CN207644643U - A kind of unmanned plane for road traffic monitoring - Google Patents
A kind of unmanned plane for road traffic monitoring Download PDFInfo
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- CN207644643U CN207644643U CN201820533518.5U CN201820533518U CN207644643U CN 207644643 U CN207644643 U CN 207644643U CN 201820533518 U CN201820533518 U CN 201820533518U CN 207644643 U CN207644643 U CN 207644643U
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 23
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 25
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 25
- 230000033001 locomotion Effects 0.000 claims abstract description 12
- 238000000034 method Methods 0.000 claims abstract description 12
- 230000002093 peripheral effect Effects 0.000 claims abstract description 12
- 230000005611 electricity Effects 0.000 claims description 12
- 238000010586 diagram Methods 0.000 description 6
- 239000004065 semiconductor Substances 0.000 description 5
- 238000009434 installation Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000007726 management method Methods 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned planes for road traffic monitoring, include the circuit board as unmanned plane skeleton.The circuit board includes circuit main board and four circuit support plates, and the circuit board is double-sided PCB, and the front of the circuit main board is application circuit, and the reverse side of the circuit main board is power circuit.The element larger to volume in the application circuit such as universal asynchronous receiving-transmitting transmitter interface, Serial Peripheral Interface (SPI), monolithic wireless transceiver chip, power interface, main control chip, global positioning system, power switch, six axis motion process component of conformability, IC bus interface, reset switch, receiver chip have done rational layout.The lithium battery is 1S lithium batteries.The body volume of the unmanned plane is small, light-weight, power consumption is low, flight is flexible, security performance is high, manipulation is easy, at low cost.
Description
Technical field
The utility model is related to a kind of equipment for road traffic monitoring, more particularly to a kind of road traffic that is used for monitor
Unmanned plane.
Background technology
With the continuous quickening of urbanization process, vehicle guaranteeding organic quantity persistently increases severely, and city road network constantly extends.However this
While a little city traffic networks bring convenient for people's lives, the numerous situation of vehicle multichannel has also been buried to traffic safety huge hidden
Suffer from, more difficult challenge more is proposed to traffic administration person.However conventional traffic management method is there is many loopholes and extremely
Angle, the defect and drawback of original base facility are constantly exposed, and the scientific and technological level of traffic administration is had too many difficulties to cope with.
Mobility, emergency, sudden the characteristics of being police work by force are traditional traffic police road surface patrol, fixed point camera shooting
What the traffic management methods such as head monitoring cannot be satisfied.And unmanned plane has action rapidly, information collects comprehensive, the spies such as controllability height
Point can meet field of traffic control for real-time various data information demands.Traffic administration especially under complex environment
Aspect, unmanned plane provides new scheme for traffic administration, can largely expand under high-risk environment and find out field,
And reduce dangerous law-enforcing environment to the life of traffic control department personnel and the harm of property safety.
It is comprehensive to use nobody on the basis of using existing communications and transportation infrastructure for vehicle supervision department
The intelligent traffics equipment such as machine in the utilization rate for improving traffic infrastructure, is accelerated to disposition speed etc. that accident occur
It has a very important significance.Fully advanced science and technology are applied in traffic administration, are realized to a certain extent " from section
Skill wants police strength " long term growth target.
As shown in Figure 1, National People's Congress's type unmanned plane includes the circuit board 1 as unmanned plane skeleton in the prior art, circuit board 1
Shape is in conformality, and circuit board 1 is single-sided circuit board, and motor 4 is distributed in four angles of circuit board 1, and the rotation axis of motor 4 is fixed with
Propeller 5.Its shortcomings that is：Body volume is big, weight is heavy, power consumption is high, flight is dumb, security performance is low, manipulation is tired
Difficult, of high cost, flight noise is big etc..
Utility model content
The technical problem to be solved by the present invention is to provide a kind of unmanned plane for road traffic monitoring, the unmanned planes
Body volume it is small, light-weight, power consumption is low, flight is flexible, security performance is high, manipulation is easy, at low cost.
In order to solve the above-mentioned technical problem, the utility model provides a kind of unmanned plane for road traffic monitoring, packet
Circuit board, four motors, four propellers as unmanned plane skeleton are included, four propellers are separately fixed at described in four
In the rotation axis of motor.
The circuit board includes circuit main board and four circuit support plates, and the shape of the circuit main board is square, four
The shape of the circuit support plate is elongated, and four circuit support plates are located at four angles of the circuit main board and are in spoke
Penetrate shape distribution, four circuit support plates and the circuit main board be integrated, four motors respectively with four electricity
Road support plate is fixedly connected.
The circuit board is double-sided PCB, the front of the circuit main board (face when unmanned plane during flying upward is front)
It is application circuit, the reverse side of the circuit main board is power circuit.
The larger element of volume has universal asynchronous receiving-transmitting transmitter interface, Serial Peripheral Interface (SPI), list in the application circuit
Piece wireless transceiver chip, power interface, main control chip, global positioning system, power switch, six axis motion process group of conformability
Part, IC bus interface, reset switch, receiver chip.
The universal asynchronous receiving-transmitting transmitter interface is arranged in the middle part of the top of the circuit main board, and the serial peripheral connects
Mouth is arranged in the middle part of the right of the circuit main board, and the monolithic wireless transceiver chip is arranged in the following of the circuit main board
Middle part, the power interface are arranged in the middle part of the left side of the circuit main board, and the main control chip is arranged in the circuit main board
Positive right middle, the global positioning system setting is in the positive lower left quarter of the circuit main board, the power switch setting
In the front of the circuit main board and positioned at the left of the global positioning system, six axis motion process component of the conformability is set
It sets in the front of the circuit main board and positioned at the top of the global positioning system, the IC bus interface setting exists
The positive upper right quarter of circuit main board, the reset switch are arranged in the front of the circuit main board and determine positioned at the whole world
Between position system and main control chip, the receiver chip is arranged in the positive right lower quadrant of the circuit main board.
The larger element of volume has single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers, lithium electricity in the power circuit
Pond.
The single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers are arranged in the middle and upper part of the circuit main board reverse side,
The lithium battery, which is arranged in the middle part of the circuit main board reverse side, is offset to the power interface, and the lithium battery is 1S lithium electricity
Pond.
The front of the circuit board has data wiring and power-supply wiring, the reverse side of the circuit board to have power-supply wiring.
The width of the data wiring is 50mil, and the width of the power-supply wiring is 45mil~55mil.
Interval between two adjacent data wirings is 18mil~22mil, adjacent two power-supply wirings
Between interval be 18mil~22mil, the adjacent data wiring the power-supply wiring between interval be 27mil
~33mil.
The application circuit has main control chip circuit, clearance lamps circuit, 3.3 regulator circuits, remote control signal receiver master control electricity
Road, gyroscope block, switch and battery input filter circuit, interface section circuit, metal-oxide-semiconductor driving circuit.
The width of the data wiring is 50mil, and the width of the power-supply wiring is 50mil.
Interval between two adjacent data wirings is 20mil, between adjacent two power-supply wirings
Interval is 20mil, and the interval between the wiring of the adjacent data and the power-supply wiring is 30mil.
Unmanned plane of the utility model for road traffic monitoring has the advantages that compared with prior art.
1, the technical program includes circuit main board and four circuit support plates, the circuit master as a result of the circuit board
The shape of plate is square, and the shape of four circuit support plates is elongated, and four circuit support plates are located at described
Four angles of circuit main board are simultaneously radially distributed, and four circuit support plates and the circuit main board are integrated, four institutes
The technological means that motor is fixedly connected with four circuit support plates respectively is stated, so, four after the area for reducing circuit main board
A propeller will not interfere, and advantage is provided for the micromation of circuit board.
2, the technical program is double-sided PCB as a result of the circuit board, front (nobody of the circuit main board
Face when machine flight upward is front) it is application circuit, the reverse side of the circuit main board is the technological means of power circuit, institute
To be not only advantageous to greatly reduce the area of circuit main board, moreover, it is also possible to effectively reduce or prevent power circuit to application
The interference of circuit.
3, the technical program has universal asynchronous receiving-transmitting transmission as a result of the larger element of volume in the application circuit
Device interface, Serial Peripheral Interface (SPI), monolithic wireless transceiver chip, power interface, main control chip, global positioning system, power supply are opened
Pass, six axis motion process component of conformability, IC bus interface, reset switch, receiver chip；The universal asynchronous receipts
Hair transmitter interfaces are arranged in the middle part of the top of the circuit main board, and the Serial Peripheral Interface (SPI) is arranged in the circuit main board
In the middle part of the right, the monolithic wireless transceiver chip is arranged in the following middle part of the circuit main board, the power interface setting
In the middle part of the left side of the circuit main board, the main control chip is arranged in the positive right middle of the circuit main board, the whole world
Positioning system be arranged in the positive lower left quarter of the circuit main board, the power switch be arranged the circuit main board front simultaneously
Positioned at the left of the global positioning system, six axis motion process component of the conformability is arranged in the front of the circuit main board
And positioned at the top of the global positioning system, the IC bus interface is arranged in the positive upper right of the circuit main board
Portion, the reset switch are arranged in the front of the circuit main board and between the global positioning system and main control chip,
The technological means in the positive right lower quadrant of the circuit main board is arranged in the receiver chip, so, the element larger to volume
Layout has made rational optimization, is not only advantageous to be distributed other smaller elements, moreover, the redundancy of circuit main board can be greatly reduced
Area can further make circuit main board micromation, lightweight in turn.
4, the technical program has data wiring and power-supply wiring, the circuit board as a result of the front of the circuit board
Reverse side have power-supply wiring；The width of the data wiring is 50mil, and the width of the power-supply wiring is 45mil~55mil phases
Interval between two adjacent data wirings is 18mil~22mil, the interval between adjacent two power-supply wirings
It is 18mil~22mil, the interval between the wiring of the adjacent data and the power-supply wiring is the skill of 27mil~33mil
Art means, so, the density of the density and power-supply wiring of data wiring is increased, the length and power-supply wiring of data wiring are shortened
Length, element integrated installation can be made, further make circuit main board micromation, lightweight.
5, the technical program has single-lithium-battery electrolytic battery charger as a result of the larger element of volume in the power circuit
With constant 5V boost pressure controllers, lithium battery；The single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers are arranged in the electricity
The middle and upper part of road mainboard reverse side, the lithium battery is arranged is offset to the power interface in the middle part of the circuit main board reverse side,
The lithium battery 20 is the technological means of 1S lithium batteries, so, can in front it is various it is improved on the basis of further mitigate
The weight of lithium battery, to mitigate the weight of complete machine significantly, it can be achieved that power consumption is low, flight is flexible, security performance is high, behaviour
Connive advantageous effect easy, at low cost.
6, the technical program has main control chip circuit as a result of the application circuit, shows corridor circuit for lamp, 3.3 voltage stabilizings electricity
Road, remote control signal receiver governor circuit, gyroscope block, switch and battery input filter circuit, interface section circuit, metal-oxide-semiconductor
The technological means of driving circuit, so, unmanned plane can be made to have multiple functions.
7, the width that the technical program is connected up as a result of the data is 50mil, and the width of the power-supply wiring is
50mil；Interval between adjacent two data wirings is 20mil, between adjacent two power-supply wirings between
Every being 20mil, the interval between the wiring of the adjacent data and the power-supply wiring is the technological means of 30mil, so, it can
The integrated installation of element is set more to optimize.
Description of the drawings
The unmanned plane to the utility model for road traffic monitoring is made into one with reference to the accompanying drawings and detailed description
The detailed description of step.
Fig. 1 is the positive primary structure schematic diagram of unmanned plane for being used for road traffic monitoring in the prior art.
Fig. 2 is the positive physical structure diagram of unmanned plane that the utility model is used for road traffic monitoring.
Fig. 3 is the positive primary structure schematic diagram of unmanned plane that the utility model is used for road traffic monitoring.
Fig. 4 is primary structure schematic diagram of the utility model for the unmanned plane reverse side of road traffic monitoring.
Fig. 5 is the utility model for the main control chip circuit diagram in the unmanned plane of road traffic monitoring.
Fig. 6 is the utility model for showing corridor circuit for lamp figure in the unmanned plane of road traffic monitoring.
Fig. 7 is the utility model for 3.3 regulator circuit figures in the unmanned plane of road traffic monitoring.
Fig. 8 is the utility model for the remote control signal receiver governor circuit figure in the unmanned plane of road traffic monitoring.
Fig. 9 is the utility model for the gyroscope block figure in the unmanned plane of road traffic monitoring.
Figure 10 is the utility model for the switch and battery input filter circuit figure in the unmanned plane of road traffic monitoring.
Figure 11 is the utility model for the interface section circuit diagram in the unmanned plane of road traffic monitoring.
Figure 12 is the utility model for the metal-oxide-semiconductor driving circuit figure in the unmanned plane of road traffic monitoring.
Figure 13 is single-lithium-battery electrolytic battery charger and constant 5V in the unmanned plane that the utility model is monitored for road traffic
Boost control circuit figure.
The reference numerals are as follows.
1~circuit board；
2~circuit main board；
3~circuit support plate；
4~motor；
5~propeller；
6~universal asynchronous receiving-transmitting transmitter interface；
7~Serial Peripheral Interface (SPI)；
8~monolithic wireless transceiver chip；
9~power interface；
10~main control chip；
11~global positioning system；
12~power switch；
13~conformability, six axis motion process component；
14~IC bus interface；
15~reset switch；
16~receiver chip；
17~data connect up；
18~power-supply wiring；
19~single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers；
20~lithium battery.
Specific implementation mode
As shown in Figures 2 to 4, the utility model provides a kind of unmanned plane for road traffic monitoring, including doubles as nothing
4, four, the motor propeller 5 of circuit board 1, four of man-machine skeleton, four propellers 5 are separately fixed at four motors
In 4 rotation axis.
The circuit board 1 includes circuit main board 2 and four circuit support plates 3, and the shape of the circuit main board 2 is square,
The shape of four circuit support plates 3 is elongated, and four circuit support plates 3 are located at four of the circuit main board 2
Angle is simultaneously radially distributed, and four circuit support plates 3 and the circuit main board 2 are integrated, four motors 4 respectively with
Four circuit support plates 3 are fixedly connected.
Present embodiment includes circuit main board and four circuit support plates, the circuit main board as a result of the circuit board
Shape it is square, the shape of four circuit support plates is elongated, and four circuit support plates are located at the electricity
Four angles of road mainboard are simultaneously radially distributed, and four circuit support plates and the circuit main board are integrated, described in four
The technological means that motor is fixedly connected with four circuit support plates respectively, so, four after the area for reducing circuit main board
Propeller will not interfere, and advantage is provided for the micromation of circuit board.
As shown in Figures 2 to 4, the circuit board 1 is double-sided PCB, and the front of the circuit main board 2 is application circuit,
The reverse side of the circuit main board 2 is power circuit.
Present embodiment is double-sided PCB as a result of the circuit board, and the front of the circuit main board is using electricity
The reverse side on road, the circuit main board is the technological means of power circuit, so, it is not only advantageous to greatly reduce the face of circuit main board
Product, moreover, it is also possible to effectively reduce or prevent interference of the power circuit to application circuit.
As shown in Figure 2 to Figure 3, in the application circuit the larger element of volume have universal asynchronous receiving-transmitting transmitter interface 6,
Serial Peripheral Interface (SPI) 7, monolithic wireless transceiver chip 8, power interface 9, main control chip 10, global positioning system 11, power supply are opened
12, six axis motion process component 13 of conformability, IC bus interface 14, reset switch 15, receiver chip 16 are closed, it is described
Universal asynchronous receiving-transmitting transmitter interface 6 is arranged in the middle part of the top of the circuit main board 2, and the setting of the Serial Peripheral Interface (SPI) 7 exists
In the middle part of the right of the circuit main board 2, the monolithic wireless transceiver chip 8 is arranged at the following middle part of the circuit main board 2,
The power interface 9 is arranged in the middle part of the left side of the circuit main board 2, and the main control chip 10 is arranged in the circuit main board 2
Positive right middle, the global positioning system 11 are arranged in 2 positive lower left quarter of the circuit main board, the power switch 12
It is arranged in the front of the circuit main board 2 and at the left of the global positioning system 11, six axis movement of the conformability
Reason component 13 is arranged in the front of the circuit main board 2 and positioned at the top of the global positioning system 11, the integrated circuit
Bus interface 14 is arranged in 2 positive upper right quarter of the circuit main board, and the reset switch 15 is arranged in the circuit main board 2
Front and positioned at the global positioning system 11 and main control chip 10 between, the receiver chip 16 setting in the circuit master
2 positive right lower quadrant of plate.
Present embodiment has universal asynchronous receiving-transmitting transmitter as a result of the larger element of volume in the application circuit
Interface, Serial Peripheral Interface (SPI), monolithic wireless transceiver chip, power interface, main control chip, global positioning system, power switch,
Six axis motion process component of conformability, IC bus interface, reset switch, receiver chip；The universal asynchronous receiving-transmitting
Transmitter interfaces are arranged in the middle part of the top of the circuit main board, and the Serial Peripheral Interface (SPI) is arranged on the right side of the circuit main board
In the middle part of side, the monolithic wireless transceiver chip is arranged at the following middle part of the circuit main board, and the power interface setting exists
In the middle part of the left side of the circuit main board, in the positive right middle of the circuit main board, the whole world is fixed for the main control chip setting
Position system is arranged in the positive lower left quarter of the circuit main board, and the power switch is arranged in the front of the circuit main board and position
In the left of the global positioning system, six axis motion process component of the conformability be arranged the circuit main board front simultaneously
Positioned at the top of the global positioning system, the IC bus interface is arranged in the positive upper right of the circuit main board
Portion, the reset switch are arranged in the front of the circuit main board and between the global positioning system and main control chip,
The technological means in the positive right lower quadrant of the circuit main board is arranged in the receiver chip, so, the element larger to volume
Layout has made rational optimization, is not only advantageous to be distributed other smaller elements, moreover, the redundancy of circuit main board can be greatly reduced
Area can further make circuit main board micromation, lightweight in turn.
As shown in figure 4, the larger element of volume has single-lithium-battery electrolytic battery charger and constant 5V boostings in the power circuit
Controller 19, lithium battery 20, the single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers 19 are arranged in the circuit main board 2
The middle and upper part of reverse side, the lithium battery 20, which is arranged in the middle part of 2 reverse side of the circuit main board, is offset to the power interface 9, institute
It is 1S lithium batteries to state lithium battery 20.
Present embodiment as a result of the larger element of volume in the power circuit have single-lithium-battery electrolytic battery charger and
Constant 5V boost pressure controllers, lithium battery；The single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers are arranged in the circuit
The middle and upper part of mainboard reverse side, the lithium battery, which is arranged in the middle part of the circuit main board reverse side, is offset to the power interface, institute
State the technological means that lithium battery 20 is 1S lithium batteries, so, can in front it is various it is improved on the basis of further mitigate lithium
The weight of battery, to mitigate the weight of complete machine significantly, it can be achieved that power consumption is low, flight is flexible, security performance is high, manipulates
It is easy, advantageous effect at low cost.
As shown in Figures 2 to 4, there are data wiring 17 and power-supply wiring 18, the circuit board 1 in the front of the circuit board 1
Reverse side have a power-supply wiring 18, the width of the data wiring 17 is 50mil, the width of the power-supply wiring 18 be 45mil~
55mil, the interval between adjacent two data wirings 17 is 18mil~22mil, adjacent two power-supply wirings
Interval between 18 is 18mil~22mil, and the interval between adjacent data wiring 17 and the power-supply wiring 18 is
27mil~33mil.
Present embodiment has data wiring and power-supply wiring as a result of the front of the circuit board, the circuit board
Reverse side has power-supply wiring；The width of the data wiring is 50mil, and the width of the power-supply wiring is 45mil~55mil adjacent
Two data wirings between interval be 18mil~22mil, the interval between adjacent two power-supply wirings is
It is 18mil~22mil, the interval between the wiring of the adjacent data and the power-supply wiring is the technology of 27mil~33mil
Means, so, the density of the density and power-supply wiring of data wiring is increased, the length and power-supply wiring of data wiring are shortened
Length can make element integrated installation, further make circuit main board micromation, lightweight.
As shown in Figure 2 to Figure 3, the application circuit has main control chip circuit, clearance lamps circuit, 3.3 regulator circuits, remote control
Signal receives governor circuit, gyroscope block, switch and battery input filter circuit, interface section circuit, metal-oxide-semiconductor driving electricity
Road.As shown in figure 4, the power circuit has single-lithium-battery electrolytic battery charger and constant 5V boost control circuits.
Present embodiment has main control chip circuit, clearance lamps circuit, 3.3 voltage stabilizings electricity as a result of the application circuit
Road, remote control signal receiver governor circuit, gyroscope block, switch and battery input filter circuit, interface section circuit, metal-oxide-semiconductor
Driving circuit, the power circuit have the technological means of single-lithium-battery electrolytic battery charger and constant 5V boost control circuits, so, it can
Unmanned plane is set to have multiple functions, simultaneously, it can be ensured that unmanned plane normal flight.
As shown in Figures 2 to 4, the width of the data wiring 17 is 50mil, and the width of the power-supply wiring 18 is
50mil,
Interval between adjacent two data wirings 17 is 20mil, adjacent two power-supply wirings 18 it
Between interval be 20mil, the adjacent data wiring 17 and the power-supply wiring 18 between interval be 30mil.
The width that present embodiment is connected up as a result of the data is 50mil, and the width of the power-supply wiring is
50mil；Interval between adjacent two data wirings is 20mil, between adjacent two power-supply wirings between
Every being 20mil, the interval between the wiring of the adjacent data and the power-supply wiring is the technological means of 30mil, so, it can
The integrated installation of element is set more to optimize.
The motor 4 is efficient 820 hollow-cup motor of lower resistance.
As shown in Figures 2 to 4, present embodiment is efficient 820 drag cup of lower resistance as a result of the motor 4
The technological means of motor, so, flight noise is small.
Claims (1)
1. it is a kind of for road traffic monitoring unmanned plane, include the circuit board (1) as unmanned plane skeleton, four motors (4),
Four propellers (5), four propellers (5) are separately fixed in the rotation axis of four motors (4), and feature exists
In：
The circuit board (1) includes circuit main board (2) and four circuit support plates (3), and the shape of the circuit main board (2) is in pros
The shape of shape, four circuit support plates (3) is elongated, and four circuit support plates (3) are located at the circuit main board
(2) four angles are simultaneously radially distributed, and four circuit support plates (3) and the circuit main board (2) are integrated, four institutes
Motor (4) is stated to be fixedly connected with four circuit support plates (3) respectively,
The circuit board (1) is double-sided PCB, and the front of the circuit main board (2) is application circuit, the circuit main board (2)
Reverse side be power circuit,
In the application circuit the larger element of volume have universal asynchronous receiving-transmitting transmitter interface (6), Serial Peripheral Interface (SPI) (7),
Monolithic wireless transceiver chip (8), power interface (9), main control chip (10), global positioning system (11), power switch (12),
Six axis motion process component (13) of conformability, IC bus interface (14), reset switch (15), receiver chip (16),
Universal asynchronous receiving-transmitting transmitter interface (6) setting is in the middle part of the top of the circuit main board (2), the serial peripheral
Interface (7) is arranged in the middle part of the right of the circuit main board (2), and the monolithic wireless transceiver chip (8) is arranged in the electricity
The following middle part of road mainboard (2), power interface (9) setting is in the middle part of the left side of the circuit main board (2), the master control core
Piece (10) setting is arranged in the circuit main board (2) positive right middle, the global positioning system (11) in the circuit master
Plate (2) positive lower left quarter, power switch (12) setting are determined in the front of the circuit main board (2) and positioned at the whole world
Position system (11) left, six axis motion process component (13) of the conformability be arranged the circuit main board (2) front simultaneously
Top positioned at the global positioning system (11), the IC bus interface (14) are arranged in the circuit main board (2)
Positive upper right quarter, reset switch (15) setting is in the front of the circuit main board (2) and is located at the global positioning system
It unites between (11) and main control chip (10), the receiver chip (16) is arranged in the circuit main board (2) positive right lower quadrant,
The larger element of volume has single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers (19), lithium electricity in the power circuit
Pond (20),
On the single-lithium-battery electrolytic battery charger and constant 5V boost pressure controllers (19) are arranged in the circuit main board (2) reverse side
Portion, lithium battery (20) setting are offset to the power interface (9), the lithium in the middle part of the circuit main board (2) reverse side
Battery (20) is 1S lithium batteries,
The front of the circuit board (1) has data wiring (17) and power-supply wiring (18), the reverse side of the circuit board (1) to have power supply
It connects up (18),
The width of the data wiring (17) is 50mil, and the width of the power-supply wiring (18) is 45mil~55mil,
Interval between two adjacent data wirings (17) is 18mil~22mil, adjacent two power-supply wirings
(18) interval between is 18mil~22mil, and the adjacent data connect up between (17) and the power-supply wiring (18)
Interval is 27mil~33mil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820533518.5U CN207644643U (en) | 2018-04-16 | 2018-04-16 | A kind of unmanned plane for road traffic monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820533518.5U CN207644643U (en) | 2018-04-16 | 2018-04-16 | A kind of unmanned plane for road traffic monitoring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207644643U true CN207644643U (en) | 2018-07-24 |
Family
ID=62876445
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820533518.5U Expired - Fee Related CN207644643U (en) | 2018-04-16 | 2018-04-16 | A kind of unmanned plane for road traffic monitoring |
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| Country | Link |
|---|---|
| CN (1) | CN207644643U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353509A (en) * | 2018-11-06 | 2019-02-19 | 江苏慕航空间信息技术有限公司 | A kind of UAV system |
| CN110658771A (en) * | 2019-10-30 | 2020-01-07 | 哈工大机器人（岳阳）军民融合研究院 | Load control device based on large-load unmanned aerial vehicle and control method thereof |
| CN112124588A (en) * | 2020-10-14 | 2020-12-25 | 郑州妙灿智能科技有限公司 | Road real-time monitoring unmanned aerial vehicle |
-
2018
- 2018-04-16 CN CN201820533518.5U patent/CN207644643U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353509A (en) * | 2018-11-06 | 2019-02-19 | 江苏慕航空间信息技术有限公司 | A kind of UAV system |
| CN110658771A (en) * | 2019-10-30 | 2020-01-07 | 哈工大机器人（岳阳）军民融合研究院 | Load control device based on large-load unmanned aerial vehicle and control method thereof |
| CN112124588A (en) * | 2020-10-14 | 2020-12-25 | 郑州妙灿智能科技有限公司 | Road real-time monitoring unmanned aerial vehicle |
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