CN220501021U - Unmanned aerial vehicle with quick loading and unloading structure for material transportation - Google Patents
Unmanned aerial vehicle with quick loading and unloading structure for material transportation Download PDFInfo
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- CN220501021U CN220501021U CN202321398493.XU CN202321398493U CN220501021U CN 220501021 U CN220501021 U CN 220501021U CN 202321398493 U CN202321398493 U CN 202321398493U CN 220501021 U CN220501021 U CN 220501021U
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- 239000000463 material Substances 0.000 title claims abstract description 68
- 230000007246 mechanism Effects 0.000 claims abstract description 11
- 230000001681 protective effect Effects 0.000 claims description 5
- 238000009434 installation Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 8
- 238000005457 optimization Methods 0.000 description 6
- 230000005540 biological transmission Effects 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle with a quick loading and unloading structure for transporting materials, which belongs to the technical field of material transportation, and the technical scheme is characterized by comprising a shell, wherein the bottom of the shell is provided with a clamping mechanism, the top of the shell is provided with a mounting assembly, the bottom of the shell is provided with a supporting assembly, and the materials can be fixed in a certain space by clamping the materials through the clamping mechanism when the unmanned aerial vehicle is used, so that the unmanned aerial vehicle is prevented from jolting when flying at high altitude, and the materials are prevented from displacing to cause accidents; the clamping mechanism can be arranged below the unmanned aerial vehicle by arranging the mounting assembly, and the mounting assembly is convenient to mount and dismount in the subsequent use process; through setting up supporting component, when using, can make the casing stand subaerial, also can lift the bottom limit of goods and materials simultaneously, prevent to drop in jolting the goods and materials, the setting of convenient to detach and installation simultaneously can be more convenient put into and take out the goods and materials.
Description
Technical Field
The utility model relates to the technical field of material transportation, in particular to an unmanned aerial vehicle with a quick loading and unloading structure for material transportation.
Background
Unmanned aerial vehicle transportation refers to the technical means such as through remote control unmanned aerial vehicle, install cargo hold and corresponding transmission device on unmanned aerial vehicle, utilize unmanned aerial vehicle to accomplish tasks such as transportation, delivery, along with unmanned aerial vehicle technology's continuous development, unmanned aerial vehicle transportation has obtained extensive application in many fields, for example express delivery goods, urban delivery, consumer electronics accessory transport, medical supplies transportation, agricultural plant protection etc., in unmanned aerial vehicle transportation, generally adopt multiaxis unmanned aerial vehicle, such as four-axis, eight axles etc. have advantages such as portable, nimble, energy-conserving, simultaneously, unmanned aerial vehicle transportation still needs to be equipped with hardware equipment such as sensor, battery, remote controller, and corresponding software system, realize unmanned aerial vehicle's autonomous flight, transmission, operation such as landing.
The current announcements are: CN207889991U discloses a material carrying platform of unmanned aerial vehicle, which comprises a main body, the spout has been seted up to the upper surface of main part, sliding connection has the baffle in the spout, the upper surface of main part is equipped with the switch, the input of switch and the output electricity of power are connected, the lower surface of baffle is equipped with the connecting plate, the lower surface of main part is equipped with the motor, the input of motor and the output electricity of switch are connected, the output shaft of motor passes through the shaft coupling and is connected with drive screw, screw threaded connection that drive screw and connecting plate upper surface were seted up, this material carrying platform of unmanned aerial vehicle has improved the stability of transportation, safer during the use, and the performance requirement to miniature unmanned aerial vehicle is lower, the cost of transportation has been reduced, the motor passes through drive screw and has moved the connecting plate, thereby make the baffle remove, it can to block the article that carries in the main part, make the baffle whereabouts when taking out, the article of being convenient for take.
This patent possesses the stability that has improved the transportation, and safer during the use, and lower to miniature unmanned aerial vehicle's performance requirement, the article of being convenient for take, convenient to use's effect, but in the in-service use, the goods and materials that can carry are limited to lack fixed protection's function, among the prior art, because the baffle has the space, when transporting too little goods and materials, can take place jolting and make the goods and materials drop, lack fixed protection to the goods and materials.
Disclosure of Invention
1. Technical problem to be solved
The utility model provides an unmanned aerial vehicle with a quick loading and unloading structure for material transportation, and aims to solve the problems that the existing unmanned aerial vehicle with the quick loading and unloading structure for material transportation is limited in carried materials and lacks of fixed protection for the materials.
2. Technical proposal
The utility model discloses an unmanned aerial vehicle with a quick loading and unloading structure for material transportation, which comprises a shell, wherein a clamping mechanism is arranged at the bottom of the shell, a mounting assembly is arranged at the top of the shell, and a supporting assembly is arranged at the bottom of the shell;
the clamping assembly comprises a servo motor, a rotating column, gears, sliding grooves, sliding blocks, clamping plates and racks, wherein the servo motor is bolted to the top of a shell, the rotating column is fixedly connected with an output shaft of the servo motor, the gears are fixedly connected to one side wall of the rotating column, the sliding grooves are formed in the bottom of the shell, the sliding blocks are slidably connected to the inside of the sliding grooves, the clamping plates are welded to the bottom of the sliding blocks, and the racks are welded to one side wall of the clamping plates respectively and meshed with the gears.
In order to achieve the effect of fixing the shell at the bottom of the unmanned aerial vehicle, the unmanned aerial vehicle with the rapid loading and unloading structure for transporting materials is preferable, the installation assembly comprises a support column and threaded holes, a plurality of support columns are welded at the top of the shell, and the threaded holes are respectively formed in the support columns.
In order to achieve the bottom limiting lifting effect of materials, the unmanned aerial vehicle with the rapid loading and unloading structure for transporting materials is preferable, wherein the supporting assembly comprises supporting legs, extending plates, supporting bars, supporting plates and threaded rods, a plurality of supporting legs are welded at the bottom of the shell, a plurality of extending plates are respectively welded on one side wall of the shell, a plurality of supporting bars are respectively welded at the bottom of the extending plates, the supporting plates are hinged on one side wall of the supporting bars, the threaded rods are respectively connected with the bottom of the supporting plates in a threaded mode, and one ends of the threaded rods penetrate into the supporting bars and are connected with the supporting bars in a threaded mode.
In order to achieve the effect of providing a certain buffer for the unmanned aerial vehicle when the unmanned aerial vehicle falls to the ground, the unmanned aerial vehicle with the rapid loading and unloading structure for transporting materials is preferable in the utility model, and rubber pads are welded at the bottoms of the supporting legs.
In order to achieve the effect of protecting the servo motor, the unmanned aerial vehicle with the rapid loading and unloading structure for transporting materials is preferable, and a protective shell is welded at the top of the shell.
In order to achieve a more stable effect of clamping materials, the unmanned aerial vehicle with a rapid loading and unloading structure for transporting materials is preferable, wherein a rubber plate is welded on one side wall of the clamping plates.
In order to achieve the effect of limiting racks, the unmanned aerial vehicle with the rapid loading and unloading structure for material transportation is preferable, and one side wall of each of the racks is welded with a limiting plate.
3. Advantageous effects
Compared with the prior art, the utility model has the beneficial effects that:
according to the unmanned aerial vehicle with the rapid loading and unloading structure for transporting the materials, the clamping mechanism is arranged, so that the materials can be fixed in a certain space by clamping the materials when the unmanned aerial vehicle is used, the unmanned aerial vehicle is prevented from jolting when flying at high altitude, and the materials are prevented from being displaced to cause accidents; the clamping mechanism can be arranged below the unmanned aerial vehicle by arranging the mounting assembly, and the mounting assembly is convenient to mount and dismount in the subsequent use process; through setting up supporting component, when using, can make the casing stand subaerial, also can lift the bottom limit of goods and materials simultaneously, prevent to drop in jolting the goods and materials, the setting of convenient to detach and installation simultaneously can be more convenient put into and take out the goods and materials.
Drawings
FIG. 1 is an overall block diagram of the present utility model;
FIG. 2 is a schematic view of the right side cross-sectional structure of the present utility model;
FIG. 3 is an enlarged view of the FIG. 2A embodiment of the present utility model;
FIG. 4 is a schematic view of a support assembly according to the present utility model;
fig. 5 is an enlarged view of the present utility model at B in fig. 4.
The reference numerals in the figures illustrate:
1. a housing; 2. a clamping mechanism; 3. a mounting assembly; 4. a support assembly; 201. a servo motor; 202. rotating the column; 203. a gear; 204. a sliding groove; 205. a sliding block; 206. a clamping plate; 207. a rack; 301. a support column; 302. a threaded hole; 401. support legs; 402. an extension plate; 403. a support bar; 404. a support plate; 405. a threaded rod; 5. a rubber pad; 6. a protective shell; 7. a rubber plate; 8. and a limiting plate.
Detailed Description
The present utility model will be further described in detail with reference to the drawings and examples, in order to achieve the objects, technical solutions and advantages of the present utility model. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the utility model.
In the description of the present utility model, it should be understood that the terms "length," "width," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, merely to facilitate describing the present utility model and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present utility model. Furthermore, in the description of the present utility model, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
Referring to fig. 1-5, the present utility model provides the following technical solutions: the unmanned aerial vehicle with the quick loading and unloading structure for material transportation comprises a shell 1, wherein a clamping mechanism 2 is arranged at the bottom of the shell 1, a mounting assembly 3 is arranged at the top of the shell 1, and a supporting assembly 4 is arranged at the bottom of the shell 1;
the clamping assembly comprises a servo motor 201, a rotating column 202, a gear 203, a sliding groove 204, a sliding block 205, a clamping plate 206 and a rack 207, wherein the servo motor 201 is bolted to the top of the shell 1, the rotating column 202 is fixedly connected to an output shaft of the servo motor 201, the gear 203 is fixedly connected to one side wall of the rotating column 202, the sliding grooves 204 are formed in the bottom of the shell 1, the sliding blocks 205 are slidably connected to the inside of the sliding grooves 204, the clamping plates 206 are welded to the bottom of the sliding blocks 205, and the racks 207 are respectively welded to one side wall of the clamping plate 206 and meshed with the gear 203.
In this embodiment: through setting up fixture 2, can be through cliying the supplies during the use, fix the supplies in certain space, prevent unmanned aerial vehicle from jolting when flying in the high altitude, make the supplies take place the displacement, cause the accident; by arranging the mounting assembly 3, the clamping mechanism 2 can be mounted below the unmanned aerial vehicle, and the mounting assembly is convenient to mount and dismount in the subsequent use process; through setting up the supporting component 4, when using, can make casing 1 stand on ground, also can be to the spacing lifting in bottom of goods and materials simultaneously, prevent that the goods and materials from dropping in jolting, the setting of convenient to detach and installation simultaneously can more convenient put into and take out the goods and materials; through setting up servo motor 201, rotation post 202, gear 203, sliding tray 204, sliding block 205, grip block 206 and rack 207, start servo motor 201 can drive rotation post 202 and gear 203 rotation, and gear 203 and rack 207 meshing can make rack 207 drive grip block 206 slide in sliding tray 204 in the rotatory in-process, makes grip block 206 keep away from the goods and materials or be close to the goods and materials, conveniently fixes the goods and materials or take out the goods and materials.
As a technical optimization scheme of the utility model, the mounting assembly 3 comprises a support column 301 and a threaded hole 302, wherein a plurality of support columns 301 are welded on the top of the shell 1, and the threaded holes 302 are respectively formed in the support columns 301.
In this embodiment: through setting up support column 301 and screw hole 302, can make casing 1 fix in unmanned aerial vehicle's bottom through screw hole 302, also easy to assemble and dismantlement in the subsequent use.
As a technical optimization scheme of the present utility model, the support assembly 4 includes a support leg 401, an extension plate 402, a support bar 403, a support bar 404 and a threaded rod 405, wherein the support legs 401 are welded at the bottom of the casing 1, the extension plates 402 are respectively welded on one side wall of the casing 1, the support bar 403 are respectively welded at the bottom of the extension plates 402, the support bar 404 is hinged on one side wall of the support bar 403, the threaded rods 405 are respectively connected at the bottom of the support bar 404 in a threaded manner, and one ends of the threaded rods 405 penetrate into the inside of the support bars 403 and are connected with the support bars 403 in a threaded manner.
In this embodiment: through setting up supporting leg 401, extension board 402, support bar 403, backup pad 404 and threaded rod 405, when using, supporting leg 401 can make casing 1 stand on ground, and support bar 403 and backup pad 404 cooperation use can be to the spacing lift in bottom of goods and materials, prevent that the goods and materials from dropping in jolting, screw up threaded rod 405 can make backup pad 404 fix in the bottom of support bar 403, when putting into the goods and materials, only need screw out threaded rod 405 can.
As a technical optimization scheme of the present utility model, rubber pads 5 are welded to the bottoms of the plurality of support legs 401.
In this embodiment: through setting up rubber pad 5, can make unmanned aerial vehicle provide certain buffering when falling to the ground, prevent damage unmanned aerial vehicle.
As a technical optimization scheme of the utility model, a protective shell 6 is welded on the top of the shell 1.
In this embodiment: by providing the protective case 6, protection can be provided to the servo motor 201.
As a technical optimization scheme of the present utility model, a rubber plate 7 is welded to one side wall of the plurality of clamping plates 206.
In this embodiment: through setting up rubber slab 7, can increase the friction of grip block 206 to the material, the material is cliied to the ability more firm, prevents simultaneously that grip block 206 from excessively hard causing the damage to the material.
As a technical optimization scheme of the utility model, a limiting plate 8 is welded on one side wall of the racks 207.
In this embodiment: by providing the limiting plate 8, the rack 207 can be limited, and the movement range of the gear 203 can be prevented from being separated.
Working principle: firstly, fix casing 1 below unmanned aerial vehicle through screw hole 302, when putting into the material, screw out threaded rod 405, rotate backup pad 404, put the material in the centre of grip block 206, start servo motor 201 and drive rotation post 202 and gear 203 rotation, make rack 207 drive grip block 206 and be close to the material, close servo motor 201 after gripping the material, reverse rotation backup pad 404, fix backup pad 404 below support bar 403 through threaded rod 405, just can start unmanned aerial vehicle and carry out the goods, take out the material and make only need screw out threaded rod 405, reverse servo motor 201 can take out the material, rubber pad 5 below supporting leg 401 can make unmanned aerial vehicle provide certain buffering when falling to the ground, prevent to damage unmanned aerial vehicle, rubber plate 7 can increase the friction of grip block 206 to the material, can more firmly clip the material, prevent grip block 206 from excessively hard causing the damage to the material simultaneously.
The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, and alternatives falling within the spirit and principles of the utility model.
Claims (7)
1. Unmanned aerial vehicle with fast loading and unloading structure for material transportation, including casing (1), its characterized in that: the bottom of the shell (1) is provided with a clamping mechanism (2), the top of the shell (1) is provided with a mounting assembly (3), and the bottom of the shell (1) is provided with a supporting assembly (4);
the clamping mechanism comprises a servo motor (201), a rotating column (202), a gear (203), a sliding groove (204), sliding blocks (205), clamping plates (206) and racks (207), wherein the servo motor (201) is bolted to the top of a shell (1), the rotating column (202) is fixedly connected to an output shaft of the servo motor (201), the gear (203) is fixedly connected to one side wall of the rotating column (202), a plurality of sliding grooves (204) are formed in the bottom of the shell (1), the sliding blocks (205) are slidably connected to the inside of the sliding grooves (204), the clamping plates (206) are welded to the bottom of the sliding blocks (205), and the racks (207) are welded to one side wall of the clamping plates (206) respectively and are meshed with the gears (203).
2. The unmanned aerial vehicle with a quick loading and unloading structure for transporting materials according to claim 1, wherein: the mounting assembly (3) comprises support columns (301) and threaded holes (302), a plurality of support columns (301) are welded at the top of the shell (1), and the threaded holes (302) are respectively formed in the support columns (301).
3. The unmanned aerial vehicle with a quick loading and unloading structure for transporting materials according to claim 1, wherein: the support assembly (4) comprises support legs (401), extension plates (402), support bars (403), support plates (404) and threaded rods (405), wherein a plurality of support legs (401) are welded at the bottom of the shell (1), a plurality of extension plates (402) are welded on one side wall of the shell (1) respectively, a plurality of support bars (403) are welded at the bottoms of the extension plates (402) respectively, the support plates (404) are hinged on one side wall of the support bars (403), a plurality of threaded rods (405) are connected with the bottoms of the support plates (404) in a threaded mode respectively, and one ends of the threaded rods (405) penetrate into the inside of the support bars (403) and are connected with the support bars (403) in a threaded mode.
4. A unmanned aerial vehicle with a quick-loading and unloading structure for transporting materials according to claim 3, wherein: rubber pads (5) are welded at the bottoms of the supporting legs (401).
5. The unmanned aerial vehicle with a quick loading and unloading structure for transporting materials according to claim 1, wherein: a protective shell (6) is welded at the top of the shell (1).
6. The unmanned aerial vehicle with a quick loading and unloading structure for transporting materials according to claim 1, wherein: a rubber plate (7) is welded to one side wall of the plurality of clamping plates (206).
7. The unmanned aerial vehicle with a quick loading and unloading structure for transporting materials according to claim 1, wherein: a limiting plate (8) is welded on one side wall of the racks (207).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321398493.XU CN220501021U (en) | 2023-06-02 | 2023-06-02 | Unmanned aerial vehicle with quick loading and unloading structure for material transportation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321398493.XU CN220501021U (en) | 2023-06-02 | 2023-06-02 | Unmanned aerial vehicle with quick loading and unloading structure for material transportation |
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| Publication Number | Publication Date |
|---|---|
| CN220501021U true CN220501021U (en) | 2024-02-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321398493.XU Active CN220501021U (en) | 2023-06-02 | 2023-06-02 | Unmanned aerial vehicle with quick loading and unloading structure for material transportation |
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| Country | Link |
|---|---|
| CN (1) | CN220501021U (en) |
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2023
- 2023-06-02 CN CN202321398493.XU patent/CN220501021U/en active Active
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