CN208746250U - Unmanned plane and its monitoring system - Google Patents
Unmanned plane and its monitoring system Download PDFInfo
- Publication number
- CN208746250U CN208746250U CN201821239485.XU CN201821239485U CN208746250U CN 208746250 U CN208746250 U CN 208746250U CN 201821239485 U CN201821239485 U CN 201821239485U CN 208746250 U CN208746250 U CN 208746250U
- Authority
- CN
- China
- Prior art keywords
- main body
- monitoring device
- unmanned plane
- device main
- monitoring
- 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.)
- Expired - Fee Related
Links
- 238000012544 monitoring process Methods 0.000 title claims abstract description 33
- 238000012806 monitoring device Methods 0.000 claims abstract description 61
- 230000003628 erosive effect Effects 0.000 claims description 5
- 239000000945 filler Substances 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 3
- 238000004064 recycling Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
Landscapes
- Closed-Circuit Television Systems (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The utility model discloses unmanned plane and its monitoring systems, including monitoring device main body, the monitoring device main body is internally provided with keyboard, the upper end of the monitoring device main body is provided with hollow hinge, the hollow hinge is internally provided with shaft, the hollow hinge upper end is provided with upper cover, the leading exterior surface of the upper cover is provided with display screen, conducting wire is provided between the monitoring device main body and display screen, monitoring system includes camera system, remote control system, positioning system, operating system, and unmanned plane includes unmanned plane main body.Unmanned plane described in the utility model and its monitoring system, the equipment under severe working environment can be prevented to be damaged, it can light mobile device by handle, conducting wire can reduce the friction between conducting wire and equipment by hollow hinge, prevent wire fracture, increase service life, this unmanned plane and its monitoring system will bring better prospect of the application.
Description
Technical field
The utility model relates to monitoring system fields, in particular to unmanned plane and its monitoring system.
Background technique
The monitoring system of unmanned plane can build ground in, can also be located on vehicle, ship or other platforms, be by monitoring
System can not only obtain the information that unmanned plane is spied out, but also can issue and instruct to unmanned plane, control its flight,
Unmanned plane is set to smoothly complete task, there are many type, main (transmitting) sides of taking off for (transmitting) device that takes off of unmanned plane
Formula has ground roll-out to take off, along guide rail transmitting, aerial dispensing etc., some small drone are by container type emitter in container
The transmitting of hydraulic or Pneumatic pressure power, the way of recycling of unmanned plane includes automatic Landing, parachute recycling and intercept net recycling etc., no
Unmanned plane under same type and different use environments may be selected different systems and constitute, such as: small drone generallys use bullet
It penetrates or rocket launching, and large-scale unmanned plane then uses undercarriage or car launcher to be emitted；Traditional Monitor Equipment is because of work
The arduous of environment is set, being easy to be damaged causes service life not grown, and in addition equipment is frequently necessary to move, and carries very not square
Just, therefore we have proposed this unmanned plane and its monitoring systems.
Utility model content
The main purpose of the utility model is to provide unmanned plane and its monitoring systems, can effectively solve in background technique
The problem of.
To achieve the above object, the technical solution that the utility model is taken are as follows:
Unmanned plane and its monitoring system, including monitoring device main body, the monitoring device main body are internally provided with keyboard,
The upper end of the monitoring device main body is provided with hollow hinge, and the hollow hinge is internally provided with shaft, the hollow conjunction
Page upper end is provided with upper cover, and the leading exterior surface of the upper cover is provided with display screen, the monitoring device main body and display screen it
Between be provided with conducting wire, monitoring system includes camera system, remote control system, positioning system, operating system, and unmanned plane includes unmanned plane
Main body, unmanned plane main body upper end outer surface are provided with camera, and the front end of the unmanned plane main body is provided with inductor, institute
The inside for stating unmanned plane main body is provided with GPS positioning instrument close to the side of camera, and the inside of the unmanned plane main body is close to GPS
The side of position indicator is provided with controller.
Preferably, the leading exterior surface of the monitoring device main body is provided with buckle, the buckle and monitoring device main body
It is fixedly connected, the quantity of the buckle is two groups, and the buckle is symmetrical about the centerline axis of monitoring device main body, the upper cover
Upper end be provided with bolt, bolt is fixedly connected with upper cover, the display screen pass through bolt, buckle and monitoring device subject activity
Connection, the leading exterior surface of the monitoring device main body are provided with handle close to the side of buckle, the monitoring device main body with
Fixed screw is provided between handle, the handle is fixedly connected by fixed screw with monitoring device main body.
Preferably, turn trough is provided between the hollow hinge and shaft, the shaft is sliding by turn trough and hollow hinge
Dynamic connection, the display screen are electrically connected by conducting wire and monitoring device main body, the input port and monitoring device of the keyboard
The output port of main body is electrically connected.
Preferably, the lower end of the inner keyboard of the monitoring device main body is provided with shockproof filler, the monitoring device
The outer surface of main body is coated with erosion shield, the output port of the camera system, remote control system, positioning system, operating system
It is connect with the input port of camera, inductor GPS positioning instrument controller by electric signal.
Preferably, the lower end of the inner keyboard of the monitoring device main body is provided with shockproof filler, the monitoring device
The outer surface of main body is coated with erosion shield, the output port of the camera system, remote control system, positioning system, operating system
It is connect with the input port of camera, inductor GPS positioning instrument controller by electric signal.
Preferably, miniature hex(agonal)screw is provided between the upper cover and display screen, the upper cover passes through miniature hexagonal spiral shell
Silk is fixedly connected with display screen, and the quantity of miniature hex(agonal)screw is four groups.
Compared with prior art, the utility model has the following beneficial effects: the unmanned plane and its monitoring system, by upper
Lid covers monitoring device main body, prevents equipment to be damaged under severe working environment, can lead to when replacing work-yard
Buckle is crossed to secure the equipment in monitoring device main body, by handle can light mobile device, conducting wire can pass through hollow hinge
Reduce the friction between conducting wire and equipment, prevent wire fracture, increase service life, by using effect relative to tradition side
Formula is more preferable.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model unmanned plane and its monitoring system；
Fig. 2 is the partial view of the utility model unmanned plane and its monitoring system；
Fig. 3 is the partial view of the utility model unmanned plane and its monitoring system；
Fig. 4 is the enlarged drawing of the A of the utility model unmanned plane and its monitoring system；
Fig. 5 is the working principle diagram of the utility model unmanned plane and its monitoring system.
In figure: 1, monitoring device main body；2, keyboard；3, upper cover；4, display screen；5, camera system；6, remote control system；7, fixed
Position system；8, operating system；9, it buckles；10, handle；11, bracket；12, unmanned plane main body；13, camera；14, inductor；
15, GPS positioning instrument；16, controller；17, conducting wire；18, hollow hinge；19, shaft.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
As shown in Figs. 1-5, unmanned plane and its monitoring system, including monitoring device main body 1, the inside of monitoring device main body 1
It is provided with keyboard 2, the upper end of monitoring device main body 1 is provided with hollow hinge 18, and hollow hinge 18 is internally provided with shaft 19,
Hollow 18 upper end of hinge is provided with upper cover 3, and the leading exterior surface of upper cover 3 is provided with display screen 4, monitoring device main body 1 and display
Conducting wire 17 is provided between screen 4, monitoring system includes camera system 5, remote control system 6, positioning system 7, operating system 8, nobody
Machine includes unmanned plane main body 12, and 12 upper end outer surface of unmanned plane main body is provided with camera 13, and the front end of unmanned plane main body 12 is set
It is equipped with inductor 14, the inside of unmanned plane main body 12 is provided with GPS positioning instrument 15, unmanned plane main body close to the side of camera 13
12 inside is provided with controller 16 close to the side of GPS positioning instrument 15.
The leading exterior surface of monitoring device main body 1 is provided with buckle 9, and buckle 9 is fixedly connected with monitoring device main body 1, blocks
The quantity of button 9 is two groups, and buckle 9 is symmetrical about the centerline axis of monitoring device main body 1, and the upper end of upper cover 3 is provided with bolt, spiral shell
Bolt is fixedly connected with upper cover 3, and display screen 4 is flexibly connected by bolt, buckle 9 with monitoring device main body 1, passes through buckle 9 and spiral shell
The cooperation of bolt can seal equipment, and the leading exterior surface of monitoring device main body 1 is provided with handle 10 close to the side of buckle 9,
Fixed screw is provided between monitoring device main body 1 and handle 10, handle 10 is fixed by fixed screw and monitoring device main body 1
Connection；Turn trough is provided between hollow hinge 18 and shaft 19, shaft 19 is slidably connected with hollow hinge 18 by turn trough, is passed through
Turn trough can reduce the friction display screen 4 between shaft 19 and hollow hinge 18 and electrically be connected by conducting wire 17 with monitoring device main body 1
It connects, the input port of keyboard 2 and the output port of monitoring device main body 1 are electrically connected；The inner keyboard 2 of monitoring device main body 1
Lower end be provided with shockproof filler, the outer surface of monitoring device main body 1 is coated with erosion shield, camera system 5, remote control system
6, the input terminal of the output port and camera 13,15 controller 16 of inductor 14GPS position indicator of positioning system 7, operating system 8
Mouth passes through electric signal and connects；The lower end of the inner keyboard 2 of monitoring device main body 1 is provided with shockproof filler, monitoring device main body 1
Outer surface be coated with erosion shield, camera system 5, remote control system 6, positioning system 7, operating system 8 output port with take the photograph
It, can be with by camera 13 as the input port of first 13, inductor 14, GPS positioning instrument 15, controller 16 is connected by electric signal
Photo is acquired, the electric signal that can receive remote control system 6 by inductor 14 passes through GPS positioning instrument 15 to control unmanned plane
The position that unmanned plane can be positioned can control unmanned plane by controller 16；It is provided between upper cover 3 and display screen 4 miniature
Hex(agonal)screw, upper cover 3 are fixedly connected by miniature hex(agonal)screw with display screen 4, and the quantity of miniature hex(agonal)screw is four groups, upper cover
3 pairs of monitoring devices play a protective role.
It should be noted that the utility model is unmanned plane and its monitoring system, when in use, user passes through bracket 11
Equipment is fixed, equipment is opened by upper cover 3, equipment is controlled by the keyboard 2 in monitoring device main body 1, it can by display screen 4
Intuitively to see the data of monitoring system collection, the camera of 12 upper end of unmanned plane main body can control by camera system 5
13 (models are as follows: A-4070), remote control system 6 can control inductor 14 (model are as follows: PSAN-01 type), pass through GPS positioning instrument 15
The cooperation of (model: good bright 20 upgrade version) and positioning system 7 can position the position of unmanned plane, pass through operating system 8 and control
The flight path that device 16 (model are as follows: XMTA type) can control unmanned plane, by hollow between upper cover 3 and monitoring device main body 1
Hinge 18 cooperates together with shaft 19, and conducting wire 17 can pass through inside hollow hinge 18, is set by handle 10
It is standby to carry, traditional unmanned plane and its monitoring system have been surmounted on prospect of the application, it is more practical.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above.Current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (6)
1. unmanned plane and its monitoring system, including monitoring device main body (1), it is characterised in that: the monitoring device main body (1)
It is internally provided with keyboard (2), the upper end of the monitoring device main body (1) is provided with hollow hinge (18), the hollow hinge
(18) be internally provided with shaft (19), hollow hinge (18) upper end is provided with upper cover (3), the front end of the upper cover (3)
Outer surface is provided with display screen (4), is provided with conducting wire (17) between the monitoring device main body (1) and display screen (4), monitoring system
System includes camera system (5), remote control system (6), positioning system (7), operating system (8), and unmanned plane includes unmanned plane main body
(12), unmanned plane main body (12) the upper end outer surface is provided with camera (13), and the front end of the unmanned plane main body (12) is set
It is equipped with inductor (14), the inside of the unmanned plane main body (12) is provided with GPS positioning instrument close to the side of camera (13)
(15), the inside of the unmanned plane main body (12) is provided with controller (16) close to the side of GPS positioning instrument (15).
2. unmanned plane according to claim 1 and its monitoring system, it is characterised in that: the monitoring device main body (1)
Leading exterior surface is provided with buckle (9), and the buckle (9) is fixedly connected with monitoring device main body (1), the number of the buckle (9)
Amount is two groups, and the buckle (9) is symmetrical about the centerline axis of monitoring device main body (1), and the upper end of the upper cover (3) is provided with
Bolt, bolt are fixedly connected with upper cover (3), and the display screen (4) passes through bolt, buckle (9) and monitoring device main body (1) activity
The leading exterior surface of connection, the monitoring device main body (1) is provided with handle (10), the monitoring close to the side of buckle (9)
Fixed screw is provided between equipment body (1) and handle (10), the handle (10) passes through fixed screw and monitoring device master
Body (1) is fixedly connected.
3. unmanned plane according to claim 1 and its monitoring system, it is characterised in that: the monitoring device main body (1)
Lower end is provided with bracket (11), and the bracket (11) is fixedly connected with monitoring device main body (1), and the quantity of the bracket (11) is
Four groups, bracket (11) the rectangular array arrangement, the lower end of the unmanned plane main body (12) is provided with idler wheel, the quantity of idler wheel
Be four groups, one end of the hollow hinge (18) is fixedly connected with monitoring device main body (1), the hollow hinge (18) it is another
End is fixedly connected with upper cover (3).
4. unmanned plane according to claim 1 and its monitoring system, it is characterised in that: the hollow hinge (18) and shaft
(19) turn trough is provided between, the shaft (19) is slidably connected by turn trough with hollow hinge (18), and the display screen (4) is logical
It crosses conducting wire (17) and monitoring device main body (1) to be electrically connected, input port and monitoring device main body (1) of the keyboard (2)
Output port is electrically connected.
5. unmanned plane according to claim 1 and its monitoring system, it is characterised in that: the monitoring device main body (1)
The lower end of inner keyboard (2) is provided with shockproof filler, and the outer surface of the monitoring device main body (1) is coated with erosion shield,
The camera system (5), remote control system (6), positioning system (7), the output port of operating system (8) and camera (13), sense
The input port of device (14) GPS positioning instrument (15) controller (16) is answered to connect by electric signal.
6. unmanned plane according to claim 1 and its monitoring system, it is characterised in that: the upper cover (3) and display screen (4)
Between be provided with miniature hex(agonal)screw, the upper cover (3) is fixedly connected by miniature hex(agonal)screw with display screen (4), miniature six
The quantity of angle screw is four groups.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821239485.XU CN208746250U (en) | 2018-08-02 | 2018-08-02 | Unmanned plane and its monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821239485.XU CN208746250U (en) | 2018-08-02 | 2018-08-02 | Unmanned plane and its monitoring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208746250U true CN208746250U (en) | 2019-04-16 |
Family
ID=66058504
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821239485.XU Expired - Fee Related CN208746250U (en) | 2018-08-02 | 2018-08-02 | Unmanned plane and its monitoring system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208746250U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111031730A (en) * | 2020-01-08 | 2020-04-17 | 济源市农业技术推广中心 | A device for operation supervision of agricultural plant protection unmanned aerial vehicle |
-
2018
- 2018-08-02 CN CN201821239485.XU patent/CN208746250U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111031730A (en) * | 2020-01-08 | 2020-04-17 | 济源市农业技术推广中心 | A device for operation supervision of agricultural plant protection unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109187884A (en) | A kind of Atmospheric components of anti-disturbance based on unmanned plane monitor system | |
| CN208746250U (en) | Unmanned plane and its monitoring system | |
| CN207389542U (en) | A kind of new unmanned plane based on remote sensing technology | |
| CN204279947U (en) | The unmanned prior-warning plane of a kind of novel long-range | |
| CN206750164U (en) | A kind of removable multifunctional business Towed bird system | |
| CN206202669U (en) | A kind of pesticide spraying unmanned plane | |
| CN204916155U (en) | Multipurpose unmanned aerial vehicle | |
| CN204776010U (en) | Many rotors unmanned vehicles | |
| CN207346109U (en) | A kind of strong unmanned plane of barrier propterty | |
| CN202953173U (en) | Smart parachute control system | |
| CN106197423A (en) | A kind of unmanned plane automatic dispenser track recording device | |
| CN109398717A (en) | A kind of multifunctional monitoring unmanned plane device | |
| CN202464135U (en) | Forest fireproofing unmanned aerial vehicle | |
| CN207985198U (en) | A kind of plant protection drone case that spreads pesticides | |
| CN207292410U (en) | A kind of unmanned plane for air monitering | |
| CN205589506U (en) | Novel medicine rack is spouted in unmanned aerial vehicle pneumatics device | |
| CN109976283A (en) | A kind of huge ship section inspection plotting board based on unmanned plane networking | |
| CN201113984Y (en) | Short wave reception optical fiber transmission system | |
| CN207658072U (en) | Unmanned plane parachute protective device | |
| CN207926609U (en) | A kind of Portable unmanned machine interferometer | |
| CN206993300U (en) | A kind of aviation management supervising device of Big Dipper aviation | |
| CN206775220U (en) | A kind of SUAV solar energy energy supplying system | |
| CN209386896U (en) | A kind of portable radiotelephone control navigation device | |
| CN203593159U (en) | Multi-purpose unmanned aerial vehicle | |
| CN207263185U (en) | The flight course planning system that a kind of complex mountainous electric operating fixed-wing unmanned plane is applicable in |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190416 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |