CN111099144A - Honeycomb aluminum plate aviation case and manufacturing method thereof - Google Patents
Honeycomb aluminum plate aviation case and manufacturing method thereof Download PDFInfo
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- CN111099144A CN111099144A CN201911385048.8A CN201911385048A CN111099144A CN 111099144 A CN111099144 A CN 111099144A CN 201911385048 A CN201911385048 A CN 201911385048A CN 111099144 A CN111099144 A CN 111099144A
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- box
- box body
- hinge
- case
- aluminum
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Classifications
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- 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
- B65D43/00—Lids or covers for rigid or semi-rigid containers
- B65D43/14—Non-removable lids or covers
- B65D43/16—Non-removable lids or covers hinged for upward or downward movement
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- 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
- B65D55/00—Accessories for container closures not otherwise provided for
- B65D55/02—Locking devices; Means for discouraging or indicating unauthorised opening or removal of closure
-
- 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
- B65D7/00—Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of metal
- B65D7/02—Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of metal characterised by shape
- B65D7/06—Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of metal characterised by shape of polygonal cross-section, e.g. tins, boxes
Abstract
A honeycomb aluminum plate aviation case and a manufacturing method thereof relate to the technical field of aviation transportation packaging. The problem that after the existing aviation case is used for a long time, the surface coating falls off, and the whole strength is reduced after moisture absorption and deformation, so that the aviation case cannot be used is solved. The both sides surface of box is equipped with a handle respectively, and the case lid passes through the hinge and is connected with one side hinge of box open end, and the opposite side edge of box open end is equipped with even buckle, and the buckle is used for locking case lid and box lid tightness, and box internal surface and case lid internal surface all are equipped with the crest sponge layer, and box lower surface four corners department is equipped with a supporting seat respectively, and case lid upper surface four corners department is equipped with a supporting seat respectively. The invention is suitable for manufacturing a honeycomb aluminum plate aviation case, and the product is suitable for transportation and packaging in the fields of electronic precision instruments, stage lighting equipment, medical instruments and equipment, audio-visual system multimedia, photoelectric industry, military industry equipment and the like.
Description
Technical Field
The invention relates to the technical field of air transportation packaging, in particular to a honeycomb aluminum plate aviation case and a manufacturing method thereof.
Background
The material that current aviation case adopted is that ABS fireproof plate makes, and this kind of aviation case advances the use back of overlength time, leads to the coating on surface to drop, and when using in moist environment, ABS fireproof plate can absorb moisture, leads to warping, and holistic structural strength reduces, can't use.
In conclusion, the existing aviation case has the problems that after the aviation case is used for a long time, the surface coating falls off, and the integral strength is reduced after the aviation case absorbs moisture and deforms, so that the aviation case cannot be used.
Disclosure of Invention
The invention provides a aviation case based on a honeycomb aluminum plate and a manufacturing method thereof, and aims to solve the problems that after the existing aviation case is used for a long time, a surface coating falls off, and the integral strength is reduced after moisture absorption and deformation, so that the aviation case cannot be used.
The invention relates to a honeycomb aluminum plate aviation case which comprises a supporting seat, a case cover, a buckle, a handle, a wave crest sponge layer, a hinge and a case body, wherein the case cover is fixedly connected with the supporting seat;
the outer surfaces of two sides of the box body are respectively provided with a handle, the box cover is hinged with one side of the opening end of the box body through a hinge, the edge of the other side of the opening end of the box body is provided with a buckle which is used for tightly locking the box cover and the box body, the inner surface of the box body and the inner surface of the box cover are respectively provided with a wave crest sponge layer, four corners of the lower surface of the box body are respectively provided with a supporting seat, and four corners of the upper surface of the box;
furthermore, the buckle, the handle and the hinge are made of white steel chromium-plated materials;
furthermore, the box cover and the hinge are connected in a riveting mode;
furthermore, the box body and the box cover are both made of 5-series high-magnesium alloy aluminum honeycomb plates;
further, the outer surface of the box body is coated with a layer of anticorrosive paint;
furthermore, the anticorrosive paint surface on the outer surface of the box body adopts fluorocarbon or electrostatic powder;
further, aluminum alloy section bars are arranged at the outer corners of the box body;
a method for manufacturing a honeycomb aluminum plate aviation case comprises the following specific steps:
firstly, processing a box body, wherein the box body adopts a stamping technology, and 5-series high-magnesium alloy aluminum honeycomb plates are placed into a stamping machine for rapid forming processing;
secondly, spraying paint on the surface of the processed box body, wherein the spraying paint adopts a fluorocarbon rolling coating or electrostatic powder spraying mode;
step three, adhering a 3-series aluminum oxide alloy section bar frame at the outer edge of the box body, and hinging the box body with a box cover through a hinge;
fourthly, handles are arranged on two sides of the box body, and supporting frames are arranged at four corners of the lower surface of the box body and connected in a riveting mode;
pasting the wave crest cotton layer into the box body and the box cover, and pasting the periphery and the bottom in the box body by using black foam cotton;
and step six, the pattern of the external panel of the box body is formed by uv spraying, and the pattern logo can be sprayed and printed according to the requirements of customers.
Compared with the prior art, the invention has the following beneficial effects:
firstly, the invention overcomes the defects of the prior art, the outer surface of the box body is coated with the anti-corrosion paint surface, and the anti-corrosion paint surface adopts fluorocarbon or electrostatic powder, thereby effectively preventing the corrosion of the box body plates and avoiding the phenomenon that the surface coating falls off after the aviation case is transported and used for a long time.
The box body and the box cover are made of 5-series high-magnesium alloy aluminum honeycomb plates, so that the phenomenon of deformation caused by use in a humid environment is effectively prevented, and the integral structural strength is improved.
And thirdly, the invention is simple to use and convenient to operate.
Drawings
FIG. 1 is a front axle view of a cellular aluminum aircraft flight chamber according to the present invention
FIG. 2 is a rear isometric view of a honeycomb aluminum flight box according to the present invention;
FIG. 3 is a bottom view of a honeycomb aluminum flight box of the present invention;
FIG. 4 is a front view of a honeycomb aluminum flight box of the present invention;
FIG. 5 is a left side view of a honeycomb aluminum flight box of the present invention;
FIG. 6 is a rear view of a honeycomb aluminum flight box of the present invention;
the box comprises a supporting seat 1, a box cover 2, a buckle 3, a handle 4, a wave crest sponge layer 5, a hinge 6 and a box body 7.
Detailed Description
The first embodiment is as follows: the embodiment is described with reference to fig. 1 to 6, and the aluminum honeycomb plate flight chamber in the embodiment comprises a supporting seat 1, a chamber cover 2, a buckle 3, a handle 4, a wave crest sponge layer 5, a hinge 6 and a chamber body 7;
the outer surfaces of two sides of the box body 7 are respectively provided with a handle 4, the box cover 2 is hinged with one side of the opening end of the box body 7 through a hinge 6, the edge of the other side of the opening end of the box body 7 is provided with a buckle 3, the buckle 3 is used for tightly and tightly covering and locking the box cover 2 and the box body 7, the inner surface of the box body 7 and the inner surface of the box cover 2 are respectively provided with a crest sponge layer 5, four corners of the lower surface of the box body 7 are respectively provided with a supporting seat 1, and four corners of the upper surface;
according to the specific embodiment, the outer surface of the box body is coated with the anti-corrosion paint, and the anti-corrosion paint is fluorocarbon or electrostatic powder, so that the corrosion of the box body plate is effectively prevented, and the phenomenon that the surface coating falls off after the aviation case is transported and used for a long time is avoided;
the honeycomb aviation case avoids the impact of heavy objects in the placing process, the buckle 3 is opened during use, the buckle 3 is locked after articles are loaded, and the aviation case is placed on the ground when placed, and the support frame 1 is forbidden to be suspended.
The second embodiment is as follows: the present embodiment will be described with reference to fig. 4, and is further limited to the aviation case according to the first embodiment, and in the aviation case of the aluminum honeycomb panel according to the present embodiment, the buckle 3, the handle 4 and the hinge 6 are all made of chrome-plated white steel.
The third concrete implementation mode: the present embodiment will be described with reference to fig. 1 and 5, and the present embodiment further defines the flight box according to the first embodiment, and the connection between the box cover 2 and the hinge 6 is formed by caulking.
The fourth concrete implementation mode: the present embodiment will be described with reference to fig. 1, and the present embodiment is a further limitation of the aviation case according to the first embodiment, and in the aviation case of the aluminum honeycomb plate according to the present embodiment, the case body 7 and the case cover 2 are both made of a 5-series high magnesium alloy aluminum honeycomb plate;
in the specific embodiment, the box body 7 and the box cover 2 both adopt 5-series high-magnesium alloy aluminum honeycomb plates, so that the phenomenon of deformation caused when the box is used in a humid environment is effectively prevented, and the integral structural strength is improved.
The fifth concrete implementation mode: the present embodiment is described with reference to fig. 1, and the present embodiment is a further limitation of the aviation case described in the fourth embodiment, in the aviation case made of a honeycomb aluminum plate described in the present embodiment, the outer surface of the case 7 is coated with a layer of anticorrosive paint;
this embodiment adopts 7 surfaces of box to scribble the anticorrosive lacquer painting of one deck, prevents that 7 surfaces of box from corroding, improves the life of aviation case.
The sixth specific implementation mode: the present embodiment is described with reference to fig. 1, and the present embodiment is a further limitation of the aviation case described in the fifth embodiment, in the aviation case made of a honeycomb aluminum plate according to the present embodiment, the anticorrosive paint surface on the outer surface of the case 7 is made of fluorocarbon or electrostatic powder;
this embodiment, the anticorrosive lacquer painting on box 7 surface adopts fluorine carbon or electrostatic powder, and the effectual box panel that prevents corrodes avoids the aviation case to transport the phenomenon that the back surface coating drops after using for a long time.
The seventh embodiment: the present embodiment will be described with reference to fig. 2, which is a further limitation of the aviation case according to the fifth embodiment, wherein in the aviation case of a honeycomb aluminum plate according to the present embodiment, aluminum alloy profiles are provided at the outer corners of the case 7;
this embodiment adopts 7 outer edges of box to be equipped with aluminium alloy type section bars, improves the holistic structural strength of box, improves the reliability.
The specific implementation mode is eight: the present embodiment will be described with reference to fig. 1 to 6, and a method for manufacturing a cellular aluminum plate flight box according to the present embodiment specifically includes the following steps:
step one, processing a box body 7, wherein the box body 7 adopts a stamping technology, and 5-series high-magnesium alloy aluminum honeycomb plates are placed into a stamping machine for rapid forming processing;
secondly, spraying paint on the surface of the processed box body 7 in a fluorocarbon rolling or electrostatic powder spraying mode;
step three, adhering a 3-series aluminum oxide alloy section bar frame at the outer edge of the box body 7, and hinging the box body 7 with the box cover 2 through a hinge 6;
fourthly, handles 4 are arranged on two sides of the box body 7, and supporting frames 1 are arranged at four corners of the lower surface of the box body 7 and connected in a riveting mode;
pasting the wave crest cotton layer into the box body 7 and the box cover 2, and pasting the periphery and the bottom in the box body by using black foam cotton;
and step six, the pattern of the outer panel of the box body 7 is formed by uv spraying, and the pattern logo can be sprayed and printed according to the requirements of customers.
Claims (8)
1. The utility model provides a honeycomb aluminum plate flight case which characterized in that: comprises a supporting seat (1), a box cover (2), a buckle (3), a handle (4), a wave crest sponge layer (5), a hinge (6) and a box body (7);
the both sides surface of box (7) is equipped with one handle (4) respectively, case lid (2) are connected with one side hinge of box (7) open end through hinge (6), the opposite side edge of box (7) open end is equipped with even buckle (3), buckle (3) are used for locking case lid (2) and box (7) lid tightly, box (7) internal surface and case lid (2) internal surface all are equipped with crest sponge layer (5), box (7) lower surface four corners department is equipped with one supporting seat (1) respectively, case lid (2) upper surface four corners department is equipped with one supporting seat (1) respectively.
2. The aluminum honeycomb panel flight chamber of claim 1, wherein: the buckle (3), the handle (4) and the hinge (6) are all made of white steel chromium-plated materials.
3. The aluminum honeycomb panel flight chamber of claim 1, wherein: the box cover (2) and the hinge (6) are connected in a riveting mode.
4. The aluminum honeycomb panel flight chamber of claim 1, wherein: the box body (7) and the box cover (2) both adopt 5-series high-magnesium alloy aluminum honeycomb plates.
5. A cellular aluminium aircraft flight box according to claim 4, wherein: the outer surface of the box body (7) is coated with a layer of anticorrosive paint.
6. The aluminum honeycomb panel flight box of claim 5, wherein: the anticorrosive paint surface on the outer surface of the box body (7) adopts fluorocarbon or electrostatic powder.
7. The aluminum honeycomb panel flight box of claim 6, wherein: and aluminum alloy profiles are arranged at the outer corners of the box body (7).
8. The method for manufacturing the cellular aluminum plate aviation case according to claim 1, wherein the method comprises the following steps: the specific method comprises the following steps:
step one, processing a box body (7), wherein the box body (7) adopts a stamping technology, and 5-series high-magnesium alloy aluminum honeycomb plates are placed into a stamping machine for rapid forming processing;
secondly, spraying paint on the surface of the processed box body (7), wherein the spraying paint adopts a fluorocarbon rolling coating or electrostatic powder spraying mode;
step three, adhering a 3-series aluminum oxide alloy section bar frame at the outer edge of the box body (7), and hinging the box body (7) with the box cover (2) through a hinge (6);
fourthly, handles (4) are arranged on two sides of the box body (7), and supporting frames 1 are arranged at four corners of the lower surface of the box body (7) and connected in a riveting mode;
pasting the wave crest cotton layer into the box body (7) and the box cover (2), and pasting the black foam cotton on the periphery and the bottom in the box body;
and step six, the pattern of the outer panel of the box body (7) is formed by uv spraying.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911385048.8A CN111099144A (en) | 2019-12-28 | 2019-12-28 | Honeycomb aluminum plate aviation case and manufacturing method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911385048.8A CN111099144A (en) | 2019-12-28 | 2019-12-28 | Honeycomb aluminum plate aviation case and manufacturing method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111099144A true CN111099144A (en) | 2020-05-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911385048.8A Pending CN111099144A (en) | 2019-12-28 | 2019-12-28 | Honeycomb aluminum plate aviation case and manufacturing method thereof |
Country Status (1)
| Country | Link |
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| CN (1) | CN111099144A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112660633A (en) * | 2021-02-22 | 2021-04-16 | 解剑峰 | Aviation case |
| CN114392973A (en) * | 2022-01-21 | 2022-04-26 | 中国人民解放军空军研究院航空兵研究所 | A washing tank for rinsing aluminium honeycomb core |
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| EP2068324A2 (en) * | 2007-12-05 | 2009-06-10 | Global Nuclear Fuel-Americas, LLC | Industrial package having pressurization capability |
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2019
- 2019-12-28 CN CN201911385048.8A patent/CN111099144A/en active Pending
Patent Citations (6)
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| EP2068324A2 (en) * | 2007-12-05 | 2009-06-10 | Global Nuclear Fuel-Americas, LLC | Industrial package having pressurization capability |
| CN202608148U (en) * | 2012-05-04 | 2012-12-19 | 东莞市华轩幕墙材料有限公司 | Honeycomb aluminum panel |
| CN204802416U (en) * | 2015-04-10 | 2015-11-25 | 北京中科遥数信息技术有限公司 | Portable aviation case for transporting unmanned aerial vehicle equipment |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112660633A (en) * | 2021-02-22 | 2021-04-16 | 解剑峰 | Aviation case |
| CN114392973A (en) * | 2022-01-21 | 2022-04-26 | 中国人民解放军空军研究院航空兵研究所 | A washing tank for rinsing aluminium honeycomb core |
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Application publication date: 20200505 |