CN109927900A - A kind of space and geographical unmanned plane for shooting - Google Patents
A kind of space and geographical unmanned plane for shooting Download PDFInfo
- Publication number
- CN109927900A CN109927900A CN201711371176.8A CN201711371176A CN109927900A CN 109927900 A CN109927900 A CN 109927900A CN 201711371176 A CN201711371176 A CN 201711371176A CN 109927900 A CN109927900 A CN 109927900A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- casing body
- bottom end
- geographical
- space
- 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.)
- Pending
Links
Landscapes
- Toys (AREA)
Abstract
The invention discloses a kind of space and geographical unmanned planes for shooting, including casing body, there are four fixed connecting rods for the top installation of the casing body, and four fixed connecting rods are evenly distributed on the surrounding of casing body in a ring, the bottom end middle position of the casing body is equipped with camera, and the corner of the bottom end of casing body four is mounted on lead screw motor, one end of four fixed connecting rods passes through hood and is fixed with driving motor, the bottom end of four lead screw motors passes through screw rod and is rotatably connected to telescopic rod, and the bottom end of four telescopic rods is respectively and fixedly provided with bradyseism foot pad, the present invention is provided with sound insulation cotton layer in the inside of hood, it solves driving motor work and is easy to produce noise, the problem of noise pollution is caused to environment, provided with telescopic rod, realize that unmanned plane supporting leg is flexible, reduce the flight resistance of unmanned plane, reduce unmanned plane during flying energy Consumption, improves the flight path of unmanned plane, keeps unmanned plane more energy-efficient.
Description
Technical field
The invention belongs to space and geographical technical fields, and in particular to a kind of space and geographical unmanned plane for shooting.
Background technique
Unmanned plane is the nothing of taking photo by plane using the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation
Man-machine is to be integrated with the remotely-piloted vehicle of high definition photography and vedio recording device, and system specifically includes that carrier aircraft, flies control, gyro holder, video
Transmission, earth station and phone system etc. are suitble to video display propaganda film and the shooting of birds-eye view etc..
But there are still certain to lack during being taken photo by plane for space and geographical unmanned plane for shooting currently on the market
It falls into, for example, unmanned plane, when taking photo by plane, driving motor work is easy to produce noise, noise pollution, and unmanned plane machine is caused to environment
Enclosure interior electric component works long hours, and is easy to produce a large amount of heat, and poor radiation is easy to cause electric component to damage,
The service life of unmanned plane being influenced, while when unmanned plane during flying, supporting leg not can be carried out contraction, increase unmanned plane during flying resistance,
Cause unmanned plane power consumption to increase, influences the flight path of unmanned plane, when in addition unmanned plane rises and falls, be easy to produce shaking, surely
Qualitative difference when flight, cannot be timed intelligent return, and intelligence is poor.
Summary of the invention
The purpose of the present invention is to provide a kind of space and geographical unmanned planes for shooting, to solve to propose in above-mentioned background technique
Noise and heat, sound-proofing and poor radiation are easy to produce when unmanned plane, while unmanned plane during flying resistance is big, energy consumption is high,
Flight path is short, intelligent poor, the problem of stability difference when in addition unmanned plane rises and falls.
To achieve the above object, the invention provides the following technical scheme: a kind of space and geographical unmanned plane for shooting, including machine
Shell, there are four fixed connecting rods for the top installation of the casing body, and four fixed connecting rods are evenly distributed on casing body in a ring
Surrounding, the bottom end middle position of the casing body is equipped with camera, and the corner of the bottom end of casing body four is respectively mounted
There is a lead screw motor, one end of four fixed connecting rods passes through hood and is fixed with driving motor, four lead screw motors
Bottom end passes through screw rod and is rotatably connected to telescopic rod, and the bottom end of four telescopic rods is respectively and fixedly provided with bradyseism foot pad, four drives
The bottom end of dynamic motor passes through shaft and is rotatably connected to main shaft, and the bottom end of four main shafts is fixed with propeller by wheel hub, and four
The outside of a propeller is mounted on shield, and the bottom of four hoods is respectively mounted that there are three connecting rods, and wherein one
One end of a connecting rod is fixed with anticollision stabilizer blade, and the side of the anticollision stabilizer blade is equipped with KS-1 anti-collision sensor, the machine
The top of shell is provided with soft-touch control, and machine enclosure interior is equipped with battery at a side position of camera, described
Machine enclosure interior is equipped with timer and VC850 infrared range-measurement system at another side position of camera, and the VC850 is infrared
Rangefinder is located at the side of timer, and NUC130 master controller is equipped at the bosom position of the casing body, and
The side of NUC130 master controller is equipped with signal transceiver, and the other side is equipped with memory, the side installation of the memory
There is wireless video transmitter, the inner wall two sides of the casing body are mounted on thermally conductive sheet, and the side of two thermally conductive sheets is fixed
It is connected with radiating fin, the battery and soft-touch control are electrically connected, and the camera electrically connects with wireless video transmission device
It connects, the driving motor, signal transceiver, memory, wireless video transmission device, timer, VC850 infrared range-measurement system, screw rod
Motor, KS-1 anti-collision sensor and soft-touch control are electrically connected with NUC130 master controller.
Preferably, the shield and connecting rod are adhesively fixed by glue.
Preferably, four shields are three/second ring structure.
Preferably, the inside of four hoods is provided with sound insulation cotton layer.
Preferably, intensive mesh is offered on two radiating fins.
Compared with prior art, the beneficial effects of the present invention are:
(1) present invention is provided with sound insulation cotton layer in the inside of hood, the sound-proof material pair when driving motor works, inside sound insulation cotton layer
The noise that driving motor drives propeller rotational to generate carries out sqouynd absorption lowering noise, solves driving motor work and is easy to produce noise,
The problem of noise pollution is caused to environment.
(2) present invention is provided with thermally conductive sheet in the inside of casing body, and when unmanned plane during flying, machine enclosure interior electric component is produced
Heat amount, thermally conductive sheet shed heat derives by radiating fin, improve the thermal diffusivity of casing body, solve unmanned plane heat dissipation
Property is poor, the problem of being easy to cause electric component to damage, influence unmanned plane service life.
(3) present invention is provided with telescopic rod, after unmanned plane takes off, lead screw motor rotation, and drive screw rod to turn by shaft
Dynamic, screw rod rotation drives telescopic rod to stretch, to realize that unmanned plane supporting leg is flexible, reduces the flight resistance of unmanned plane,
Unmanned plane during flying energy consumption is reduced, the flight path of unmanned plane is improved, keeps unmanned plane more energy-efficient.
(4) present invention is provided with bradyseism foot pad, and bradyseism foot pad is fixedly connected by bradyseism spring with telescopic rod, and unmanned plane rises
When falling, under the action of bradyseism spring performance, alleviates the shaking that unmanned plane generates, increase stabilization when unmanned plane rises and falls
Property, it is poor to avoid stability when unmanned plane rises and falls, and unmanned plane is caused to jolt the problem of falling down damage.
(5) present invention is provided with timer, and when unmanned plane during flying, staff can pass through the flight of remote control setting unmanned plane
Time, when setting time reaches, timer feeds back signal to NUC130 master controller, NUC130 master controller reception signal,
And signal is analyzed, is handled, then NUC130 main controller controls driving motor works, realize that unmanned plane carries out return,
When solving unmanned plane during flying, intelligent return, the problem of intelligence difference cannot be timed.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is top view of the invention；
Fig. 3 is circuit partial block diagram of the invention；
In figure: 1- driving motor；2- fixes connecting rod；3- radiating fin；4- thermally conductive sheet；5- signal transceiver；6-NUC130 master control
Device processed；7- memory；8- wireless video transmission device；9- casing body；10- battery；11- camera；12- timer；13-
VC850 infrared range-measurement system；14- bradyseism foot pad；15- telescopic rod；16- lead screw motor；17- wheel hub；18- shield；19- anticollision branch
Foot；20- connecting rod；21- main shaft；22- hood；23-KS-1 anti-collision sensor；24- propeller；25- soft-touch control.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-3 is please referred to, the present invention provides a kind of technical solution: a kind of space and geographical unmanned plane for shooting, including casing
Body 9, there are four fixed connecting rods 2 for the top installation of casing body 9, and four fixed connecting rods 2 are evenly distributed on casing body 9 in a ring
Surrounding, the bottom end middle position of casing body 9 is equipped with camera 11, and the corner of the bottom end of casing body 9 four is mounted on
Lead screw motor 16 in order to rotate using lead screw motor 16, and drives screw rod rotation by shaft, and screw rod rotation drives flexible
Bar 15 stretches, and realizes that unmanned plane supporting leg is flexible, reduces the flight resistance of unmanned plane, reduces unmanned plane during flying energy consumption, and four
One end of a fixed connecting rod 2 passes through hood 22 and is fixed with driving motor 1, and the bottom end of four lead screw motors 16 is turned by screw rod
It is dynamic to be connected with telescopic rod 15, and the bottom end of four telescopic rods 15 is respectively and fixedly provided with bradyseism foot pad 14, bradyseism foot pad 14 passes through bradyseism bullet
Spring is fixedly connected with telescopic rod 15, when unmanned plane rises and falls, under the action of bradyseism spring performance, alleviates what unmanned plane generated
It shakes, increases stability when unmanned plane rises and falls, the bottom end of four driving motors 1 passes through shaft and is rotatably connected to main shaft
21, and the bottom end of four main shafts 21 is fixed with propeller 24 by wheel hub 17, the outside of four propellers 24 is mounted on shield
18, the bottom of four hoods 22 is respectively mounted there are three connecting rod 20, and one end of one of connecting rod 20 is fixed with anticollision branch
Foot 19, the side of anticollision stabilizer blade 19 are equipped with KS-1 anti-collision sensor 23, and the top of casing body 9 is provided with soft-touch control 25,
And 9 inside of casing body is equipped with battery 10 at a side position of camera 11,9 inside of casing body is close to camera 11
Timer 12 and VC850 infrared range-measurement system 13 are installed, VC850 infrared range-measurement system 13 is located at timer 12 at another side position
Side is equipped with NUC130 master controller 6, and the side installation of NUC130 master controller 6 at the bosom position of casing body 9
There is signal transceiver 5, the other side is equipped with memory 7, and the side of memory 7 is equipped with wireless video transmission device 8, casing body 9
Inner wall two sides be mounted on thermally conductive sheet 4, and the side of two thermally conductive sheets 4 is fixedly connected to radiating fin 3, can lead in this way
Thermally conductive sheet 4 is crossed by heat derives, is shed by radiating fin 3, the thermal diffusivity of casing body, battery 10 and soft-touch control 25 are improved
It is electrically connected, camera 11 and wireless video transmission device 8 are electrically connected, driving motor 1, signal transceiver 5, memory 7, wireless
Video transmitter 8, timer 12, VC850 infrared range-measurement system 13, lead screw motor 16, KS-1 anti-collision sensor 23 and touch are opened
25 are closed to be electrically connected with NUC130 master controller 6.
For the ease of the fixation of shield 18 and connecting rod 20, in the present embodiment, it is preferred that shield 18 passes through with connecting rod 20
Glue is adhesively fixed.
Propeller 24 is protected for the ease of shield 18, in the present embodiment, it is preferred that four shields 18 are 2/3rds rings
Shape structure.
The noise that generates carries out sqouynd absorption lowering noise when in order to realize that hood 22 works to driving motor, in the present embodiment, preferably
, the inside of four hoods 22 is provided with sound insulation cotton layer.
Heat dissipation is aerated for the ease of radiating fin 3, in the present embodiment, it is preferred that open up on two radiating fins 3
There is intensive mesh.
Working principle: when in use, staff first passes through external power supply and is full of 10 electricity of battery, then leads to for the invention
It crosses finger touching soft-touch control 25 and opens unmanned plane power switch, signal transceiver 5 is connect with external remote control terminal by signal,
Realize staff can remote control, instructed by remote terminal, the reception command signal of NUC130 master controller 6 and is controlled
Driving motor 1 processed works, the work rotation of driving motor 1, and drives propeller 24 to rotate by main shaft 21, and unmanned plane is made to exist
It flies under the rotation of propeller 24, during unmanned plane during flying, NUC130 master controller 6 controls camera 11 and clapped
Work is taken the photograph, the video of shooting, picture are fed back to NUC130 master controller 6 by camera 11, and NUC130 master controller 6 receives view
Frequently, image data, and store data into memory 7, while data are passed through wireless video transmission by NUC130 master controller 6
Device 8 is transmitted to ground monitoring terminal, to realize that unmanned plane is taken photo by plane, in addition, staff can be by remotely setting nobody
The flight time of machine, when setting time reaches, timer 12 feeds back signal to NUC130 master controller 6, NUC130 main control
Device 6 receives signal, and is analyzed signal, handled, and then NUC130 master controller 6 controls driving motor 1 and works, and realizes nothing
Man-machine carry out return, improves the intelligence of unmanned plane, and when taking off, bradyseism foot pad 14 utilizes bradyseism spring performance, alleviates nothing
The shaking of man-machine generation, increases stability of unmanned plane when rising and falling, VC850 infrared range-measurement system 13 measure unmanned plane and ground away from
From when distance reaches setting value, signal is fed back the NUC130 master into NUC130 master controller 6 by VC850 infrared range-measurement system 13
Controller 6 receives signal, and to signal analysis, processing, i.e. control lead screw motor 16 works, and lead screw motor 16 rotates, and
Screw rod rotation is driven by shaft, screw rod rotation drives telescopic rod 15 to stretch, to realize that unmanned plane supporting leg is flexible, subtracts
The flight resistance of small unmanned plane reduces unmanned plane during flying energy consumption, the flight path of unmanned plane is improved, in unmanned plane process
In, whether there are obstacles for 23 real-time detection shield of KS-1 anti-collision sensor, 18 surrounding installed on anticollision stabilizer blade 19, effectively
Prevent the thermally conductive sheet 4 for colliding, while installing inside casing body 9 during unmanned plane during flying to 9 inside electric appliance of casing body
The heat that component work generates is exported, and is shed by radiating fin 3, to realize the heat dissipation inside casing body 9.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (5)
1. a kind of space and geographical unmanned plane for shooting, including casing body (9), it is characterised in that: pacify on the top of the casing body (9)
There are four fixed connecting rod (2) for dress, and four fixed connecting rods (2) are evenly distributed on the surrounding of casing body (9), the casing in a ring
The bottom end middle position of body (9) is equipped with camera (11), and the corner of the bottom end of casing body (9) four is mounted on screw rod
Motor (16), one end of four fixed connecting rods (2) pass through hood (22) and are fixed with driving motor (1), four silks
The bottom end of bar motor (16) passes through screw rod and is rotatably connected to telescopic rod (15), and the bottom end of four telescopic rods (15) is respectively and fixedly provided with
Bradyseism foot pad (14), the bottom end of four driving motors (1) passes through shaft and is rotatably connected to main shaft (21), and four main shafts
(21) bottom end is fixed with propeller (24) by wheel hub (17), and the outside of four propellers (24) is mounted on shield
(18), the bottom of four hoods (22) is respectively mounted there are three connecting rod (20), and one end of one of connecting rod (20)
It is fixed with anticollision stabilizer blade (19), the side of the anticollision stabilizer blade (19) is equipped with KS-1 anti-collision sensor (23), the casing
The top of body (9) is provided with soft-touch control (25), and is equipped at a side position of casing body (9) internal close camera (11)
Battery (10), the casing body (9) is internal be equipped at another side position of camera (11) timer (12) and
VC850 infrared range-measurement system (13), the VC850 infrared range-measurement system (13) are located at the side of timer (12), the casing body (9)
Bosom position at be equipped with NUC130 master controller (6), and the side of NUC130 master controller (6) be equipped with signal receipts
It sends out device (5), the other side is equipped with memory (7), and the side of the memory (7) is equipped with wireless video transmission device (8), described
The inner wall two sides of casing body (9) are mounted on thermally conductive sheet (4), and the side of two thermally conductive sheets (4) is fixedly connected to heat radiating fin
Piece (3), the battery (10) and soft-touch control (25) are electrically connected, the camera (11) and wireless video transmission device (8)
It is electrically connected, the driving motor (1), signal transceiver (5), memory (7), wireless video transmission device (8), timer
(12), VC850 infrared range-measurement system (13), lead screw motor (16), KS-1 anti-collision sensor (23) and soft-touch control (25) with
NUC130 master controller (6) is electrically connected.
2. a kind of space and geographical unmanned plane for shooting according to claim 1, it is characterised in that: the shield (18) and company
Extension bar (20) is adhesively fixed by glue.
3. a kind of space and geographical unmanned plane for shooting according to claim 1, it is characterised in that: four shields (18)
It is three/second ring structure.
4. a kind of space and geographical unmanned plane for shooting according to claim 1, it is characterised in that: four hoods (22)
Inside be provided with sound insulation cotton layer.
5. a kind of space and geographical unmanned plane for shooting according to claim 1, it is characterised in that: two radiating fins
(3) intensive mesh is offered on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711371176.8A CN109927900A (en) | 2017-12-19 | 2017-12-19 | A kind of space and geographical unmanned plane for shooting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711371176.8A CN109927900A (en) | 2017-12-19 | 2017-12-19 | A kind of space and geographical unmanned plane for shooting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109927900A true CN109927900A (en) | 2019-06-25 |
Family
ID=66983267
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711371176.8A Pending CN109927900A (en) | 2017-12-19 | 2017-12-19 | A kind of space and geographical unmanned plane for shooting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109927900A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111137466A (en) * | 2020-01-13 | 2020-05-12 | 深圳市星图智控科技有限公司 | Unmanned aerial vehicle capable of being monitored and monitoring shooting method of unmanned aerial vehicle |
-
2017
- 2017-12-19 CN CN201711371176.8A patent/CN109927900A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111137466A (en) * | 2020-01-13 | 2020-05-12 | 深圳市星图智控科技有限公司 | Unmanned aerial vehicle capable of being monitored and monitoring shooting method of unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204096095U (en) | A kind of unmanned plane full angle image aerial device | |
| CN106043676A (en) | Aircraft capable of automatically blocking light | |
| CN206954524U (en) | A kind of SUAV photoelectric nacelle | |
| CN206100216U (en) | Multi -functional many rotor unmanned aerial vehicle | |
| CN109927900A (en) | A kind of space and geographical unmanned plane for shooting | |
| CN206639928U (en) | A kind of Mobile portable formula flat-plate satellite communication antenna device | |
| CN206552283U (en) | A kind of equipment of taking photo by plane applied to unmanned plane | |
| CN207943170U (en) | A kind of space and geographical unmanned plane for shooting | |
| CN108910040A (en) | Mobile device aircraft | |
| CN206750169U (en) | A kind of governor motion of unmanned plane shooting angle | |
| CN207670659U (en) | A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation | |
| CN207242027U (en) | Detecting aerial survey unmanned plane | |
| CN211167458U (en) | Remote control unmanned aerial vehicle high altitude anti-wind anti-shake device | |
| CN206520749U (en) | One kind is taken photo by plane unmanned plane | |
| CN208165258U (en) | A kind of AGV unmanned plane of laser radar positioning function | |
| CN109204802A (en) | A kind of unmanned plane that landing stability is good | |
| CN207106868U (en) | Aerial image collection unmanned plane provided with rotary camera device | |
| CN206914660U (en) | A kind of unmanned plane camera bracket for being easy to regulation | |
| CN108762166A (en) | A kind of the environmental information collection device and its application method of intelligent robot | |
| CN207106869U (en) | 360 ° of monitor-type rotor wing unmanned aerial vehicles | |
| CN108275265A (en) | A kind of unmanned plane | |
| CN209479965U (en) | A kind of solar power flight parasols | |
| CN203612208U (en) | Spherical aircraft | |
| CN211107998U (en) | Unmanned aerial vehicle with anticollision institution | |
| CN207725615U (en) | The self-balancing wing of unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190625 |