CN219155097U - Aircraft box with excellent compression resistance - Google Patents
Aircraft box with excellent compression resistance Download PDFInfo
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- CN219155097U CN219155097U CN202222540186.2U CN202222540186U CN219155097U CN 219155097 U CN219155097 U CN 219155097U CN 202222540186 U CN202222540186 U CN 202222540186U CN 219155097 U CN219155097 U CN 219155097U
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- limiting
- sliding
- box
- box body
- fixing plate
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model belongs to the technical field of aircraft boxes, and discloses an aircraft box with excellent compression resistance, which comprises: the box body, the upper end of box body is equipped with flip, be equipped with first fixed plate and second fixed plate in the box body, the utility model is through setting up two movable limiting plates, slip subassembly and first limiting subassembly etc. when needs are fixed according to the size of putting into the interior article of box, put into first fixed plate and second fixed plate between earlier, pull up the limiting block that shifts out in the spacing groove later, can adjust the interval between two limiting plates through the slider moving in the spout later, after adjusting the interval between two limiting plates according to the article, turn to the laminating on the second fixed plate again, then inlay the limiting block in the spacing groove, can conveniently fix the product of equidimension not, the problem that the article is easy to jolt in the packing carton and make the product damage in the transportation is solved.
Description
Technical Field
The utility model belongs to the technical field of aircraft boxes, and particularly relates to an aircraft box with excellent compression resistance.
Background
The aircraft box adopts the material of resistance to compression, and its compressive property is superior, even also can the resistance to compression fall under adverse circumstances, can effectively receive the wild delivery of express delivery, reduces the transportation damage, reduces high after-market cost, is applicable to the E-commerce and packs the delivery and use.
But the aircraft box on the present market has certain defect, and traditional aircraft box is when using, is inconvenient to fix it in the aircraft box according to the size of article to the article is easy jolt and makes the product damage in the packing carton in the in-process of transportation, and in addition, the sealed effect of traditional aircraft box is poor, and the flip at top drops easily, causes the inside article of aircraft box to drop.
Disclosure of Invention
The utility model aims to provide an airplane box with excellent compression resistance, which solves the problems that the traditional airplane box provided in the background art is inconvenient to fix in the airplane box according to the size of an article and has poor sealing effect, and a flip cover at the top is easy to fall off.
In order to achieve the above purpose, the present utility model provides the following technical solutions: an aircraft box having excellent compression resistance, comprising:
the box body is provided with a flip cover at the upper end, a first fixing plate and a second fixing plate are arranged in the box body, the first fixing plate and the second fixing plate are oppositely arranged at the bottom of the box body, and two movable limiting plates are arranged between the first fixing plate and the second fixing plate;
the sliding component is arranged in the first fixed plate and is used for realizing the movement of the limiting plate on the first fixed plate and the second fixed plate;
the first limiting assembly is used for limiting the limiting plate on the first fixing plate and the second fixing plate;
the second limiting component is arranged on one side of the upper end face of the box body and used for limiting after the flip cover is sealed on the box body.
Preferably, the sliding assembly comprises two sliding blocks and a sliding groove, the sliding groove is formed in the upper end face of the first fixing plate, the two sliding blocks are embedded into the sliding groove, and the upper end faces of the two sliding blocks are hinged to one end of one limiting plate.
Preferably, the first limiting component comprises a limiting groove and limiting blocks, the limiting grooves are formed in the second fixing plate at equal intervals, the limiting blocks are mounted at one ends, far away from the sliding blocks, of the limiting plates, and the limiting blocks are embedded into the limiting grooves.
Preferably, the second limiting component comprises a slot and an inserting block provided with a groove, the slot is formed in one side of the upper end face of the box body, the inserting block is arranged on one side of the lower end face of the flip cover, the inserting block is embedded into the slot, a third limiting component is arranged in the inserting block, and a moving component is arranged in the flip cover and located at one end, far away from the slot, of the inserting block.
Preferably, the third limiting assembly comprises a limiting hole, a limiting rod and a spring, wherein the limiting hole is formed in one side of the inner wall of the slot, the limiting hole is communicated with the slot, one end of the limiting rod is embedded into the limiting hole, the other end of the limiting rod is embedded into the inserting block, and the spring is installed inside the inserting block.
Preferably, the movable component is a sliding rod, a through groove is formed in one end of the flip cover, which is close to the inserting block, the through groove is communicated with a groove in the inserting block, a supporting plate is arranged in the through groove, one end of the sliding rod penetrates through a slideway in the supporting plate and is embedded into the inserting block, one side of one end of the sliding rod embedded into the inserting block is connected with one end of the limiting rod, which is far away from the limiting hole, and the other side of one end of the sliding rod embedded into the inserting block is connected with one end of the spring.
Compared with the prior art, the utility model has the beneficial effects that:
(1) According to the utility model, by arranging the two movable limiting plates, the sliding assembly, the first limiting assembly and the like, when the article is required to be fixed according to the size of the article placed in the box body, the article is placed between the first fixing plate and the second fixing plate, then the limiting plates are pulled upwards to move out of the limiting blocks in the limiting grooves, then the distance between the two limiting plates can be adjusted by moving the sliding blocks in the sliding grooves, after the distance between the two limiting plates is adjusted according to the article, the limiting plates are turned to be attached to the second fixing plate, and then the limiting blocks are embedded into the limiting grooves, so that the article can be conveniently fixed in the box body according to the different sizes of the article, and the problem that the article is easy to bump in the packaging box in the transportation process to damage the article is solved.
(2) According to the utility model, the second limiting assembly, the third limiting assembly and the moving assembly are arranged, when the aircraft box is used, the sliding rod is firstly moved towards one end of the connecting spring on the supporting plate, the limiting rod can be moved into the inserting block, then the flip cover is covered on the box body, then the inserting block is embedded into the slot, then the sliding rod is loosened, and the limiting rod connected to the other end of the sliding rod is embedded into the limiting hole through the elasticity of the spring to carry out sealing and limiting, so that the problems that the sealing effect of the traditional aircraft box is poor, the flip cover at the top is easy to fall off, and articles in the aircraft box fall off are solved.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of the structure of the flip cover of the present utility model;
FIG. 3 is a top view of the support plate of the present utility model;
FIG. 4 is a schematic structural view of a first spacing assembly according to the present utility model;
in the figure: 1. a case body; 2. a first fixing plate; 3. a chute; 4. a slide block; 5. a limiting plate; 6. a second fixing plate; 7. a limit groove; 8. a limiting block; 9. a slot; 10. a flip cover; 11. inserting blocks; 12. a through groove; 13. a support plate; 14. a slide bar; 15. a spring; 16. a limit rod; 17. and a limiting hole.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, the present utility model provides the following technical solutions: an aircraft box having excellent compression resistance, comprising:
the box body 1, the upper end of the box body 1 is provided with a flip cover 10, a first fixed plate 2 and a second fixed plate 6 are arranged in the box body 1, the first fixed plate 2 and the second fixed plate 6 are oppositely arranged at the bottom of the box body 1, and two movable limiting plates 5 are arranged between the first fixed plate 2 and the second fixed plate 6;
the sliding component is arranged in the first fixed plate 2 and is used for realizing the movement of the limiting plate 5 on the first fixed plate 2 and the second fixed plate 6;
the first limiting assembly is used for limiting the limiting plate 5 on the first fixing plate 2 and the second fixing plate 6;
the second limiting component is arranged on one side of the upper end face of the box body 1 and is used for limiting after the flip cover 10 is sealed on the box body 1.
Referring to fig. 1 and 4, the sliding assembly includes two sliding blocks 4 and a sliding groove 3, the sliding groove 3 is formed on an upper end surface of the first fixing plate 2, the two sliding blocks 4 are embedded into the sliding groove 3, and the upper end surfaces of the two sliding blocks 4 are hinged with one end of a limiting plate 5.
The first limiting component comprises a limiting groove 7 and limiting blocks 8, the limiting grooves 7 are formed in the second fixing plate 6 at equal intervals, the limiting blocks 8 are arranged at one ends, far away from the sliding blocks 4, of the limiting plates 5, and the limiting blocks 8 are embedded into the limiting grooves 7.
Through the technical scheme: when the size of the article placed in the box body 1 is required to be fixed, the article is placed between the first fixed plate 2 and the second fixed plate 6, then the limiting plate 5 is pulled upwards to move the limiting block 8 in the limiting groove 7 out, then the spacing between the two limiting plates 5 can be adjusted by moving the sliding block 4 in the sliding groove 3, after the spacing between the two limiting plates 5 is adjusted according to the article, the limiting plate 5 is turned to be attached to the second fixed plate 6, and then the limiting block 8 is embedded into the limiting groove 7, so that the article can be conveniently fixed in the box body 1 according to different sizes of the article, and the problem that the article is easy to jolt in the packaging box in the transportation process to damage the product is solved.
Referring to fig. 1-3, the second limiting component includes a slot 9 and an insert 11 with a groove, the slot 9 is opened on one side of the upper end surface of the box 1, the insert 11 is installed on one side of the lower end surface of the flip 10, the insert 11 is embedded into the slot 9, a third limiting component is disposed in the insert 11, and a moving component is disposed in the flip 10 and at one end of the insert 11 far from the slot 9.
The third spacing subassembly includes spacing hole 17, gag lever post 16 and spring 15, and spacing hole 17 is seted up in the inner wall one side of slot 9, and spacing hole 17 link up mutually with slot 9, and in the one end embedding of gag lever post 16 was to spacing hole 17, the other end of gag lever post 16 was inlayed to in the inserted block 11, and spring 15 installs inside the inserted block 11.
The movable component is a slide bar 14, one end of the flip cover 10, which is close to the insert block 11, is provided with a through groove 12, the through groove 12 is communicated with a groove on the insert block 11, a supporting plate 13 is arranged in the through groove 12, one end of the slide bar 14 penetrates through a slide way in the supporting plate 13 and is embedded into the insert block 11, one side of the slide bar 14 embedded into the insert block 11 is connected with one end of a limiting rod 16, which is far away from a limiting hole 17, and the other side of the slide bar 14 embedded into the insert block 11 is connected with one end of a spring 15
Through the technical scheme: when the aircraft box is used, firstly, the slide bar 14 moves towards one end of the connecting spring 15 on the supporting plate 13, the limiting rod 16 can be moved into the inserting block 11, then the flip cover 10 is covered on the box body 1, then the inserting block 11 is embedded into the inserting groove 9, then the slide bar 14 is loosened, the limiting rod 16 connected with the other end of the slide bar 14 is embedded into the limiting hole 17 through the elasticity of the spring 15 for sealing and limiting, and the problems that the sealing effect of a traditional aircraft box is poor, the flip cover 10 at the top is easy to fall off, and articles in the aircraft box fall off are solved.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. An aircraft box having excellent compression resistance, comprising:
the novel box comprises a box body (1), wherein a flip cover (10) is arranged at the upper end of the box body (1), a first fixing plate (2) and a second fixing plate (6) are arranged in the box body (1), the first fixing plate (2) and the second fixing plate (6) are oppositely arranged at the bottom of the box body (1), and two movable limiting plates (5) are arranged between the first fixing plate (2) and the second fixing plate (6);
the sliding component is arranged in the first fixed plate (2) and is used for realizing the movement of the limiting plate (5) on the first fixed plate (2) and the second fixed plate (6);
the first limiting assembly is used for limiting the limiting plate (5) on the first fixing plate (2) and the second fixing plate (6);
the second limiting component is arranged on one side of the upper end face of the box body (1) and used for limiting after the flip cover (10) is sealed on the box body (1).
2. An aircraft box with excellent compression resistance according to claim 1, wherein: the sliding assembly comprises two sliding blocks (4) and a sliding groove (3), wherein the sliding groove (3) is formed in the upper end face of the first fixing plate (2), the two sliding blocks (4) are embedded into the sliding groove (3), and the upper end faces of the two sliding blocks (4) are hinged to one end of a limiting plate (5).
3. An aircraft box with excellent compression resistance according to claim 2, characterized in that: the first limiting component comprises limiting grooves (7) and limiting blocks (8), the limiting grooves (7) are formed in the second fixing plate (6) at equal intervals, the limiting blocks (8) are arranged at one ends, far away from the sliding blocks (4), of the limiting plates (5), and the limiting blocks (8) are embedded into the limiting grooves (7).
4. An aircraft box with excellent compression resistance according to claim 3, wherein: the second limiting component comprises a slot (9) and an inserting block (11) with a groove, the slot (9) is formed in one side of the upper end face of the box body (1), the inserting block (11) is arranged on one side of the lower end face of the flip (10), the inserting block (11) is embedded into the slot (9), a third limiting component is arranged in the inserting block (11), and a moving component is arranged in the flip (10) and located at one end, far away from the slot (9), of the inserting block (11).
5. An aircraft box with excellent compression resistance according to claim 4, wherein: the third limiting assembly comprises a limiting hole (17), a limiting rod (16) and a spring (15), wherein the limiting hole (17) is formed in one side of the inner wall of the slot (9), the limiting hole (17) is communicated with the slot (9), one end of the limiting rod (16) is embedded into the limiting hole (17), the other end of the limiting rod (16) is embedded into the inserting block (11), and the spring (15) is arranged inside the inserting block (11).
6. An aircraft box with excellent compression resistance according to claim 5, wherein: the movable assembly is a sliding rod (14), a through groove (12) is formed in one end, close to the plug block (11), of the flip (10), the through groove (12) is communicated with a groove in the plug block (11), a supporting plate (13) is arranged in the through groove (12), one end of the sliding rod (14) penetrates through a sliding way in the supporting plate (13) and is embedded into the plug block (11), one side, embedded into the plug block (11), of the sliding rod (14) is connected with one end, far away from a limiting hole (17), of a limiting rod (16), and the other side, embedded into the plug block (11), of the sliding rod (14) is connected with one end of a spring (15).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222540186.2U CN219155097U (en) | 2022-09-26 | 2022-09-26 | Aircraft box with excellent compression resistance |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222540186.2U CN219155097U (en) | 2022-09-26 | 2022-09-26 | Aircraft box with excellent compression resistance |
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Publication Number | Publication Date |
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CN219155097U true CN219155097U (en) | 2023-06-09 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202222540186.2U Active CN219155097U (en) | 2022-09-26 | 2022-09-26 | Aircraft box with excellent compression resistance |
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CN (1) | CN219155097U (en) |
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2022
- 2022-09-26 CN CN202222540186.2U patent/CN219155097U/en active Active
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