CN219969514U - Unmanned aerial vehicle operation car can be dismantled to pick up - Google Patents
Unmanned aerial vehicle operation car can be dismantled to pick up Download PDFInfo
- Publication number
- CN219969514U CN219969514U CN202321743762.1U CN202321743762U CN219969514U CN 219969514 U CN219969514 U CN 219969514U CN 202321743762 U CN202321743762 U CN 202321743762U CN 219969514 U CN219969514 U CN 219969514U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- cabin
- unmanned
- pick
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000035939 shock Effects 0.000 claims abstract description 25
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 30
- 229910052744 lithium Inorganic materials 0.000 claims description 30
- 239000006096 absorbing agent Substances 0.000 claims description 18
- 239000000523 sample Substances 0.000 claims description 9
- 230000007704 transition Effects 0.000 claims description 6
- 238000012856 packing Methods 0.000 claims description 5
- 238000010521 absorption reaction Methods 0.000 abstract description 3
- 239000004065 semiconductor Substances 0.000 description 10
- 230000007547 defect Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012857 repacking Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model relates to a pickup detachable unmanned aerial vehicle operation vehicle, which comprises a pickup chassis, a front carriage and a rear carriage which are arranged on the pickup chassis, wherein an unmanned aerial vehicle cabin is arranged in the rear carriage, a shock absorption and quick disassembly device is arranged at the bottom of the unmanned aerial vehicle cabin, an unmanned aerial vehicle power supply system, an unmanned aerial vehicle control system and an unmanned aerial vehicle cabin temperature control system are arranged in the unmanned aerial vehicle cabin, the unmanned aerial vehicle is connected with the unmanned aerial vehicle power supply system in a pluggable manner, and the unmanned aerial vehicle is connected with the unmanned aerial vehicle control system in a communication manner. According to the unmanned aerial vehicle cabin loading system, the unmanned aerial vehicle cabin is loaded by adopting the pick-up, and equipment such as an unmanned aerial vehicle power supply system, an unmanned aerial vehicle control system, an unmanned aerial vehicle cabin temperature control system and an unmanned aerial vehicle is contained in the unmanned aerial vehicle cabin, so that the daily external operation requirement of unmanned aerial vehicle field operation is met.
Description
Technical Field
The utility model relates to a pickup detachable unmanned aerial vehicle operation vehicle.
Background
Currently, there are more and more refitted vehicle types based on light passenger chassis, especially there are more and more unmanned aerial vehicle working vehicles, but the current unmanned aerial vehicle working vehicles also have the following limitations:
firstly, the cross-country capability of the traditional light passenger chassis is poor, and many field operation environments and road conditions are poor, so that the traditional light passenger chassis cannot pass through and cannot reach an operation destination;
secondly, based on the unmanned aerial vehicle command car of traditional light visitor repacking, its unmanned aerial vehicle loading equipment and power supply unit are all the dispersed installation in the car entirely, if the vehicle breaks down temporarily then unable operation of going out, influence the task progress.
Disclosure of Invention
The utility model aims to solve the technical problem of overcoming the defects of the prior art and providing the unmanned aerial vehicle operation vehicle with the detachable pick-up.
In order to solve the technical problems, the utility model provides a pickup detachable unmanned aerial vehicle operation vehicle, which comprises a pickup chassis, a front carriage and a rear carriage, wherein the front carriage and the rear carriage are arranged on the pickup chassis, an unmanned aerial vehicle cabin is arranged in the rear carriage, a shock absorption and quick disassembly device is arranged at the bottom of the unmanned aerial vehicle cabin, an unmanned aerial vehicle power supply system, an unmanned aerial vehicle control system and an unmanned aerial vehicle cabin temperature control system are arranged in the unmanned aerial vehicle cabin, the unmanned aerial vehicle is connected with the unmanned aerial vehicle power supply system in a pluggable manner, and the unmanned aerial vehicle is connected with the unmanned aerial vehicle control system in a communication manner.
According to the unmanned aerial vehicle cabin, the unmanned aerial vehicle cabin is loaded by the pickup, and the power supply system and the control system are integrated in the unmanned aerial vehicle cabin, so that the unmanned aerial vehicle cabin is suitable for field operation environments, particularly poor road condition operation environments, and provides power supply equipment and the control system for unmanned aerial vehicle operation, can provide power for the unmanned aerial vehicle when a vehicle breaks down, and is convenient for unmanned aerial vehicle operation.
The optimized technical scheme of the utility model is as follows:
further, unmanned aerial vehicle power supply system includes lithium electric system and rechargeable battery package, rechargeable battery package links to each other with lithium electric system, but lithium electric system and unmanned aerial vehicle plug are connected.
In the above-mentioned structure, in order to satisfy unmanned aerial vehicle's in-vehicle demand of charging, install lithium electricity system in unmanned aerial vehicle cabin, can provide 15 degrees power, can satisfy unmanned aerial vehicle's long-time work demand in the field.
Furthermore, the lithium battery system can be connected with an unmanned aerial vehicle control system and an unmanned cabin temperature control system.
Furthermore, the unmanned cabin temperature control system comprises an air conditioner, a heater and a temperature controller, wherein the air conditioner and the heater are respectively connected with the temperature controller; the temperature controller comprises a temperature sensing probe and a control panel, wherein the temperature sensing probe is arranged inside the unmanned cabin, the control panel is arranged on the side face of the unmanned cabin, the temperature sensing probe is connected with the control panel, and the control panel is connected with motors of an air conditioner and a heater through a PLC (programmable logic controller) of an unmanned aerial vehicle control system respectively.
Because the unmanned cabin is provided with a plurality of electrical devices, in order to ensure the normal operation of the devices, the unmanned cabin is provided with a temperature control system, and the temperature control system comprises a semiconductor air conditioner, a heater and a temperature controller, and when detecting that the temperature in the unmanned cabin is different from the design temperature, the unmanned cabin can control the operation of heating or refrigerating devices so as to maintain the optimal operation temperature in the unmanned cabin.
Further, unmanned aerial vehicle control system includes industrial computer, camera, PLC controller, switch, router, GPS antenna and integral type weather station, industrial computer, camera are installed in unmanned aerial vehicle cabin, the industrial computer is connected with camera, switch, integral type weather station respectively, the switch passes through the router and is connected with the GPS antenna, the PLC controller is connected with unmanned aerial vehicle cabin temperature control system's air conditioner, heater and temperature controller's control panel.
Above-mentioned unmanned aerial vehicle control system comprises industrial computer, PLC controller, switch, 5G router, integral type weather station, roof GPS antenna, webcam etc. can realize the function of automated inspection surrounding environment and unmanned aerial vehicle position and then judge whether can carry out unmanned aerial vehicle task of taking off through control system, if meet bad weather steerable unmanned aerial vehicle back voyage such as strong wind heavy rain to reach the effect of protection unmanned aerial vehicle.
Further, the side of unmanned aerial vehicle cabin is equipped with automatically controlled panel and remote controller box, be provided with unmanned aerial vehicle remote controller in the remote controller box, unmanned aerial vehicle passes through unmanned aerial vehicle remote controller and is connected with industrial computer communication, automatically controlled panel is connected with the industrial computer.
Further, shock attenuation and quick detach device include rings, bumper shock absorber and transition mounting panel, rings are installed in unmanned aerial vehicle cabin's top surface four corners position, unmanned aerial vehicle cabin's bottom surface four corners is equipped with the bumper shock absorber respectively, through hasp subassembly swing joint between the box of bumper shock absorber and unmanned aerial vehicle cabin, the bumper shock absorber passes through the floor fixed connection of bolt and back packing box.
By adopting the structure, the function of rapidly disassembling and protecting electrical equipment in the unmanned aerial vehicle cabin can be realized, and the circular shock absorber is arranged at the bottom of the unmanned aerial vehicle cabin. The unmanned cabin is connected with the shock absorber through a transition mounting plate, and a hanging ring is mounted at the top of the unmanned cabin. When the unmanned cabin is disassembled, the whole unmanned cabin can be quickly disassembled through the hanging ring only by disassembling the transition mounting plate.
Further, the top of preceding carriage is provided with the luggage rack, install solar charging panel on the luggage rack, solar charging panel is connected with unmanned aerial vehicle power supply system's rechargeable battery package or lithium battery system.
Therefore, the solar charging panel is arranged on the roof of the vehicle, so that power supply during emergency conditions such as power supply equipment failure, insufficient electric quantity and the like can be ensured during field operation.
Furthermore, an external commercial power interface is arranged on the side face of the unmanned aerial vehicle cabin, one end of the external commercial power interface is respectively connected with the rechargeable battery pack and the lithium battery system, and the other end of the external commercial power interface is connected with an external commercial power supply in a pluggable manner.
Furthermore, the unmanned cabin is a square box body with one side open, a side box cover is arranged at the open position of the square box body, and the side box cover is hinged with the bottom surface of the square box body through a hinge.
According to the unmanned aerial vehicle cabin loading system, the unmanned aerial vehicle cabin is loaded by adopting the pick-up, and equipment such as an unmanned aerial vehicle power supply system, an unmanned aerial vehicle control system, an unmanned aerial vehicle cabin temperature control system and an unmanned aerial vehicle is contained in the unmanned aerial vehicle cabin, so that the daily external operation requirement of unmanned aerial vehicle field operation is met.
The utility model has the following advantages:
(1) The unmanned cabin is designed to be integrally and quickly disassembled, so that different chassis can be switched according to specific use conditions, and meanwhile, the unmanned cabin is convenient to maintain quickly in the later period by adopting a modularized design, and can be disassembled from the chassis to perform other operations under the condition of no unmanned operation;
(2) The solar panel is provided, so that the solar panel can be used in an emergency under the condition of insufficient electric quantity or failure of a power supply system;
(3) The unmanned aerial vehicle control system can detect the atmospheric environment, and can automatically control the unmanned aerial vehicle to return to the air when severe weather is encountered, so that the unmanned aerial vehicle is prevented from being damaged by the severe weather;
(4) The temperature control system can monitor the temperature in the unmanned aerial vehicle cabin at any time, and control the temperature of the unmanned aerial vehicle cabin within a temperature range set in advance so as to ensure that all electrical equipment in the unmanned aerial vehicle cabin normally work.
Drawings
Fig. 1 is a side view of the present utility model.
Fig. 2 is a top view of the present utility model.
Fig. 3 is a rear view of the present utility model.
Fig. 4 is an open schematic view of an unmanned cabin in the present utility model.
Fig. 5 is a schematic view of the internal structure of the unmanned cabin in the present utility model.
Fig. 6 is a schematic side view of an unmanned nacelle of the present utility model.
Fig. 7 is a front view of an unmanned nacelle in the present utility model.
Fig. 8 is a cross-sectional view taken along A-A of fig. 7.
Fig. 9 is a B-B cross-sectional view of fig. 8.
Fig. 10 is a partial enlarged view of fig. 9C.
Fig. 11 is a side view of an unmanned nacelle in accordance with the present utility model.
Fig. 12 is a partial enlarged view of D in fig. 11.
Fig. 13 is a rear view of the unmanned cabin of the present utility model.
In the figure: 1. front compartment, 2, rear cargo box, 3, unmanned cabin, 4, luggage rack, 5, solar charging panel, 6, lifting ring, 7, external utility interface, 8, hinge, 9, unmanned aerial vehicle, 10, lithium battery system, 11, rechargeable battery pack, 12, semiconductor air conditioner, 13, heater, 14, industrial control computer, 15, network camera, 16, control panel, 17, electric control panel, 18, remote control box, 19, inverter, 20, screw, 21, battery press plate, 22, lithium battery pack, 23, inner layer of the box, 24, outer layer of the box, 25, thermal insulation, 26, shock absorber, 27, snap fastener, 28, pre-buried bolts, 29, rear cargo box floor, 30, all hook press plate,
Detailed Description
Example 1
The unmanned aerial vehicle operation car can be dismantled to pick up that this embodiment provided, its structure is as shown in fig. 1 through 6, including pick up chassis and install preceding carriage 1 and back packing box 2 on pick up chassis, be provided with unmanned aerial vehicle cabin 3 in the back packing box 2, unmanned aerial vehicle cabin 3 is the open square box in one side, and the open department of square box is equipped with the side case lid, and the side case lid passes through hinge 8 and hinges with the bottom surface of square box, and adopts joint strip to seal between side case lid and the square box. The case of the unmanned nacelle 3 includes a case outer layer 24, a case inner layer 23, and a heat insulating material 25 provided between the case outer layer 24 and the case inner layer 23, and steel pipes are supported between the case inner layer 23 and the case outer layer 24. The bottom of unmanned aerial vehicle cabin 3 is provided with shock attenuation and quick detach device, and the inside of unmanned aerial vehicle cabin 3 is provided with unmanned aerial vehicle 9, unmanned aerial vehicle power supply system, unmanned aerial vehicle control system and unmanned aerial vehicle cabin temperature control system, but unmanned aerial vehicle 9 and unmanned aerial vehicle power supply system plug are connected, and unmanned aerial vehicle 9 and unmanned aerial vehicle control system communication are connected.
Unmanned aerial vehicle power supply system includes lithium electric system 10 and rechargeable battery package 11, and rechargeable battery package 11 links to each other with lithium electric system 10, but lithium electric system 10 and unmanned aerial vehicle 9 plug are connected, charge for unmanned aerial vehicle 9, and lithium electric system 10 still can be connected with unmanned aerial vehicle control system, unmanned cabin temperature control system. The side of unmanned cabin 3 is equipped with external commercial power interface 7, and rechargeable battery package 11 and lithium electric system 10 are connected respectively to the one end of external commercial power interface 7, and the other end is pluggable with external commercial power. In addition, a luggage rack 4 is provided at the top of the front compartment 1, and a solar charging panel 5 is mounted on the luggage rack 4, and the solar charging panel 5 may be connected with a rechargeable battery pack 11 or a lithium battery system 10. The lithium battery system 10 includes a lithium battery pack 22 and an inverter 19 that are connected to each other, the lithium battery pack 22 is mounted on the bottom surface of the unmanned cabin 3 through a battery bracket, the battery bracket includes a battery tray 31, a tray bracket 32, a screw 20 and a battery pressing plate 21, the battery tray 31 is mounted on the bottom surface of the unmanned cabin 3 through the tray bracket 32, the lithium battery pack 22 is disposed on the battery tray 31, the screw 20 passes through the lithium battery pack 22 and is fixedly connected to the battery tray, and the battery pressing plate 21 is disposed on the top surface of the screw 20 located on the lithium battery pack 22.
The unmanned aerial vehicle control system comprises an industrial personal computer 14, a network camera 15, a PLC controller, a switch, a 5G router, a roof GPS antenna and an integrated weather station, wherein the industrial personal computer 14 and the camera 5 are arranged in an unmanned aerial vehicle cabin 3, the industrial personal computer 141 is respectively connected with the network camera 15, the switch and the integrated weather station, the switch is connected with the roof GPS antenna through the 5G router, and the PLC controller is connected with a semiconductor air conditioner 12 of the unmanned aerial vehicle cabin temperature control system, a heater 13 and a control panel 16 of the temperature controller. An electric control panel 17 and a remote controller box 18 are arranged on the side face of the unmanned cabin 3, an unmanned aerial vehicle remote controller is arranged in the remote controller box 18, the unmanned aerial vehicle 9 is in communication connection with the industrial personal computer 14 through the unmanned aerial vehicle remote controller, and the electric control panel 17 is also connected with the industrial personal computer 14. The industrial personal computer 14 is also connected with the lithium battery system 10 and the circuit board of the rechargeable battery pack 11 to realize the function of controlling the power supply or charging of the charging system.
The unmanned cabin temperature control system comprises a semiconductor air conditioner 12, a heater 13 and a temperature controller, wherein the heater 13 adopts a fan heater, the semiconductor air conditioner 12 adopts a semiconductor refrigerating fan, the semiconductor refrigerating fan is connected with the side wall of the unmanned cabin 3 through a self-palace wire, and the fan heater adopts a transition plate and bolts to be fixedly connected with a mounting frame in the unmanned cabin 3. The semiconductor air conditioner 12 and the heater 13 are respectively connected with a temperature controller. The temperature controller includes temperature sensing probe and control panel 16, and temperature sensing probe sets up in the inside of unmanned cabin 3, and control panel 16 sets up in the side of unmanned cabin 3, and temperature sensing probe is connected with control panel 16 for show the temperature in the unmanned cabin 3 on control panel 16 in real time. The control panel 16 is connected with motors of the semiconductor air conditioner 12 and the heater 13 through a PLC controller of the unmanned aerial vehicle control system, respectively. The control panel 16, the main machine of the semiconductor air conditioner 12 and the motor of the fan heater are respectively connected with the lithium battery system 10, and are powered by the lithium battery system 10.
The shock absorption and quick release device comprises a hanging ring 6, a shock absorber 26 and a transition mounting plate 27, wherein the cross section of the shock absorber 26 is circular, and rubber materials and springs can be adopted. The lifting ring 6 is arranged at four corners of the top surface of the unmanned cabin 3, shock absorbers 26 are respectively arranged at four corners of the bottom surface of the unmanned cabin 3, the shock absorbers 26 are movably connected with the box body of the unmanned cabin 3 through a hasp assembly, and the shock absorbers 26 are fixedly connected with a rear cargo box floor 29 through embedded bolts 28. The hasp assembly comprises a hasp buckle plate 27 and a hook pressing plate 30, one end of the hasp buckle plate 27 is movably arranged on the box body of the unmanned cabin 3, the other end of the hasp buckle plate is hinged with one end of the hook pressing plate 30, and the other end of the hook pressing plate 30 is fixedly connected with the shock absorber 26.
The utility model develops a pickup detachable unmanned aerial vehicle operation vehicle based on the defect of a wide light passenger vehicle type and the characteristic of strong wild property of a pickup chassis. The automobile type is designed based on the pick-up chassis, and the function of multi-environment field operation can be achieved by utilizing the characteristic that Pi Kama force is large and wild is strong. According to the unmanned cabin, the integral design is carried out, and the shock absorber is arranged between the unmanned cabin and the chassis, so that the unmanned cabin and equipment inside the unmanned cabin can be effectively protected when a vehicle is off-road. Meanwhile, the unmanned cabin is detachably connected with the pick-up chassis, when the pick-up chassis fails or unmanned aerial vehicle operation is not needed, the unmanned cabin can be rapidly detached from the pick-up rear cargo box, and the unmanned cabin is hoisted to other standby chassis through the hoisting ring for operation or standby. An unmanned aerial vehicle power supply system and a control system are installed in the unmanned aerial vehicle cabin to provide power for unmanned aerial vehicle operation and control unmanned aerial vehicle operation, and the cabin body of the whole unmanned aerial vehicle cabin is waterproof.
In addition to the embodiments described above, other embodiments of the utility model are possible. All technical schemes formed by equivalent substitution or equivalent transformation fall within the protection scope of the utility model.
Claims (10)
1. The utility model provides an unmanned aerial vehicle operation car can be dismantled to pick up, includes pick up chassis and installs preceding carriage and back packing box on pick up chassis, its characterized in that: be provided with unmanned cabin in the back packing box, the bottom in unmanned cabin is provided with shock attenuation and quick detach device, unmanned aerial vehicle power supply system, unmanned aerial vehicle control system and unmanned aerial cabin temperature control system are provided with to the inside in unmanned cabin, unmanned aerial vehicle and unmanned aerial vehicle power supply system pluggable connection, unmanned aerial vehicle and unmanned aerial vehicle control system communication connection.
2. The unmanned aerial vehicle detachable from a pick-up according to claim 1, wherein: the unmanned aerial vehicle power supply system comprises a lithium battery system and a rechargeable battery pack, wherein the rechargeable battery pack is connected with the lithium battery system, and the lithium battery system is connected with the unmanned aerial vehicle in a pluggable manner.
3. The unmanned aerial vehicle detachable from a pick-up according to claim 2, wherein: the lithium battery system can be connected with an unmanned aerial vehicle control system and an unmanned cabin temperature control system.
4. The unmanned aerial vehicle detachable from a pick-up according to claim 1, wherein: the unmanned cabin temperature control system comprises an air conditioner, a heater and a temperature controller, wherein the air conditioner and the heater are respectively connected with the temperature controller; the temperature controller comprises a temperature sensing probe and a control panel, wherein the temperature sensing probe is arranged inside the unmanned cabin, the control panel is arranged on the side face of the unmanned cabin, the temperature sensing probe is connected with the control panel, and the control panel is connected with motors of an air conditioner and a heater through a PLC (programmable logic controller) of an unmanned aerial vehicle control system respectively.
5. The unmanned aerial vehicle detachable from a pick-up according to claim 1, wherein: the unmanned aerial vehicle control system comprises an industrial personal computer, a camera, a PLC (programmable logic controller), a switch, a router, a GPS (global positioning system) antenna and an integrated weather station, wherein the industrial personal computer and the camera are installed in an unmanned aerial vehicle cabin, the industrial personal computer is respectively connected with the camera, the switch and the integrated weather station, the switch is connected with the GPS antenna through the router, and the PLC is connected with an air conditioner, a heater and a control panel of the unmanned aerial vehicle cabin temperature control system.
6. The unmanned aerial vehicle of claim 5, wherein the unmanned aerial vehicle comprises: the side in unmanned cabin is equipped with automatically controlled panel and remote controller box, be provided with unmanned aerial vehicle remote controller in the remote controller box, unmanned aerial vehicle passes through unmanned aerial vehicle remote controller and is connected with industrial computer communication, automatically controlled panel is connected with the industrial computer.
7. The unmanned aerial vehicle detachable from a pick-up according to claim 1, wherein: the shock attenuation and quick assembly disassembly device comprises a hanging ring, shock absorbers and a transition mounting plate, wherein the hanging ring is arranged at four corners of the top surface of the unmanned cabin, the shock absorbers are respectively arranged at four corners of the bottom surface of the unmanned cabin, the shock absorbers are movably connected with the box body of the unmanned cabin through a hasp assembly, and the shock absorbers are fixedly connected with the floor of the rear cargo box through bolts.
8. The unmanned aerial vehicle detachable from a pick-up according to claim 1, wherein: the top of preceding carriage is provided with the luggage rack, install solar charging panel on the luggage rack, solar charging panel is connected with unmanned aerial vehicle power supply system's rechargeable battery package or lithium electric system.
9. The unmanned aerial vehicle detachable from a pick-up according to claim 1, wherein: the side of unmanned cabin is equipped with external commercial power interface, rechargeable battery package and lithium electric system are connected respectively to the one end of external commercial power interface, but the other end and external commercial power supply plug connection.
10. The unmanned aerial vehicle detachable from a pick-up according to claim 1, wherein: the unmanned aerial vehicle cabin is a square box body with one open side, a side box cover is arranged at the open position of the square box body, and the side box cover is hinged with the bottom surface of the square box body through a hinge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321743762.1U CN219969514U (en) | 2023-07-05 | 2023-07-05 | Unmanned aerial vehicle operation car can be dismantled to pick up |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321743762.1U CN219969514U (en) | 2023-07-05 | 2023-07-05 | Unmanned aerial vehicle operation car can be dismantled to pick up |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219969514U true CN219969514U (en) | 2023-11-07 |
Family
ID=88596311
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321743762.1U Active CN219969514U (en) | 2023-07-05 | 2023-07-05 | Unmanned aerial vehicle operation car can be dismantled to pick up |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219969514U (en) |
-
2023
- 2023-07-05 CN CN202321743762.1U patent/CN219969514U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9812685B2 (en) | Battery pack for electric vehicle | |
| CN201534570U (en) | Car roof structure with battery chamber for placing power battery | |
| US7795837B1 (en) | Portable solar power supply trailer with a security containment area and multiple power interfaces | |
| CN217754141U (en) | Fixed intelligent airport capable of retracting unmanned aerial vehicle and being suitable for outdoor environment | |
| CN102310829A (en) | Emergency safe disengagement device for power battery of electric automobile | |
| CN112441248B (en) | Vehicle-mounted airport of unmanned aerial vehicle and control method thereof | |
| CN219969514U (en) | Unmanned aerial vehicle operation car can be dismantled to pick up | |
| CN209921155U (en) | On-vehicle unmanned aerial vehicle equipment of patrolling and examining and vehicle of patrolling and examining | |
| CN202320042U (en) | Emergency charging square cabin of pickup truck | |
| CN219918930U (en) | One-vehicle one-stop type high-integration maneuvering measurement and control station | |
| CN115801105B (en) | One-vehicle one-stop type high-integration maneuvering measurement and control station | |
| CN212447269U (en) | Modularized unmanned aerial vehicle material transport vehicle | |
| US20240025340A1 (en) | Lighting system and method | |
| CN109760106B (en) | Modularization rail-hanging type intelligent inspection robot for comprehensive pipe rack | |
| CN205022436U (en) | Multi -functional mobile police service platform | |
| CN211731013U (en) | Electric mine car | |
| CN214492673U (en) | Comprehensive logging truck | |
| CN211731548U (en) | Electric motor coach | |
| CN209224072U (en) | A kind of security patrol robot mobile command center | |
| CN211731549U (en) | Chassis assembly and passenger car | |
| CN210883575U (en) | Intelligent finished grain storage and transportation integrated container with self-generating device | |
| CN219856778U (en) | Large-scale quick change battery package, AGV dolly and electric automobile | |
| CN111017025A (en) | Electric motor coach | |
| CN218021366U (en) | Operation car with hangar for unmanned aerial vehicle | |
| CN109434834A (en) | A kind of security patrol robot mobile command center |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |