CN212922533U - Aviation case convenient to it is fixed - Google Patents
Aviation case convenient to it is fixed Download PDFInfo
- Publication number
- CN212922533U CN212922533U CN202021350119.9U CN202021350119U CN212922533U CN 212922533 U CN212922533 U CN 212922533U CN 202021350119 U CN202021350119 U CN 202021350119U CN 212922533 U CN212922533 U CN 212922533U
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- China
- Prior art keywords
- aviation case
- plate
- aviation
- aircraft flight
- dwang
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- Expired - Fee Related
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- 230000006978 adaptation Effects 0.000 claims description 2
- 238000004873 anchoring Methods 0.000 claims 2
- 239000011120 plywood Substances 0.000 claims 1
- 230000005484 gravity Effects 0.000 abstract description 3
- 238000000151 deposition Methods 0.000 abstract description 2
- 230000001737 promoting effect Effects 0.000 abstract description 2
- 239000011435 rock Substances 0.000 abstract description 2
- 230000035939 shock Effects 0.000 description 6
- 230000003139 buffering effect Effects 0.000 description 5
- 238000004806 packaging method and process Methods 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
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- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
Abstract
The utility model belongs to the technical field of aviation case, a aviation case convenient to fix is disclosed, including aviation case, set up the holding chamber in the aviation case and be used for covering the open-close plate that closes the holding chamber opening, the holding chamber is equipped with and is symmetrical the clamping part of arranging in the inner wall and runs through the thing board of putting of holding chamber bottom, aviation case bottom is equipped with and is used for supporting connecting plate, piston rod and the cylinder body of putting the thing board, still symmetrical dwang and the fixed part articulated with the dwang that is used for promoting the clamping part that is equipped with in the aviation case, the dwang tip still is connected with and is promoted by the thing board so that the dwang rotates along the fixed part baffle, the baffle is arranged in; this device will deposit article and arrange in on putting the thing board, drive through gravity and put the thing board and move down in order to adjust the dwang angle, and then promote the fixed article of depositing of clamping part, guarantee to deposit article and can not produce the collision when the aviation case takes place to rock, improve the security.
Description
Technical Field
The utility model belongs to the technical field of the aviation case, very much relate to an aviation case convenient to it is fixed.
Background
The aviation case is a traditional simple wooden case packaging and transporting method which can not solve the defects that the high-tech products can not be effectively protected and have poor maneuverability in the long-distance transportation process, and therefore a new packaging product for replacing transportation is generated aiming at the defect. Increasingly frequent cross-country trade steps the use and development of aviation boxes into the golden stage, and is particularly 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 packaging, military equipment transportation and the like.
According to the aviation case that chinese patent No. CN 207843749U's damage that collides with is reduced, including the case lid, the aviation case body, the universal wheel, the fixed plate, the shock attenuation piece, the uide bushing, the slider, spring damper, connecting rod and collision board, the inside standing groove that is provided with of aviation case, the universal wheel rotates to be connected at aviation case body terminal surface down, the case lid sets up at aviation case body upside, and block with the aviation case body, the fixed plate sets up at the inside standing groove side terminal surface of aviation case body, the collision board sets up at the aviation case body side, the shock attenuation piece sets up terminal surface in the collision board, the uide bushing sets up at the shock attenuation piece right-hand member, the uide bushing cover is located the connecting rod outside, the connecting rod passes through spring damper and fixed plate zonulae occludens, the slider cover is located the connecting rod right-hand member, this design utilizes the bumper shock absorber to carry out.
The existing and mentioned aviation boxes are combined, certain problems of the aviation boxes in use can be found, the aviation boxes are frequently displaced and can collide with each other to be acted, and objects on the inner sides of the aviation boxes are not fixed by a good device, so that the objects on the inner sides of the aviation boxes are frequently impacted and damaged and cannot be used, great loss is brought, working difficulty is increased, time and energy are wasted, normal progress of working is delayed, and economic loss is brought; meanwhile, the buffering device is additionally arranged outside the aviation case, so that the buffering and shock absorption of the interior of the aviation case on stored articles cannot be guaranteed, and the stored articles are extremely easy to damage.
Disclosure of Invention
The utility model aims at providing an aviation case convenient to fix for solve the above-mentioned can find that aviation case has certain problem when using, because the aviation case often displacement, so can collide and receive the effort, and the article of aviation case inboard does not have better device to be fixed, lead to the object of aviation case inboard often to receive the striking and damage, can't use, not only brought great loss, increased the work degree of difficulty simultaneously, wasted time and energy, delayed the normal progress of work, brought economic loss's problem; meanwhile, the buffering device is additionally arranged outside the aviation case, so that the buffering and shock absorption of the interior of the aviation case on stored articles cannot be guaranteed, and the stored articles are extremely easy to damage.
The utility model provides a technical scheme that its technical problem adopted provides a aviation case convenient to it is fixed, include the aviation box, set up in holding chamber in the aviation box closes with being used for the cover holding chamber open-ended open-close board, the holding chamber is equipped with and is the symmetric clamping part of arranging the inner wall in and runs through the thing board of putting of holding chamber bottom, aviation bottom half is equipped with for supporting connecting plate, piston rod and the cylinder body of putting the thing board, it is used for promoting still to be equipped with symmetrically in the aviation box the dwang of clamping part and with dwang articulated fixed part, the dwang tip still is connected with and is put the thing board promotion so that the dwang is followed fixed part pivoted baffle, the baffle is arranged in and is put thing bottom half.
Further preferably, the inner wall of the accommodating cavity is provided with a strip-shaped hole for the rotating rod to extend into.
Further preferably, the inner wall of the accommodating cavity is further provided with a slide way for the object placing plate to move back and forth along the accommodating cavity.
Further preferably, sliding wheels capable of moving back and forth along the slide rails are arranged on two sides of the object placing plate.
Further preferably, the bottom of the clamping part is connected with a first flexible supporting plate, and an elastic part is arranged between the first flexible supporting plate and the inner wall of the accommodating cavity.
Further preferably, the aviation case body is symmetrically provided with grooves for the opening and closing plates to move.
Further preferably, the inner wall of the accommodating cavity is symmetrically and fixedly provided with second flexible supporting plates for supporting the opening plate.
Further preferably, the open-close plate is including being first apron and the second apron that the symmetry set up in the recess, first apron stretches out in the recess and is equipped with the arch towards second apron one side, the second apron stretch out in the recess and towards first apron one side be equipped with the draw-in groove of protruding adaptation.
Further preferably, a holding part is connected to the upper surfaces of the first cover plate and the second cover plate.
Further preferably, one side of the clamping part facing the object placing plate is arc-shaped.
The utility model has the advantages that:
this device will deposit article and arrange in on putting the thing board, drive through gravity and put the thing board and move down in order to adjust the dwang angle, and then promote the fixed article of depositing of clamping part, guarantee to deposit article and can not produce the collision when the aviation case takes place to rock, improve the security.
Drawings
Fig. 1 is a plan side view of an overall structure of an aviation case convenient to fix according to an embodiment of the present invention;
fig. 2 is a plan view of an overall structure of an aviation case convenient to fix according to an embodiment of the present invention;
fig. 3 is a plan view of another structure of an aviation case convenient to fix according to an embodiment of the present invention.
In the figure: 1-aviation case body, 11-rotating rod, 12-fixing part, 13-baffle, 14-groove, 2-containing cavity, 21-clamping part, 22-containing plate, 23-strip-shaped hole, 24-slideway, 25-sliding wheel, 26-first flexible supporting plate, 27-elastic part, 28-second flexible supporting plate, 3-opening plate, 31-first cover plate, 32-second cover plate, 33-bulge, 34-clamping groove, 35-holding part, 4-connecting plate, 5-piston rod and 6-cylinder body.
Detailed Description
In order to more clearly illustrate embodiments and/or technical solutions in the prior art, embodiments of the present invention will be described below with reference to the accompanying drawings. It is obvious that the drawings in the following description are only examples of the invention, and that for a person skilled in the art, other drawings and embodiments can be obtained from these drawings without inventive effort. In addition, the term "orientation" merely indicates a relative positional relationship between the respective members, not an absolute positional relationship.
Please refer to fig. 1, fig. 2 and fig. 3, the aviation case convenient to fix of this embodiment includes an aviation case body 1, a holding chamber 2 arranged in the aviation case body 1 and an opening plate 3 for covering the opening of the holding chamber 2, the holding chamber 2 is provided with a clamping portion 21 symmetrically arranged on the inner wall and an object placing plate 22 penetrating the bottom of the holding chamber 2, the bottom of the aviation case body 1 is provided with a connecting plate 4, a piston rod 5 and a cylinder body 6 for supporting the object placing plate 22, the aviation case body 1 is further symmetrically provided with a rotating rod 11 for pushing the clamping portion 21 and a fixing portion 12 hinged to the rotating rod 11, the end of the rotating rod 11 is further connected with a baffle 13 pushed by the object placing plate 22 to enable the rotating rod 11 to rotate along the fixing portion 12, and the baffle 13 is arranged at the bottom of the object placing plate 22.
The containing cavity 2 is arranged in the middle of the aviation case body 1, the bottom of the containing cavity is provided with a through hole for the object placing plate 22 to reciprocate up and down along the inner wall of the containing cavity 2, and when articles are placed on the object placing plate 22, the object placing plate 22 can be pressed downwards by the gravity of the articles; a connecting plate 4, a piston rod 5 connected with the bottom of the connecting plate 4 and a cylinder body 6 sleeved outside the piston rod 5 are sequentially connected between the bottom of the object placing plate 22 and the bottom of the inner wall of the aviation case 1, one end of the piston rod 5 extends into the cylinder body 6 and can axially reciprocate along the cylinder body 6 under the movement of the object placing plate 22, so that the object placing plate 22 can buffer stored objects; the inner side wall of the aviation case body 1 is symmetrically provided with fixing parts 12, the fixing parts 12 can be fixed blocks with hinged parts, and the hinged parts are hinged with the middle part of the rotating rod 11; it should be noted here that the rotating rod 11 may be formed by connecting two connecting rods with an included angle of 120 degrees, and the connecting position may be hinged to the hinge portion of the fixing portion 12 through a nut; 11 one end of dwang is connected with clamping part 21 through seting up in the bar hole 23 of 2 lateral walls in holding chamber, and the other end is arranged in through L type baffle 13 and is put thing board 22 below, and the accessible drives baffle 13 when putting the vertical downstream of thing board 22 and rotates clockwise along fixed part 12 in order to realize dwang 11, and then deposits article with the clamping part 21 is fixed.
The inner wall of the accommodating cavity 2 is also provided with a slide way 24 for the object placing plate 22 to reciprocate along the accommodating cavity 2; the sliding wheels 25 capable of reciprocating along the sliding rails 24 are disposed on two sides of the object placing plate 22, so that the object placing plate 22 can move without shifting.
In a preferred embodiment, a first flexible supporting plate 26 is connected to the bottom of the clamping portion 21, and an elastic member 27 is arranged between the first flexible supporting plate 26 and the inner wall of the accommodating cavity 2; the clamping part 21 can be concentrated on the middle upper part of the fixed storage article as shown in fig. 1, and in order to increase the application range of the clamping part 21, a first flexible supporting plate 26 for assisting the lower half part of the fixed storage article is arranged at the bottom of the clamping part 21; the first flexible supporting plate 26 is provided with elasticity to play a role in buffering, and the elastic member 27 is connected to provide a damping effect for the clamping portion 21 and the first flexible supporting plate 26, so as to further ensure the integrity of the stored articles.
As a preferred embodiment, as shown in fig. 2 and fig. 3, the opening plate 3 includes a first cover plate 31 and a second cover plate 32 symmetrically disposed in the groove 14, the first cover plate 31 extends out of the groove and has a protrusion 33 facing one side of the second cover plate 32, and the second cover plate 32 extends out of the groove and has a slot 34 facing one side of the first cover plate 31 and adapted to the protrusion 33.
The first cover 31 and the second cover 32 have a grip 35 connected to their upper surfaces.
In order to better cover the stored articles, a first cover plate 31 and a second cover plate 32 which can move back and forth along the groove 14 are symmetrically arranged above the stored articles, and the first cover plate 31 and the second cover plate 32 can move towards each other by manually pulling the holding part 35 until the protrusion 33 is clamped in the clamping groove 34.
The foregoing is a more detailed description of the present invention, taken in conjunction with the specific preferred embodiments thereof, and it is not intended that the invention be limited to the specific embodiments shown and described. To the utility model belongs to the technical field of ordinary technical personnel, do not deviate from the utility model discloses under the prerequisite of design, can also make a plurality of simple deductions or replacement, all should regard as belonging to the utility model discloses a protection scope.
Claims (10)
1. The utility model provides an aviation case convenient to it is fixed which characterized in that: comprises an aviation box body (1), an accommodating cavity (2) arranged in the aviation box body (1) and an opening-closing plate (3) used for covering the opening of the accommodating cavity (2), the holding cavity (2) is provided with clamping parts (21) which are symmetrically arranged on the inner wall and an object placing plate (22) which penetrates through the bottom of the holding cavity (2), the bottom of the aviation case body (1) is provided with a connecting plate (4) for supporting the object placing plate (22), a piston rod (5) and a cylinder body (6), a rotating rod (11) used for pushing the clamping part (21) and a fixing part (12) hinged with the rotating rod (11) are symmetrically arranged in the aviation case body (1), dwang (11) tip still is connected with and receives thing board (22) to promote so that dwang (11) are followed fixed part (12) pivoted baffle (13), baffle (13) are arranged in and are put thing board (22) bottom.
2. An aircraft flight chamber facilitating immobilisation according to claim 1, wherein: the inner wall of the accommodating cavity (2) is provided with a strip-shaped hole (23) for the rotating rod (11) to extend into.
3. An aircraft flight chamber facilitating immobilisation according to claim 2, wherein: the inner wall of the accommodating cavity (2) is also provided with a slide way (24) for the object placing plate (22) to move back and forth along the accommodating cavity (2).
4. An aircraft flight chamber facilitating immobilisation according to claim 3 wherein: sliding wheels (25) capable of moving back and forth along the slide ways (24) are arranged on two sides of the object placing plate (22).
5. An aircraft flight chamber facilitating immobilisation according to claim 3 wherein: the bottom of the clamping part (21) is connected with a first flexible supporting plate (26), and an elastic piece (27) is arranged between the first flexible supporting plate (26) and the inner wall of the accommodating cavity (2).
6. An aircraft flight chamber facilitating immobilisation according to claim 1, wherein: the aviation case body (1) upper portion symmetry is seted up and is supplied recess (14) that plywood (3) removed.
7. An aircraft flight chamber for facilitating anchoring as claimed in claim 6, wherein: and second flexible supporting plates (28) for supporting the opening-closing plates (3) are symmetrically and fixedly arranged on the inner wall of the accommodating cavity (2).
8. An aircraft flight chamber facilitating immobilisation according to claim 1, wherein: open-close plate (3) are including being first apron (31) and second apron (32) that the symmetry set up in recess (14), first apron (31) stretch out in the recess and be equipped with arch (33) towards second apron (32) one side, second apron (32) stretch out in the recess and be equipped with towards first apron (31) one side with draw-in groove (34) of arch (33) adaptation.
9. An aircraft flight chamber for facilitating anchoring as claimed in claim 8, wherein: the upper surfaces of the first cover plate (31) and the second cover plate (32) are connected with a holding part (35).
10. An aircraft flight chamber facilitating immobilisation according to claim 1, wherein: one side of the clamping part (21) facing the object placing plate (22) is arc-shaped.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021350119.9U CN212922533U (en) | 2020-07-10 | 2020-07-10 | Aviation case convenient to it is fixed |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021350119.9U CN212922533U (en) | 2020-07-10 | 2020-07-10 | Aviation case convenient to it is fixed |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212922533U true CN212922533U (en) | 2021-04-09 |
Family
ID=75329167
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021350119.9U Expired - Fee Related CN212922533U (en) | 2020-07-10 | 2020-07-10 | Aviation case convenient to it is fixed |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212922533U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113772220A (en) * | 2021-08-19 | 2021-12-10 | 桂冰宇 | Power equipment conveyer |
| CN115303646A (en) * | 2022-07-22 | 2022-11-08 | 大连海事大学 | Container array bearing platform suitable for sea-air combined transport |
| CN115783477A (en) * | 2022-12-07 | 2023-03-14 | 华芯半导体科技有限公司 | MO source bottle fixing device and MO source bottle temperature control device |
-
2020
- 2020-07-10 CN CN202021350119.9U patent/CN212922533U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113772220A (en) * | 2021-08-19 | 2021-12-10 | 桂冰宇 | Power equipment conveyer |
| CN115303646A (en) * | 2022-07-22 | 2022-11-08 | 大连海事大学 | Container array bearing platform suitable for sea-air combined transport |
| CN115303646B (en) * | 2022-07-22 | 2024-04-05 | 大连海事大学 | Container array bearing platform suitable for sea-air intermodal transportation |
| CN115783477A (en) * | 2022-12-07 | 2023-03-14 | 华芯半导体科技有限公司 | MO source bottle fixing device and MO source bottle temperature control device |
| CN115783477B (en) * | 2022-12-07 | 2024-02-23 | 华芯半导体科技有限公司 | MO source bottle fixing device and MO source bottle temperature control device |
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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: 20210409 |