CN207943170U - 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
- CN207943170U CN207943170U CN201721776239.3U CN201721776239U CN207943170U CN 207943170 U CN207943170 U CN 207943170U CN 201721776239 U CN201721776239 U CN 201721776239U CN 207943170 U CN207943170 U CN 207943170U
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- China
- Prior art keywords
- unmanned plane
- casing body
- bottom end
- lead screw
- geographical
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Abstract
The utility model 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 is fixed with driving motor by hood,The bottom end of four lead screw motors is rotatably connected to telescopic rod by lead screw,And the bottom end of four telescopic rods is respectively and fixedly provided with bradyseism foot pad,The utility model is provided with sound insulation cotton layer in the inside of hood,It solves driving motor work and easy tos produce noise,The problem of noise pollution is caused to environment,Provided with telescopic rod,Realize that unmanned plane support leg is flexible,Reduce the flight resistance of unmanned plane,Reduce unmanned plane during flying energy consumption,Improve the flight path of unmanned plane,Keep unmanned plane more energy-efficient.
Description
Technical field
The utility model belongs to space and geographical technical field, and in particular to a kind of space and geographical unmanned plane for shooting.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, nothing of taking photo by plane
Man-machine is the remotely-piloted vehicle for being integrated with high definition photography and vedio recording device, and system includes mainly：Carrier aircraft flies control, gyro holder, video
Transmission, earth station and phone system etc. are suitble to the shooting etc. of video display propaganda film and birds-eye view.
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 easy tos produce noise, and noise pollution, and unmanned plane machine are caused to environment
Enclosure interior electric component works long hours, and easy tos produce a large amount of heat, and poor radiation is easy to cause electric component damage,
The service life of unmanned plane is influenced, while when unmanned plane during flying, support leg cannot be shunk, increases 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, easy to produce shaking, surely
Qualitative difference when flight, cannot be timed intelligent return, intelligent difference.
Utility model content
The purpose of this utility model is to provide a kind of space and geographical unmanned planes for shooting, to solve in above-mentioned background technology
It proposes to easy to produce noise and heat, sound-proofing and poor radiation when unmanned plane, while unmanned plane during flying resistance is big, energy consumption
Greatly, flight path is short, intelligent difference, the problem of stability difference when in addition unmanned plane rises and falls.
To achieve the above object, the utility model provides the following technical solutions：A kind of space and geographical unmanned plane for shooting, packet
Casing body is included, there are four fixed connecting rods for the top installation of the casing body, and four fixed connecting rods are evenly distributed on machine in a ring
The bottom end middle position of the surrounding of shell, the casing body is equipped with camera, and the corner of the bottom end of casing body four is equal
Lead screw motor is installed, one end of four fixed connecting rods is fixed with driving motor, four lead screw electricity by hood
The bottom end of machine is rotatably connected to telescopic rod by lead screw, and the bottom end of four telescopic rods is respectively and fixedly provided with bradyseism foot pad, four institutes
The bottom end for stating driving motor is rotatably connected to main shaft by shaft, and the bottom end of four main shafts is fixed with spiral by wheel hub
Paddle, the outsides of four propellers are mounted on shield, and the bottoms of four hoods is respectively mounted that there are three connecting rods, and its
In one end of a connecting rod be fixed with anticollision stabilizer blade, the side of the anticollision stabilizer blade is equipped with KS-1 anti-collision sensors, institute
The top for stating casing body is provided with soft-touch control, and machine enclosure interior is equipped with accumulator at a side position of camera,
The machine enclosure interior is equipped with timer and VC850 infrared range-measurement systems, the VC850 at another side position of camera
Infrared range-measurement system is located at the side of timer, and NUC130 master controllers are equipped at the bosom position of the casing body, and
The side of NUC130 master controllers 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 both 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 accumulator is electrically connected with soft-touch control, 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 systems, lead screw
Motor, KS-1 anti-collision sensors and soft-touch control are electrically connected with NUC130 master controllers.
Preferably, the shield is adhesively fixed with connecting rod by glue.
Preferably, four shields are three/second ring structure.
Preferably, the inside of four hoods is both provided with sound insulation cotton layer.
Preferably, intensive mesh is offered on two radiating fins.
Compared with prior art, the utility model has the beneficial effects that：
（1）The utility model is provided with sound insulation cotton layer in the inside of hood, when driving motor works, inside sound insulation cotton layer
The noise that sound-proof material generates driving motor driving propeller rotational carries out sqouynd absorption lowering noise, solves driving motor work and is easy production
The problem of giving birth to noise, noise pollution caused to environment.
（2）The utility model is provided with thermally conductive sheet, when unmanned plane during flying, machine enclosure interior electric appliance portion in the inside of casing body
Part generates heat, and thermally conductive sheet sheds heat derives by radiating fin, improves the thermal diffusivity of casing body, solves unmanned plane
The problem of poor radiation is easy to cause electric component damage, influences unmanned plane service life.
（3）The utility model is provided with telescopic rod, after unmanned plane takes off, lead screw motor rotation, and silk is driven by shaft
Bar rotates, and lead screw rotation drives telescopic rod to stretch, and to realize that unmanned plane support leg is flexible, reduces the flight resistance of unmanned plane
Power reduces unmanned plane during flying energy consumption, improves the flight path of unmanned plane, keep unmanned plane more energy-efficient.
（4）The utility model is provided with bradyseism foot pad, and bradyseism foot pad is fixedly connected by bradyseism spring with telescopic rod, nobody
When machine rises and falls, under the action of bradyseism spring performance, alleviates the shaking that unmanned plane generates, increase when unmanned plane rises and falls
Stability, avoids when unmanned plane rises and falls that stability is poor, and unmanned plane is caused to jolt the problem of falling down damage.
（5）The utility model is provided with timer, and when unmanned plane during flying, staff can pass through remote control setting unmanned plane
Flight time, when setting time reaches, signal is fed back to NUC130 master controllers by timer, and NUC130 master controllers receive letter
Number, and signal is analyzed, is handled, then NUC130 main controller controls driving motor works, and realizes that unmanned plane is returned
Journey when solving unmanned plane during flying, cannot be timed intelligent return, the problem of intelligent difference.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the vertical view of the utility model；
Fig. 3 is the circuit partial block diagram of the utility model；
In figure：1- driving motors；2- fixes connecting rod；3- radiating fins；4- thermally conductive sheets；5- signal transceivers；6-NUC130
Master controller；7- memories；8- wireless video transmission devices；9- casing bodies；10- accumulators；11- cameras；12- timers；13-
VC850 infrared range-measurement systems；14- bradyseism foots pad；15- telescopic rods；16- lead screw motors；17- wheel hubs；18- shields；19- anticollision branch
Foot；20- connecting rods；21- main shafts；22- hoods；23-KS-1 anti-collision sensors；24- propellers；25- soft-touch controls.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the utility model 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 in a ring
The bottom end middle position of the surrounding of body 9, casing body 9 is equipped with camera 11, and the corner of the bottom end of casing body 9 four is pacified
Equipped with lead screw motor 16, in order to be rotated using lead screw motor 16, and lead screw rotation, lead screw rotation is driven to drive by shaft
Telescopic rod 15 stretches, and realizes that unmanned plane support leg is flexible, reduces the flight resistance of unmanned plane, reduces unmanned plane during flying energy
Consumption, one end of four fixed connecting rods 2 are fixed with driving motor 1 by hood 22, and the bottom end of four lead screw motors 16 passes through
Lead screw 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, and bradyseism foot pad 14 passes through
Bradyseism spring is fixedly connected with telescopic rod 15, when unmanned plane rises and falls, under the action of bradyseism spring performance, alleviates unmanned plane
The shaking of generation, increases stability when unmanned plane rises and falls, and the bottom end of four driving motors 1 is rotatably connected to by shaft
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 bottoms of four hoods 22 are respectively mounted there are three connecting rod 20, and one end of one of connecting rod 20 be fixed with it is anti-
Stabilizer blade 19 is hit, the side of anticollision stabilizer blade 19 is equipped with KS-1 anti-collision sensors 23, and the top of casing body 9 is provided with soft-touch control
25, and 9 inside of casing body is equipped with accumulator 10 at a side position of camera 11,9 inside of casing body is close to camera
Timer 12 and VC850 infrared range-measurement systems 13 are installed, VC850 infrared range-measurement systems 13 are located at timer at 11 another side position
12 side is equipped with NUC130 master controllers 6, and the side of NUC130 master controllers 6 at the bosom position of casing body 9
Signal transceiver 5 is installed, the other side is equipped with memory 7, and the side of memory 7 is equipped with wireless video transmission device 8, casing
The inner wall both sides of body 9 are mounted on thermally conductive sheet 4, and the side of two thermally conductive sheets 4 has been fixedly connected with radiating fin 3, such energy
Heat derives are shed by thermally conductive sheet 4 by radiating fin 3 enough, improve the thermal diffusivity of casing body, accumulator 10 is opened with touch
25 are closed to be electrically connected, camera 11 and wireless video transmission device 8 are electrically connected, driving motor 1, signal transceiver 5, memory 7,
Wireless video transmission device 8, timer 12, VC850 infrared range-measurement systems 13, lead screw motor 16, KS-1 anti-collision sensors 23 and touch
Switch 25 is touched to be electrically connected with NUC130 master controllers 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.
In order to which the noise that is generated when realizing that hood 22 works to driving motor carries out sqouynd absorption lowering noise, in the present embodiment, preferably
, the inside of four hoods 22 is both provided with sound insulation cotton layer.
It is aerated heat dissipation for the ease of radiating fin 3, in the present embodiment, it is preferred that opened up on two radiating fins 3
There is intensive mesh.
Operation principle：When in use, staff first passes through external power supply and is full of 10 electricity of accumulator the utility model,
Soft-touch control 25 is touched by finger again and opens unmanned plane power switch, signal transceiver 5 passes through signal with external remote control terminal
Connection, realize staff can remote control, instructed by remote terminal, NUC130 master controllers 6 reception command signal,
And control driving motor 1 and work, the work rotation of driving motor 1, and drive propeller 24 to rotate by main shaft 21, make nobody
Machine flies under the rotation of propeller 24, during unmanned plane during flying, NUC130 master controllers 6 control camera 11 into
The video of shooting, picture are fed back to NUC130 master controllers 6 by row shooting work, camera 11, and NUC130 master controllers 6 receive
Video, image data, and store data into memory 7, while NUC130 master controllers 6 pass data by wireless video
Defeated device 8 is transmitted to ground monitoring terminal, to realize that unmanned plane is taken photo by plane, in addition, staff can by remote control setting without
The man-machine flight time, when setting time reaches, signal is fed back to NUC130 master controllers 6, NUC130 master controls by timer 12
Device 6 processed receives signal, and is analyzed signal, handled, and then NUC130 master controllers 6 control driving motor 1 and work, and realizes
Unmanned plane carries out return, improves the intelligent of unmanned plane, and when taking off, bradyseism foot pad 14 utilizes bradyseism spring performance, alleviates
The shaking that unmanned plane generates, stability when increase unmanned plane rises and falls, the measurement unmanned plane of VC850 infrared range-measurement systems 13 and ground
Distance, when distance reaches setting value, VC850 infrared range-measurement systems 13 feed back to signal in NUC130 master controllers 6, NUC130
Master controller 6 receives signal, and to signal analysis, processing, that is, controls lead screw motor 16 and work, and lead screw motor 16 rotates,
And drive lead screw rotation, lead screw rotation that telescopic rod 15 is driven to stretch by shaft, to realize that unmanned plane support leg is flexible,
Reduce the flight resistance of unmanned plane, reduces unmanned plane during flying energy consumption, the flight path of unmanned plane is improved, in unmanned plane mistake
Cheng Zhong, the KS-1 anti-collision sensors 23 installed on anticollision stabilizer blade 19 detection 18 surrounding whether there are obstacles of shield in real time, has
Effect prevents from colliding during unmanned plane during flying, while the thermally conductive sheet 4 that 9 inside of casing body is installed is to 9 inside electricity of casing body
The heat that device component working generates is exported, and is shed by radiating fin 3, to realize the heat dissipation inside casing body 9.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of space and geographical unmanned plane for shooting, including casing body（9）, it is characterised in that：The casing body（9）Top peace
There are four fixed connecting rods for dress（2）, and four fixed connecting rods（2）It is evenly distributed on casing body in a ring（9）Surrounding, the casing
Body（9）Bottom end middle position camera is installed（11）, and casing body（9）The corner of bottom end four be mounted on lead screw
Motor（16）, four fixed connecting rods（2）One end pass through hood（22）It is fixed with driving motor（1）, four silks
Bar motor（16）Bottom end telescopic rod is rotatably connected to by lead screw（15）, and four telescopic rods（15）Bottom end be respectively and fixedly provided with
Bradyseism foot pad（14）, four driving motors（1）Bottom end main shaft is rotatably connected to by shaft（21）, and four main shafts
（21）Bottom end pass through wheel hub（17）It is fixed with propeller（24）, four propellers（24）Outside be mounted on shield
（18）, four hoods（22）Bottom be respectively mounted there are three connecting rod（20）, and one of connecting rod（20）One end
It is fixed with anticollision stabilizer blade（19）, the anticollision stabilizer blade（19）Side KS-1 anti-collision sensors are installed（23）, the casing
Body（9）Top be provided with soft-touch control（25）, and casing body（9）Internal close camera（11）A side position at be equipped with
Accumulator（10）, the casing body（9）Internal close camera（11）Another side position at timer is installed（12）With
VC850 infrared range-measurement systems（13）, the VC850 infrared range-measurement systems（13）Positioned at timer（12）Side, the casing body（9）
Bosom position at NUC130 master controllers are installed（6）, and NUC130 master controllers（6）Side be equipped with signal receipts
Send out device（5）, the other side is equipped with memory（7）, the memory（7）Side wireless video transmission device is installed（8）, described
Casing body（9）Inner wall both sides be mounted on thermally conductive sheet（4）, and two thermally conductive sheets（4）Side be fixedly connected with heat radiating fin
Piece（3）, the accumulator（10）With soft-touch control（25）It is electrically connected, the camera（11）With 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 systems（13）, lead screw motor（16）, KS-1 anti-collision sensors（23）And soft-touch control（25）With
NUC130 master controllers（6）It 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）With company
Extension bar（20）It 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 both 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）On offer intensive mesh.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721776239.3U CN207943170U (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 |
|---|---|---|---|
| CN201721776239.3U CN207943170U (en) | 2017-12-19 | 2017-12-19 | A kind of space and geographical unmanned plane for shooting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207943170U true CN207943170U (en) | 2018-10-09 |
Family
ID=63704388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721776239.3U Expired - Fee Related CN207943170U (en) | 2017-12-19 | 2017-12-19 | A kind of space and geographical unmanned plane for shooting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207943170U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112912312A (en) * | 2018-10-19 | 2021-06-04 | 安炳烈 | Unmanned aerial vehicle who possesses conflict prevention and retrieve function |
-
2017
- 2017-12-19 CN CN201721776239.3U patent/CN207943170U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112912312A (en) * | 2018-10-19 | 2021-06-04 | 安炳烈 | Unmanned aerial vehicle who possesses conflict prevention and retrieve function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181009 Termination date: 20201219 |