CN221294183U - Landing charging apron monitoring device for unmanned aerial vehicle - Google Patents
Landing charging apron monitoring device for unmanned aerial vehicle Download PDFInfo
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- CN221294183U CN221294183U CN202323023234.1U CN202323023234U CN221294183U CN 221294183 U CN221294183 U CN 221294183U CN 202323023234 U CN202323023234 U CN 202323023234U CN 221294183 U CN221294183 U CN 221294183U
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- fixedly connected
- unmanned aerial
- aerial vehicle
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- 238000012806 monitoring device Methods 0.000 title claims abstract description 18
- 230000007246 mechanism Effects 0.000 claims abstract description 23
- 230000017525 heat dissipation Effects 0.000 claims description 3
- 238000012544 monitoring process Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 5
- 230000005540 biological transmission Effects 0.000 abstract description 3
- 230000008569 process Effects 0.000 abstract description 3
- 230000006698 induction Effects 0.000 description 5
- 230000004044 response Effects 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model discloses a landing charging apron monitoring device for an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The utility model comprises a shell, wherein the shell comprises a buffer mechanism, the buffer mechanism comprises a plurality of fixed blocks fixedly connected to the inner wall of the shell, the top surface of each fixed block is fixedly connected with two first sliding rods, the top surface of each fixed block is fixedly connected with a second sliding rod, the outer surface of each second sliding rod is wound with a spring, the outer surface of each second sliding rod is slidably connected with a moving block, each first sliding rod penetrates through each moving block, each first sliding rod is slidably connected with each moving block, and the side surface of each moving block is fixedly connected with an L-shaped supporting plate; according to the utility model, the buffer mechanism is arranged, so that when the unmanned aerial vehicle falls on the top surface of the power supply assembly, the spring can be compressed to absorb energy generated in the falling process, and the spring can effectively reduce the transmission of impact force.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to a landing charging apron monitoring device for an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is the aircraft that obtains rapid development in recent years, has advantages such as the cost is lower and convenient to use, is widely used in a plurality of fields such as scientific research, industry, commodity circulation transportation, agriculture, military, and unmanned aerial vehicle has various functions, makes it adapt to various different demands, and unmanned aerial vehicle can be equipped with various sensors and equipment, for example high resolution camera, thermal infrared imager and laser radar etc. in order to carry out various tasks.
In the prior art, through retrieving, found that chinese patent discloses "a device for unmanned aerial vehicle drops and charges", and its application number is "CN202121230856.X", and this patent mainly can let unmanned aerial vehicle's electric port access power, can also avoid unmanned aerial vehicle to break away from on the charge plate simultaneously, is unmanned aerial vehicle charges more stably.
But the device is not provided with buffer gear, and unmanned aerial vehicle can receive great impact force when the landing on the charging plate to lead to the damage of equipment, perhaps make unmanned aerial vehicle unable normal work even, this will need more frequent maintenance and change, has increased use cost and maintenance difficulty, and the device does not set up fixed mechanism and fixes unmanned aerial vehicle's position, only relies on the electric port to fail to ensure the stability when unmanned aerial vehicle charges normally.
Disclosure of utility model
The utility model aims to provide a landing charging apron monitoring device for an unmanned aerial vehicle, which solves the problem of large buffering force when the unmanned aerial vehicle lands on a charging plate, and is provided with an induction module which is mutually connected with a buffering mechanism, so that the electric leakage danger of the charging plate during long-term power supply is avoided, and the overall safety and reliability of the device are ensured.
In order to solve the technical problems, the utility model is realized by the following technical scheme:
The utility model relates to a landing charging apron monitoring device for an unmanned aerial vehicle, which comprises a shell, wherein the shell comprises a buffer mechanism and a charging mechanism;
the buffer mechanism comprises a plurality of fixed blocks fixedly connected to the inner wall of the shell, the top surface of each fixed block is fixedly connected with two first sliding rods, the top surface of each fixed block is fixedly connected with a second sliding rod, springs are wound on the outer surfaces of the second sliding rods, moving blocks are slidably connected to the outer surfaces of the second sliding rods, the top ends of the springs are fixedly connected with the bottom surfaces of the moving blocks, the bottom ends of the springs are fixedly connected with the top surfaces of the fixed blocks, the first sliding rods penetrate through the moving blocks, the first sliding rods are slidably connected with the moving blocks, the side surfaces of the moving blocks are fixedly connected with L-shaped supporting plates, first sensing modules are arranged on the side surfaces of the moving blocks, and second sensing modules are arranged on the side surfaces of the fixed blocks.
Further, the charging mechanism comprises a power supply assembly and a fixing assembly, wherein the power supply assembly is fixedly connected to the top surface of the L-shaped supporting plate, the power supply assembly comprises a power supply socket arranged on the top surface of the power supply assembly, and a plurality of grooves are formed in the top surface of the power supply assembly.
Further, fixed subassembly includes a plurality of slide rails of fixed connection at power supply module top surface, the slide rail is located the top of recess, the surface sliding connection of slide rail has two electric sliders, the side surface fixedly connected with limiting plate of slide rail, the side surface fixedly connected with grip block of electric sliders.
Further, the top surface of shell is provided with control sensing module.
Further, the side surface of the housing is provided with a plurality of heat dissipation holes.
Further, the bottom surface of shell fixedly connected with four supporting baseplate.
The utility model has the following beneficial effects:
1. According to the utility model, the buffer mechanism is arranged, so that the unmanned aerial vehicle can be compressed when falling on the top surface of the power supply assembly, energy generated in the falling process is absorbed, the transmission of impact force can be effectively reduced by the spring, the damage to the power supply assembly or the unmanned aerial vehicle is prevented, in addition, the buffer mechanism can also provide stable support, the unmanned aerial vehicle can be balanced in the falling process, the integrity of the power supply assembly and the normal operation of the unmanned aerial vehicle are ensured, and the service life of the unmanned aerial vehicle is prolonged.
2. According to the utility model, the fixing assembly is arranged, so that when the unmanned aerial vehicle falls on the top surface of the power supply assembly, the first induction module is connected with the second induction module, and the electric sliding block drives the clamping plates to be close to each other, so that the bottom of the unmanned aerial vehicle is fixed, the stability of the whole device is improved, and the unmanned aerial vehicle can be stably charged.
Of course, it is not necessary for any one product to practice the utility model to achieve all of the advantages set forth above at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic diagram of the overall structure of a landing charging apron monitoring device for an unmanned aerial vehicle according to the present utility model;
FIG. 2 is a schematic top cross-sectional view of a landing charge tarmac monitoring device for an unmanned aerial vehicle according to the present utility model;
FIG. 3 is a schematic structural view of a buffer mechanism for a landing charge tarmac monitoring device for an unmanned aerial vehicle according to the present utility model;
Fig. 4 is a schematic structural view of a charging mechanism for a landing charging apron monitoring device of an unmanned aerial vehicle according to the present utility model;
fig. 5 is a schematic structural view of a fixing assembly of a landing charging apron monitoring device for an unmanned aerial vehicle according to the present utility model.
In the drawings, the list of components represented by the various numbers is as follows:
1. A housing; 2. a buffer mechanism; 3. a charging mechanism; 11. monitoring the induction module; 12. a heat radiation hole; 13. a support base plate; 21. a fixed block; 22. a first slide bar; 23. a second slide bar; 24. a spring; 25. a moving block; 26. an L-shaped support plate; 27. a first sensing module; 28. a second sensing module; 31. a power supply assembly; 311. a power supply socket; 312. a groove; 32. a fixing assembly; 321. a slide rail; 322. an electric slide block; 323. a limiting plate; 324. and a clamping plate.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, the utility model relates to a landing charging apron monitoring device for an unmanned aerial vehicle, which comprises a shell 1, wherein the shell 1 comprises a buffer mechanism 2 and a charging mechanism 3;
The buffer mechanism 2 comprises a plurality of fixed blocks 21 fixedly connected to the inner wall of the shell 1, the top surface of each fixed block 21 is fixedly connected with two first sliding rods 22, the top surface of each fixed block 21 is fixedly connected with a second sliding rod 23, the outer surface of each second sliding rod 23 is wound with a spring 24, the outer surface of each second sliding rod 23 is slidably connected with a moving block 25, the top end of each spring 24 is fixedly connected with the bottom surface of each moving block 25, the bottom end of each spring 24 is fixedly connected with the top surface of each fixed block 21, each first sliding rod 22 penetrates through each moving block 25, each first sliding rod 22 is slidably connected with each moving block 25, the side surface of each moving block 25 is fixedly connected with an L-shaped supporting plate 26, each side surface of each moving block 25 is provided with a first sensing module 27, and each side surface of each fixed block 21 is provided with a second sensing module 28.
As shown in fig. 4, the charging mechanism 3 includes a power supply assembly 31 and a fixing assembly 32, the power supply assembly 31 is fixedly connected to the top surface of the L-shaped support plate 26, the power supply assembly 31 includes a power supply socket 311 disposed on the top surface of the power supply assembly 31, and a plurality of grooves 312 are disposed on the top surface of the power supply assembly 31.
Through being provided with recess 312 and power supply socket 311, make unmanned aerial vehicle when descending in recess 312 top, power supply socket 311 can provide electric power charging for unmanned aerial vehicle.
As shown in fig. 5, the fixing assembly 32 includes a plurality of sliding rails 321 fixedly connected to the top surface of the power supply assembly 31, the sliding rails 321 are located above the grooves 312, two electric sliders 322 are slidably connected to the outer surfaces of the sliding rails 321, a limiting plate 323 is fixedly connected to the side surfaces of the sliding rails 321, and a clamping plate 324 is fixedly connected to the side surfaces of the electric sliders 322.
Through being provided with electric slider 322 and slide rail 321, make two electric slider 322 can drive clamping plate 324 and draw close each other to fix unmanned aerial vehicle.
Wherein the top surface of the housing 1 is provided with a monitoring sensing module 11 as shown in fig. 1.
Through being provided with control induction module 11, make unmanned aerial vehicle when charging it can carry out the screen recording supervision to unmanned aerial vehicle in real time, can improve unmanned aerial vehicle's security and management efficiency.
Wherein the side surface of the housing 1 is provided with a number of heat dissipation holes 12, as shown in fig. 1.
By providing a number of heat dissipating holes 12, it is enabled to provide sufficient ventilation and air flow to rapidly transfer heat from the interior of the device to the external environment.
As shown in fig. 1, four support base plates 13 are fixedly connected to the bottom surface of the housing 1.
By providing four support floors 13, it is made possible to increase the stability of the overall device.
One specific application of this embodiment is: when unmanned aerial vehicle descends to power supply module 31 top surface, spring 24 can be compressed, absorb the energy that descends the in-process and produce, spring 24 can reduce the transmission of impact force effectively, prevent that it from causing the damage to power supply module 31 or unmanned aerial vehicle itself, in addition, this buffer gear 2 can also provide stable support, ensure the integrality of power supply module 31 and unmanned aerial vehicle's normal operating, lengthen its life, and spring 24 is being compressed the back, first response module 27 and the mutual contact hookup of second response module 28, make electric slider 322 drive grip block 324 be close to each other, thereby make it fix the unmanned aerial vehicle bottom, make power supply module 31 supply power to power supply socket 311 simultaneously, ensure that unmanned aerial vehicle can carry out stable charging, at the in-process of charging, monitor response module 11 can carry out the screen recording supervision to unmanned aerial vehicle in real time, in order to improve unmanned aerial vehicle's security and management efficiency.
In the description of the present specification, the descriptions of the terms "one embodiment," "example," "specific example," and the like, mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present utility model. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiments or examples. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the utility model disclosed above are intended only to assist in the explanation of the utility model. The preferred embodiments are not exhaustive or to limit the utility model to the precise form disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best understand and utilize the utility model. The utility model is limited only by the claims and the full scope and equivalents thereof.
Claims (6)
1. Landing charging apron monitoring device for unmanned aerial vehicle, including shell (1), its characterized in that: the shell (1) comprises a buffer mechanism (2) and a charging mechanism (3);
The buffer mechanism (2) comprises a plurality of fixed blocks (21) fixedly connected to the inner wall of the shell (1), two first sliding rods (22) are fixedly connected to the top surface of each fixed block (21), a second sliding rod (23) is fixedly connected to the top surface of each fixed block (21), a spring (24) is wound on the outer surface of each second sliding rod (23), a moving block (25) is slidably connected to the outer surface of each second sliding rod (23), the top end of each spring (24) is fixedly connected to the bottom surface of each moving block (25), the bottom end of each spring (24) is fixedly connected to the top surface of each fixed block (21), each first sliding rod (22) penetrates through each moving block (25), each first sliding rod (22) is slidably connected with each moving block (25), an L-shaped supporting plate (26) is fixedly connected to the side surface of each moving block (25), and a first sensing module (27) is arranged on the side surface of each fixed block (21).
2. The landing charging apron monitoring device for an unmanned aerial vehicle according to claim 1, wherein the charging mechanism (3) comprises a power supply assembly (31) and a fixing assembly (32), the power supply assembly (31) is fixedly connected to the top surface of the L-shaped supporting plate (26), the power supply assembly (31) comprises a power supply socket (311) arranged on the top surface of the power supply assembly (31), and a plurality of grooves (312) are formed in the top surface of the power supply assembly (31).
3. The landing charging apron monitoring device for an unmanned aerial vehicle according to claim 2, wherein the fixing assembly (32) comprises a plurality of sliding rails (321) fixedly connected to the top surface of the power supply assembly (31), the sliding rails (321) are located above the grooves (312), two electric sliding blocks (322) are slidably connected to the outer surfaces of the sliding rails (321), limiting plates (323) are fixedly connected to the side surfaces of the sliding rails (321), and clamping plates (324) are fixedly connected to the side surfaces of the electric sliding blocks (322).
4. A landing charging apron monitoring device for an unmanned aerial vehicle according to claim 1, wherein the top surface of the housing (1) is provided with a monitoring sensing module (11).
5. A landing charging apron monitoring device for an unmanned aerial vehicle according to claim 1, wherein the side surface of the housing (1) is provided with a number of heat dissipation holes (12).
6. A landing charging apron monitoring device for an unmanned aerial vehicle according to claim 1, wherein the bottom surface of the housing (1) is fixedly connected with four supporting base plates (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323023234.1U CN221294183U (en) | 2023-11-09 | 2023-11-09 | Landing charging apron monitoring device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323023234.1U CN221294183U (en) | 2023-11-09 | 2023-11-09 | Landing charging apron monitoring device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221294183U true CN221294183U (en) | 2024-07-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323023234.1U Active CN221294183U (en) | 2023-11-09 | 2023-11-09 | Landing charging apron monitoring device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221294183U (en) |
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2023
- 2023-11-09 CN CN202323023234.1U patent/CN221294183U/en active Active
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