CN217705990U - Composite material heat-preservation type flying wing carriage - Google Patents
Composite material heat-preservation type flying wing carriage Download PDFInfo
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- CN217705990U CN217705990U CN202221533686.7U CN202221533686U CN217705990U CN 217705990 U CN217705990 U CN 217705990U CN 202221533686 U CN202221533686 U CN 202221533686U CN 217705990 U CN217705990 U CN 217705990U
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- material heat
- composite material
- preservation type
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- 238000004321 preservation Methods 0.000 title claims abstract description 25
- 239000002131 composite material Substances 0.000 title claims abstract description 19
- 238000005192 partition Methods 0.000 claims abstract description 17
- 230000032258 transport Effects 0.000 abstract description 30
- 239000000463 material Substances 0.000 abstract description 14
- 239000011435 rock Substances 0.000 abstract description 6
- 238000009413 insulation Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model provides a combined material heat preservation type all-wing aircraft carriage. A composite insulated winged vehicle cabin, comprising: a vehicle shell; the middle inside the carriage is fixedly provided with a partition plate, and both sides of the bottom of the outer surface of the partition plate are fixedly provided with bottom plates; the motor cavity set up in the inside bottom of division board, the centre at motor cavity top is provided with sets up the chamber, sets up the centre of chamber surface and is provided with the spout, and the inside in motor cavity is provided with servo motor. The utility model provides a combined material heat preservation type all-wing aircraft carriage rotates through external power source control servo motor's output shaft and drives the positive and negative rotation of threaded rod to meshing stop device reciprocates along the division board, makes stop device remove and pushes down the transport case, and this device simple structure, the practicality is strong, and the protection transport case can not rock when the transportation, has protected the stability when transport case transports.
Description
Technical Field
The utility model relates to a flying wing car field especially relates to a combined material heat preservation type flying wing carriage.
Background
The flying wing vehicle is an improvement of a common van vehicle, can open special vehicles of wing plates on two sides of a carriage through a manual device or a hydraulic device, and is a very popular transport tool for modern logistics enterprises due to the advantages of high loading and unloading speed, high efficiency, side loading and unloading and the like.
The flying wing vehicle becomes the best choice of large-scale commodity circulation company transportation, because in recent years, a large amount of light new materials are applied to wing exhibition vehicle series for the carriage dead weight reduces, and the carriage design is pleasing to the eye, and freight transportation safety and reliability expects to possess a place in high-end commodity circulation transportation market, and van-type two wing vehicle principle is to discharge through the storage battery and promote hydraulic system work through power pack and reach the effect of lifting, and the height of lifting can surpass the carriage, is close to 90 degrees angles.
When the transportation, generally all pack the goods that need transport and put into the box in the carriage is adorned one by one, but the carriage in goods is less sometimes, and the goods box body of loading is less, and vacant space is great in the carriage, and when the transportation, inside goods rocks along with the automobile body easily and collapses, and then damages article.
Therefore, it is necessary to provide a composite material thermal insulation type flying wing vehicle cabin to solve the above technical problems.
SUMMERY OF THE UTILITY MODEL
The utility model provides a combined material heat preservation type all-wing aircraft carriage has solved goods less in the carriage sometimes, and the goods box body of loading is less, and the vacant space is great in the carriage, and when the transportation, inside goods rocks along with the automobile body easily and collapses, and then damages the problem of article.
In order to solve the technical problem, the utility model provides a pair of combined material heat preservation type all-wing aircraft carriage, include: a vehicle shell;
the middle inside the carriage is fixedly provided with a partition plate, and two sides of the bottom of the outer surface of the partition plate are fixedly provided with bottom plates;
the motor cavity is arranged at the bottom of the interior of the partition plate, a setting cavity is arranged in the middle of the top of the motor cavity, a sliding groove is arranged in the middle of the outer surface of the setting cavity, a servo motor is arranged in the motor cavity, and a threaded rod is arranged at one end of an output shaft of the servo motor;
and the limiting device is in threaded engagement with the outer surface of the threaded rod.
Preferably, the limiting device comprises a moving block, a threaded hole is formed in the middle of the top of the moving block, pressing plates are fixedly mounted on two sides of the moving block, and a cushion pad is arranged at the bottom of each pressing plate.
Preferably, the cushion pad is made of rubber.
Preferably, the bottom of the carriage inner cavity is provided with a limiting groove, the bottom of the limiting groove is communicated with a setting groove, and a screw rod is arranged in the setting groove.
Preferably, a thread block is fixedly mounted at the bottom of the partition plate, and a thread groove is formed in one side of the thread block.
Preferably, the bottom of the pressing plate is provided with a limiting groove, a threaded column is arranged inside the limiting groove, and a moving device is meshed with the outer surface of the threaded column in a threaded manner.
Preferably, the moving device comprises a limiting block, a threaded cavity is formed in one side of the limiting block, and a push plate is fixedly connected to the bottom of the limiting block.
Compared with the prior art, the utility model provides a pair of combined material heat preservation type all-wing aircraft carriage has following beneficial effect:
the utility model provides a combined material heat preservation type all-wing aircraft carriage rotates through external power source control servo motor's output shaft and drives the positive and negative rotation of threaded rod to meshing stop device reciprocates along the division board, makes stop device remove and pushes down the transport case, and this device simple structure, the practicality is strong, and the protection transport case can not rock when the transportation, has protected the stability when transport case transports.
Drawings
Fig. 1 is a schematic structural view of a first embodiment of a composite material heat-preservation type flying wing vehicle compartment provided by the present invention;
FIG. 2 is a schematic view of the structure of the position limiting device shown in FIG. 1;
FIG. 3 is an enlarged view of portion A of FIG. 1;
FIG. 4 is an enlarged view of the portion B shown in FIG. 1;
FIG. 5 is a schematic structural view of a second embodiment of a composite material thermal insulation type flying wing car
Fig. 6 is an enlarged schematic view of the portion C shown in fig. 5.
Reference numbers in the figures: 1. the car shell, 2, the winged door, 3, the carriage, 4, the division board, 5, stop device, 51, the movable block, 52, the screw hole, 53, the clamp plate, 54, the rubber pad, 6, the bottom plate, 7, servo motor, 8, set up the chamber, 9, the threaded rod, 10, the spout, 11, the motor chamber, 12, set up the groove, 13, the spacing groove, 14, the screw block, 15, the thread groove, 16, the lead screw, 17, the spacing groove, 18, the screw post, 19, the mobile device, 191, the stopper, 192, the thread chamber, 193, the push pedal.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and embodiments.
Referring to fig. 1, fig. 2, fig. 3 and fig. 4, wherein fig. 1 is a schematic structural view of a composite material thermal insulation type all-wing vehicle cabin according to a first embodiment of the present invention; FIG. 2 is a schematic view of the structure of the limiting device shown in FIG. 1; FIG. 3 is an enlarged view of portion A of FIG. 1; fig. 4 is an enlarged schematic view of a portion B shown in fig. 1. A composite insulated winged vehicle cabin comprising: a vehicle case 1;
the middle inside the carriage 3 is fixedly provided with a partition plate 4, and two sides of the bottom of the outer surface of the partition plate 4 are fixedly provided with bottom plates 6;
the motor cavity 11 is arranged at the bottom inside the partition plate 4, the middle of the top of the motor cavity 11 is provided with a setting cavity 8, the middle of the outer surface of the setting cavity 8 is provided with a sliding chute 10, the inside of the motor cavity 11 is provided with a servo motor 7, and one end of an output shaft of the servo motor 7 is provided with a threaded rod 9;
and the limiting device 5 is in threaded engagement with the outer surface of the threaded rod 9.
The threaded rod 9 is arranged in the arrangement cavity 8, the moving block 51 is in threaded engagement with the outer surface of the threaded rod 9 through the threaded hole 52, and the moving block 51 slides up and down in the sliding groove 10.
The interior of the carriage is made of heat-preservation composite materials, and the carriage has a good heat-preservation effect.
The limiting device 5 comprises a moving block 51, a threaded hole 52 is formed in the middle of the top of the moving block 51, pressing plates 53 are fixedly mounted on two sides of the moving block 51, and a buffering pad 54 is arranged at the bottom of each pressing plate 53.
Stop device 5 is provided with four, and two clamp plates 53 are fixed respectively in the left and right sides of movable block 51, and blotter 54 is used for the extrusion transport case and can not damage the transport case, strengthens the frictional force between stop device 5 and the transport case, reduces and rocks.
The cushion pad 54 is made of rubber.
The bottom of the inner cavity of the carriage 3 is provided with a limiting groove 13, the bottom of the limiting groove 13 is communicated with a setting groove 12, and a screw rod 16 is arranged inside the setting groove 12.
The screw block 14 is limited by the limiting groove 13 and can only move left and right, the screw rod 16 is arranged in the arrangement groove 12, and the left end and the right end of the screw rod 16 respectively extend out of the left side and the right side of the vehicle shell 1, so that a user can conveniently rotate the screw rod 16.
A thread block 14 is fixedly mounted at the bottom of the partition plate 4, and a thread groove 15 is formed in one side of the thread block 14.
When a user rotates the screw rod 16 to be meshed with the thread block 14, the thread block moves left and right, so that the partition plate 4 moves left and right and is moved out of the carriage 3, and the transport box close to the inside and close to the partition plate 4 is taken out by the user conveniently.
The utility model provides a pair of combined material heat preservation type all-wing aircraft carriage's theory of operation as follows:
during operation, the transport box is firstly placed on the top of the bottom plate 6, other transport boxes are placed on the top of the pressing plate 53, and then the output shaft of the servo motor 7 is controlled by the external power supply to rotate so as to drive the threaded rod 9 to rotate and engage with the threaded hole 52 of the moving block 51, so that the pressing plate 53 moves downwards.
The pressing plate 53 presses the top of the transport case through the cushion pad 54 to limit the transport case and keep the transport case stable.
When the transport box is detached, the output shaft of the servo motor 7 is controlled to rotate reversely by an external power supply, so that the pressure plate 53 loosens the transport box.
Compared with the prior art, the utility model provides a pair of combined material heat preservation type all-wing aircraft carriage has following beneficial effect:
the utility model provides a combined material heat preservation type all-wing aircraft carriage rotates through external power source control servo motor 7's output shaft and drives threaded rod 9 just reverse rotation to meshing stop device 5 reciprocates along division board 4, makes stop device 5 remove and pushes down the transport case, this device simple structure, and the practicality is strong, and the protection transport case can not rock when the transportation, has protected the stability when transport case transports.
Second embodiment
Referring to fig. 5 and 6 in combination, a composite material thermal insulation type flying wing vehicle cabin is provided based on the first embodiment of the present application, and a second embodiment of the present application provides another composite material thermal insulation type flying wing vehicle cabin. The second embodiment is only the preferred mode of the first embodiment, and the implementation of the second embodiment does not affect the implementation of the first embodiment alone.
Specifically, the composite material heat preservation type all-wing vehicle compartment provided in the second embodiment of the present application is different in that a limiting groove 17 is provided at the bottom of the pressing plate 53, a threaded column 18 is provided inside the limiting groove 17, and a moving device 19 is threadedly engaged with the outer surface of the threaded column 18.
The end of the threaded post 18 remote from the divider plate 4 extends beyond the outer surface of the pressure plate 53 for easy rotation.
The moving device 19 comprises a limiting block 191, a threaded cavity 192 is arranged on one side of the limiting block 191, and a push plate 193 is fixedly connected to the bottom of the limiting block 191.
The threaded cavity 192 is disposed on the side of the stop block 191 close to the separation plate 4 and extends to the outside of the side far from the separation plate 4, and the threaded cavity 192 is in threaded engagement with the threaded post 18.
The utility model provides a pair of combined material heat preservation type all-wing aircraft carriage's theory of operation as follows:
during operation, the threaded column 18 is rotated to be meshed with the threaded cavity 192 of the limiting block 191, the limiting block 191 slides along the limiting groove 17, and the push plate 193 pushes the transport case out to facilitate carrying.
After the transport case is taken out, the threaded column 18 is rotated reversely, so that the push plate 193 is close to the partition plate 4, and the transport case can be loaded next time.
Compared with the prior art, the utility model provides a pair of combined material heat preservation type all-wing aircraft carriage has following beneficial effect:
the utility model provides a combined material heat preservation type all-wing aircraft carriage drives push pedal 193 through the screw thread chamber 192 that rotates 18 meshing stoppers 191 of screw thread post and removes for push pedal 193 releases the transport case, this device simple structure, and the practicality is strong, and the person of facilitating the use transport case of taking.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.
Claims (7)
1. A composite material heat preservation type all-wing vehicle carriage is characterized by comprising: a vehicle shell;
the middle inside the carriage is fixedly provided with a partition plate, and two sides of the bottom of the outer surface of the partition plate are fixedly provided with bottom plates;
the motor cavity is arranged at the bottom of the interior of the partition plate, a setting cavity is arranged in the middle of the top of the motor cavity, a sliding groove is arranged in the middle of the outer surface of the setting cavity, a servo motor is arranged in the motor cavity, and a threaded rod is arranged at one end of an output shaft of the servo motor;
and the limiting device is in threaded engagement with the outer surface of the threaded rod.
2. The composite material heat-preservation type flying wing carriage according to claim 1, wherein the limiting device comprises a moving block, a threaded hole is formed in the middle of the top of the moving block, pressing plates are fixedly mounted on two sides of the moving block, and a cushion pad is arranged at the bottom of each pressing plate.
3. The composite material heat-insulating type flying wing vehicle compartment according to claim 2, wherein the cushion is made of rubber.
4. The composite material heat-preservation type flying wing carriage according to claim 1, wherein a limiting groove is formed in the bottom of the inner cavity of the carriage, the bottom of the limiting groove is communicated with a setting groove, and a screw rod is arranged inside the setting groove.
5. The composite material heat preservation type flying wing vehicle compartment according to claim 1, wherein a threaded block is fixedly mounted at the bottom of the partition plate, and a threaded groove is formed in one side of the threaded block.
6. The composite material heat-preservation type flying wing carriage according to claim 2, wherein a limiting groove is formed in the bottom of the pressing plate, a threaded column is arranged inside the limiting groove, and a moving device is meshed with the outer surface of the threaded column in a threaded manner.
7. The composite material heat-preservation type flying wing carriage according to claim 6, wherein the moving device comprises a limiting block, a threaded cavity is arranged on one side of the limiting block, and a push plate is fixedly connected to the bottom of the limiting block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221533686.7U CN217705990U (en) | 2022-06-17 | 2022-06-17 | Composite material heat-preservation type flying wing carriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221533686.7U CN217705990U (en) | 2022-06-17 | 2022-06-17 | Composite material heat-preservation type flying wing carriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217705990U true CN217705990U (en) | 2022-11-01 |
Family
ID=83800455
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221533686.7U Active CN217705990U (en) | 2022-06-17 | 2022-06-17 | Composite material heat-preservation type flying wing carriage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217705990U (en) |
-
2022
- 2022-06-17 CN CN202221533686.7U patent/CN217705990U/en active Active
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