CN205872498U - A unmanned vehicles for take photo by plane - Google Patents
A unmanned vehicles for take photo by plane Download PDFInfo
- Publication number
- CN205872498U CN205872498U CN201620725584.3U CN201620725584U CN205872498U CN 205872498 U CN205872498 U CN 205872498U CN 201620725584 U CN201620725584 U CN 201620725584U CN 205872498 U CN205872498 U CN 205872498U
- Authority
- CN
- China
- Prior art keywords
- control
- support
- flying
- motor
- case
- 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
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model discloses an unmanned vehicles for take photo by plane, including flying to control case, blade, motor, support, bumper shock absorber and workstation, fly to control the right side that the mainboard is located the video signal transmitter, the remote control receiving ware is received through the antenna and is come from the control signal that ground personnel sent, solar cell panel installs at the upside that flies to control the case, motor support is installed to the right -hand member that flies to control the case, the right -hand member at motor support is installed to the motor, the support is installed to the lower extreme right side position that flies to control the case, the bumper shock absorber is installed to the bottom of support, the bottom plate is installed to the bottom of bumper shock absorber, the upper portion position welding of support has the horizontal pole, three -axis gyroscope is installed to the intermediate position of horizontal pole, the workstation is installed to three -axis gyroscope's lower extreme, the utility model discloses the range of application extensively, convenient to use, the operation of being convenient for, can cooperate multiple shooting disposition of equipment.
Description
Technical field
This utility model relates to a kind of aircraft, a kind of unmanned vehicle for taking photo by plane.
Background technology
The shooting means as a kind of fashion and advanced person of taking photo by plane are very popular, take photo by plane and can photograph a lot of shake
The scene shaken, allows people look down the earth from the air, experiences different visual experience；Aerial photography unmanned aerial vehicle is as boat in recent years
The necessary equipment clapped the most develops rapidly, the takeoff and landing of aerial photography aircraft be aircraft be easiest to break down time
Between, so needing the takeoff and landing of aerial photography aircraft is designed some safety devices, such as amortisseur.
Utility model content
The purpose of this utility model is to provide a kind of unmanned vehicle for taking photo by plane, to solve in above-mentioned background technology
The problem proposed.
For achieving the above object, the following technical scheme of this utility model offer:
A kind of unmanned vehicle for taking photo by plane, including flying to control case, blade, motor, support, amortisseur and workbench；
Accumulator is arranged on the inner chamber leftward position flying to control case；Video signal transmission device is arranged on the right side of accumulator；Fly to control mainboard position
Right side in video signal transmission device；Receiver of remote-control sytem receives the control signal sent from ground staff by antenna；The sun
The upside flying to control case can be arranged on by cell panel；Hold-down support is flying between control case and solar panel；Described antenna is installed
Flying to control the upside of case；The described right-hand member flying to control case is provided with support of motor；Described motor is arranged on support of motor
Right-hand member；The described lower end right positions flying to control case is provided with support；The bottom of described support is provided with amortisseur；Described amortisseur
Inside include spring pedestal, spring, expansion link and limited block；The upper end of described spring connects expansion link, and lower end connects
There is spring pedestal；The bottom of described amortisseur is provided with base plate；The upper position of described support is welded with cross bar；Described cross bar
Centre position is provided with three-axis gyroscope；The lower end of described three-axis gyroscope is provided with workbench；Lower warning lamp is arranged on three axles
The left side of gyroscope.
As further program of the utility model: described in fly control case material be rustless steel, disc cavity structure, interior
Portion's cavity is provided with accumulator, video signal transmission device, flies to control mainboard, receiver of remote-control sytem and GPS navigator.
As further program of the utility model: upper warning lamp is positioned at the right side of antenna.
Compared with prior art, the beneficial effects of the utility model are:
This utility model has wide range of applications, easy to use, convenient to operate, multiple capture apparatus can be coordinated to use；Subtract
Shake device design can well absorb aircraft land in a flash due to the gravitational thrusts caused that runs out of steam suddenly, can
Well to protect aircraft, can also well protect capture apparatus simultaneously；Video signal transmission device can be by capture apparatus
The video of shooting is transferred to ground constantly.
Accompanying drawing explanation
Fig. 1 is the structural representation for the unmanned vehicle taken photo by plane.
Fig. 2 is the structural representation of amortisseur in the unmanned vehicle for taking photo by plane.
Fig. 3 is the control block diagram in the unmanned vehicle for taking photo by plane.
In figure: 1-solar panel；2-hold-down support；3-flies to control case；4-flies to control mainboard；5-receiver of remote-control sytem；6-days
Line；The upper warning lamp of 7-；8-blade；9-motor；10-support of motor；11-GPS navigator；12-base plate；13-amortisseur；
14-support；15-cross bar；16-workbench；17-three-axis gyroscope；Warning lamp under 18-；19-video signal transmission device；20-electric power storage
Pond；21-spring pedestal；22-spring；23-expansion link；24-limited block.
Detailed description of the invention
Below in conjunction with detailed description of the invention, the technical scheme of this patent is described in more detail.
Referring to Fig. 1-3, a kind of unmanned vehicle for taking photo by plane, including flying to control case 3, blade 8, motor 9, support
14, amortisseur 13 and workbench 16；The described material flying to control case 3 is rustless steel, and disc cavity structure is installed in internal cavities
There are accumulator 20, video signal transmission device 19, fly to control mainboard 4, receiver of remote-control sytem 5 and GPS navigator 11；Described accumulator 20 is pacified
It is contained in the inner chamber leftward position flying to control case 3, for storing the electric energy that solar panel 1 sends, also provides for motor 9 simultaneously
Electric energy；Described video signal transmission device 19 is arranged on the right side of accumulator 20, for aerial camera constantly by the video of shooting
It is transferred to the accepter on ground, it is simple to ground staff watches constantly；The described control mainboard 4 that flies is positioned at video signal transmission device 19
Right side, for controlling and adjusting the letter that flight attitude is simultaneously used for processing the signal of GPS navigator and receiver of remote-control sytem 5 receives
Number；Described GPS navigator 11, for navigating for flight path, facilitates ground controller to control flight path；Described distant
Control receptor 5 receives, by antenna 6, the control signal sent from ground staff, it is simple to ground staff's flight appearance to aircraft
State is adjusted；Described solar panel 1 is arranged on the upside flying to control case 3, for providing electric energy for motor, improves flight
The flying power of device；Described hold-down support 2 is flying between control case 3 and solar panel 1, is used for supporting and fixing solar energy
Cell panel 1；Described antenna 6 is arranged on the upside flying to control case 3, is positioned at the right side of solar panel 1, by electric wire 6 and remote control
Receptor 5 connects；Upper warning lamp 7 is positioned at the right side of antenna 6, plays warning function when flight at night；The described right side flying to control case 3
End is provided with support of motor 10, for supporting and fixed motor 9；Described motor 9 is arranged on the right side of support of motor 10
End, rotates for band moving vane 8, provides lift for aircraft；The described lower end right positions flying to control case 3 is provided with support 14；
The bottom of described support 14 is provided with amortisseur 13；The inside of described amortisseur 13 includes spring pedestal 21, spring 22, stretches
Bar 23 and limited block 24；The upper end of described spring 22 connects expansion link 23, and lower end connects has spring pedestal 21, by spring 22
Elastic deformation can reach the purpose of damping, reduce impulsive force during aircraft landing；The bottom of described amortisseur 13 is installed
There is base plate 12；The upper position of described support 14 is welded with cross bar 15；The centre position of described cross bar 15 is provided with three axle gyros
Instrument 17；The lower end of described three-axis gyroscope 17 is provided with workbench 16, is used for installing the capture apparatus such as video camera；Lower warning lamp 18
It is arranged on the left side of three-axis gyroscope 17.
Above the better embodiment of this patent is explained in detail, but this patent is not limited to above-mentioned embodiment party
Formula, in the ken that one skilled in the relevant art is possessed, it is also possible on the premise of without departing from this patent objective
Make a variety of changes.
Claims (3)
1. for the unmanned vehicle taken photo by plane, including flying to control case, blade, motor, support, amortisseur and workbench；Its
Being characterised by, accumulator is arranged on the inner chamber leftward position flying to control case；Video signal transmission device is arranged on the right side of accumulator；Fly
Control mainboard is positioned at the right side of video signal transmission device；Receiver of remote-control sytem receives, by antenna, the control sent from ground staff to be believed
Number；Solar panel is arranged on the upside flying to control case；Hold-down support is flying between control case and solar panel；Described sky
Line is arranged on the upside flying to control case；The described right-hand member flying to control case is provided with support of motor；Described motor is arranged on motor
The right-hand member of support；The described lower end right positions flying to control case is provided with support；The bottom of described support is provided with amortisseur；Described
The inside of amortisseur includes spring pedestal, spring, expansion link and limited block；The upper end of described spring connects expansion link, under
End connection has spring pedestal；The bottom of described amortisseur is provided with base plate；The upper position of described support is welded with cross bar；Described
The centre position of cross bar is provided with three-axis gyroscope；The lower end of described three-axis gyroscope is provided with workbench；Lower warning lamp is installed
Left side at three-axis gyroscope.
Unmanned vehicle for taking photo by plane the most according to claim 1, it is characterised in that described in fly to control the material of case for not
Rust steel, disc cavity structure, internal cavities is provided with accumulator, video signal transmission device, flies to control mainboard, receiver of remote-control sytem
And GPS navigator.
Unmanned vehicle for taking photo by plane the most according to claim 1, it is characterised in that upper warning lamp is positioned at the right side of antenna
Side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725584.3U CN205872498U (en) | 2016-07-11 | 2016-07-11 | A unmanned vehicles for take photo by plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725584.3U CN205872498U (en) | 2016-07-11 | 2016-07-11 | A unmanned vehicles for take photo by plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205872498U true CN205872498U (en) | 2017-01-11 |
Family
ID=57695521
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620725584.3U Expired - Fee Related CN205872498U (en) | 2016-07-11 | 2016-07-11 | A unmanned vehicles for take photo by plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205872498U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911191A (en) * | 2019-04-16 | 2019-06-21 | 无锡森孚软件有限公司 | A kind of telemetry station with fixed point flight function |
| CN109969380A (en) * | 2018-11-28 | 2019-07-05 | 北京汉能光伏投资有限公司 | A kind of solar energy unmanned plane and its flight control method |
-
2016
- 2016-07-11 CN CN201620725584.3U patent/CN205872498U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109969380A (en) * | 2018-11-28 | 2019-07-05 | 北京汉能光伏投资有限公司 | A kind of solar energy unmanned plane and its flight control method |
| CN109911191A (en) * | 2019-04-16 | 2019-06-21 | 无锡森孚软件有限公司 | A kind of telemetry station with fixed point flight function |
| CN109911191B (en) * | 2019-04-16 | 2022-12-27 | 无锡森孚软件有限公司 | Telemetry station with fixed-point flight function |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107899166B (en) | Accurate fire extinguishing system and method based on unmanned aerial vehicle and intelligent fire-fighting robot | |
| CN204776013U (en) | Six unmanned aerial vehicle | |
| US9650134B2 (en) | Unmanned aerial rescue system | |
| CN205574268U (en) | A multimachine is four rotor aircraft system in coordination for high tension transmission line patrols and examines | |
| JP2019177869A (en) | Flight body and method for control of flight body | |
| US20170205536A1 (en) | Image and/or radio signals capturing platform | |
| CN107792348B (en) | Auxiliary device rises and falls based on wireless battery charging outfit of unmanned aerial vehicle | |
| CN106741734B (en) | A kind of lifebuoy is jettisoninged carry and unmanned plane | |
| CN204956946U (en) | Unmanned aerial vehicle with flexible cloud platform | |
| CN205872498U (en) | A unmanned vehicles for take photo by plane | |
| US20200317337A1 (en) | Unmanned Aerial Vehicle With Ducted Rotors | |
| CN206841708U (en) | A kind of vapour-pressure type multi-rotor unmanned aerial vehicle undercarriage | |
| CN206485252U (en) | A kind of fire communication command car of use unmanned plane wireless video transmission system | |
| CN204409382U (en) | One drives bird unmanned vehicle system | |
| CN206050093U (en) | A kind of outdoor special glare atmosphere is taken pictures rotor wing unmanned aerial vehicle | |
| CN2305819Y (en) | Ramote control type aerial photographic device | |
| CN104058110B (en) | Remote sensing satellite system | |
| CN106005464B (en) | A kind of energy-saving unmanned plane energy ancillary equipment | |
| CN106184795B (en) | A kind of plant protection unmanned plane charging station | |
| CN105978458B (en) | A kind of adjustable supporting | |
| KR102597619B1 (en) | Drone for advertisement using light-emitting diode persistence of vision | |
| KR101749453B1 (en) | Drone energy charging station using energy harvested from piezo-electric road | |
| CN109417971A (en) | A kind of wisdom balloon system and rain making method for rain making | |
| CN107284684A (en) | One kind is shot without dead angle Intelligent unattended machine | |
| CN113074698A (en) | Intelligent tower inclination detection system based on machine vision |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170111 Termination date: 20170711 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |