CN211108078U - Unmanned aerial vehicle ground power supply vehicle - Google Patents
Unmanned aerial vehicle ground power supply vehicle Download PDFInfo
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- CN211108078U CN211108078U CN201922159367.9U CN201922159367U CN211108078U CN 211108078 U CN211108078 U CN 211108078U CN 201922159367 U CN201922159367 U CN 201922159367U CN 211108078 U CN211108078 U CN 211108078U
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Abstract
The utility model provides an unmanned aerial vehicle ground power supply car, include: a chassis mounted with a plurality of tires and a drawbar; a body including a housing disposed on the chassis; the power module and the power distribution system are arranged in the shell and comprise a power module, a winder and a switch; the control and display panel is arranged on the shell and is communicated and electrically connected with the power supply module and the power distribution system; and the output panel is arranged on the shell and is electrically connected with the power supply module and the power distribution system. The utility model discloses an unmanned aerial vehicle ground power supply vehicle, which integrally adopts a vehicle body structure of a chassis and a box body, so as to solve the problem that the gravity center is unstable and is easy to topple over when in use; the large-size inflatable wheel is adopted to solve the problem of inconvenient movement and transition; the integrated design and the separation of the input and output operation panels are adopted to solve the problems of inconvenient operation and poor safety in the use process. The power supply vehicle is provided with a storage drawer for storing related tools and cables.
Description
Technical Field
The utility model belongs to the unmanned aerial vehicle field relates to unmanned aerial vehicle's comprehensive support system, concretely relates to unmanned aerial vehicle ground supply vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be divided into military unmanned aerial vehicles and civil unmanned aerial vehicles according to the application field. The military unmanned aerial vehicle has the characteristics of exquisite structure, strong concealment, convenient use, low manufacturing cost, flexible performance and the like, is mainly used for battlefield reconnaissance, electronic interference, carrying of weapons such as cluster bombs and guided missiles to execute aggressive missions, is used as a military unmanned aerial vehicle such as an aerial communication relay platform, a nuclear test sampler, nuclear explosion and nuclear radiation reconnaissance machine to serve as one member of modern aerial military strength, has the characteristics of no casualties, less use limitation, good concealment, high cost effectiveness ratio and the like, and has increasingly prominent status and effect in modern war.
With the blowout type development of the unmanned aerial vehicle technology, the unmanned aerial vehicle comprehensive guarantee technology is rapidly developed and perfected. To the large-and-medium-sized integrated unmanned aerial vehicle of beating of scouting, need stable ground electrical power generating system when ground test. The existing ground power supply system technology of the unmanned aerial vehicle mainly adopts a Wei-Tu cabinet structure or an independent power supply module. The prior art does not consider and design from the angle that outfield personnel conveniently used, and the focus is unstable when having the use, emptys easily, and it is inconvenient to remove and change, and the use operation is inconvenient, the relatively poor scheduling problem of security.
SUMMERY OF THE UTILITY MODEL
Not enough to the above-mentioned that exists among the prior art, the utility model relates to an unmanned aerial vehicle ground power supply car, include:
a chassis mounted with a plurality of tires and a drawbar;
a body including a housing disposed on the chassis;
the power module and the power distribution system are arranged in the shell and comprise a power module, a winder and a switch;
the control and display panel is arranged on the shell and is communicated and electrically connected with the power supply module and the power distribution system;
and the output panel is arranged on the shell and is electrically connected with the power supply module and the power distribution system.
Furthermore, the control and display panel is provided with A, B two-way voltage and current monitoring instruments, an input voltage detecting instrument, a grounding indicator light, A, B two-way operation switch buttons and a main power supply air switch.
Furthermore, an output aerial socket and a wall socket are arranged on the output panel, and the A, B two-way operation switch respectively controls the output aerial socket and the wall socket.
And the alarm lamp is arranged at the top of the shell, and the alarm lamp operation switch button is arranged on the control and display panel.
Further, the chassis comprises a steering mechanism arranged at the front end of the chassis, and the traction rod is arranged on the steering mechanism.
Further, the chassis includes a pair of front wheels provided on the steering mechanism and a pair of rear wheels provided at the rear of the chassis.
Further, the control and display panel is arranged on the top of one side face of the shell and has a fixed inclination angle, and the output panel is arranged on the top of one side face of the shell and has a fixed inclination angle.
Furthermore, each side of the shell is provided with two doors, and the rear part of the shell is provided with one door.
Furthermore, two drawers are arranged on one side surface of the shell, and a storage box is arranged on the rear portion of the shell.
Further, the pair of front wheels and the pair of rear wheels have pneumatic tires.
The utility model discloses an unmanned aerial vehicle ground power supply vehicle, which integrally adopts a vehicle body structure of a chassis and a box body, so as to solve the problem that the gravity center is unstable and is easy to topple over when in use; the large-size inflatable wheel is adopted to solve the problem of inconvenient movement and transition; the integrated design and the separation of the input and output operation panels are adopted to solve the problems of inconvenient operation and poor safety in the use process. The power supply vehicle is provided with a storage drawer for storing related tools and cables.
Drawings
The above and other objects, features and advantages of the present disclosure will become more apparent by describing in greater detail exemplary embodiments thereof with reference to the attached drawings, in which like reference numerals generally represent like parts throughout.
Fig. 1 shows the utility model discloses unmanned aerial vehicle ground power supply vehicle's constitution sketch map.
Fig. 2 shows a schematic diagram of a power module according to an embodiment of the present invention.
Fig. 3 shows a schematic view of a car body door and a panel according to an embodiment of the present invention.
Fig. 4 shows a schematic diagram of a control and display panel according to an embodiment of the present invention.
Fig. 5 shows a schematic diagram of an output panel according to an embodiment of the present invention.
Reference numerals:
1-traction ring, 2-handle, 3-traction rod, 4-pneumatic tire, 5-front door, 6-rear door with wire outlet, 7-rear drawer, 8-mudguard, 9-rear door, 10-storage cabinet, 11-front panel, 12-warning lamp, 13-beautiful protection board, 14-front drawer, 15-power module, 16-switching power supply, 17-winder, 18-rear panel, 19-back door, 20-back front door, 21-A path voltage monitoring unit, 22-A path current monitoring unit, 23-input voltage monitoring unit, 24-A path switch, 25-B path switch, 26-warning lamp switch, 27-system power supply idle switch, 28-grounding indicator lamp, 29-B path current monitoring unit, 30-B path voltage monitoring unit, 31-output wall plug and 32-output aerial plug.
Detailed Description
Preferred embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While the preferred embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art.
The utility model relates to an unmanned aerial vehicle ground power supply car, include:
a chassis mounted with a plurality of tires and a drawbar;
a body including a housing disposed on the chassis;
the power module and the power distribution system are arranged in the shell and comprise a power module, a winder and a switch;
the control and display panel is arranged on the shell and is communicated and electrically connected with the power supply module and the power distribution system;
and the output panel is arranged on the shell and is electrically connected with the power supply module and the power distribution system.
The power supply main mainly comprises the following subsystems: chassis, automobile body, power module and distribution system. The automobile body is provided with a shell, a control and display panel and an output panel are arranged on the shell, a front attractive protection guard plate and 5 doors are arranged on the automobile body shell to facilitate assembly and maintenance, and two drawers and a storage box are arranged on the side face of the shell to store cables, tools and the like.
The control and display panel is provided with A, B voltage and current monitoring instruments, an input voltage detection instrument, a grounding indicator light, A, B two-way operation switch buttons, a warning light operation switch button and a main power supply air switch. The output panel is provided with an output aviation plug and a wall plug. The chassis comprises a chassis support, and a traction rod, a steering mechanism and large-size tires which are arranged on the chassis support, wherein the number of the tires is 4, and the front three-point layout is adopted. The power module and the power distribution system mainly comprise a power module (with high power of 8kW), a winder, a switching power supply, an alarm lamp and a corresponding operation display unit (arranged on a control and display panel).
The working principle of the ground power supply vehicle of the unmanned aerial vehicle is as follows: before using this supply vehicle, be connected to between unmanned aerial vehicle and the supply vehicle output navigation plug with output cable earlier, stretch the cable in the winder to suitable position, insert the commercial power, then for system power-on through the switch on control and the display panel, through the switch control A, B two-way break-make of A, B two-way switch, and then control A way and B way and go up the electricity. A. The B-path voltage and current monitoring unit displays the voltage and current values of the B-path voltage and current monitoring unit in real time, and the input voltage monitoring unit displays the input voltage value in real time. The grounding indicator lamp displays whether grounding is normal in real time, and if the grounding is abnormal, the indicator lamp is turned on. When the system works for a long time, the warning lamp switch is pressed down, and the warning lamp is turned on to warn passers-by.
To facilitate understanding of the solution and effects of the embodiments of the present invention, a specific application example is given below. It will be understood by those skilled in the art that this example is merely for the purpose of facilitating understanding of the invention, and that any specific details thereof are not intended to limit the invention in any way.
As shown in fig. 1-5, the ground power cart for the drone includes a chassis and a body. The chassis is provided with a plurality of pneumatic tires 4 and a traction rod 3, the traction rod 3 is provided with a traction ring 1 and a handle 2, and a mudguard 8 is arranged above the rear tire. The automobile body is including setting up casing on the chassis, and the side of casing is provided with just preceding door 5 and takes out the line mouth just back door 6, and power module 15 and switching power supply 16 are placed respectively at just preceding door 5 and take out the line mouth just back door 6 behind, and winder 17 is placed in taking out the line mouth just back door 6, can draw forth through the outlet, is connected to the commercial power. A front drawer 14 and a rear drawer 7 are arranged on the front door 5 and the rear door 6 with the wire outlet. The tail part of the shell is provided with a rear door 9 and a storage cabinet 10, the top part of the shell is provided with an alarm lamp 12, and the top part of the front end of the shell is provided with an attractive protection plate 13. A back door 19 and a back front door 20 are provided on the other side of the housing.
The front panel 11 and the rear panel 18 are respectively disposed on top of one side of the housing with a fixed inclination angle. The control and display panel is mounted on the front panel 11 and the output panel is mounted on the rear panel 18. The control and display panel includes an a-path voltage monitoring unit 21, an a-path current monitoring unit 22, an input voltage monitoring unit 23, an a-path switch 24, a B-path switch 25, an alarm lamp switch 26, a system power supply idle switch 27, a ground indicator lamp 28, a B-path current monitoring unit 29, and a B-path voltage monitoring unit 30. The control and display panel is electrically connected to the power module 15 and the switching power supply 16, and is used for controlling the detectable power module and the power distribution system. The output panel includes an output wall insert 31 and an output navigation insert 32.
In the embodiment, the whole power supply vehicle is 1400mm long, 828mm wide and 950mm high. The multifunctional winder has the advantages of low center of gravity, stable structure, easy traction, external field use and the like, and the winder is adopted to facilitate the use and storage of cables. The inclination angle of the input and output panel and the horizontal plane is about 60 degrees, so that a user can conveniently operate the buttons and read the required physical quantity. The adoption of the warning lamp enables the safety coefficient of long-time operation such as copying to be improved.
Having described embodiments of the present disclosure, the foregoing description is intended to be exemplary, not exhaustive, and not limited to the disclosed embodiments. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments. The terminology used herein is chosen in order to best explain the principles of the embodiments, the practical application, or improvements made to the technology in the marketplace, or to enable others of ordinary skill in the art to understand the embodiments disclosed herein.
Claims (10)
1. An unmanned aerial vehicle ground power supply car which characterized in that includes:
a chassis mounted with a plurality of tires and a drawbar;
a body including a housing disposed on the chassis;
the power module and the power distribution system are arranged in the shell and comprise a power module, a winder and a switch;
the control and display panel is arranged on the shell and is communicated and electrically connected with the power supply module and the power distribution system;
and the output panel is arranged on the shell and is electrically connected with the power supply module and the power distribution system.
2. The ground power supply vehicle for the unmanned aerial vehicle as claimed in claim 1, wherein the control and display panel is provided with A, B two-way voltage and current monitoring instrument, an input voltage detection instrument, a grounding indicator light, A, B two-way operation switch button and a main power supply air switch.
3. The ground power supply vehicle for the unmanned aerial vehicle as claimed in claim 2, wherein the output panel is provided with an output aerial socket and a wall socket, and the A, B two-way operation switch controls the output aerial socket and the wall socket respectively.
4. The ground power supply vehicle for the unmanned aerial vehicle as claimed in claim 1, further comprising a warning lamp disposed on the top of the housing, wherein a warning lamp operating switch button is disposed on the control and display panel.
5. The unmanned aerial vehicle ground power supply vehicle of claim 1, wherein the chassis includes a steering mechanism disposed at a front end of the chassis, the tow bar being disposed on the steering mechanism.
6. The unmanned ground power cart of claim 5, wherein the chassis comprises a pair of front wheels disposed on the steering mechanism and a pair of rear wheels disposed rearward of the chassis.
7. The ground power supply vehicle for unmanned aerial vehicle as claimed in claim 1, wherein the control and display panel is disposed on top of one side of the housing and has a fixed inclination angle, and the output panel is disposed on top of one side of the housing and has a fixed inclination angle.
8. The unmanned aerial vehicle ground power supply vehicle of claim 1, wherein the housing has two doors on each side and one door on the rear.
9. The ground power supply vehicle for the unmanned aerial vehicle as claimed in claim 1, wherein two drawers are provided at one side of the housing, and a storage box is provided at the rear.
10. The drone ground power cart of claim 6, wherein the pair of front wheels and the pair of rear wheels have pneumatic tires.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922159367.9U CN211108078U (en) | 2019-12-05 | 2019-12-05 | Unmanned aerial vehicle ground power supply vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922159367.9U CN211108078U (en) | 2019-12-05 | 2019-12-05 | Unmanned aerial vehicle ground power supply vehicle |
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| Publication Number | Publication Date |
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| CN211108078U true CN211108078U (en) | 2020-07-28 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201922159367.9U Active CN211108078U (en) | 2019-12-05 | 2019-12-05 | Unmanned aerial vehicle ground power supply vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102511739B1 (en) * | 2022-04-18 | 2023-03-23 | 주식회사 샤프에비에이션케이 | Devices for Preventing GPU Towing Movement between Ground Power Supplies |
-
2019
- 2019-12-05 CN CN201922159367.9U patent/CN211108078U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102511739B1 (en) * | 2022-04-18 | 2023-03-23 | 주식회사 샤프에비에이션케이 | Devices for Preventing GPU Towing Movement between Ground Power Supplies |
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