CN212739194U - Spacecraft transport case - Google Patents
Spacecraft transport case Download PDFInfo
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- CN212739194U CN212739194U CN202021003106.4U CN202021003106U CN212739194U CN 212739194 U CN212739194 U CN 212739194U CN 202021003106 U CN202021003106 U CN 202021003106U CN 212739194 U CN212739194 U CN 212739194U
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- sliding groove
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Abstract
The utility model relates to the technical field of transportation devices, in particular to a spacecraft transportation box, which comprises a bottom plate, wherein the top end of the bottom plate is transversely provided with a mounting groove, the inside of the mounting groove is transversely and fixedly provided with a slide bar, the left side and the right side of the slide bar are movably sleeved with movable blocks matched with the mounting groove, the left side and the right side of the slide bar are sleeved with first springs, the two ends of each first spring are respectively and fixedly connected with the movable blocks and the groove wall, and the top end of each movable block is fixedly provided with a first connecting seat. Is worthy of popularization and application.
Description
Technical Field
The utility model relates to a conveyer technical field especially relates to a spacecraft transport case.
Background
The existing spacecraft transport case does not comprise a fixing device for a spacecraft, the spacecraft is only hoisted into the transport case, the spacecraft is stabilized by means of friction force between the spacecraft and the bottom of the transport case, or the spacecraft is bound in the transport case by using a rope, so that the situation that the spacecraft moves in the transport case to collide with the wall of the transport case easily occurs in the transport process of the spacecraft, vibration can be generated in the transport process, internal parts of the spacecraft are damaged, and therefore the spacecraft transport case is provided to solve the problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the defects existing in the prior art and providing a spacecraft transport case.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a spacecraft transport case is designed, and comprises a bottom plate, wherein the top end of the bottom plate is transversely provided with a mounting groove, the interior of the mounting groove is transversely and fixedly provided with a slide bar, the left side and the right side of the slide bar are movably sleeved with movable blocks matched with the mounting groove, the left side and the right side of the slide bar are sleeved with first springs, two ends of each first spring are respectively fixedly connected with the movable blocks and the groove wall, the top end of each movable block is fixedly provided with a first connecting seat, the middle part of each first connecting seat is movably provided with a connecting rod, the top ends of the two connecting rods are jointly movably provided with a second connecting seat, the top end of each second connecting seat is fixedly provided with a top plate, the middle part of the top end of each top plate is longitudinally provided with a first chute, the interior of each first chute is longitudinally and movably provided with a first threaded rod through a pair of first bearings, the top end of the top plate is transversely provided with a second sliding groove, the second sliding groove and the first sliding groove are distributed in a cross manner and are communicated with the first sliding groove, a second threaded rod is transversely and movably installed inside the second sliding groove through a pair of second bearings, second sliding blocks matched with the second sliding groove are respectively sleeved on the left side and the right side of the second threaded rod in a threaded manner, clamping plates are respectively and fixedly installed at the top ends of the second sliding blocks and the first sliding blocks, a first motor is fixedly installed at the lower part of the front side of the top plate through a first motor shell, the front end of the first threaded rod penetrates through the first sliding groove and is fixedly connected with an output shaft of the first motor, a second motor is fixedly installed at the upper part of the left side of the top plate through a second motor shell, the left end of the second threaded rod penetrates through the second sliding groove and is fixedly connected with an output shaft of the second motor, a protective shell is fixedly installed, lifting buckles are fixedly arranged at four corners of the top end of the top cover.
Preferably, the lower part of the outer side of the top cover is provided with a sealing gasket.
Preferably, four corners of the bottom end of the bottom plate are fixedly provided with heavy casters.
Preferably, the bottom four corners of the top plate are fixedly provided with base plates, the bottom of the base plates is vertically fixedly provided with a telescopic rod, the bottom of the telescopic rod is fixedly connected to the top end of the bottom plate, the outside of the telescopic rod is sleeved with a second spring, and two ends of the second spring are fixedly connected with the base plates and the bottom plate respectively.
Preferably, the inner side of the clamping plate is provided with an anti-skid rubber pad.
Preferably, opposite-direction threads are arranged on the front side and the rear side of the first threaded rod, opposite-direction threads are arranged on the left side and the right side of the second threaded rod, and the second threaded rod is located above the first threaded rod.
Preferably, the height of the first sliding block is twice that of the second sliding block, and the top ends of the first sliding block and the second sliding block are flush with the top end of the top plate.
The utility model provides a pair of spacecraft transport case, beneficial effect lies in: when the lifting device is used, the four lifting buckles are fixedly connected with lifting ropes, the top cover is lifted by the lifting device to be away from the protective shell, the spacecraft is lifted into the protective shell by the lifting device and is positioned at the top end of the top plate, the first motor is started, the output shaft of the first motor rotates to drive the first threaded rod to rotate, the first threaded rod drives the pair of first sliding blocks to move in the first sliding groove along the surfaces of the first sliding blocks, so that the connected clamping plates move close to each other to fix the front side and the rear side of the spacecraft, the second motor is started, the output shaft of the second motor rotates to drive the second threaded rod to rotate so as to drive the pair of second sliding blocks to move in the second sliding groove along the surfaces of the second sliding blocks, so that the connected clamping plates move close to clamp the left side and the right side of the spacecraft, and the distance between the front clamping plate and the rear clamping plate can be adjusted to adapt to the fixation of the front side and the rear side of the, the space between the left clamping plate and the right clamping plate can be adjusted to adapt to the fixation of the left side and the right side of the spacecraft with different sizes, the spacecraft is more stable in transportation by fixing the periphery of the spacecraft, the situation that the spacecraft moves to collide with the protective shell cannot occur, the top cover is hoisted to the protective shell to seal the protective shell after the spacecraft is completed, the top plate drives the second connecting seat to move downwards when being vibrated in the transportation process, the second connecting seat drives the pair of movable blocks to move in the mounting groove along the surface of the slide bar through the pair of connecting rods and the pair of first connecting seats, the movable blocks compress the first spring to deform the first spring to generate acting force during the movement, the acting force generated by the first spring is utilized to buffer the vibration to realize the shock absorption, the telescopic rod and the second spring are compressed downwards when the top plate is vibrated, the acting force generated by the deformation of the second spring buffers the, the protection of the spacecraft can be better realized by damping through multiple buffering.
The utility model discloses simple structure, it is easy and simple to handle, can carry out the centre gripping of all around four sides to the spacecraft of equidimension not fixed for the spacecraft is stable more in the transportation can not appear the condition of collision protecting sheathing, and realizes the shock attenuation through multiple buffering, and better protection spacecraft avoids damaging its inside part, and self is convenient for remove as required, is worth promoting and using.
Drawings
Fig. 1 is a schematic structural view of a spacecraft transport case provided by the present invention;
fig. 2 is a left side view structural schematic diagram of a spacecraft transport case provided by the utility model;
fig. 3 is the utility model provides a section structure schematic diagram is overlooked to spacecraft transport case.
In the figure: the device comprises a bottom plate 1, a mounting groove 2, a sliding rod 3, a moving block 4, a first spring 5, a first connecting seat 6, a connecting rod 7, a second connecting seat 8, a top plate 9, a first sliding groove 10, a first threaded rod 11, a first sliding block 12, a second sliding groove 13, a second threaded rod 14, a second sliding block 15, a clamping plate 16, a first motor 17, a second motor 18, a protective shell 19, a top cover 20, a lifting buckle 21, a sealing gasket 22, a heavy caster 23, a telescopic rod 24, a second spring 25 and a base plate 26.
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.
Referring to fig. 1-3, a spacecraft transport case, includes bottom plate 1, and mounting groove 2 has transversely been seted up on the top of bottom plate 1, and the equal fixed mounting in bottom four corners of bottom plate 1 has heavy truckle 23, and heavy truckle 23 is convenient for the transport case and is removed as required, and heavy truckle 23 has self-locking function, thereby can realize that the locking is fixed the position of transport case.
A slide bar 3 is transversely and fixedly arranged in the mounting groove 2, moving blocks 4 matched with the mounting groove 2 are movably sleeved on the left side and the right side of the slide bar 3, first springs 5 are sleeved on the left side and the right side of the slide bar 3, two ends of each first spring 5 are respectively and fixedly connected with the corresponding moving block 4 and a groove wall, a first connecting seat 6 is fixedly arranged at the top end of each moving block 4, a connecting rod 7 is movably arranged in the middle of each first connecting seat 6, a second connecting seat 8 is movably arranged at the top end of each connecting rod 7, a top plate 9 is fixedly arranged at the top end of each second connecting seat 8, base plates 26 are fixedly arranged at four corners of the bottom end of each top plate 9, a telescopic rod 24 is vertically and fixedly arranged at the bottom end of each base plate 26, the bottom end of each telescopic rod 24 is fixedly connected with the top end of the corresponding, through the cooperation of four telescopic links 24 and second spring 25 can provide the support to roof 9 and make roof 9 more stable, and when roof 9 received vibrations, thereby downwards compression telescopic link 24 and second spring 25, thereby second spring 25 deformation produces the effort and cushions the realization shock attenuation to the power that vibrations produced, protects the spacecraft above roof 9.
A first sliding groove 10 is longitudinally arranged in the middle of the top end of the top plate 9, a first threaded rod 11 is longitudinally movably arranged in the first sliding groove 10 through a pair of first bearings, first sliding blocks 12 matched with the first sliding groove 10 are respectively sleeved on the front side and the rear side of the first threaded rod 11 in a threaded manner, a second sliding groove 13 is transversely arranged on the top end of the top plate 9, the second sliding grooves 13 are distributed in a cross manner with the first sliding groove 10 and are communicated with the first sliding groove 10, a second threaded rod 14 is transversely movably arranged in the second sliding groove 13 through a pair of second bearings, second sliding blocks 15 matched with the second sliding grooves 13 are respectively sleeved on the left side and the right side of the second threaded rod 14 in a threaded manner, opposite-direction threads are arranged on the front side and the rear side of the first threaded rod 11, opposite-direction threads are arranged on the left side and the right side of the second threaded rod 14, the second threaded rod 14 is positioned above the first threaded rod 11, and when the first threaded rod 11 rotates, similarly, the second threaded rod 14 rotates to drive the pair of second sliding blocks 15 to move toward or away from each other.
The height of first slider 12 is the twice of second slider 15, and the top of first slider 12 and second slider 15 all with the top parallel and level of roof 9 to make the splint 16 that first slider 12 and second slider 15 are connected be located same height, and the laminating of the bottom of splint 16 and roof 9 top makes splint 16 use stability better.
The front side lower part of roof 9 has first motor 17 through first motor casing fixed mounting, the output shaft fixed connection of first spout 10 and first motor 17 is passed to the front end of first threaded rod 11, there is second motor 18 on the left side upper portion of roof 9 through second motor casing fixed mounting, the output shaft fixed connection of second spout 13 and second motor 18 is passed to the left end of second threaded rod 14, the top fixed mounting of roof 9 has protecting sheathing 19, top cap 20 is installed on protecting sheathing 19's top, top cap 20's outside lower part is equipped with sealed 22, increase top cap 20's seal nature, prevent that external moisture from entering into the inside part of the inside corrosion ware of protecting sheathing 19.
The working principle is as follows: when in use, the four lifting buckles 21 are fixedly connected with lifting ropes, the top cover 20 is lifted by the lifting device to be away from the protective shell 19, the spacecraft is lifted into the protective shell 19 by the lifting device and is positioned at the top end of the top plate 9, the first motor 17 is started, the output shaft of the first motor 17 rotates to drive the first threaded rod 11 to rotate, the first threaded rod 11 drives the pair of first sliders 12 to move along the surfaces of the first sliders in the first sliding groove 10 in a mutually approaching manner, so as to drive the pair of connected clamping plates 16 to move in a mutually approaching manner to fix the front side and the rear side of the spacecraft, the second motor 18 is started, the output shaft of the second motor 18 rotates to drive the second threaded rod 14 to rotate so as to drive the pair of second sliders 15 to move along the surfaces of the second sliders in the second sliding groove 13 in a mutually approaching manner, so as to drive the pair of connected clamping plates 16 to move in a mutually approaching manner so as to clamp the left side, the space between the front clamping plate 16 and the rear clamping plate 16 can be adjusted to adapt to the fixation of the front side and the rear side of the spacecrafts with different sizes, the space between the left clamping plate 16 and the right clamping plate 16 can be adjusted to adapt to the fixation of the left side and the right side of the spacecrafts with different sizes, the spacecrafts can be more stable in transportation by fixing the periphery of the spacecrafts, the situation that the spacecrafts collide with the protective shell 19 in a moving way can not occur, after the completion, the top cover 20 is hoisted onto the protective shell 19 to seal the protective shell 19, the top plate 9 drives the second connecting seat 8 to move downwards when being vibrated in the transportation process, the second connecting seat 8 drives the pair of moving blocks 4 to move away from each other in the mounting groove 2 along the surface of the sliding rod 3 through the pair of connecting rods 7 and the pair of first connecting seats 6, the moving blocks 4 compress the first spring, realize the shock attenuation, compress telescopic link 24 and second spring 25 downwards when roof 9 receives vibrations simultaneously, thereby second spring 25 deformation produces the effort and cushions the realization shock attenuation to the power that vibrations produced, can be better through multiple buffering carry out the protection that the shock attenuation realized the spacecraft.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (7)
1. A spacecraft transport case comprises a bottom plate (1) and is characterized in that a mounting groove (2) is transversely formed in the top end of the bottom plate (1), a slide bar (3) is transversely and fixedly mounted in the mounting groove (2), moving blocks (4) matched with the mounting groove (2) are movably sleeved on the left side and the right side of the slide bar (3), first springs (5) are sleeved on the left side and the right side of the slide bar (3), two ends of each first spring (5) are respectively and fixedly connected with the corresponding moving block (4) and a groove wall, a first connecting seat (6) is fixedly mounted on the top end of each moving block (4), connecting rods (7) are movably mounted in the middle of each first connecting seat (6), a second connecting seat (8) is movably mounted on the top ends of the two connecting rods (7) together, and a top plate (9) is fixedly mounted on the top end of the second connecting, a first sliding groove (10) is longitudinally formed in the middle of the top end of the top plate (9), a first threaded rod (11) is longitudinally movably mounted inside the first sliding groove (10) through a pair of first bearings, first sliding blocks (12) matched with the first sliding groove (10) are in threaded sleeve connection on the front side and the rear side of the first threaded rod (11), a second sliding groove (13) is transversely formed in the top end of the top plate (9), the second sliding groove (13) and the first sliding groove (10) are in cross distribution and are communicated with the first sliding groove (10), a second threaded rod (14) is transversely movably mounted inside the second sliding groove (13) through a pair of second bearings, second sliding blocks (15) matched with the second sliding groove (13) are in threaded sleeve connection on the left side and the right side of the second threaded rod (14), clamping plates (16) are fixedly mounted on the top ends of the second sliding blocks (15) and the first sliding blocks (12), the utility model discloses a roof, including roof (9), top cover (20), first motor (17) are installed through first motor casing fixed mounting to the front side lower part of roof (9), the output shaft fixed connection of first spout (10) and first motor (17) is passed through to the front end of first threaded rod (11), the left side upper portion of roof (9) has second motor (18) through second motor casing fixed mounting, the output shaft fixed connection of second spout (13) and second motor (18) is passed through to the left end of second threaded rod (14), the top fixed mounting of roof (9) has protecting sheathing (19), top cover (20) are installed on the top of protecting sheathing (19), the equal fixed mounting in top four corners of top cover (20) has lifting buckle (21).
2. A spacecraft transport box according to claim 1, wherein the lower outer side of the roof (20) is provided with a gasket (22).
3. A spacecraft transport case according to claim 1, wherein the bottom four corners of the base plate (1) are each fixedly provided with a heavy caster (23).
4. The spacecraft transport case of claim 1, wherein base plates (26) are fixedly mounted at four corners of the bottom end of the top plate (9), an expansion rod (24) is vertically and fixedly mounted at the bottom end of each base plate (26), the bottom end of each expansion rod (24) is fixedly connected to the top end of the corresponding bottom plate (1), a second spring (25) is sleeved outside each expansion rod (24), and two ends of each second spring (25) are respectively fixedly connected with the corresponding base plate (26) and the corresponding bottom plate (1).
5. A spacecraft transport case according to claim 1, wherein the inner side of the clamping plate (16) is provided with a non-slip rubber pad.
6. A spacecraft transport box according to claim 1, wherein the first threaded bar (11) is provided with threads in opposite directions on the front and rear sides thereof, and the second threaded bar (14) is provided with threads in opposite directions on the left and right sides thereof, and the second threaded bar (14) is positioned above the first threaded bar (11).
7. A spacecraft transport box according to claim 1, wherein the first slider (12) has twice the height of the second slider (15), and the top ends of the first slider (12) and the second slider (15) are flush with the top end of the top plate (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021003106.4U CN212739194U (en) | 2020-06-04 | 2020-06-04 | Spacecraft transport case |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021003106.4U CN212739194U (en) | 2020-06-04 | 2020-06-04 | Spacecraft transport case |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212739194U true CN212739194U (en) | 2021-03-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021003106.4U Active CN212739194U (en) | 2020-06-04 | 2020-06-04 | Spacecraft transport case |
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| Country | Link |
|---|---|
| CN (1) | CN212739194U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113978908A (en) * | 2021-12-10 | 2022-01-28 | 杭州职业技术学院 | Logistics distribution device based on big data |
| CN115108150A (en) * | 2022-08-29 | 2022-09-27 | 阳信诺瑞织品有限公司 | Carpet transportation is with depositing case |
-
2020
- 2020-06-04 CN CN202021003106.4U patent/CN212739194U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113978908A (en) * | 2021-12-10 | 2022-01-28 | 杭州职业技术学院 | Logistics distribution device based on big data |
| CN115108150A (en) * | 2022-08-29 | 2022-09-27 | 阳信诺瑞织品有限公司 | Carpet transportation is with depositing case |
| CN115108150B (en) * | 2022-08-29 | 2022-11-18 | 阳信诺瑞织品有限公司 | Carpet transportation is with depositing case |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230531 Address after: 712000, No. 202, 2nd Floor, Building 2, Block A, New City South, Qianhai Life Insurance Silk Road, Airport New City, Xixian New District, Xianyang City, Shaanxi Province Patentee after: Xi'an Baose New Technology Co.,Ltd. Patentee after: Zhao Feng Address before: 233100 South North Garden team, Hetang village, Hongxin Town, Fengyang County, Chuzhou City, Anhui Province Patentee before: Deng Kaiqiang |
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| TR01 | Transfer of patent right |