CN220069067U - Suitcase that can joint each other for civil aviation ware - Google Patents
Suitcase that can joint each other for civil aviation ware Download PDFInfo
- Publication number
- CN220069067U CN220069067U CN202321710392.1U CN202321710392U CN220069067U CN 220069067 U CN220069067 U CN 220069067U CN 202321710392 U CN202321710392 U CN 202321710392U CN 220069067 U CN220069067 U CN 220069067U
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- China
- Prior art keywords
- aircraft
- butt
- fixedly connected
- butt joint
- suitcase
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Links
- 210000001503 joint Anatomy 0.000 claims abstract description 24
- 230000006835 compression Effects 0.000 abstract description 5
- 238000007906 compression Methods 0.000 abstract description 5
- 230000005389 magnetism Effects 0.000 abstract description 3
- 238000003032 molecular docking Methods 0.000 description 30
- 230000003139 buffering effect Effects 0.000 description 4
- 230000001012 protector Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000001125 extrusion Methods 0.000 description 3
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
Abstract
The utility model relates to the technical field of aircraft suitcases and discloses a mutually-clamped suitcase for a civil aircraft, which comprises an aircraft suitcase, wherein the top of the aircraft suitcase is provided with a clamping device, and the clamping device comprises a butt joint plate, a butt joint seat, a butt joint plugboard, a tooth part of the butt joint plugboard, a side elastic rubber pad, a butt joint groove, a connecting jacking block, a connecting bearing, a middle connecting thin rod, an inner rotating rod, a connecting frame, an auxiliary bracket, a magnetic attraction block and a magnet block. This but suitcase of mutual joint for civil aircraft is provided with the joint device, and in the butt joint seat was inserted to the butt joint picture peg tooth, can extrude side elastic rubber pad when inserting, makes its compression, can closely laminate with the inner wall of butt joint groove, cooperates the magnetism to inhale piece and magnet piece, and the two can adsorb together after the contact to accomplish the butt joint of aircraft suitcase, and set up a plurality of butt joint components, can increase the intensity of connection, be difficult for dividing to take off the use that influences the device, effectual when using.
Description
Technical Field
The utility model relates to the technical field of aircraft suitcases, in particular to a mutually-clamped suitcase for a civil aircraft.
Background
Luggage, also known as a trunk or a draw-bar box, is a box carried at the exit for placing articles, and is usually used for placing clothes, personal care products and souvenirs required during the journey, and the size of the luggage on the market is generally according to the standard specified by the sizes of the portable boarding box and the carrying box of an airline company, so that the luggage can be used in civil aircraft.
The prior art discloses the publication number: the utility model discloses a mutually combinable luggage case, which comprises a luggage case body and a clamping device, wherein one side surface of the luggage case body is provided with an opening, the clamping device is arranged in the opening of the luggage case body and on the opposite side surface of the side surface with the opening, the opening and the clamping device are positioned on one side of the combining surfaces of two case covers of the luggage case body and on the same side of the combining surfaces, and the opening and the closing processes of the luggage case are not influenced by the opening and the clamping device.
However, the above-mentioned clamping structure of the luggage case capable of being clamped with each other is only a simple buckle and a clamping seat, and is similar to the existing structure, and the strength is general when in connection, and the use is affected by being easily separated by stress, so that the effect is poor when in use, and improvement is needed.
Disclosure of Invention
The utility model aims to provide a mutually-clamped luggage case for a civil aircraft, which solves the problems in the background art.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a but suitcase of mutual joint for civil aircraft, includes the aircraft suitcase, the front of aircraft suitcase is provided with protector, the top of aircraft suitcase is provided with carries the handle, the top of aircraft suitcase is provided with clamping device.
The clamping device comprises an abutting plate, an abutting seat, an abutting plug board tooth part, a side elastic rubber pad, an abutting groove, a connecting jacking block, a connecting bearing, a middle connecting thin rod, an inner rotating rod, a connecting frame, an auxiliary support, a magnetic attraction block and a magnet block.
Preferably, the protection device comprises a surface protection plate and an inner rubber cushion pad, wherein the surface protection plate is fixedly connected to the front surface of the aircraft trunk, and the inner rubber cushion pad is fixedly connected to the front surface of the aircraft trunk.
Preferably, the front surface of the inner rubber cushion pad is connected to the inner back surface of the surface protection plate, and the inner rubber cushion pad is arranged to play a role in protection through the buffering of the inner rubber cushion pad, so that the protection is assisted.
Preferably, the tooth parts of the docking plate and the elastic rubber pads at the side ends are inserted into the docking seat, the widths of the tooth parts of the docking plate and the elastic rubber pads at the side ends are larger than the widths of the docking groove, and the widths of the tooth parts of the docking plate and the elastic rubber pads at the side ends are larger than the widths of the docking groove, so that the elastic rubber pads at the side ends can be extruded during insertion, so that the elastic rubber pads at the side ends are compressed, and reverse extrusion force can be generated after the compression, the elastic rubber pads can be tightly attached to the inner wall of the docking groove, and clamping can be performed.
Preferably, the bottom area of the magnet is equal to the top area of the magnet, the magnet is magnetically attracted to be connected to the magnet, and the magnet are arranged in a contact mode, so that the contact area of the magnet and the magnet is equal, the connection is tighter during contact connection, and the magnet is not easy to separate.
Preferably, the number of the clamping devices is two, and the two clamping devices are symmetrically distributed on the left side and the right side of the top of the luggage case of the aircraft.
Preferably, the inner rotating rod is fixedly connected to the inner ring of the connecting bearing, and the middle connecting thin rod is fixedly connected to the side face of the inner rotating rod.
Compared with the prior art, the utility model has the beneficial effects that:
1. this but suitcase of mutual joint for civil aircraft inserts in the butt joint seat through being provided with the joint device, and the butt joint picture peg tooth can extrude side elastic rubber pad when inserting, makes its compression, can closely laminate with the inner wall of butt joint groove, cooperates the magnetism to inhale piece and magnet piece, and the two can adsorb together after the contact to accomplish the butt joint of aircraft suitcase, and set up a plurality of butt joint subassemblies, can increase the intensity of connection, be difficult for separating and take off the use that influences the device, effectual when using.
2. This but suitcase of mutual joint for civil aircraft, through being provided with protector, the striking can not directly be used on the aircraft suitcase when openly receiving to collide with but can strike on the surface protection board, can separate, and can play the effect of protection through the buffering of interior rubber blotter, increase the life of aircraft suitcase.
Drawings
FIG. 1 is a schematic view of the overall perspective top view structure of the present utility model;
FIG. 2 is an enlarged schematic view of the structure of FIG. 1A according to the present utility model;
FIG. 3 is a schematic view of the overall perspective and front view structure of the present utility model;
fig. 4 is an enlarged view of the structure of fig. 3B according to the present utility model.
In the figure: 1. aircraft luggage; 2. a protective device; 201. a surface protection plate; 202. an inner rubber cushion pad; 3. a carrying handle; 4. a clamping device; 401. an abutting plate; 402. a butt joint seat; 403. a docking board; 404. a socket tooth; 405. a side elastic rubber pad; 406. a butt joint groove; 408. connecting a top block; 409. connecting a bearing; 410. the middle is connected with a thin rod; 411. an inner rotating lever; 412. a connecting frame; 413. an auxiliary bracket; 414. a magnetic suction block; 415. a magnet block.
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:
the utility model provides a but suitcase of mutual joint for civil aircraft, includes aircraft suitcase 1, and the front of aircraft suitcase is provided with protector 2, and the top of aircraft suitcase 1 is provided with carries 3, and the top of aircraft suitcase 1 is provided with clamping device 4.
The clamping device 4 comprises a butt plate 401, a butt seat 402, a butt plug plate 403, a butt plug plate tooth part 404, a side end elastic rubber pad 405, a butt joint groove 406, a connecting jacking block 408, a connecting bearing 409, a middle connecting thin rod 410, an inner rotating rod 411, a connecting frame 412, an auxiliary bracket 413, a magnetic attraction block 414 and a magnet block 415, wherein the butt plug plate 401 is fixedly connected to the top of the aircraft trunk 1, the butt seat 402 is fixedly connected to the top of the aircraft trunk 1, the butt plug plate 403 is fixedly connected to the back surface of the butt plug plate 401, the butt plug plate tooth part 404 is fixedly connected to the back surface of the butt plug plate 403, the side end elastic rubber pad 405 is fixedly connected to the side surface of the butt plug plate tooth part 404, the butt joint groove 406 is formed at the top of the butt plug plate 402, the connecting jacking block 408 is fixedly connected to the top of the aircraft trunk 1, the connecting bearing 409 is fixedly connected to the top of the butt plug plate 401, the connecting frame 412 is fixedly connected to the surface of the connecting frame 412, the auxiliary bracket 413 is fixedly connected to the surface of the middle connecting thin rod 410, the magnetic attraction block 414 is fixedly connected to the bottom of the connecting frame 412, the magnet block 415 is fixedly connected to the top of the connecting jacking block 408, the inner rotating rod 411 is fixedly connected to the inner ring of the connecting bearing 409, the middle connecting thin rod 410 is fixedly connected to the side surface of the inner rotating rod 411, the tooth part 404 of the docking plate and the elastic rubber pad 405 of the side end are inserted into the docking base 402, the widths of the tooth part 404 of the docking plate and the elastic rubber pad 405 of the side end are larger than the width of the docking groove 406, the elastic rubber pad 405 of the side end is extruded when the docking plate is inserted, so that the docking plate is compressed, and after the compression, the opposite extrusion force can be generated, the docking plate can be tightly attached to the inner wall of the docking groove 406, the docking plate can be tightly clamped, the bottom area of the magnet block 414 is equal to the top area of the magnet block 415, the magnet block 415 is magnetically connected to the magnet block 414, the magnet block 414 and the magnet block 415 are equal in contact area, connection during contact connection is tighter, separation is not easy, the number of the clamping devices 4 is two, and the two clamping devices 4 are symmetrically distributed on the left side and the right side of the top of the aircraft trunk 1.
The protection device 2 comprises a surface protection plate 201 and an inner rubber buffer pad 202, wherein the surface protection plate 201 is fixedly connected to the front surface of the aircraft trunk 1, the inner rubber buffer pad 202 is fixedly connected to the front surface of the aircraft trunk 1, the front surface of the inner rubber buffer pad 202 is connected to the inner back surface of the surface protection plate 201, and the inner rubber buffer pad 202 is arranged to play a role in protection through buffering of the inner rubber buffer pad 202, so that protection is assisted.
When the aircraft luggage case 1 is closed, the front half part and the rear half part of the aircraft luggage case 1 are connected, the docking plate 403 on the back of the docking plate 401 and the docking plate tooth part 404 on the back of the docking plate can be aligned and inserted into the docking groove 406 in the docking seat 402, the side elastic rubber pad 405 can also be inserted into the docking groove 406, and the width of the docking plate tooth part 404 and the side elastic rubber pad 405 is larger than the width of the docking groove 406, the side elastic rubber pad 405 can be pressed during insertion, so that the side elastic rubber pad 405 is compressed, and the reverse extrusion force can be generated after the compression, the docking plate 403 can be tightly attached to the inner wall of the docking groove 406, the docking plate 403 can be clamped, the connecting frame 412 can be turned after the docking plate 403 is clamped, the inside dwang 411 is driven to overturn backward in connecting bearing 409 until the magnetism of link 412 bottom inhale piece 414 upset to contact with magnet piece 415, both can adsorb together after the contact, thereby accomplish the butt joint of aircraft suitcase 1, and set up a plurality of butt joint components, can increase the intensity of connection, be difficult for separating and take off the use that influences the device, effectually when using, and be provided with protector 2 in the front of aircraft suitcase 1, the striking can not directly be acted on aircraft suitcase 1 but can strike on surface protection board 201 when the front receives the bump, can carry out the separation, and can play the effect of protection through the buffering of interior rubber buffer pad 202, increase the life of aircraft suitcase 1.
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 (7)
1. The utility model provides a but suitcase of mutual joint for civil aircraft, includes aircraft suitcase (1), its characterized in that: the front of the aircraft luggage case is provided with a protection device (2), the top of the aircraft luggage case (1) is provided with a carrying handle (3), and the top of the aircraft luggage case (1) is provided with a clamping device (4);
the clamping device (4) comprises a butt plate (401), a butt seat (402), a butt plug board (403), a butt plug board tooth part (404), a side elastic rubber pad (405), a butt joint groove (406), a connecting top block (408), a connecting bearing (409), a middle connecting slender rod (410), an inner rotating rod (411), a connecting frame (412), an auxiliary support (413), a magnetic attraction block (414) and a magnet block (415), wherein the butt plate (401) is fixedly connected to the top of an aircraft trunk (1), the butt seat (402) is fixedly connected to the top of the aircraft trunk (1), the butt plug board (403) is fixedly connected to the back surface of the butt plug board (401), the butt plug board tooth part (404) is fixedly connected to the back surface of the butt plug board (403), the side elastic rubber pad (405) is fixedly connected to the side surface of the butt plug board tooth part (404), the butt joint groove (406) is formed in the top of the butt plug board (402), the connecting top block (408) is fixedly connected to the top of the aircraft trunk (1), the butt joint groove (406) is fixedly connected to the top of the aircraft trunk (1), the butt plug board (412) is fixedly connected to the top of the connecting frame (412), the surface of the auxiliary support (412) is fixedly connected to the middle connecting rod (410), the magnetic attraction block (414) is fixedly connected to the bottom of the connecting frame (412), and the magnet block (415) is fixedly connected to the top of the connecting top block (408).
2. The mutually-clampable luggage case for civil aircraft according to claim 1, wherein: the protection device (2) comprises a surface protection plate (201) and an inner rubber buffer pad (202), wherein the surface protection plate (201) is fixedly connected to the front face of the aircraft trunk (1), and the inner rubber buffer pad (202) is fixedly connected to the front face of the aircraft trunk (1).
3. The mutually-clampable luggage case for civil aircraft according to claim 2, wherein: the front surface of the inner rubber cushion pad (202) is connected to the inner back surface of the surface protection plate (201).
4. The mutually-clampable luggage case for civil aircraft according to claim 1, wherein: the butt-joint socket is characterized in that the tooth parts (404) of the butt-joint socket and the elastic rubber pads (405) at the side ends are inserted into the butt-joint seat (402), and the widths of the tooth parts (404) of the butt-joint socket and the elastic rubber pads (405) at the side ends are larger than the widths of the butt-joint grooves (406).
5. The mutually-clampable luggage case for civil aircraft according to claim 1, wherein: the bottom area of the magnet block (414) is equal to the top area of the magnet block (415), and the magnet block (415) is magnetically connected to the magnet block (414).
6. The mutually-clampable luggage case for civil aircraft according to claim 1, wherein: the number of the clamping devices (4) is two, and the two clamping devices (4) are symmetrically distributed on the left side and the right side of the top of the aircraft trunk (1).
7. The mutually-clampable luggage case for civil aircraft according to claim 1, wherein: the inner rotating rod (411) is fixedly connected to the inner ring of the connecting bearing (409), and the middle connecting thin rod (410) is fixedly connected to the side face of the inner rotating rod (411).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321710392.1U CN220069067U (en) | 2023-07-03 | 2023-07-03 | Suitcase that can joint each other for civil aviation ware |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321710392.1U CN220069067U (en) | 2023-07-03 | 2023-07-03 | Suitcase that can joint each other for civil aviation ware |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220069067U true CN220069067U (en) | 2023-11-24 |
Family
ID=88816044
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321710392.1U Active CN220069067U (en) | 2023-07-03 | 2023-07-03 | Suitcase that can joint each other for civil aviation ware |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220069067U (en) |
-
2023
- 2023-07-03 CN CN202321710392.1U patent/CN220069067U/en active Active
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| GR01 | Patent grant |