CN112660633A - Aviation case - Google Patents
Aviation case Download PDFInfo
- Publication number
- CN112660633A CN112660633A CN202110196375.XA CN202110196375A CN112660633A CN 112660633 A CN112660633 A CN 112660633A CN 202110196375 A CN202110196375 A CN 202110196375A CN 112660633 A CN112660633 A CN 112660633A
- Authority
- CN
- China
- Prior art keywords
- box
- case
- type mouth
- outer ring
- aluminum
- 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.)
- Pending
Links
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 73
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 63
- 239000004411 aluminium Substances 0.000 claims description 15
- 239000004593 Epoxy Substances 0.000 claims description 4
- 239000002023 wood Substances 0.000 claims description 3
- 230000006978 adaptation Effects 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 9
- 238000005507 spraying Methods 0.000 abstract description 8
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000004806 packaging method and process Methods 0.000 abstract description 3
- 239000004033 plastic Substances 0.000 abstract description 3
- 229920003023 plastic Polymers 0.000 abstract description 3
- 239000002131 composite material Substances 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 7
- 239000011248 coating agent Substances 0.000 description 5
- 238000000576 coating method Methods 0.000 description 5
- 238000007731 hot pressing Methods 0.000 description 5
- 239000000853 adhesive Substances 0.000 description 4
- 230000001070 adhesive effect Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000007547 defect Effects 0.000 description 3
- 238000005406 washing Methods 0.000 description 3
- KUBDPQJOLOUJRM-UHFFFAOYSA-N 2-(chloromethyl)oxirane;4-[2-(4-hydroxyphenyl)propan-2-yl]phenol Chemical compound ClCC1CO1.C=1C=C(O)C=CC=1C(C)(C)C1=CC=C(O)C=C1 KUBDPQJOLOUJRM-UHFFFAOYSA-N 0.000 description 2
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000003063 flame retardant Substances 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 239000005022 packaging material Substances 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- RNFJDJUURJAICM-UHFFFAOYSA-N 2,2,4,4,6,6-hexaphenoxy-1,3,5-triaza-2$l^{5},4$l^{5},6$l^{5}-triphosphacyclohexa-1,3,5-triene Chemical compound N=1P(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP=1(OC=1C=CC=CC=1)OC1=CC=CC=C1 RNFJDJUURJAICM-UHFFFAOYSA-N 0.000 description 1
- 229920002396 Polyurea Polymers 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 239000002216 antistatic agent Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000007590 electrostatic spraying Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 210000003128 head Anatomy 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 210000001331 nose Anatomy 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
Images
Landscapes
- Packaging Of Annular Or Rod-Shaped Articles, Wearing Apparel, Cassettes, Or The Like (AREA)
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
Abstract
The invention discloses an aviation case, which comprises a case body EVA outer ring lining B case cover, a case cover, an aluminum plate and concave aluminum, wherein the case body EVA outer ring lining A is sleeved on the outer side of the case body EVA outer ring lining B case cover, a buffer groove A is arranged in the middle position inside the case body EVA outer ring lining B case cover, one side inside the case body EVA outer ring lining B case cover is provided with the buffer groove A, the case cover is matched with the case body EVA outer ring lining B case cover, a connecting plate is arranged inside the concave aluminum, hinge strips are arranged on two sides of the bottom of the concave aluminum, and one ends of the hinge strips, far away from the concave aluminum, are hinged with the connecting plate; the device has the advantages of high material holding rate in the popular market, easy material concentration in a short time, relatively low cost and high manufacturing efficiency, can be quickly assembled and quickly produced under the condition of complete spraying plastic composite hot-pressed plates, achieves the aim of timely replenishing the packaging box, and further improves the practicability of the device.
Description
Technical Field
The invention relates to the technical field of flight boxes, in particular to a flight box.
Background
As is known, an aviation case is a storage and arrangement product which is effective and widely applied to the protection of high-end science and technology products in the transportation process, the existing aviation case can efficiently protect the products in storage and transportation under a general environment, but the protection under special conditions is weaker when military products are used, the military aviation case is special in use conditions, and the severity of uncertain climate change under extreme environments, such as wind and rain, needs to be moisture-proof and has a certain weight to slow down the damage caused by movement; the packaging material can effectively absorb load when used under extreme conditions, such as explosion in wartime, and the technical requirement is that the direction and the size of the force can be changed even if the packaging material is broken, so that the loss of the content is reduced;
the prior practical use process has the following defects: 1. in the using process of the existing device, the material is possibly more precious, the retention rate is low, the strengthening cost is higher, and the practicability of the device is further reduced; 2. the packaging that the violent shock of sudden transport probably brought became invalid, probably also can influence the quick manufacturing after the packing box damage and supply at the in-process of using of current device, and then also reduced the use variety of device, and the structure is complicated, and the operation is inconvenient.
Disclosure of Invention
The present invention is directed to an aviation case to solve the above problems of the prior art.
In order to achieve the purpose, the invention provides the following technical scheme: an aviation case comprises a case body EVA outer ring lining B case cover, a case cover, an aluminum plate and concave aluminum, wherein a case body EVA outer ring lining A is sleeved on the outer side of the case body EVA outer ring lining B case cover, a buffer groove A is arranged in the middle position inside the case body EVA outer ring lining B case cover, a buffer groove A is arranged on one side inside the case body EVA outer ring lining B case cover, the case cover is matched with the case body EVA outer ring lining B case cover, a connecting plate is arranged inside the concave aluminum, hinge strips are arranged on two sides of the bottom of the concave aluminum, one end, away from the concave aluminum, of each hinge strip is hinged with the connecting plate, support hinges are hinged on two sides of the top of the concave aluminum, convex aluminum is arranged on the top of the concave aluminum, one end, away from the concave aluminum, of each support hinge is hinged with the convex aluminum, wrap angles are arranged at four corners of the outer side of the concave aluminum, the both sides of protruding type mouth aluminium are articulated to have the ball angle, aluminum plate's one end is provided with epoxy, epoxy keeps away from aluminum plate's one end and is provided with the multiply wood.
Preferably, the buffer grooves a have a convex structure.
Preferably, clamping blocks are arranged on two sides of the bottom of the box cover.
Preferably, universal wheels are arranged at four corners of the bottom of the concave aluminum.
Preferably, the number of the spherical angles is multiple groups.
Preferably, the wrap angle is formed by a V-shaped structure.
Compared with the prior art, the invention has the beneficial effects that: the flight box;
1. the material has high market retention rate, is easy to concentrate materials in a short time, has relatively low price cost and high manufacturing efficiency, can be quickly assembled and quickly produced under the condition of preparing the plastic spraying composite hot-pressing plate, achieves the aim of replenishing the packaging box in time, and further improves the practicability of the device;
2. the lining EVA material can also be added with molecular materials to ensure special purposes, and antistatic and electromagnetic shielding resistance can be realized by adding an antistatic agent if shielding prevention is needed for some military articles; for example, still some military articles box burning need take out the incasement product fast, just need the inside lining slow combustion, then can add the fire retardant, reach the flame retardant efficiency of certain degree, and then also improved the device's use variety.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a cross-sectional view of the present invention;
fig. 3 is a drawing showing the connection of the aluminum sheet and the multilayer sheet of the present invention.
In the figure: 1. a hinge strip; 2. a connecting plate; 5. a ball angle; 6. wrapping corners; 7. convex-opening aluminum; 8. concave aluminum; 9. a support hinge; 11. a buffer tank A; 12. a buffer tank B; 14. an aluminum plate; 15. an epoxy resin; 16. a multilayer board; 21. an EVA outer ring inner lining A of the box body; 22. a lining B is arranged on an EVA outer ring of the box body; 23. and a box cover.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides an embodiment: an aviation case comprises a case body EVA outer ring lining B case cover 22, a case cover 23, an aluminum plate 14 and a concave aluminum 8, wherein a case body EVA outer ring lining A21 is sleeved on the outer side of the case body EVA outer ring lining B case cover 22 to facilitate lining, a buffer groove A12 is arranged in the middle position inside the case body EVA outer ring lining B case cover 22, a buffer groove A11 is arranged on one side inside the case body EVA outer ring lining B case cover 22, the case cover 23 is matched with the case body EVA outer ring lining B case cover 22, a connecting plate 2 is arranged inside the concave aluminum 8, hinge strips 1 are arranged on two sides of the bottom of the concave aluminum 8, one ends of the hinge strips 1 far away from the concave aluminum 8 are hinged with the connecting plate 2, support hinges 9 are hinged on two sides of the top of the concave aluminum 8 to facilitate supporting, a convex aluminum 7 is arranged on the top of the concave aluminum 8 to facilitate matching, one end of the support hinges 9 far away from the concave aluminum 8 is hinged with the convex aluminum 7, the four corners department in concave type mouth aluminium 8's the outside is provided with cornerite 6, and the both sides of protruding type mouth aluminium 7 are articulated to have a spherical corner 5, and aluminum plate 14's one end is provided with epoxy 15, and epoxy 15 keeps away from aluminum plate 14's one end and is provided with multiply wood 16.
In this implementation, dashpot A12 comprises protruding type structure, the buffering of being convenient for, 23 the both sides of case lid bottom are provided with the fixture block, are convenient for fixed, and the four corners department of the bottom of concave type mouth aluminium 8 all is provided with the universal wheel, is convenient for remove, and the quantity of ball angle 5 is the multiunit, is convenient for connect, and cornerite 6 comprises V font structure, the protection of being convenient for.
The working principle is as follows: firstly, through a multi-layer plate 16 hot-pressing aviation box, through plate hot-pressing preparation, considering the poor adhesive force of an aluminum product to a spraying coating, the subsequent process of the multi-layer plate 16 hot-pressing aluminum plate is provided, and the analysis of the adhesive force defect of the surface treatment of the aluminum product is aimed at, and the special conditions that certain pressure and temperature are needed on the surface during the hot-pressing manufacture of the plate, the application of a plastic spraying process is provided, wherein the method comprises the steps of cleaning the surface of the aluminum plate 14, removing oil, washing with water, pickling with water, washing with water, adjusting the surface, phosphating, washing with water, heating, hot-blowing the surface of an aluminum skin, after hanging, generating negative high pressure by an electrostatic generator, adsorbing army green acrylic powder on the aluminum plate 14 by utilizing the corona discharge phenomenon, after electrostatic single-side spraying, entering an oven for melting, leveling and curing, opening the oven, taking out, the hot-press aluminum plate 14 used as a box cover 23 material comprises an upper layer of base plate and a lower layer of base plate, epoxy resin 15 is evenly sprayed between two layers of multi-layer plates 16, after the spraying is carried out for ten minutes, the multi-layer plates 16 subjected to electrostatic spraying are subjected to cold pressing and compounding at normal temperature by a high-pressure press for hours, the multi-layer plates 16 are arranged according to the size of an aviation box, the multi-layer plates 16 of the box body and the box cover 23 which are respectively combined by straight nails are firstly formed into two five-sided cuboid frames, the right angle positions of the box body and the box cover 23 are riveted by stainless steel rivets to be connected with two side surfaces of the box body or the box cover by right angle aluminum, four sides of the upper part of the box body are buckled by concave aluminum 8, four sides of the lower part of the box cover are buckled by convex openings, the box body and the box cover 23 are assembled in a trial way, the stainless steel rivets are used after completely, finally, polyurea double-component waterproof layers are sprayed inside the ball corners 5 of the eight ball corners 5 devices of the whole box body and the box cover 23, the bolt hole positions of the tail parts of the rivets, the inner corner parts of the box body and the box cover 23, the joints of the lock noses and the bottom of the box are mainly concerned, the coating is removed after multiple spraying, and the coating defect cannot be seen after the coating is sprayed again or multiple spraying. After the waterproof coating inside the aviation case is completely formed into a film, the EVA outer ring lining A21 or the return adhesive of the case body with different hardness, different color and special requirement is additionally arranged inside the case body case cover 23 according to the characteristic requirement of the product, the EVA outer ring lining A21 or the return adhesive of the case body with different thickness and different hardness is carved and milled according to the shape of the product, and the handle part of the case body is conveniently loaded or unloaded by carving and milling around the outline of the lining object. In order to realize the batched management of the articles in the box, the inner liner in the box can be additionally provided with an identifier, and the articles in the box are managed in batches while keeping secret; and in order to rapidly replace products in the box, the box inner lining is divided into two parts, namely a box EVA outer ring inner lining A21 and a box EVA outer ring inner lining B22, if the batch of products in the box needs to be replaced, only the box EVA outer ring inner lining A21 and the box EVA outer ring inner lining B22 of the box are replaced, so that the batch of military materials can be efficiently managed.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are only for convenience in describing and simplifying the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, e.g., as being fixed or detachable or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Claims (6)
1. The utility model provides an aviation case, includes box EVA outer lane inside lining B case lid (22), case lid (23), aluminum plate (14) and concave type mouth aluminium (8), its characterized in that: the outer side cover of box EVA outer lane inside lining B case lid (22) is equipped with box EVA outer lane inside lining A (21), the inside intermediate position department of box EVA outer lane inside lining B case lid (22) is provided with dashpot A (12), the inside one side of box EVA outer lane inside lining B case lid (22) is provided with dashpot A (11), case lid (23) and box EVA outer lane inside lining B case lid (22) looks adaptation, the inside of concave type mouth aluminium (8) is provided with connecting plate (2), the both sides of concave type mouth aluminium (8) bottom are provided with articulated strip (1) and articulated strip (1) keep away from the one end of concave type mouth aluminium (8) and hinge with connecting plate (2) mutually, the both sides at concave type mouth aluminium (8) top articulate and support hinge (9), the top of concave type mouth aluminium (8) is provided with convex type mouth aluminium (7), and supports hinge (9) and keep away from the one end of concave type mouth aluminium (8) and hinge with protruding type mouth aluminium (7) mutually, the four corners department in the outside of concave type mouth aluminium (8) is provided with cornerite (6), the both sides of convex type mouth aluminium (7) are articulated to have ball angle (5), the one end of aluminum plate (14) is provided with epoxy (15), the one end that aluminum plate (14) were kept away from in epoxy (15) is provided with multiply wood (16).
2. An aviation case according to claim 1, wherein: the buffer groove A (12) is formed by a convex structure.
3. An aviation case according to claim 1, wherein: and clamping blocks are arranged on two sides of the bottom of the box cover (23).
4. An aviation case according to claim 1, wherein: the four corners of the bottom of the concave aluminum (8) are provided with universal wheels.
5. An aviation case according to claim 1, wherein: the number of the spherical angles (5) is multiple groups.
6. An aviation case according to claim 1, wherein: the wrap angle (6) is formed by a V-shaped structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110196375.XA CN112660633A (en) | 2021-02-22 | 2021-02-22 | Aviation case |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110196375.XA CN112660633A (en) | 2021-02-22 | 2021-02-22 | Aviation case |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112660633A true CN112660633A (en) | 2021-04-16 |
Family
ID=75399485
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110196375.XA Pending CN112660633A (en) | 2021-02-22 | 2021-02-22 | Aviation case |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112660633A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH275042A (en) * | 1947-07-22 | 1951-04-30 | Dauphin Andre Lucien | Container for transport, of the so-called "container" type. |
| CN203445940U (en) * | 2013-07-31 | 2014-02-19 | 北京神舟航天软件技术有限公司 | Portable multimedia aviation communication box |
| CN206969240U (en) * | 2017-04-26 | 2018-02-06 | 贵州天义电器有限责任公司 | A kind of box for transporting material |
| CN207265487U (en) * | 2017-10-12 | 2018-04-20 | 深圳市泰明辉铝箱制品有限公司 | Full bevel edge aviation case |
| CN209889368U (en) * | 2019-05-20 | 2020-01-03 | 广州市华崴演出器材有限公司 | Follow spot lamp flight case that water-proof effects is good |
| CN111099144A (en) * | 2019-12-28 | 2020-05-05 | 东北轻合金有限责任公司 | Honeycomb aluminum plate aviation case and manufacturing method thereof |
-
2021
- 2021-02-22 CN CN202110196375.XA patent/CN112660633A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH275042A (en) * | 1947-07-22 | 1951-04-30 | Dauphin Andre Lucien | Container for transport, of the so-called "container" type. |
| CN203445940U (en) * | 2013-07-31 | 2014-02-19 | 北京神舟航天软件技术有限公司 | Portable multimedia aviation communication box |
| CN206969240U (en) * | 2017-04-26 | 2018-02-06 | 贵州天义电器有限责任公司 | A kind of box for transporting material |
| CN207265487U (en) * | 2017-10-12 | 2018-04-20 | 深圳市泰明辉铝箱制品有限公司 | Full bevel edge aviation case |
| CN209889368U (en) * | 2019-05-20 | 2020-01-03 | 广州市华崴演出器材有限公司 | Follow spot lamp flight case that water-proof effects is good |
| CN111099144A (en) * | 2019-12-28 | 2020-05-05 | 东北轻合金有限责任公司 | Honeycomb aluminum plate aviation case and manufacturing method thereof |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20210416 |