CN212125985U - Aviation case with layered structure - Google Patents
Aviation case with layered structure Download PDFInfo
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- CN212125985U CN212125985U CN202020563832.5U CN202020563832U CN212125985U CN 212125985 U CN212125985 U CN 212125985U CN 202020563832 U CN202020563832 U CN 202020563832U CN 212125985 U CN212125985 U CN 212125985U
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- aviation case
- case body
- aviation
- layered structure
- fixed mounting
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- 238000005192 partition Methods 0.000 claims description 27
- 238000005096 rolling process Methods 0.000 claims description 9
- 238000003780 insertion Methods 0.000 claims description 5
- 230000037431 insertion Effects 0.000 claims description 5
- 239000000463 material Substances 0.000 abstract description 7
- 230000006978 adaptation Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 10
- 230000008569 process Effects 0.000 description 6
- 230000008859 change Effects 0.000 description 4
- 230000007547 defect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000006260 foam Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000004806 packaging method and process Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000008521 reorganization Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model relates to an aviation case technical field just discloses an aviation case with layered structure, including the aviation case body, the equal fixed mounting in the left and right sides of aviation case body bottom has the gyro wheel. This aviation case with layered structure, when needs carry out the layering to the aviation case body, at first make first baffle and second baffle turn to vertical state with first pivot and second pivot, rotate the screw rod after that, owing to set up the screw hole with screw rod looks adaptation in removing the loop bar, and be equipped with slurcam and dead lever on removing the loop bar, make the rotation of removing the loop bar limited, when the screw rod rotates, it receives its screw thread thrust and back-and-forth movement to remove the loop bar, two spacing inserted bars remove simultaneously and block gradually the draw-in groove that first baffle and second baffle were seted up through slurcam promotion upper and lower, can fix first baffle and second baffle, make the inner chamber layering of aviation case body, thereby conveniently put in order the musical instrument component of different materials and size.
Description
Technical Field
The utility model relates to an aviation case technical field specifically is an aviation case with layered structure.
Background
The aviation case is a novel packaging product which is produced by aiming at the defects that the traditional simple wooden case packaging transportation can not solve the problem that the high-tech product cannot be effectively protected and has poor mobility in the long-distance transportation process and can replace the transportation.
The existing aviation case becomes a stock product for people to go out, no matter go out for travel or work, the aviation case can not be opened almost, the existing aviation case generally has the defect of inconvenient storage, and a certain layered structure is not arranged in the existing aviation case, so that when the aviation case is provided with musical instrument components, products of different materials and body types can not be integrated, certain collision can occur between the components which are not well integrated in the aviation case in the transportation process, and articles are easy to damage, and therefore the aviation case with the layered structure is provided to solve the problem.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides a not enough to prior art, the utility model provides an aviation case with layered structure possesses the advantage such as being convenient for accomodate, has solved present aviation case and has generally had the shortcoming of being not convenient for to accomodate, because it does not set up certain layered structure inside it, make aviation case when device musical instrument class component, can not put in order the product of different materials and size, at the in-process of transportation, certain collision can take place between the component that does not carry out good putting in order in the aviation case, lead to the problem that the article damaged easily.
(II) technical scheme
For the purpose of realizing above-mentioned be convenient for accomodate, the utility model provides a following technical scheme: an aviation case with a layered structure comprises an aviation case body, wherein rollers are fixedly mounted on the left side and the right side of the bottom of the aviation case body, an anti-collision cushion is fixedly mounted on the inner wall of the aviation case body, a first rotating shaft is fixedly mounted on the left side of the inner bottom wall of the aviation case body, a first partition plate is movably mounted on the left side of the inner bottom wall of the aviation case body through the first rotating shaft, a second rotating shaft is fixedly mounted on the right side of the inner bottom wall of the aviation case body, a second partition plate is movably mounted on the right side of the inner bottom wall of the aviation case body through the second rotating shaft, fixing frames are fixedly mounted on the left side and the right side of the aviation case body, first springs are fixedly mounted at the upper end and the lower end of an inner cavity of each fixing frame, buffer plates are movably mounted on the left side and the right side of the aviation case body, and movable push rods are, the utility model discloses an aviation case body, including aviation case body, fixed plate, catch bar, fixed plate and aviation case body, the front of aviation case body and the equal fixed mounting in back have quantity to be two fixed plates, fixed mounting has quantity to be two dead lever, two between fixed plate and the aviation case body movable mounting has the catch bar between the dead lever, the outside fixed mounting of dead lever has the second spring, one side fixed mounting that the aviation case body was kept away from to the catch bar has the removal loop bar, one side fixed mounting that the catch bar is located the aviation case body has one end to run through and extend to aviation case body inner chamber and with aviation case body swing joint spacing inserted bar, one side movable mounting that the aviation case body was kept away from to the fixed plate has one end.
Preferably, the screw rod comprises threaded rod, change and rolling bearing, one side fixed mounting that the threaded rod is located the fixed plate has the change, one side fixed mounting that the threaded rod is located the aviation case body has rolling bearing, and the threaded rod passes through rolling bearing and aviation case body swing joint.
Preferably, the right side of the movable sleeve rod is provided with a threaded hole, the threaded hole is matched with the screw, and the fixed rod and the aviation case body are vertically installed at ninety degrees.
Preferably, the number of the screw rods is four, two round holes are formed in one side, back to back, of the fixing frame, and the round holes are matched with the movable push rods.
Preferably, the front and the back of the first partition plate and the second partition plate are both provided with two clamping grooves, the clamping grooves are matched with the limiting insertion rods, and the anti-collision cushion is a spongy cushion.
Preferably, the movable push rod is T-shaped, and the movable push rod and the buffer plate are vertically arranged at ninety degrees.
(III) advantageous effects
Compared with the prior art, the utility model provides an aviation case with layered structure possesses following beneficial effect:
1. the aviation case with the layered structure is characterized in that the first rotating shaft and the second rotating shaft are arranged, when the aviation case body needs to be layered, the first rotating shaft and the second rotating shaft are firstly used for enabling the first partition plate and the second partition plate to be turned to be in a vertical state, then the screw rod is rotated, the threaded hole matched with the screw rod is formed in the movable sleeve rod, the movable sleeve rod is provided with the pushing plate and the fixed rod, the rotation of the movable sleeve rod is limited, when the screw rod rotates, the movable sleeve rod moves back and forth under the thrust of the threads of the screw rod, the upper limiting insertion rod and the lower limiting insertion rod are pushed by the pushing plate to move simultaneously and are gradually clamped into the clamping grooves formed in the first partition plate and the second partition plate, the first partition plate and the second partition plate can be fixed, the inner cavity of the aviation case body is layered, when the layering is not needed, the screw rod is similarly reversed, so that the first partition plate and the second partition plate are, can be with first baffle and second baffle income aviation case bottom, can control the inside space of aviation case body in a flexible way to the convenience is put in order the musical instrument component of different materials and size, has improved the practicality of device greatly, satisfies the demand that people used more.
2. This aviation case with layered structure through setting up the buffer board in the outside of aviation case body, when the aviation case body receives the collision, the buffer board receives the punching press and will promote movable push rod and remove to extrude first spring, through the continuous energy that slows down its collision, can reduce the collision that the aviation case body received, thereby carry out effectual protection to its inside musical instrument component, the security and the practicality of device have been improved greatly, satisfy the demand that people used more.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a side view of the flight box body of the present invention;
fig. 3 is an enlarged view of a portion a in fig. 2 according to the present invention.
In the figure: 1 crashproof pad, 2 first pivot, 3 aviation case bodies, 4 second pivots, 5 gyro wheels, 6 mounts, 7 first springs, 8 buffer boards, 9 second baffles, 10 first baffles, 11 activity push rods, 12 screw rods, 13 removal loop bars, 14 fixed plates, 15 second springs, 16 kickboards, 17 spacing inserted bars, 18 dead levers.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, an aviation case with a layered structure comprises an aviation case body 3, wherein rollers 5 are fixedly mounted on the left side and the right side of the bottom of the aviation case body 3, an anti-collision pad 1 is fixedly mounted on the inner wall of the aviation case body 3, a first rotating shaft 2 is fixedly mounted on the left side of the inner bottom wall of the aviation case body 3, the first rotating shaft 2 and a second rotating shaft 4 are arranged, when the aviation case body 3 needs to be layered, the first separating plate 10 and the second separating plate 9 are firstly rotated to be in a vertical state by the first rotating shaft 2 and the second rotating shaft 4, then the screw rod 12 is rotated, as a threaded hole matched with the screw rod 12 is formed in the movable sleeve rod 13, and a pushing plate 16 and a fixing rod 18 are arranged on the movable sleeve rod 13, so that the movable sleeve rod 13 is limited in rotation, when the screw rod 12 rotates, the movable sleeve rod 13 moves back and forth under the thrust of the thread thereof, and forth movement are pushed by the pushing plate 16, and forth movement of two upper and lower limit inserting rods 17 are 9, the first clapboard 10 and the second clapboard 9 can be fixed, so that the inner cavity of the aviation case body 3 is layered, when the layering is not needed, the screw 12 is reversed, so that the first clapboard 10 and the second clapboard 9 are not limited by the limit inserted link 17, the first clapboard 10 and the second clapboard 9 can be put into the bottom of the aviation case, the space in the aviation case body 3 can be flexibly controlled, thereby facilitating the reorganization of musical instrument components with different materials and body types, greatly improving the practicability of the device, and meeting the use requirements of people, the first clapboard 10 is movably arranged on the left side of the inner bottom wall of the aviation case body 3 through the first rotating shaft 2, the front and the back of the first clapboard 10 and the second clapboard 9 are both provided with two clamping grooves, the clamping grooves are matched with the limit inserted link 17, the crash pad 1 is a foam pad, and the foam pad has excellent cushioning property and flexibility, the instrument component inside the aviation case body 3 can be well protected, so that the safety of the instrument component is improved, the right side of the bottom wall inside the aviation case body 3 is fixedly provided with the second rotating shaft 4, the right side of the bottom wall inside the aviation case body 3 is movably provided with the second partition plate 9 through the second rotating shaft 4, the left side and the right side of the aviation case body 3 are both fixedly provided with the fixed frame 6, the upper end and the lower end of the inner cavity of the fixed frame 6 are both fixedly provided with the first spring 7, the left side and the right side of the aviation case body 3 are both movably provided with the buffer plate 8, by arranging the buffer plate 8 outside the aviation case body 3, when the aviation case body 3 is collided, the buffer plate 8 is punched to push the movable push rod 11 to move left and right, so as to extrude the first spring 7, and by continuously slowing down the collision energy of the aviation case body 3, the collision of the aviation case body 3 can be reduced, greatly improved the security and the practicality of device, satisfy the demand that people used more, the equal fixed mounting in one side that two buffer boards 8 are relative has movable push rod 11, movable push rod 11 is the T font, movable push rod 11 is ninety degrees perpendicular installation with buffer board 8, the front of aviation case body 3 and the equal fixed mounting in the back have fixed plate 14 that quantity is two, fixed mounting has quantity to be two dead lever 18 between fixed plate 14 and the aviation case body 3, movable mounting has slurcam 16 between two dead levers 18, the outside fixed mounting of dead lever 18 has second spring 15, one side fixed mounting that aviation case body 3 was kept away from to slurcam 16 has removal loop bar 13, the right side of removal loop bar 13 has seted up threaded hole, and threaded hole and screw rod 12 looks adaptation, dead lever 18 is ninety degrees perpendicular installation with aviation case body 3, slurcam 16 is located one side fixed mounting of aviation case body 3 and has one end to run through and extend to aviation case body 3 inner chamber and with aviation case body 3 inner chamber Spacing inserted bar 17 of 3 swing joints of body, one side movable mounting that the fixed plate 14 kept away from aviation case body 3 has one end and removes loop bar 13 swing joint's screw rod 12, the quantity of screw rod 12 is four, the round hole that quantity is two is all seted up to one side that two mounts 6 carried on the back mutually, and round hole and movable push rod 11 looks adaptation, screw rod 12 is by the threaded rod, change and rolling bearing constitute, one side fixed mounting that the threaded rod is located fixed plate 14 has the change, one side fixed mounting that the threaded rod is located aviation case body 3 has rolling bearing, and the threaded rod passes through rolling bearing and aviation case body 3 swing joint.
In summary, according to the aviation case with the layered structure, by arranging the first rotating shaft 2 and the second rotating shaft 4, when the aviation case body 3 needs to be layered, the first rotating shaft 2 and the second rotating shaft 4 are firstly used for enabling the first partition board 10 and the second partition board 9 to be turned to be in a vertical state, then the screw 12 is rotated, because the threaded hole matched with the screw 12 is formed in the movable sleeve rod 13, the pushing plate 16 and the fixing rod 18 are arranged on the movable sleeve rod 13, the rotation of the movable sleeve rod 13 is limited, when the screw 12 is rotated, the movable sleeve rod 13 moves forwards and backwards under the thrust of the threads, the pushing plate 16 pushes the upper and lower limiting insertion rods 17 to simultaneously move and gradually clamp the clamping grooves formed in the first partition board 10 and the second partition board 9, so that the first partition board 10 and the second partition board 9 can be fixed, the inner cavity of the aviation case body 3 is layered, when the layering is not needed, in a similar way, the reverse screw 12 makes the first partition board 10 and the second partition board 9 no longer receive the restriction of the limiting inserted bar 17, and the first partition board 10 and the second partition board 9 can be taken into the bottom of the aviation case, so that the space inside the aviation case body 3 can be flexibly controlled, the components of musical instruments made of different materials and body types can be conveniently rounded, the practicability of the device is greatly improved, and the use requirements of people are met.
Moreover, by arranging the buffer plate 8 at the outer side of the aviation case body 3, when the aviation case body 3 is collided, the buffer plate 8 is punched to push the movable push rod 11 to move left and right, so as to extrude the first spring 7, and the collision of the aviation case body 3 can be reduced by continuously slowing down the collision energy, thereby effectively protecting the musical instrument components in the aviation case body, greatly improving the safety and the practicability of the device, further meeting the use requirements of people, solving the defect that the existing aviation case is not convenient to store, because the interior of the existing aviation case is not provided with a certain layered structure, the aviation case can not put in order products of different materials and body types when being provided with musical instrument components, and in the transportation process, certain collision can occur between the components which are not put in order well in the aviation case, easily causing the problem of object damage.
It is to be noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. An aviation case with a layered structure, comprising an aviation case body (3), characterized in that: the anti-collision device is characterized in that rollers (5) are fixedly mounted on the left side and the right side of the bottom of the aviation case body (3), an anti-collision pad (1) is fixedly mounted on the inner wall of the aviation case body (3), a first rotating shaft (2) is fixedly mounted on the left side of the inner bottom wall of the aviation case body (3), a first partition plate (10) is movably mounted on the left side of the inner bottom wall of the aviation case body (3) through the first rotating shaft (2), a second rotating shaft (4) is fixedly mounted on the right side of the inner bottom wall of the aviation case body (3), a second partition plate (9) is movably mounted on the right side of the inner bottom wall of the aviation case body (3) through the second rotating shaft (4), fixing frames (6) are fixedly mounted on the left side and the right side of the aviation case body (3), first springs (7) are fixedly mounted on the upper end and the lower end of the inner cavity of the fixing frames (6), and buffer plates (, two the equal fixed mounting in one side that buffer board (8) are relative has movable push rod (11), the front of aviation case body (3) has fixed plate (14) that quantity is two with the equal fixed mounting in the back, fixed mounting has dead lever (18) that quantity is two between fixed plate (14) and aviation case body (3), two movable mounting has slurcam (16) between dead lever (18), the outside fixed mounting of dead lever (18) has second spring (15), one side fixed mounting that aviation case body (3) were kept away from in slurcam (16) has removal loop bar (13), one side fixed mounting that slurcam (16) are located aviation case body (3) has one end to run through and extend to aviation case body (3) inner chamber and with aviation case body (3) swing joint spacing inserted bar (17), one side movable mounting that aviation case body (3) were kept away from in fixed plate (14) has one end and removes loop bar (13) swing joint The screw (12).
2. An aviation case with a layered structure as claimed in claim 1, wherein: the screw rod (12) comprises threaded rod, swivel and rolling bearing, one side fixed mounting that the threaded rod is located fixed plate (14) has the swivel, one side fixed mounting that the threaded rod is located aviation case body (3) has rolling bearing, and the threaded rod passes through rolling bearing and aviation case body (3) swing joint.
3. An aviation case with a layered structure as claimed in claim 1, wherein: the right side of the movable loop bar (13) is provided with a threaded hole, the threaded hole is matched with the screw rod (12), and the fixed bar (18) and the aviation case body (3) are vertically installed at ninety degrees.
4. An aviation case with a layered structure as claimed in claim 1, wherein: the number of the screw rods (12) is four, two round holes are formed in the two opposite sides of the fixing frame (6), and the round holes are matched with the movable push rods (11).
5. An aviation case with a layered structure as claimed in claim 1, wherein: the front and the back of the first partition plate (10) and the second partition plate (9) are provided with two clamping grooves, the clamping grooves are matched with the limiting insertion rods (17), and the anti-collision pad (1) is a spongy cushion.
6. An aviation case with a layered structure as claimed in claim 1, wherein: the movable push rod (11) is T-shaped, and the movable push rod (11) and the buffer plate (8) are vertically arranged at ninety degrees.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020563832.5U CN212125985U (en) | 2020-04-16 | 2020-04-16 | Aviation case with layered structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020563832.5U CN212125985U (en) | 2020-04-16 | 2020-04-16 | Aviation case with layered structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212125985U true CN212125985U (en) | 2020-12-11 |
Family
ID=73690151
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020563832.5U Expired - Fee Related CN212125985U (en) | 2020-04-16 | 2020-04-16 | Aviation case with layered structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212125985U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116639419A (en) * | 2023-06-25 | 2023-08-25 | 李媛 | Electronic organ carrying frame suitable for music teaching |
-
2020
- 2020-04-16 CN CN202020563832.5U patent/CN212125985U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116639419A (en) * | 2023-06-25 | 2023-08-25 | 李媛 | Electronic organ carrying frame suitable for music teaching |
| CN116639419B (en) * | 2023-06-25 | 2024-03-08 | 淄博师范高等专科学校 | Electronic organ carrying frame suitable for music teaching |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201211 |