to put the length that plate extends from the bottom plate, for the relatively described hook in the external plate bottom plate vertical folding relatively
Plate fitting folds and cuts wire casing phase holding with described.
According to the specific embodiment of the utility model one, the outer end of the interior buckle is further provided with being used for and the line of cut
The corresponding arc-shaped insert plate of groove.
According to the specific embodiment of the utility model one, the interior buckle is towards first side plate and second side plate
Side is further provided with the swollen plate of arc.
According to the specific embodiment of the utility model one, the swollen plate of arc is set close to the outer end of the interior buckle.
According to the specific embodiment of the utility model one, the hanger plate includes mainboard, connecting plate and the hook being sequentially connected
Buckle, the mainboard extend from the outer end of first side plate and second side plate, the side of the connecting plate readme mainboard
Extend further out, the fastener plate is connected with the connecting plate and forms neck with the mainboard, and the neck is used for
First side plate and the relatively described bottom plate vertical folding of second side plate and relatively described first side plate of the hanger plate and
Another fastener plate is accommodated during the second side plate vertical folding.
According to the specific embodiment of the utility model one, the aircraft box also includes successively stretching out from first side plate
Cover plate and the 5th side plate, two sides of the cover plate are connected with ladder type board, and the side of the 5th side plate is connected with triangle
Plate.
According to the specific embodiment of the utility model one, the outer end of the 5th side plate is further provided with plate, the bottom plate
The slot for housing the plate is provided between first side plate.
The beneficial effects of the utility model are：The situation of prior art is different from, what the utility model embodiment provided flies
Machine box structure is novel, by hanger plate non-overlapped splicing is chimeric each other may be such that aircraft box is molded when structure it is well-balanced attractive in appearance.
Brief description of the drawings
Technical scheme in order to illustrate the embodiments of the present invention more clearly, make required in being described below to embodiment
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present invention, for
For those of ordinary skill in the art, on the premise of not paying creative work, other can also be obtained according to these accompanying drawings
Accompanying drawing, wherein：
Fig. 1 is the planar structure schematic diagram for the aircraft box spread shape that the embodiment of the utility model one provides；
Fig. 2 is the dimensional structure diagram for the aircraft box folded state that the embodiment of the utility model one provides.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only the part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
Also referring to Fig. 1 and Fig. 2, the embodiment of the utility model one provides a kind of aircraft box, and the aircraft box can use each
Kind suitable material (such as paper material) excision forming, the aircraft box include bottom plate 10 and are connected to 10 4 sides of bottom plate
The both ends of first side plate 11, the second side plate 12, the 3rd side plate 13 and the 4th side plate 14, the first side plate 11 and the second side plate 12 are entered
One step is connected with hanger plate 111, the first side plate 11 and the vertical folding of 12 opposed bottom of the second side plate 10 and hanger plate 111 it is relative
When the first side plate 11 and the second 12 vertical folding of side plate, non-overlapped splicing is chimeric each other for hanger plate 111.
Wherein, bottom plate 10 is provided with cutting wire casing 101, cutting in the marginal position close to the 3rd side plate 13 and the 4th side plate 14
Wire casing 101 can be 4 shown in figure, it is of course also possible to be the quantity such as 2 or 6, depending on packaging structure intensity needs
It is fixed.
3rd side plate 13 and the 4th side plate 14 include external plate 131 and the internal buckle to stretch out successively from the side of bottom plate 10
Plate 132, external plate 131 extend from the length that bottom plate 10 extends with hanger plate 111 from the first side plate 11 and the second side plate 12
Same length, external plate 131 be used in the first side plate 11 and the vertical folding of 12 opposed bottom of the second side plate 10 and hook
The vertical folding of opposed bottom 10 is with the hanger plate 111 that reclines when plate 111 is with respect to the first side plate 11 and the second 12 vertical folding of side plate,
The same length that interior buckle 132 extends from the length that external plate 131 extends with external plate 131 from bottom plate 10, is used for
In 131 10 vertical folding of opposed bottom of external plate, the relative fitting of hanger plate 111 folds and with cutting the phase holding of wire casing 101, together
When keep two pieces of hanger plates 111 to fasten and do not release.
Preferably, the outer end of interior buckle 132 is further provided with for the arc-shaped insert plate 133 corresponding with cutting wire casing 101,
Arc-shaped insert plate 133 matches with cutting wire casing 101.The side of interior buckle 132 towards the first side plate 11 and the second side plate 12 enters one
Step is provided with the swollen plate 134 of arc, and arc is swollen, and plate 134 can further lift the structural strength after the shaping of aircraft box.Arc is swollen, and plate 134 can
Set close to the outer end of interior buckle 132, the quantity such as 2,4 or 6 specifically can be set.
In the embodiment of the utility model one, hanger plate 111 includes mainboard 112, connecting plate 113 and the hook being sequentially connected
Buckle 114, mainboard 112 extend from the outer end of the first side plate 11 and the second side plate 12, the side of the readme mainboard 122 of connecting plate 113
Extend further out, fastener plate 114 is connected with connecting plate 113 and forms neck 115 with mainboard 112, and neck 115 is used for
First side plate 11 and the vertical folding of 12 opposed bottom of the second side plate 10 and hanger plate 111 relative first side plate 11 and the second side plate
Another fastener plate 114 (as shown in Figure 2) is accommodated during 12 vertical folding.Certainly, the concrete shape of hanger plate 111 and in being limited to accompanying drawing
It is shown, it can also be that other can arbitrarily carry out the structure that non-overlapped splicing is chimeric each other.
In addition, aircraft box also includes the side plate 16 of cover plate 15 and the 5th to stretch out successively from the first side plate 11, cover plate 15
Two sides be connected with ladder type board 151, the side of the 5th side plate 16 is connected with triangular plate 161.
Further, the outer end of the 5th side plate 16 is further provided with plate 162, is provided between the side plate 11 of bottom plate 10 and first
The slot 102 of accommodating plate 162.
In summary, it should be readily apparent to one skilled in the art that the aircraft box structure of the utility model embodiment offer is novel,
By hanger plate 111 non-overlapped splicing is chimeric each other may be such that aircraft box is molded when structure it is well-balanced attractive in appearance.
Embodiments of the invention are the foregoing is only, are not intended to limit the scope of the invention, it is every to utilize this hair
The equivalent structure or equivalent flow conversion that bright specification and accompanying drawing content are made, or directly or indirectly it is used in other related skills
Art field, is included within the scope of the present invention.
Claims (10)
1. a kind of aircraft box, it is characterised in that the aircraft box includes bottom plate and is connected to described four sides of bottom plate
The both ends of first side plate, the second side plate, the 3rd side plate and the 4th side plate, first side plate and second side plate are further
Be connected with hanger plate, first side plate and the relatively described bottom plate vertical folding of second side plate and the hanger plate it is relative
When first side plate and the second side plate vertical folding, non-overlapped splicing is chimeric each other for the hanger plate.
2. aircraft box according to claim 1, it is characterised in that the bottom plate is close to the 3rd side plate and described the
The marginal position of four side plates is provided with cutting wire casing.
3. aircraft box according to claim 2, it is characterised in that the 3rd side plate and the 4th side plate are included certainly
The external plate and interior buckle that the bottom plate side stretches out successively, the length and institute that the external plate extends from the bottom plate
It is identical with length that second side plate extends from first side plate to state hanger plate, the external plate is used for described first
Side plate and the relatively described bottom plate vertical folding of second side plate and relatively described first side plate of the hanger plate and described second
Relatively described bottom plate vertical folding is with the hanger plate that reclines during side plate vertical folding.
4. aircraft box according to claim 3, it is characterised in that the length that the interior buckle extends from the external plate
It is identical with the length that the external plate extends from the bottom plate, for relative in the external plate bottom plate vertical folding relatively
The hanger plate fitting folds and cuts wire casing phase holding with described.
5. aircraft box according to claim 4, it is characterised in that the outer end of the interior buckle is further provided with being used for and institute
State the corresponding arc-shaped insert plate of cutting wire casing.
6. aircraft box according to claim 4, it is characterised in that the interior buckle is towards first side plate and described
The side of two side plates is further provided with the swollen plate of arc.
7. aircraft box according to claim 6, it is characterised in that the swollen plate of arc is set close to the outer end of the interior buckle
Put.
8. aircraft box according to claim 1, it is characterised in that the hanger plate includes mainboard, the connection being sequentially connected
Plate and fastener plate, the mainboard extend from the outer end of first side plate and second side plate, the connecting plate readme master
The side of plate extends further out, and the fastener plate is connected with the connecting plate and forms neck, the card with the mainboard
Groove is used in first side plate and the relatively described bottom plate vertical folding of second side plate and the hanger plate relatively described the
Another fastener plate is accommodated when side plate and the second side plate vertical folding.
9. aircraft box according to claim 1, it is characterised in that the aircraft box is also included from first side plate successively
The cover plate and the 5th side plate to stretch out, two sides of the cover plate are connected with ladder type board, the side connection of the 5th side plate
There is triangular plate.
10. aircraft box according to claim 9, it is characterised in that the outer end of the 5th side plate is further provided with plate,
The slot for housing the plate is provided between the bottom plate and first side plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721078490.2U CN207191659U (en) | 2017-08-25 | 2017-08-25 | Aircraft box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721078490.2U CN207191659U (en) | 2017-08-25 | 2017-08-25 | Aircraft box |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207191659U true CN207191659U (en) | 2018-04-06 |
Family
ID=61795462
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721078490.2U Expired - Fee Related CN207191659U (en) | 2017-08-25 | 2017-08-25 | Aircraft box |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207191659U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108438419A (en) * | 2018-04-23 | 2018-08-24 | 恒铭达包装材料（惠州）有限公司 | A kind of aircraft box for exempting from bottom tongue |
| CN111348303A (en) * | 2018-12-21 | 2020-06-30 | 上海昆之翔纸业有限公司 | Double-layer paper box |
-
2017
- 2017-08-25 CN CN201721078490.2U patent/CN207191659U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108438419A (en) * | 2018-04-23 | 2018-08-24 | 恒铭达包装材料（惠州）有限公司 | A kind of aircraft box for exempting from bottom tongue |
| CN111348303A (en) * | 2018-12-21 | 2020-06-30 | 上海昆之翔纸业有限公司 | Double-layer paper box |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180406 Termination date: 20180825 |