CN205770672U - A kind of removable aviation case - Google Patents
A kind of removable aviation case Download PDFInfo
- Publication number
- CN205770672U CN205770672U CN201620508913.9U CN201620508913U CN205770672U CN 205770672 U CN205770672 U CN 205770672U CN 201620508913 U CN201620508913 U CN 201620508913U CN 205770672 U CN205770672 U CN 205770672U
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- China
- Prior art keywords
- main body
- aviation case
- side plate
- lobe
- plate
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- Expired - Fee Related
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- 230000001012 protector Effects 0.000 claims description 27
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 235000004443 Ricinus communis Nutrition 0.000 claims description 3
- 230000007423 decrease Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 3
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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Abstract
The utility model discloses a kind of removable aviation case, aviation case main body including before and after's opening, aviation case main body includes top body plate, main body base plate, main body side plate and demountable structure, the upper end of the main body side plate that two are oppositely arranged is connected by demountable structure with the two ends, left and right of top body plate respectively, lower end is connected by demountable structure with the two ends, left and right of main body base plate respectively, demountable structure includes lobe and concave part, lobe includes spacing preiection, the width of spacing preiection increases along the direction away from lobe, concave part includes limited impression, limited impression adapts with the shape of spacing preiection, spacing preiection inserts limited impression with fixing boss and concave part.By demountable structure, aviation case main body can be disassembled into top body plate, main body base plate and main body side plate, compared with the aviation case main body being assembled into casing, considerably reduces the space occupied in transportation, decreases freight.
Description
Technical field
This utility model relates to equipment conveying field, particularly relates to a kind of removable aviation case.
Background technology
Current aviation case is made up of protecgulum, aviation case main body, bonnet three part, is mainly used in light, dance
Various processors and the installation of light units, LED video processor and the deposit position of power amplifier and protection thereof in platform
Effect.The protecgulum of existing aviation case can separate with aviation case main body with bonnet, but aviation case main body is originally
Body is non-dismountable, takes up space very big during transport aviation case, and freight is expensive.
Utility model content
The purpose of this utility model is to propose a kind of removable aviation case, the aviation case main body of this aviation case
Detachably, the space occupied during transport aviation case and expense are reduced.
For reaching this purpose, this utility model by the following technical solutions:
A kind of removable aviation case, including the aviation case main body of before and after's opening, described aviation case main body includes
Top body plate, main body base plate, main body side plate and demountable structure, two described main body side plates being oppositely arranged
Upper end be connected by described demountable structure with the two ends, left and right of described top body plate respectively, lower end respectively with
The two ends, left and right of described main body base plate are connected by described demountable structure, and described demountable structure includes projection
Portion and concave part, described lobe includes spacing preiection, and the width of described spacing preiection is along away from described projection
The direction in portion increases, and described concave part includes the shape of limited impression, described limited impression and described spacing preiection
Shape adapts, and described spacing preiection inserts described limited impression with fixing described lobe and described concave part.
Wherein, described top body plate is fixed with described lobe, the upper end of described main body side plate and described groove
Portion is fixed；Or
Described top body plate is fixed with described concave part, and the upper end of described main body side plate is fixed with described lobe；
Described main body base plate is fixed with described lobe, and the lower end of described main body side plate is fixed with described concave part；
Or
Described main body base plate is fixed with described concave part, and the lower end of described main body side plate is fixed with described lobe.
Wherein, described lobe also includes that the first holding tank, described concave part also include the second holding tank:
Described spacing preiection is arranged at, with described first holding tank, the two ends that described lobe is relative, described spacing
Groove and described second holding tank are arranged at the orthogonal two ends of described concave part, or
Described spacing preiection and described first holding tank are arranged at the orthogonal two ends of described lobe, described
Limited impression is arranged at, with described second holding tank, the two ends that described concave part is relative.
Wherein, described spacing preiection includes being perpendicular to described lobe end the first confined planes and second spacing
Face, and the stationary plane being gradually increased along the direction width away from described lobe, described first confined planes,
Stationary plane and the second confined planes are sequentially connected with along the direction away from described lobe.
Wherein, also including main part corner protector, described main part corner protector includes orthogonal Corner protecting board, described
The middle part of Corner protecting board is provided with Corner protecting board and fixes groove, and the outer surface of described Corner protecting board runs through fixing hole, inner surface
There are the screw corresponding with the position of described fixing hole, described top body plate, described main body base plate and main body side
Plate all runs through fixing hole, and described main part corner protector is fixed at the drift angle of described aviation case main body.
Wherein, castor, described main body side it have been bolted inside the drift angle of the bottom of described main body base plate
Plate is fixed with Handheld Division.
Wherein, also include that end cap, described end cap include end cap base plate and be vertically fixed on described end cap base plate four
The end cap side plate in week, described end cap side plate is provided with lower snap close, and described main body side plate is provided with snap close, institute
State lower snap close and described upper snap close mutually fastens so that two described end caps close off described aviation case main body
Opening front and back.
Wherein, described end cap also includes that straight corner protector, spherical corner protector and aluminum corner brace, described straight corner protector are positioned at described end
Lid is at the drift angle of described main body side plate one end, and described spherical corner protector is positioned at described end cap away from described main body
At the drift angle of one end of side plate, described aluminum corner brace is positioned at the described end cap edge away from the side of described main body side plate.
Wherein, described end cap is additionally provided with raised line, described aviation near the edge of the side of described main body side plate
Before and after box main body, opening part is provided with recessed bar, before and after two described end caps close described aviation case main body
During opening, described raised line is pressed into described recessed bar.
Wherein, described end cap base plate and described end cap side plate are PLASTIC LAMINATED.
Beneficial effect: this utility model provides a kind of removable aviation case, including the aviation of before and after's opening
Box main body, described aviation case main body includes top body plate, main body base plate, main body side plate and demountable structure,
The upper end of two described main body side plates being oppositely arranged is passed through described with the two ends, left and right of described top body plate respectively
Demountable structure connects, and lower end is respectively with the two ends, left and right of described main body base plate by described demountable structure even
Connecing, described demountable structure includes that lobe and concave part, described lobe include spacing preiection, described limit
The width of position projection increases along the direction away from described lobe, and described concave part includes limited impression, described
Limited impression adapts with the shape of described spacing preiection, and described spacing preiection inserts described limited impression with solid
Fixed described lobe and described concave part.By demountable structure, aviation case main body can be disassembled into main body top
Plate, main body base plate and main body side plate, compared with the aviation case main body being assembled into casing, considerably reduce
The space occupied in transportation, decreases freight.
Accompanying drawing explanation
Fig. 1 is the side view of aviation case main body of the present utility model.
Fig. 2 is the front view of aviation case main body of the present utility model.
Fig. 3 is the partial enlarged drawing at the A of Fig. 2.
Fig. 4 is the structural representation of demountable structure of the present utility model.
Fig. 5 is the structural representation of main part corner protector of the present utility model.
Fig. 6 is the structural representation of another angle of main part corner protector of the present utility model.
Fig. 7 is the side view of end cap of the present utility model.
Wherein:
1-aviation case main body, 11-top body plate, 12-main body base plate, 121-castor, 13-main body side plate, 131-
Handheld Division, the upper snap close of 132-, 14-demountable structure, 141-lobe, 1411-spacing preiection, 14111-
First confined planes, 14112-stationary plane, 14113-the second confined planes, 1412-the first holding tank, 142-groove
Portion, 1421-limited impression, 1422-the second holding tank, 15-main part corner protector, 151-Corner protecting board, 1511-
Corner protecting board fixes groove, 2-end cap, 21-end cap side plate, snap close under 211-, the straight corner protector of 22-, the spherical corner protector of 23-,
24-aluminum corner brace, 25-raised line, the recessed bar of 26-.
Detailed description of the invention
For making this utility model solve the technical problem that, the technical scheme that uses and the technique effect that reaches more
Clear, further illustrate the technical solution of the utility model below in conjunction with the accompanying drawings and by detailed description of the invention.
Refer to Fig. 1 to Fig. 4, embodiment of the present utility model provides a kind of removable aviation case, including
The aviation case main body 1 of opening front and back, aviation case main body 1 includes top body plate 11, main body base plate 12, main body
Side plate 13 and demountable structure 14, the upper end of two described main body side plates 13 being oppositely arranged is respectively with described
The two ends, left and right of top body plate 11 are connected by described demountable structure 14, lower end respectively with described main body at the bottom of
The two ends, left and right of plate 12 are connected by described demountable structure 14, and demountable structure 14 includes lobe 141
With concave part 142, lobe 141 includes spacing preiection 1411, and the width of spacing preiection 1411 is along away from convex
The direction playing portion 141 increases, i.e. convex more than close away from the width at lobe 141 in spacing preiection 1411
Playing the width at portion 141, spacing preiection 1411 is wide outside and narrow inside, and concave part 142 includes limited impression 1421,
Limited impression 1421 adapts with the shape of spacing preiection 1411, and spacing preiection 1411 inserts limited impression 1421
With fixing boss 141 and concave part 142, owing to spacing preiection 1411 is wide outside and narrow inside, therefore spacing preiection
After 1411 insert limited impression 1421, it is inseparable in the direction being perpendicular to grafting, can effectively consolidate
Fixing limit protruding 1411 and limited impression 1421, thus effectively fix and be connected with demountable structure 14
Top body plate 11, main body base plate 12 and main body side plate 13.By demountable structure 14, aviation case main body 1
Top body plate 11, main body base plate 12 and main body side plate 13 can be disassembled into, with the aviation case being assembled into casing
Main body 1 is compared, and considerably reduces the space occupied in transportation, decreases freight.
In the present embodiment, the two ends of main body side plate 13 are passed through with top body plate 11 and main body base plate 12 respectively can
Detaching structure 14 connects, and in concrete attachment structure, the position of lobe 141 and concave part 142 is permissible
Exchanging, do not affect its dismountable effect, therefore attachment structure has various ways: top body plate 11 is with main
In the connection of side plate 13, can be that top body plate 11 is fixed with lobe 141, main body side plate 13 upper
End is fixed with concave part 142；Or top body plate 11 is fixing with concave part 142, the upper end of main body side plate 13
Fix with lobe 141；In the connection of main body base plate 12 and main body side plate 13, it can be main body base plate 12
Fixing with lobe 141, the lower end of main body side plate 13 is fixed with concave part 142；Or main body base plate 12 with
Concave part 142 is fixed, and the lower end of main body side plate 13 is fixed with lobe 141.
For ease of lobe 141 and concave part 142 and remaining part, i.e. top body plate 11, main body base plate 12,
Or main body side plate 13 connects, lobe 141 also includes the first holding tank 1412 for connecting remaining part,
Concave part 142 also includes the second holding tank 1422 for connecting remaining part.After being assembled into casing,
Main body side plate 13 is vertical with top body plate 11 and main body base plate 12 respectively, therefore lobe 141 and groove
After portion 142 grafting, the first holding tank 1412 should be mutually perpendicular to the second holding tank 1422, and first accommodates
The position of groove 1412 and the second holding tank 1422 could be arranged to: spacing preiection 1411 and the first holding tank 1412
Being arranged at the two ends that lobe is relative, limited impression 1421 and the second holding tank 1422 are arranged at concave part 142
Orthogonal two ends；Or spacing preiection 1411 is arranged at lobe with the first holding tank 1412 and is mutually perpendicular to
Two ends, limited impression 1421 is arranged at, with the second holding tank 1422, the two ends that concave part 142 is relative.
Spacing preiection 1411 includes that the first confined planes 14111 and second being perpendicular to lobe 141 end is spacing
Face 14113, and the stationary plane 14112 being gradually increased along the direction width away from lobe 141, the first limit
Plane 14111, stationary plane 14112 and the second confined planes 14113 connect successively along the direction away from lobe 141
Connect.The shape of limited impression 1421 adapts with spacing preiection 1411, and the first of spacing preiection 1411 is spacing
Face 14111 and the second confined planes 14113 are for limiting the spacing preiection 1411 position in limited impression 1421
Put, and stationary plane 14112 forms structure wide outside and narrow inside, so that spacing preiection 1411 can not be with slotting
Enter vertical direction and depart from limited impression 1421, can only move along direction of insertion.
With reference to Fig. 1, Fig. 2, Fig. 5 and Fig. 6, in the present embodiment, aviation case also includes main part corner protector 15.
After aviation case main body 1 is assembled into casing, it is the edge of the junction of two parts at drift angle, needs main part
Corner protector 15 is to reinforcing herein, and main part corner protector 15 includes orthogonal Corner protecting board 151, Corner protecting board
The middle part of 151 is provided with Corner protecting board and fixes groove 1511, and two parts being connected are individually positioned in main part corner protector
Two Corner protecting boards of 15 are fixed in groove 1511, and the outer surface of Corner protecting board 151 runs through fixing hole, and inner surface has
The screw corresponding with the position of fixing hole, top body plate 11, main body base plate 12 and main body side plate 13 all pass through
It is installed with fixing hole, is putting into after Corner protecting board fixes groove 1511, by bolt through corresponding fixing hole, with
Screw connects, and effectively fixes the drift angle of aviation case main body 1.
For ease of movement and the gripping of aviation case, it is bolted inside the drift angle of the bottom of main body base plate 12
Castor 121, main body side plate 13 is had to be fixed with Handheld Division 131.
Refer to Fig. 1 and Fig. 7, in the present embodiment, before and after aviation case main body 1, two ends need to close, therefore
Also include that end cap 2, end cap 2 include end cap base plate and be vertically fixed on the end cap side plate 21 of end cap base plate surrounding,
Dismounting with aviation case main body 1 for ease of end cap 2, end cap side plate 21 is provided with lower snap close 211, main body side plate
13 are provided with snap close 132, and lower snap close 211 and upper snap close 132 mutually fasten so that two end caps 2 are distinguished
Close opening before and after aviation case main body 1.Optionally, end cap 2 also includes straight corner protector 22, spherical corner protector 23
With aluminum corner brace 24, straight corner protector 22 is positioned at end cap 2 at the drift angle of main body side plate 13 one end, leans on end cap 2
Nearly main body side plate 13 one end is protected, and spherical corner protector 23 is positioned at end cap 2 one end away from main body side plate 13
Drift angle at, both end cap 2 was protected away from one end of main body side plate 13, and used spherical being also prevented from
Staff etc. is caused unexpected injury by the sharp-pointed drift angle of end cap 2, and aluminum corner brace 24 is positioned at end cap 2 away from main body side
The edge of the side of plate 13, the edge of protection end cap 2.
Stablizing for making to fasten between end cap 2 and aviation case main body 1, end cap 2 is near the one of main body side plate 13
The edge of side is additionally provided with raised line 25, and before and after aviation case main body 1, opening part is provided with recessed bar 26, two
When end cap 2 closes opening before and after aviation case main body 1, raised line 25 is pressed into recessed bar 26.End cap base plate and end cap
Side plate 21 is PLASTIC LAMINATED, to the protection of the instrument within aviation case more preferably.
Above content is only preferred embodiment of the present utility model, for those of ordinary skill in the art, depends on
According to thought of the present utility model, the most all will change, this explanation
Book content should not be construed as restriction of the present utility model.
Claims (10)
1. a removable aviation case, it is characterised in that include the aviation case main body (1) of before and after's opening,
Described aviation case main body (1) include top body plate (11), main body base plate (12), main body side plate (13) and
Demountable structure (14), the upper end of two described main body side plates (13) being oppositely arranged respectively with described main body
The two ends, left and right of top board (11) by described demountable structure (14) connect, lower end respectively with described main body
The two ends, left and right of base plate (12) are connected by described demountable structure (14), described demountable structure (14)
Including lobe (141) and concave part (142), described lobe (141) includes spacing preiection (1411),
The width of described spacing preiection (1411) increases along the direction away from described lobe (141), described groove
Portion (142) includes limited impression (1421), described limited impression (1421) and described spacing preiection (1411)
Shape adapt, described spacing preiection (1411) inserts described limited impression (1421) with fixing described
Lobe (141) and described concave part (142).
2. aviation case as claimed in claim 1, it is characterised in that described top body plate (11) is convex with described
Playing portion (141) to fix, the upper end of described main body side plate (13) is fixed with described concave part (142)；Or
Described top body plate (11) and described concave part (142) are fixed, described main body side plate (13) upper
End is fixed with described lobe (141)；
Described main body base plate (12) is fixed with described lobe (141), under described main body side plate (13)
End is fixed with described concave part (142)；Or
Described main body base plate (12) is fixed with described concave part (142), under described main body side plate (13)
End is fixed with described lobe (141).
3. aviation case as claimed in claim 1, it is characterised in that described lobe (141) also includes the
One holding tank (1412), described concave part (142) also includes the second holding tank (1422):
It is relative that described spacing preiection (1411) is arranged at described lobe with described first holding tank (1412)
Two ends, described limited impression (1421) and described second holding tank (1422) are arranged at described concave part
(142) orthogonal two ends, or
It is mutual that described spacing preiection (1411) and described first holding tank (1412) are arranged at described lobe
Vertical two ends, described limited impression (1421) is arranged at described recessed with described second holding tank (1422)
The two ends that groove portion (142) is relative.
4. aviation case as claimed in claim 1, it is characterised in that described spacing preiection (1411) includes hanging down
Directly the first confined planes (14111) in described lobe (141) end and the second confined planes (14113),
And along the stationary plane (14112) being gradually increased away from the direction width of described lobe (141), described the
One confined planes (14111), stationary plane (14112) and the second confined planes (14113) are along away from described projection
The direction in portion (141) is sequentially connected with.
5. aviation case as claimed in claim 1, it is characterised in that also include main part corner protector (15), institute
State main part corner protector (15) and include orthogonal Corner protecting board (151), the middle part of described Corner protecting board (151)
Being provided with Corner protecting board and fix groove (1511), the outer surface of described Corner protecting board (151) runs through fixing hole, interior table
There are the screw corresponding with the position of described fixing hole, described top body plate (11), described main body base plate (12) in face
All running through with main body side plate (13) and have fixing hole, described main part corner protector (15) is fixed on described aviation case
At the drift angle of main body (1).
6. aviation case as claimed in claim 1, it is characterised in that the bottom of described main body base plate (12)
Drift angle inside be bolted castor (121), described main body side plate (13) is fixed with Handheld Division (131).
7. aviation case as claimed in claim 1, it is characterised in that also include end cap (2), described end cap
(2) include end cap base plate and be vertically fixed on the end cap side plate (21) of described end cap base plate surrounding, described end
Lid side plate (21) is provided with lower snap close (211), and described main body side plate (13) is provided with snap close (132),
Described lower snap close (211) and described upper snap close (132) mutually fasten so that two described end caps (2) are distinguished
Close opening before and after described aviation case main body (1).
8. aviation case as claimed in claim 7, it is characterised in that described end cap (2) also includes straight corner protector
(22), spherical corner protector (23) and aluminum corner brace (24), described straight corner protector (22) is positioned at described end cap (2) and leans on
At the drift angle of nearly described main body side plate (13) one end, described spherical corner protector (23) is positioned at described end cap (2)
At drift angle away from one end of described main body side plate (13), described aluminum corner brace (24) is positioned at described end cap (2)
Edge away from the side of described main body side plate (13).
9. aviation case as claimed in claim 7, it is characterised in that described end cap (2) is near described main body
The edge of the side of side plate (13) is additionally provided with raised line (25), opens before and after described aviation case main body (1)
Recessed bar (26) it is provided with, before and after two described end caps (2) close described aviation case main body (1) at Kou
During opening, described raised line (25) is pressed into described recessed bar (26).
10. aviation case as claimed in claim 7, it is characterised in that described end cap base plate and described end cover side
Plate (21) is PLASTIC LAMINATED.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620508913.9U CN205770672U (en) | 2016-05-30 | 2016-05-30 | A kind of removable aviation case |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620508913.9U CN205770672U (en) | 2016-05-30 | 2016-05-30 | A kind of removable aviation case |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205770672U true CN205770672U (en) | 2016-12-07 |
Family
ID=59979848
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620508913.9U Expired - Fee Related CN205770672U (en) | 2016-05-30 | 2016-05-30 | A kind of removable aviation case |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205770672U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516338A (en) * | 2016-12-31 | 2017-03-22 | 重庆煌固包装制造有限公司 | Conveying packaging box |
| JP2019163079A (en) * | 2018-03-20 | 2019-09-26 | 株式会社カネカ | Constant temperature storage transport container and transport method |
| CN112441326A (en) * | 2019-09-02 | 2021-03-05 | 中久物流有限公司 | Assembled rack |
| CN114364065A (en) * | 2020-10-13 | 2022-04-15 | 芜湖尼晶电子科技有限公司 | Outer heat preservation device of semiconductor heater |
| CN116216041A (en) * | 2022-12-16 | 2023-06-06 | 深圳市元创时代科技有限公司 | Socket storage box |
-
2016
- 2016-05-30 CN CN201620508913.9U patent/CN205770672U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516338A (en) * | 2016-12-31 | 2017-03-22 | 重庆煌固包装制造有限公司 | Conveying packaging box |
| JP2019163079A (en) * | 2018-03-20 | 2019-09-26 | 株式会社カネカ | Constant temperature storage transport container and transport method |
| JP7301500B2 (en) | 2018-03-20 | 2023-07-03 | 株式会社カネカ | Temperature-controlled storage container and transportation method |
| CN112441326A (en) * | 2019-09-02 | 2021-03-05 | 中久物流有限公司 | Assembled rack |
| CN114364065A (en) * | 2020-10-13 | 2022-04-15 | 芜湖尼晶电子科技有限公司 | Outer heat preservation device of semiconductor heater |
| CN116216041A (en) * | 2022-12-16 | 2023-06-06 | 深圳市元创时代科技有限公司 | Socket storage box |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20161207 Termination date: 20190530 |