CN113525878A - Aviation case stable in structure, protect function is strong - Google Patents
Aviation case stable in structure, protect function is strong Download PDFInfo
- Publication number
- CN113525878A CN113525878A CN202110888283.8A CN202110888283A CN113525878A CN 113525878 A CN113525878 A CN 113525878A CN 202110888283 A CN202110888283 A CN 202110888283A CN 113525878 A CN113525878 A CN 113525878A
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- column
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- built
- protection function
- strong
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- 239000006260 foam Substances 0.000 claims abstract description 14
- 230000003014 reinforcing effect Effects 0.000 claims description 23
- 238000009434 installation Methods 0.000 claims description 16
- 238000013016 damping Methods 0.000 claims description 11
- 230000001681 protective effect Effects 0.000 claims description 7
- 238000005192 partition Methods 0.000 claims description 6
- 239000000853 adhesive Substances 0.000 claims description 2
- 230000001070 adhesive effect Effects 0.000 claims description 2
- 238000013461 design Methods 0.000 abstract description 22
- 230000000694 effects Effects 0.000 abstract description 7
- 239000000463 material Substances 0.000 abstract description 4
- 230000035939 shock Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 4
- 210000005056 cell body Anatomy 0.000 description 3
- 230000007547 defect Effects 0.000 description 3
- 230000003993 interaction Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 230000002787 reinforcement Effects 0.000 description 3
- HUAUNKAZQWMVFY-UHFFFAOYSA-M sodium;oxocalcium;hydroxide Chemical compound [OH-].[Na+].[Ca]=O HUAUNKAZQWMVFY-UHFFFAOYSA-M 0.000 description 3
- 229910001294 Reinforcing steel Inorganic materials 0.000 description 2
- 239000002274 desiccant Substances 0.000 description 2
- 238000004806 packaging method and process Methods 0.000 description 2
- 206010066054 Dysmorphism Diseases 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
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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
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/02—Internal fittings
-
- 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
- B65D21/00—Nestable, stackable or joinable containers; Containers of variable capacity
- B65D21/08—Containers of variable capacity
- B65D21/086—Collapsible or telescopic containers
-
- 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
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/02—Internal fittings
- B65D25/04—Partitions
-
- 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
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/02—Internal fittings
- B65D25/10—Devices to locate articles in containers
-
- 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
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/02—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
- B65D81/05—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
-
- 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
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/02—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
- B65D81/05—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
- B65D81/051—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents using pillow-like elements filled with cushioning material, e.g. elastic foam, fabric
- B65D81/052—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents using pillow-like elements filled with cushioning material, e.g. elastic foam, fabric filled with fluid, e.g. inflatable elements
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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
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/18—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents providing specific environment for contents, e.g. temperature above or below ambient
-
- 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
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/24—Adaptations for preventing deterioration or decay of contents; Applications to the container or packaging material of food preservatives, fungicides, pesticides or animal repellants
- B65D81/26—Adaptations for preventing deterioration or decay of contents; Applications to the container or packaging material of food preservatives, fungicides, pesticides or animal repellants with provision for draining away, or absorbing, or removing by ventilation, fluids, e.g. exuded by contents; Applications of corrosion inhibitors or desiccators
- B65D81/266—Adaptations for preventing deterioration or decay of contents; Applications to the container or packaging material of food preservatives, fungicides, pesticides or animal repellants with provision for draining away, or absorbing, or removing by ventilation, fluids, e.g. exuded by contents; Applications of corrosion inhibitors or desiccators for absorbing gases, e.g. oxygen absorbers or desiccants
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Food Science & Technology (AREA)
- Buffer Packaging (AREA)
Abstract
The invention discloses an aviation case with stable structure and strong protection function, and relates to the technical field of aviation cases, in particular to a case body and an outer sheath column. This stable in structure, air tank that protect function is strong, the design of support column can carry out nimble adjustment spacing according to the shape of article, effectively reduces the use limitation, and the design of the inside foam post of support column and rubber pad can be more stable when spacing article, can not lose article simultaneously and have good shock attenuation effect to material quality between the aforesaid is lighter, can not increase the weight of whole box, person of facilitating the use's use.
Description
Technical Field
The invention relates to the technical field of flight boxes, in particular to a flight box with a stable structure and a strong protection function.
Background
The traditional simple wooden box packaging and transporting can not solve the defects that the high-tech products can not be effectively protected in the long-distance transportation process and have poor maneuverability, and a new packaging product, namely the aviation box, which replaces the transportation is generated aiming at the defect. The use and development of the aviation case step into the gold stage by the increasingly frequent transnational trade, and the aviation case is widely applied to the fields of high-tech equipment such as stage lighting equipment, medical instrument equipment, audio-visual system multimedia, photoelectric industry, military transportation package, military equipment transportation and the like.
The shape of placing article is inconvenient according to needs to carry out nimble spacing in the use of current aviation case to and at spacing in-process protection degree is not good, and inconvenient problem of addding accommodation area according to the use needs.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides the aviation case with stable structure and strong protection function, and solves the problems that the existing aviation case is inconvenient to flexibly limit the position according to the shape of an object to be placed in the using process, the protection degree is poor in the limiting process, and the accommodating area is inconvenient to be increased according to the using requirement in the background technology.
In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides a stable in structure, air box that protect function is strong, includes box and oversheath post, the inside of box is provided with built-in chamber, and all installs the baffle at the both ends of built-in intracavity portion, the outside one end of baffle is provided with the installation cell body, and the internally mounted of installation cell body has the support column, the inner wall in built-in chamber is provided with auxiliary assembly, the damping hinge is installed to the outside right-hand member of box, and the outside one end of damping hinge is provided with the door plant, the externally mounted of bottom half has the end frame, and the inside both ends of end frame all are provided with built-in groove, the internally mounted of built-in groove has hydraulic pressure gas pole, and the outside at the top of hydraulic pressure gas pole is provided with the switching piece, the internally mounted of end frame has built-in backplate, the oversheath post is located the outside one end of built-in backplate.
Optionally, an installation plate is arranged at the top inside the outer sheath column, a middle-placed column is arranged in the middle inside the outer sheath column, and a protection belt is arranged outside the bottom of the middle-placed column.
Optionally, the outer portion of the protective band is connected with the outer sheath column in an adhesive manner, two outer sheath columns are arranged, and the outer portion of each outer sheath column is movably connected with the middle-placed column.
Optionally, the inside of support column is provided with the rubber pad, and the foam post is installed to the outside one end of rubber pad, the outside middle part in support column bottom is provided with the fixture block, and the externally mounted of fixture block bottom has supplementary frame.
Optionally, the support columns are distributed equidistantly, the insides of the support columns are tightly attached to the rubber pads, and the insides of the rubber pads are fixedly connected with the foam columns.
Optionally, the inside of auxiliary frame is provided with the adjustment subassembly, and the adjustment subassembly includes draw-in groove, buffer board, mounting groove and activity chamber, the external surface of draw-in groove is provided with the buffer board, and the externally mounted of buffer board bottom has the mounting groove, the inside of mounting groove is provided with the activity chamber.
Optionally, the inside of the movable cavity is of a hollow structure, the outside of the movable cavity is movably connected with the mounting groove, and the outside of the mounting groove and the auxiliary frame are of an integrated structure.
Optionally, the inside of the clamping groove is connected with the clamping block in a clamping manner, and the clamping block and the supporting column are of an integrated structure.
Optionally, the auxiliary assembly includes an auxiliary plate, a reinforcing column and an air bag, the reinforcing column is arranged inside the auxiliary plate, and the air bag is mounted outside the reinforcing column.
Optionally, the number of the auxiliary plates is four, the inner portions of the auxiliary plates are welded to the reinforcing columns, and the outer portions of the reinforcing columns are tightly attached to the air bags.
The invention provides an aviation case with stable structure and strong protection function, which has the following beneficial effects:
can carry out spacing fixed processing to it according to the shape of article in the use, be convenient for use some dysmorphism article, simple structure, convenient to use person controls, and can carry out dampproofing the processing to the article of placing, can cushion the protection around the outside simultaneously to can expand today to current area of holding according to the use needs.
1. The aviation case with the stable structure and the strong protection function can utilize the interaction of the hydraulic air rod and the switching block to move the height of the case up and down, so that when the use space of the aviation case is not required to be increased, the whole case can be accommodated into the bottom frame under the action of the hydraulic air rod and the switching block, the design of the bottom frame can be utilized to play a preliminary protection role, the design of the hydraulic air rod and the switching block can be reused to enable the case to move out of the bottom frame when the use area is insufficient, and the inner area of the bottom frame can be used;
2. according to the aviation case with the stable structure and the strong protection function, the outer sheath columns are arranged in the bottom frame at equal intervals, the outer sheath columns are connected with the case body and the bottom frame through the mounting plate and the screws, the outer sheath columns and the middle post can move relatively in the protection belt when the hydraulic air rod moves up and down, the outer sheath columns can be disassembled according to the shape and size of an article due to the design of the positions and the number of the outer sheath columns, the region which is not needed to be used is reserved, and the article can be limited by the design of the outer sheath columns;
3. according to the aviation case with the stable structure and the strong protection function, the design of the supporting column can be flexibly adjusted and limited according to the shape of an article, the use limitation is effectively reduced, the design of the foam column and the rubber pad inside the supporting column can be more stable when the article is limited, meanwhile, the article is not lost, the good damping effect is achieved, the material quality of the foam column and the rubber pad is light, the weight of the whole case body is not increased, and the aviation case is convenient for a user to use;
4. the aviation case is stable in structure and strong in protection function, when an article is limited, the whole supporting column is clamped and connected with the clamping groove in the auxiliary frame, so that the supporting column can be pulled outwards according to the shape of the article to enable the supporting column to be separated from the clamping groove, space and area are provided for placing the article, the auxiliary frame can be designed to fill and level the installation groove body of the region where the article needs to be placed, the article is placed more stably, the auxiliary frame enables the movable cavity region in the adjusting assembly to be in contact with the article when the installation groove body is filled, and the desiccant soda lime stored in the movable cavity can appropriately perform moisture-proof treatment on the article;
5. this air box stable in structure, protect function are strong utilizes the reinforcement column to be a reinforcing bar and links together with the accessory plate, has good firm performance, can not produce the deformation easily when receiving the collision to be provided with the gasbag that fills into certain gas inside in the outside of reinforcement column, can cushion the power when receiving the striking, reduce the damage that local pressure brought.
Drawings
FIG. 1 is a schematic top view of the present invention;
FIG. 2 is a schematic view of the distribution structure of the foam pillars and the auxiliary frames according to the present invention;
FIG. 3 is a schematic view of the inner structure of the auxiliary frame according to the present invention;
FIG. 4 is a schematic side view of the internal partial connection structure of the present invention;
fig. 5 is a schematic view of the connection structure of the outer sheath column according to the present invention.
In the figure: 1. a box body; 2. a cavity is arranged inside; 3. an auxiliary component; 301. an auxiliary plate; 302. reinforcing columns; 303. an air bag; 4. a partition plate; 5. installing a groove body; 6. a support pillar; 7. a damping hinge; 8. a door panel; 9. a foam column; 10. a rubber pad; 11. a clamping block; 12. an auxiliary frame; 13. an adjustment assembly; 1301. a card slot; 1302. a buffer plate; 1303. mounting grooves; 1304. a movable cavity; 14. a bottom frame; 15. a guard plate is arranged inside; 16. a hydraulic gas lever; 17. a built-in groove; 18. a transfer block; 19. an outer jacket post; 20. mounting a plate; 21. a middle post; 22. a protective band.
Detailed Description
Referring to fig. 1 to 5, the present invention provides a technical solution: an aviation case with stable structure and strong protection function comprises a case body 1, a built-in cavity 2, an auxiliary assembly 3, an auxiliary plate 301, a reinforcing column 302, an air bag 303, a partition plate 4, an installation groove body 5, a support column 6, a damping hinge 7, a door plate 8, a foam column 9, a rubber gasket 10, a fixture block 11, an auxiliary frame 12, an adjusting assembly 13, a clamping groove 1301, a buffer plate 1302, an installation groove 1303, a movable cavity 1304, a bottom frame 14, a built-in protective plate 15, a hydraulic air rod 16, a built-in groove 17, a switching block 18, an outer sheath column 19, an installation plate 20, a built-in column 21 and a protective belt 22, wherein the built-in cavity 2 is arranged inside the case body 1, the partition plate 4 is respectively installed at two ends inside the built-in cavity 2, the installation groove body 5 is arranged at one end outside the partition plate 4, the support columns 6 are installed inside the installation groove body 5, the support columns 6 are distributed at equal intervals, and the inside of the support columns 6 is tightly attached to the rubber gasket 10, the inside of the rubber pad 10 is fixedly connected with the foam column 9, the rubber pad 10 is arranged inside the supporting column 6, the foam column 9 is arranged at one end of the outside of the rubber pad 10, the fixture block 11 is arranged in the middle of the outside of the bottom of the supporting column 6, the auxiliary frame 12 is arranged outside the bottom of the fixture block 11, the auxiliary assembly 3 is arranged on the inner wall of the built-in cavity 2, the damping hinge 7 is arranged at the right end of the outside of the box body 1, the door plate 8 is arranged at one end of the outside of the damping hinge 7, the bottom frame 14 is arranged outside the bottom of the box body 1, the built-in grooves 17 are arranged at two ends inside the bottom frame 14, the hydraulic air rod 16 is arranged inside the built-in grooves 17, the adapter block 18 is arranged outside the top of the hydraulic air rod 16, the built-in guard plate 15 is arranged inside the bottom frame 14, the outer sheath column 19 is arranged at one end of the outside of the built-in guard plate 15, and the mounting plate 20 is arranged on the top inside the outer sheath column 19, a middle-placed column 21 is arranged in the middle of the inner part of the outer sheath column 19, and a protective belt 22 is arranged outside the bottom of the middle-placed column 21;
the operation is that firstly the door panel 8 can be opened and closed by the damping hinge 7, the height of the box body 1 can be moved up and down by the interaction of the hydraulic air rod 16 and the adapter block 18, so that when the use space of the aviation box is not required to be increased, the whole box body 1 can be accommodated into the bottom frame 14 by the action of the hydraulic air rod 16 and the adapter block 18, the design of the bottom frame 14 can be used for preliminary protection, when the use area is insufficient, the box body 1 can be moved out from the inside of the bottom frame 14 by the design of the hydraulic air rod 16 and the adapter block 18, so that the inner area of the bottom frame 14 can be used, the outer sheath columns 19 are equidistantly arranged in the bottom frame 14, the outer sheath columns 19 are connected with the box body 1 and the bottom frame 14 by the mounting plates 20 and the screws, and when the hydraulic air rod 16 moves up and down, the outer sheath columns 19 and the adapter block 21 can move relatively in the inner part of the protective belt 22, the design of 19 positions of oversheath post and quantity can be in need dismantling oversheath post 19 according to the shape size of article, the region that does not need to use remains, usable oversheath post 19's design is spacing to article, and the design of support column 6 can carry out nimble adjustment spacing according to the shape of article, effectively reduce the use limitation, and the design of 6 inside foam columns 9 of support column and rubber pad 10 can be more stable when spacing article are carried out, article can not be lost simultaneously and good shock attenuation effect has, and above-mentioned material quality between them is lighter, can not increase whole box 1's weight, the use of person of facilitating the use.
As shown in fig. 1, 2 and 3, an adjusting assembly 13 is disposed inside the auxiliary frame 12, and the adjusting assembly 13 includes a card slot 1301, a buffer board 1302, a mounting groove 1303 and a movable cavity 1304, the buffer board 1302 is disposed on an outer surface of the card slot 1301, the mounting groove 1303 is mounted on an outer portion of a bottom of the buffer board 1302, the movable cavity 1304 is disposed inside the mounting groove 1303, the movable cavity 1304 is of a hollow structure, the outer portion of the movable cavity 1304 is movably connected with the mounting groove 1303, the outer portion of the mounting groove 1303 is integrated with the auxiliary frame 12, the inner portion of the card slot 1301 is connected with the card block 11, and the card block 11 is integrated with the support post 6;
when article are limited, the whole supporting column 6 is connected with the clamping groove 1301 in the auxiliary frame 12 in a clamping manner, the supporting column 6 can be pulled outwards according to the shape of the article to enable the supporting column 6 and the clamping groove 1301 to be separated, space and area are provided for placing the article, the installation groove body 5 in the region where the article needs to be placed can be filled and leveled by the aid of the design of the auxiliary frame 12, the article can be placed more stably, the auxiliary frame 12 enables the movable cavity 1304 region in the adjusting assembly 13 to be in contact with the article when the installation groove body 5 is filled, and the desiccant soda lime stored in the movable cavity 1304 can be used for carrying out proper moisture-proof treatment on the article.
As shown in fig. 1, the auxiliary assembly 3 includes an auxiliary plate 301, four reinforcing columns 302 and four air bags 303, the reinforcing columns 302 are arranged inside the auxiliary plate 301, the air bags 303 are mounted outside the reinforcing columns 302, the inner part of the auxiliary plate 301 is welded to the reinforcing columns 302, and the outer part of the reinforcing columns 302 is tightly attached to the air bags 303;
the reinforcing column 302 is a reinforcing steel bar and is connected with the auxiliary plate 301, the reinforcing steel bar has good firmness, deformation cannot easily occur when the reinforcing column 302 is collided, and the air bag 303 filled with certain gas is arranged outside the reinforcing column 302, so that force can be buffered when the reinforcing column is collided, and damage caused by local pressure is reduced.
In conclusion, when the aviation case with stable structure and strong protection function is used, firstly, the door panel 8 can be opened and closed by using the damping hinge 7, a user can place objects, and can move the height of the case body 1 up and down by using the interaction of the hydraulic air rod 16 and the adapter block 18, so that when the use space of the aviation case is not required to be increased, the whole case body 1 can be accommodated into the bottom frame 14 by the action of the hydraulic air rod 16 and the adapter block 18, a primary protection effect can be achieved by using the design of the bottom frame 14, when the use area is insufficient, the case body 1 can be moved out from the inside of the bottom frame 14 by using the design of the hydraulic air rod 16 and the adapter block 18, so that the inner area of the bottom frame 14 can be used, the outer sheath columns 19 are arranged in the bottom frame 14 at equal intervals, the outer sheath columns 19 are connected with the case body 1 and the bottom frame 14 by the mounting plate 20 and screws, and the hydraulic air rod 16 can move relatively in the protection belt 22 when moving up and down between the outer sheath column 19 and the middle column 21, the design of the position and the quantity of the outer sheath column 19 can be realized by disassembling the outer sheath column 19 according to the shape and the size of the object, the region which is not needed to be used is reserved, the object can be limited by the design of the outer sheath column 19, the design of the support column 6 can be flexibly adjusted and limited according to the shape of the object, the use limitation is effectively reduced, when the object is limited, the whole support column 6 is clamped and connected with the clamping groove 1301 in the auxiliary frame 12, so that the support column 6 can be pulled outwards according to the shape of the object to separate the support column 6 from the clamping groove 1301, space and area are provided for placing the object, and the design of the auxiliary frame 12 can be used for filling and leveling the installation groove body 5 of the region which needs to place the object, make article more steady when placing, and auxiliary frame 12 can make the regional article that contact with movable chamber 1304 in the adjustment subassembly 13 when filling in the level to installation cell body 5, can make the inside drier soda lime of depositing of movable chamber 1304 carry out appropriate dampproofing processing to article, the design of the inside foam column 9 of support column 6 and rubber pad 10 can be more stable when spacing article carry out simultaneously, can not lose article simultaneously and have good shock attenuation effect, and the material quality between the two is lighter, can not increase the weight of whole box 1, user's use of facilitating the use, it is a reinforcing bar and the accessory plate 301 links together to utilize the reinforcement post 302 at last, good fastness can have, can not produce the deformation easily when receiving the collision.
Claims (10)
1. The aviation case with stable structure and strong protection function is characterized by comprising a case body (1) and an outer sheath column (19), wherein a built-in cavity (2) is arranged inside the case body (1), partition plates (4) are respectively arranged at two ends inside the built-in cavity (2), an installation groove body (5) is arranged at one end outside each partition plate (4), a support column (6) is arranged inside each installation groove body (5), an auxiliary assembly (3) is arranged on the inner wall of the built-in cavity (2), a damping hinge (7) is arranged at the right end outside the case body (1), a door plate (8) is arranged at one end outside each damping hinge (7), a bottom frame (14) is arranged outside the bottom of the case body (1), built-in grooves (17) are respectively arranged at two ends inside the bottom frame (14), and a hydraulic air rod (16) is arranged inside each built-in groove (17), and the outside at the top of hydraulic pressure gas pole (16) is provided with switching block (18), the internally mounted of putting frame (14) at the bottom has built-in backplate (15), oversheath post (19) is located the outside one end of built-in backplate (15).
2. The airbox with stable structure and strong protection function according to claim 1, wherein a mounting plate (20) is arranged at the top of the inside of the outer sheath column (19), a middle column (21) is arranged in the middle of the inside of the outer sheath column (19), and a protection belt (22) is arranged outside the bottom of the middle column (21).
3. The airbox with stable structure and strong protection function according to claim 2, wherein the outer part of the protective belt (22) is connected with the outer sheath column (19) in an adhesive manner, two outer sheath columns (19) are provided, and the outer part of the outer sheath column (19) is movably connected with the middle column (21).
4. The airbox with stable structure and strong protection function as claimed in claim 1, wherein a rubber pad (10) is arranged inside the supporting column (6), a foam column (9) is installed at one end of the outer portion of the rubber pad (10), a clamping block (11) is arranged in the middle of the outer portion of the bottom of the supporting column (6), and an auxiliary frame (12) is installed at the outer portion of the bottom of the clamping block (11).
5. The airbox with stable structure and strong protection function as claimed in claim 4, wherein the supporting columns (6) are distributed equidistantly, the inner parts of the supporting columns (6) are tightly attached to the rubber pads (10), and the inner parts of the rubber pads (10) are fixedly connected with the foam columns (9).
6. The airbox with stable structure and strong protection function according to claim 4, characterized in that an adjusting component (13) is arranged inside the auxiliary frame (12), the adjusting component (13) comprises a clamping groove (1301), a buffer plate (1302), a mounting groove (1303) and a movable cavity (1304), the buffer plate (1302) is arranged on the outer surface of the clamping groove (1301), the mounting groove (1303) is mounted on the outer portion of the bottom of the buffer plate (1302), and the movable cavity (1304) is arranged inside the mounting groove (1303).
7. The airbox with stable structure and strong protection function according to claim 6, wherein the interior of the movable cavity (1304) is a hollow structure, the outer part of the movable cavity (1304) is movably connected with the mounting groove (1303), and the outer part of the mounting groove (1303) is in an integrated structure with the auxiliary frame (12).
8. The airbox with stable structure and strong protection function according to claim 6, characterized in that the inside of the slot (1301) is connected with the block (11) in a snap fit manner, and the block (11) is integrated with the support column (6).
9. A structurally stable, functionally strong aviation case according to claim 1 wherein said auxiliary assembly (3) comprises an auxiliary plate (301), a reinforcing post (302) and an air bag (303), and wherein the reinforcing post (302) is disposed inside the auxiliary plate (301) and the air bag (303) is mounted outside the reinforcing post (302).
10. A structurally stable, functionally strong flight box according to claim 9 wherein there are four auxiliary panels (301), and there are welded connections between the inner portions of the auxiliary panels (301) and the reinforcing columns (302), and the outer portions of the reinforcing columns (302) are tightly fitted to the air bags (303).
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CN202110888283.8A CN113525878A (en) | 2021-08-03 | 2021-08-03 | Aviation case stable in structure, protect function is strong |
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CN202110888283.8A CN113525878A (en) | 2021-08-03 | 2021-08-03 | Aviation case stable in structure, protect function is strong |
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