CN206155807U - Current surveying unmanned aerial vehicle that makes a video recording - Google Patents
Current surveying unmanned aerial vehicle that makes a video recording Download PDFInfo
- Publication number
- CN206155807U CN206155807U CN201621231893.1U CN201621231893U CN206155807U CN 206155807 U CN206155807 U CN 206155807U CN 201621231893 U CN201621231893 U CN 201621231893U CN 206155807 U CN206155807 U CN 206155807U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- aerial vehicle
- unmanned aerial
- flow measurement
- radar
- 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
Abstract
The utility model relates to a current surveying unmanned aerial vehicle that makes a video recording, including unmanned aerial vehicle, unmanned aerial vehicle includes the fuselage, installs battery, satellite navigation device and radio control apparatus in the fuselage, and the both sides of fuselage are equipped with horizontal wing respectively, the tip of each horizontal wing do not extends the flank to the fore -and -aft direction, and vertical orientation two coaxial driving motor are installed to the tip of each flank, and two driving motor's output shaft backward sets up, and the screw is installed in each driving motor's pivot, each driving motor and battery and radio control apparatus are connected, the radar frame is installed to the fuselage bottom, installs the video transmission device on the radar frame, and the bottom of radar frame has hung current surveying radar and camera device, and video transmission device, current surveying radar and camera device all are connected with battery and radio control apparatus, the fuselage install folding undercarriage respectively with the junction wing.
Description
Technical field
The utility model is related to a kind of flow measuring device, and in particular to a kind of flow measurement images unmanned aerial vehicle.
Background technology
Need to be monitored cross section of river, water flow velocity, flow etc. in Flood Prevention, flood-fighting.Legacy equipment is such as
Flow measurement ship enters water gaging and there is larger risk when rivers current speed is larger, is easily washed away by current, causes the loss of equipment.It is existing
Some flow measuring devices generally do not include camera function, in flood region occurred frequently, it is impossible to enough to do effective monitoring to regimen.
The content of the invention
To solve deficiency of the prior art, the purpose of this utility model is to provide a kind of nothing for carrying radar and shooting
People's aircraft.
The technical scheme that the utility model is taken is：
A kind of flow measurement images unmanned aerial vehicle, including unmanned plane, and unmanned plane includes fuselage, battery, satellite are provided with fuselage
Guider and control device of wireless, fuselage is respectively provided on two sides with horizontal wings, the end of each horizontal wings respectively to
Fore-and-aft direction extends flank, and the end of each flank is provided with two coaxial motors of vertical direction, two motors
Output shaft is oppositely arranged, and the rotating shaft of each motor is provided with screw；Each motor connects with battery and control device of wireless
Connect；Fuselage bottom is provided with radar frame, and video transmission device is provided with radar frame, and the bottom hung of radar frame has flow measurement thunder
Up to and camera head, video transmission device, flow measurement radar and camera head are connected with battery and control device of wireless；Fuselage
Be separately installed with folding undercarriage with the junction of wing.
Further, the camera head includes vertical steering wheel, horizontal steering wheel and camera, and vertical steering wheel is installed on thunder
Up to the bottom of frame, the output end of vertical steering wheel is provided with fork, and horizontal steering wheel is installed on the swinging end of fork, and camera is installed on
The output end of horizontal steering wheel.
Further, the folding undercarriage includes A-frame and undercarriage, and A-frame is installed on fuselage and wing
Between, undercarriage is articulated with a base angle of A-frame, and a flap, flap Jing two are hinged with another base angle of A-frame
Level connecting rod is connected with undercarriage, is articulated and connected between two-stage connecting rod, and the two ends of two-stage connecting rod are hingedly connected to flap and undercarriage；Three
Angle support is provided with limiting section, and the limiting section is spacing to the pin joint of two-stage connecting rod；Draw between the drift angle and flap of A-frame
Stretching has spring.
Further, the equal eccentric setting of tie point of the two-stage connecting rod and spring on flap.
Further, a circle LED operation display lamp is equipped with each motor.
Further, the battery is removably insertable from afterbody.
Yet further, the flow measurement radar is installed horizontal by 45 degree of oblique angles.
After taking above technical scheme, the beneficial effects of the utility model are：
1. flow measurement radar and camera head are installed on unmanned plane, while flow measurement radar flow measurement, image data Jing is regarded
Frequency conveyer is back at monitoring, is easy to understand streamflow regime and regimen；
2., using the unmanned plane of the screw of four axles, eight motor eight, two motors are installed in the end of four side wings, two motors
The screw of output end is distributed in the both sides up and down of the side wing, in flight, if one of motor breaks down, does not interfere with
The flight of unmanned plane, improves stability and reliability, reduces the risk of failure；LED works are separately installed with each motor
Make status lamp, the working condition of a motor can be effectively shown when unmanned plane is powered or in work process, be easy to dimension in time
Repair, it is to avoid unnecessary loss；
3. camera head has vertical steering wheel and horizontal servos control, it is possible to achieve the action for swinging and rotating upwardly and downwardly,
Increase shooting overlay area；
4. undercarriage adopts folding mode, using connecting rod principle, when being gear down that two-stage connecting rod is stretched to machine
Tool dead-centre position, it is spacing to connecting rod by limiting section, while spring straining forms rock-steady structure；When needing to pack up, it is believed that promote
The hinged place of two-stage connecting rod so as to cross the maximum tension position of dead-centre position and spring, spring institute energy storage power drives undercarriage to receive
Rise.
Description of the drawings
Fig. 1 is front view of the present utility model；
Fig. 2 is top view of the present utility model；
Fig. 3 is the schematic enlarged-scale view of camera head；
Fig. 4 is the schematic enlarged-scale view for folding undercarriage.
Specific embodiment
Specific embodiment of the present utility model is further described below in conjunction with accompanying drawing：
As illustrated, a kind of flow measurement images unmanned aerial vehicle, including unmanned plane, unmanned plane includes being installed in fuselage 1, fuselage 1
There are battery 2, Satellite Navigation Set 3 and a control device of wireless 4, fuselage is respectively provided on two sides with horizontal wings 5, each Horizontal machine
Respectively forwardly rear direction extends flank 6 for the end of the wing 5, and the end of each flank is provided with two coaxial driving electricity of vertical direction
Machine 7, the output shaft of two motors is oppositely arranged, and the rotating shaft of each motor 7 is provided with screw；It is all provided with each motor
There is a circle LED operation display lamp 24.The head of fuselage 1 is provided with illuminating lamp 8, and the bottom of fuselage 1 is provided with radar frame 9, radar frame 9
On video transmission device 10 is installed, the bottom hung of radar frame 9 has flow measurement radar 11 and camera head 12；Flow measurement radar 11 with
Horizontal plane is installed in 45 degree of oblique angles.Each motor 7, video transmission device 10, flow measurement radar 11 and camera head 12
It is connected with battery 2 and control device of wireless 4；Being separately installed with the junction of wing 5 for fuselage 2 folds undercarriage 13.
Camera head 12 includes vertical steering wheel 13, horizontal steering wheel 14 and camera 15, and vertical steering wheel 13 is installed on radar
The bottom of frame 9, the output end of vertical steering wheel 13 is provided with fork 16, and horizontal steering wheel 14 is installed on the swinging end of fork 16, shooting
15 output ends for being installed on horizontal steering wheel 14.
Folding undercarriage includes A-frame 17 and undercarriage 18, and A-frame 17 is installed between fuselage 1 and wing 5,
Undercarriage 18 is articulated with a base angle of A-frame 17, and a flap 19, flap are hinged with another base angle of A-frame 17
19 Jing two-stages connecting rods 20 are connected with undercarriage 18, are articulated and connected between two-stage connecting rod 20, and the two ends of two-stage connecting rod 20 are hingedly connected to
Flap 19 and undercarriage 18；A-frame 17 is provided with limiting section 21, and the limiting section 21 is limited the pin joint 22 of two-stage connecting rod
Position；Stretching between the drift angle and flap 19 of A-frame 17 has spring 23.The two-stage connecting rod 20 and spring 23 are on flap 19
The equal eccentric setting of tie point.
Claims (7)
1. a kind of flow measurement images unmanned aerial vehicle, including unmanned plane, and unmanned plane includes fuselage, battery, satellite is provided with fuselage and led
Boat device and control device of wireless, fuselage is respectively provided on two sides with horizontal wings, and the end of each horizontal wings is respectively forwardly
Rear direction extends flank, and the end of each flank is provided with two coaxial motors of vertical direction, two motors it is defeated
Shaft is oppositely arranged, and the rotating shaft of each motor is provided with screw；Each motor is connected with battery and control device of wireless；
Characterized in that, fuselage bottom is provided with radar frame, video transmission device, the bottom hung of radar frame are installed on radar frame
Have flow measurement radar and a camera head, video transmission device, flow measurement radar and camera head with battery and control device of wireless
Connection；Fuselage with the junction of wing is separately installed with folding undercarriage.
2. a kind of flow measurement according to claim 1 images unmanned aerial vehicle, it is characterised in that the camera head includes vertical
Steering wheel, horizontal steering wheel and camera, vertical steering wheel is installed on the bottom of radar frame, and the output end of vertical steering wheel is provided with pendulum
Bar, horizontal steering wheel is installed on the swinging end of fork, and camera is installed on the output end of horizontal steering wheel.
3. a kind of flow measurement according to claim 1 images unmanned aerial vehicle, it is characterised in that the folding undercarriage includes three
Angle support and undercarriage, A-frame is installed between fuselage and wing, and undercarriage is articulated with a base angle of A-frame, and three
A flap is hinged with another base angle of angle support, flap Jing two-stage connecting rods are connected with undercarriage, are articulated and connected between two-stage connecting rod,
The two ends of two-stage connecting rod are hingedly connected to flap and undercarriage；A-frame is provided with limiting section, and the limiting section is to two cascades
The pin joint of bar is spacing；Stretching between the drift angle and flap of A-frame has spring.
4. a kind of flow measurement according to claim 3 images unmanned aerial vehicle, it is characterised in that the two-stage connecting rod and spring exist
The equal eccentric setting of tie point on flap.
5. a kind of flow measurement according to claim 1 images unmanned aerial vehicle, it is characterised in that be all provided with each motor
There is a circle LED operation display lamp.
6. a kind of flow measurement according to claim 1 images unmanned aerial vehicle, it is characterised in that the battery can from afterbody
Dismounting insertion.
7. a kind of flow measurement according to claim 1 images unmanned aerial vehicle, it is characterised in that the flow measurement radar and horizontal plane
Install in 45 degree of oblique angles.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621231893.1U CN206155807U (en) | 2016-11-17 | 2016-11-17 | Current surveying unmanned aerial vehicle that makes a video recording |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621231893.1U CN206155807U (en) | 2016-11-17 | 2016-11-17 | Current surveying unmanned aerial vehicle that makes a video recording |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206155807U true CN206155807U (en) | 2017-05-10 |
Family
ID=58660008
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621231893.1U Active CN206155807U (en) | 2016-11-17 | 2016-11-17 | Current surveying unmanned aerial vehicle that makes a video recording |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206155807U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741994A (en) * | 2016-11-17 | 2017-05-31 | 袁红泉 | A kind of flow measurement images unmanned aerial vehicle |
| CN108180898A (en) * | 2017-12-28 | 2018-06-19 | 佛山市仲淳伟业科技有限公司 | A kind of flow measurement unmanned plane |
| CN108698706A (en) * | 2017-08-11 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Rack components and unmanned plane |
| RU2802978C1 (en) * | 2023-02-02 | 2023-09-05 | Общество с ограниченной ответственностью "ПЛАЗ" | Unmanned aircraft video surveillance device, video camera assembly for such video surveillance device |
-
2016
- 2016-11-17 CN CN201621231893.1U patent/CN206155807U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741994A (en) * | 2016-11-17 | 2017-05-31 | 袁红泉 | A kind of flow measurement images unmanned aerial vehicle |
| CN108698706A (en) * | 2017-08-11 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Rack components and unmanned plane |
| CN108698706B (en) * | 2017-08-11 | 2021-10-22 | 深圳市大疆创新科技有限公司 | Frame subassembly and unmanned aerial vehicle |
| CN108180898A (en) * | 2017-12-28 | 2018-06-19 | 佛山市仲淳伟业科技有限公司 | A kind of flow measurement unmanned plane |
| RU2802978C1 (en) * | 2023-02-02 | 2023-09-05 | Общество с ограниченной ответственностью "ПЛАЗ" | Unmanned aircraft video surveillance device, video camera assembly for such video surveillance device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106741994A (en) | A kind of flow measurement images unmanned aerial vehicle | |
| CN206155807U (en) | Current surveying unmanned aerial vehicle that makes a video recording | |
| CN106887807B (en) | Inspection robot for overhead transmission line | |
| CN104483987B (en) | Unmanned plane is left a blank monitoring system | |
| CN206634203U (en) | A kind of police unmanned plane of investigation type | |
| CN104149971B (en) | A kind of unmanned plane | |
| CN106129890B (en) | A kind of mountain area high-voltage electric power circuit upkeep operation unmanned plane | |
| CN109696328B (en) | Mobile acquisition device for water quality monitoring | |
| CN204021041U (en) | A kind of traveling gear for overhead power transmission line crusing robot | |
| CN203612198U (en) | Front-pull rear-push type multifunctional fixed-wing unmanned aerial vehicle | |
| CN205738078U (en) | A kind of unmanned aerial vehicle flow measuring device carrying radar | |
| CN111634418A (en) | Ice and snow monitoring lifting device of remote sensing unmanned aerial vehicle | |
| CN205770205U (en) | A kind of portable general type unmanned plane automatic detection device | |
| CN107963210A (en) | A kind of fixed wing aircraft of VTOL | |
| CN207029584U (en) | The tension measuring device of the electronic unmanned plane propeller motor of fixed-wing | |
| CN205854482U (en) | The undercarriage of many rotor wing unmanned aerial vehicles and many rotor wing unmanned aerial vehicles | |
| CN106628138B (en) | Solar power supply vertical lifting unmanned aerial vehicle | |
| CN207258003U (en) | A kind of hooking device and its unmanned plane | |
| CN208102281U (en) | A kind of unmanned plane for the weighing of large bulk goods | |
| CN208602704U (en) | A kind of construction quality evidence obtaining photo taking type unmanned plane | |
| CN207120872U (en) | A kind of fixed-wing unmanned plane | |
| CN107651202A (en) | A kind of hooking device and its unmanned plane | |
| CN202961882U (en) | Aeromodelling aircraft aerial photo triaxial tripod head with photographic device | |
| CN204297083U (en) | A kind of four fins are flat claps flapping wing aircraft | |
| CN204331478U (en) | Unmanned plane is left a blank supervisory system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190425 Address after: 225400 Guanzhuang Village, Taixing Border Town, Taizhou City, Jiangsu Province, 6 Groups Patentee after: Jiangsu Yuneng Water Conservancy Engineering Co., Ltd. Address before: 225400 Jiangsu Taizhou City, Taixing City, Jiangsu Province, Boundary Town, Boundary Village 32 Group 2 Patentee before: Yuan Hongquan |