CN106184789A - One is taken photo by plane Helicopter System - Google Patents
One is taken photo by plane Helicopter System Download PDFInfo
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- CN106184789A CN106184789A CN201510232882.9A CN201510232882A CN106184789A CN 106184789 A CN106184789 A CN 106184789A CN 201510232882 A CN201510232882 A CN 201510232882A CN 106184789 A CN106184789 A CN 106184789A
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- helicopter
- camera
- plane
- antidetonation
- knuckle support
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Abstract
The present invention relates to one take photo by plane Helicopter System, including interconnective helicopter and ground control station, described helicopter includes aerial device, this aerial device includes three axle antidetonation The Cloud Terrace and cameras, described camera is fixed on three axle antidetonation The Cloud Terraces, and is arranged at bottom helicopter fuselage by three axle antidetonation The Cloud Terraces.Compared with prior art, due to the fact that the mode that have employed three axle antidetonation The Cloud Terrace fixed cameras, therefore camera is with good expansibility, and compared to the most commonly used photographic head and the frame mode of fuselage integration, can effectively reduce maintenance cost.
Description
Technical field
The present invention relates to one take photo by plane technology, especially relate to one and take photo by plane Helicopter System.
Background technology
2012, China's generation forest fire 3966, nearly 1.4 ten thousand hectares of injured area, injures and deaths 21 people, for
Lose one of minimum time.In the forest fire of part number of times, owing to there is no preferable early stage reconnaissance measure,
Therefore the time of suing and labouring is later, and some originally can be strangled the fire in cradle not die young.
Except forest fire is unexpected, also urban fire control, ultra-high-tension power transmission line, oil filed pipeline etc., it is also desirable to have very
Good daily monitoring, but the layout areas of a lot of ultra-high-tension power transmission lines and oil filed pipeline etc. the most all with forest one
Sample is positioned at some unfrequented places, and the mode relying on manpower to make an inspection tour causes the waste of substantial amounts of labouring population.And
And some places belong to original ecology, then add too much automation control appliance and ecological environment will necessarily be caused one
The most fixed impact, be capable of the monitoring to forest fire prevention and control etc., can be reduced as far as nature again simultaneously
The infringement of ecological environment seems have realistic meaning.
Chinese patent CN 103950536 A discloses a kind of scouting unmanned helicopter system, including controller,
First blade group control module, the second blade group control module, laser detection module, infrared sensing module, probe
Revolution control module, probe pitch control module, wireless communication module, GPS locating module, video acquisition mould
Block, gyro locating module.But this scouting unmanned helicopter system is the hugest, disappear only needing to carry out forest
There is redundancy functionally during the situations such as anti-and oil filed pipeline inspection, additionally this scouting unmanned helicopter system does not has yet
There is good image-capturing apparatus, therefore can not meet the mission requirements of forest fire prevention and control well.
Summary of the invention
Defect that the purpose of the present invention is contemplated to overcome above-mentioned prior art to exist and provide one to take photo by plane helicopter
System.
The purpose of the present invention can be achieved through the following technical solutions:
One is taken photo by plane Helicopter System, and including interconnective helicopter and ground control station, described helicopter includes
Aerial device, this aerial device includes three axle antidetonation The Cloud Terrace and cameras, and described camera is fixed on three axle antidetonation The Cloud Terraces,
And be arranged at bottom helicopter fuselage by three axle antidetonation The Cloud Terraces.
Described three axle antidetonation The Cloud Terraces include:
Extending bracket, is connected with bottom helicopter fuselage, for adjusting the course angle of camera；
Knuckle support, its one end is connected with extending bracket, for adjusting the roll angle of camera；
Fixed support, is connected with the other end of knuckle support, for fixed camera the angle of pitch that adjusts camera.
Described extending bracket includes the first housing and the first rotary shaft being placed in the first housing, described first rotary shaft
Two ends are connected with helicopter fuselage and knuckle support respectively.
Described knuckle support includes the second housing and the second rotary shaft being placed in the second housing, described second rotary shaft
Two ends are connected with knuckle support and fixed support respectively.
Described fixed support includes:
Object stage, is connected with knuckle support and rotates under knuckle support drives, for fixed camera；
3rd rotary shaft, is provided with two altogether, is symmetricly set in object stage both sides and is connected with camera both sides respectively, uses
In the angle of pitch adjusting camera.
It is equipped with amortisseur between described extending bracket and knuckle support and knuckle support and fixed support.
Described ground control station includes that the first radar transceiver, described helicopter include and the first radar transceiver pairing
The second radar transceiver connected；
When the second radar transceiver and the first radar transceiver disconnecting, helicopter makes a return voyage automatically.
Described helicopter also includes protecting parachute assembly, when helicopter vertical direction acceleration is acceleration of gravity
Time, described protection parachute assembly automatically turns on to reduce the mechanical energy of helicopter.
Compared with prior art, the invention have the advantages that
1) owing to have employed the mode of three axle antidetonation The Cloud Terrace fixed cameras, therefore camera is with good expansibility,
Compared to the most commonly used photographic head and the frame mode of fuselage integration, can effectively reduce maintenance cost.
2) extending bracket, knuckle support and fixed support are sequentially connected with, and the length of three supports can be as required
Customization, is adapted to different fuselages, and support has length simultaneously, therefore can improve degree of accuracy during adjustment.
3) the 3rd rotary shaft is provided with two altogether, can clamp camera from both direction, improve the stability of camera.
5) when the second radar transceiver and the first radar transceiver disconnecting, helicopter makes a return voyage automatically, permissible
Avoid helicopter out of control.
6) protection parachute assembly can avoid injuring during helicopter freely falling body the crowd on ground, and destroys building
Thing.
Accompanying drawing explanation
Fig. 1 is the structural representation of helicopter of the present invention；
Fig. 2 is the control configuration diagram of actuating unit of the present invention；
Wherein: 1, helicopter, 2, ground control station, 11, three axle antidetonation The Cloud Terraces, 12, camera, 13, spiral shell
Rotation oar, 14, fold arm, 15, undercarriage, 16, controller, 17, power motor, 18, GPS device.
Detailed description of the invention
The present invention is described in detail with specific embodiment below in conjunction with the accompanying drawings.The present embodiment is with the technology of the present invention side
Implement premised on case, give detailed embodiment and concrete operating process, but the protection model of the present invention
Enclose and be not limited to following embodiment.
One is taken photo by plane Helicopter System, as in figure 2 it is shown, include interconnective helicopter 1 and ground control station 2,
As it is shown in figure 1, helicopter 1 includes aerial device, this aerial device includes three axle antidetonation The Cloud Terrace 11 and cameras 12,
Camera 12 is fixed on three axle antidetonation The Cloud Terraces 11, and is arranged at helicopter 1 fuselage by three axle antidetonation The Cloud Terraces 11
Bottom, specially belly.
Three axle antidetonation The Cloud Terraces 11 include:
Extending bracket, is connected with helicopter 1 fuselage bottom, for adjusting the course angle of camera 12；
Knuckle support, its one end is connected with extending bracket, for adjusting the roll angle of camera 12；
Fixed support, is connected with the other end of knuckle support, for fixed camera 12 pitching that adjusts camera 12
Angle.
Extending bracket includes the first housing and the first rotary shaft being placed in the first housing, and the first rotating shaft terminal is respectively
It is connected with helicopter 1 fuselage and knuckle support.
Knuckle support includes the second housing and the second rotary shaft being placed in the second housing, and the second rotating shaft terminal is respectively
It is connected with knuckle support and fixed support.
Fixed support includes:
Object stage, is connected with knuckle support and rotates under knuckle support drives, for fixed camera 12；
3rd rotary shaft, is provided with two altogether, be symmetricly set in object stage both sides and be connected with camera 12 both sides respectively,
For adjusting the angle of pitch of camera 12.
It is equipped with amortisseur between extending bracket and knuckle support and knuckle support and fixed support.
As it is shown in figure 1, helicopter 1 includes actuating unit and is located at two undercarriages 15 below fuselage,
Actuating unit includes six propeller external members, and propeller external member includes folding arm 14 and being fixed on folding arm 14
The propeller 13 of one end, the other end folding arm 14 is connected with fuselage.
As in figure 2 it is shown, actuating unit includes controller 16 and six power motors being all connected with controller 16
17, six power motors 17 be respectively arranged on six fold on arms 14 and respectively with six corresponding connections of propeller 13.
Helicopter 1 is provided with the GPS device 18 for obtaining reconnaissance helicopter positional information, this GPS device
18 are connected with controller 16, and GPS device 18 can notify to receive whole world fortune position satellite system signal and base station
Signal, completes the determination of position in conjunction with architecture data and satellite location data, collocation GPS self-navigation system
System, can lock helicopter height and position, steadily hovering so that shoot from arbitrarily angled optional position exactly
Become practical.And GPS can also show the aircraft side relative to user by flight radar in real time
Position.
Being additionally provided with Inertial Measurement Unit on helicopter 1, this Inertial Measurement Unit includes the line for measuring helicopter 1
Three accelerometers of acceleration and for measuring the gyroscope of fuselage angular velocity, gyroscope and three accelerometers are equal
It is located at helicopter 1 fuselage interior and is connected with controller 16, according further to needs, helicopter 1 can also select
It is used in the barometer measuring atmospheric pressure.
Ground control station 2 include the first radar transceiver, helicopter 1 include with first radar transceiver pairing be connected
The second radar transceiver, when the second radar transceiver and the first radar transceiver disconnecting, helicopter 1
Automatically make a return voyage.
Ground control station 2 also includes
For receiving and dispatching the first communication antenna of control signal, for receiving the second of the picture signal of camera 12 shooting
Communication antenna and for showing the display screen of image captured by camera 12, the first communication antenna passes through 2.4GHz
Radio wave is connected with controller 16, and the second communication antenna is connected with controller 16 by 5.8GHz radio wave.
Control signal and picture signal use separate first communication antenna and the second communication antenna respectively with controller
16 connect, and also have employed different frequency ranges, decrease interference each other, additionally, due to picture signal
The radio wave that have employed 5.8GHz is connected with controller 16, and transmission range height is up to 1000 meters, and scope can
Reach 1500 meters, and transfer rate can be increased.It is additionally provided with on ground control station 2 and transports for controlling helicopter 1
The control rocking bar of dynamic attitude.
User can control the motion of helicopter by ground control station 2, and the picture that camera 12 photographs also may be used
To show on ground control station 2.
Helicopter 1 also includes protecting parachute assembly, when helicopter 1 vertical direction acceleration is acceleration of gravity,
Protection parachute assembly automatically turns on to reduce the mechanical energy of helicopter 1.
Claims (8)
1. a Helicopter System of taking photo by plane, it is characterised in that include interconnective helicopter (1) and ground control
System station (2), described helicopter (1) includes aerial device, and this aerial device includes three axles antidetonation The Cloud Terrace (11)
With camera (12), described camera (12) is fixed on three axles antidetonation The Cloud Terrace (11), and by three axle antidetonation clouds
Platform (11) is arranged at helicopter (1) fuselage bottom.
One the most according to claim 1 is taken photo by plane Helicopter System, it is characterised in that described three axle antidetonations
The Cloud Terrace (11) including:
Extending bracket, is connected with helicopter (1) fuselage bottom, is used for adjusting the course angle of camera (12)；
Knuckle support, its one end is connected with extending bracket, is used for adjusting the roll angle of camera (12)；
Fixed support, is connected with the other end of knuckle support, for fixed camera (12) and adjust camera (12)
The angle of pitch.
One the most according to claim 2 is taken photo by plane Helicopter System, it is characterised in that described extending bracket
Including the first housing and the first rotary shaft of being placed in the first housing, described first rotating shaft terminal respectively with helicopter
(1) fuselage and knuckle support connect.
One the most according to claim 2 is taken photo by plane Helicopter System, it is characterised in that described knuckle support
Including the second housing and the second rotary shaft of being placed in the second housing, described second rotating shaft terminal respectively with articular branches
Frame and fixed support connect.
One the most according to claim 2 is taken photo by plane Helicopter System, it is characterised in that described fixed support
Including:
Object stage, is connected with knuckle support and rotates under knuckle support drives, for fixed camera (12)；
3rd rotary shaft, is provided with two altogether, is symmetricly set in object stage both sides and connects with camera (12) both sides respectively
Connect, for adjusting the angle of pitch of camera (12).
One the most according to claim 2 is taken photo by plane Helicopter System, it is characterised in that described extending bracket
And it is equipped with amortisseur between knuckle support and knuckle support and fixed support.
One the most according to claim 1 is taken photo by plane Helicopter System, it is characterised in that described ground controls
Stand (2) include the first radar transceiver, described helicopter (1) to include with the first radar transceiver pairing being connected
Second radar transceiver；
When the second radar transceiver and the first radar transceiver disconnecting, helicopter (1) makes a return voyage automatically.
One the most according to claim 1 is taken photo by plane Helicopter System, it is characterised in that described helicopter (1)
Also include protecting parachute assembly, when helicopter (1) vertical direction acceleration is acceleration of gravity, described guarantor
Protect parachute assembly and automatically turn on to reduce the mechanical energy of helicopter (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510232882.9A CN106184789A (en) | 2015-05-08 | 2015-05-08 | One is taken photo by plane Helicopter System |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510232882.9A CN106184789A (en) | 2015-05-08 | 2015-05-08 | One is taken photo by plane Helicopter System |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184789A true CN106184789A (en) | 2016-12-07 |
Family
ID=57459185
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510232882.9A Pending CN106184789A (en) | 2015-05-08 | 2015-05-08 | One is taken photo by plane Helicopter System |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184789A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107000833A (en) * | 2016-12-26 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Unmanned plane |
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| JP2007038925A (en) * | 2005-08-04 | 2007-02-15 | Yamaha Motor Co Ltd | Unmanned helicopter |
| CN101445156A (en) * | 2008-05-15 | 2009-06-03 | 龚文基 | Technology for integrating intelligent aerial robotic system |
| CN102556359A (en) * | 2010-12-28 | 2012-07-11 | 中国科学院沈阳自动化研究所 | Airborne air-photo image-stabilizing cloud deck of unmanned aerial vehicle |
| CN103029834A (en) * | 2012-11-26 | 2013-04-10 | 北京兰亭华谊文化传媒有限责任公司 | Small electric unmanned helicopter aerial photography system based on front-end triaxial-type pan-tilt |
| CN203666995U (en) * | 2013-12-05 | 2014-06-25 | 张锦海 | Three-shaft aerial shooting holder |
| CN104002963A (en) * | 2014-05-12 | 2014-08-27 | 国家电网公司 | Unmanned patrol aircraft for power transmission lines |
| CN104477399A (en) * | 2014-11-26 | 2015-04-01 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle (UAV) for searching and rescuing at night |
| CN104507799A (en) * | 2014-04-28 | 2015-04-08 | 深圳市大疆创新科技有限公司 | Protection control method of air vehicle, device and air vehicle |
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2015
- 2015-05-08 CN CN201510232882.9A patent/CN106184789A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007038925A (en) * | 2005-08-04 | 2007-02-15 | Yamaha Motor Co Ltd | Unmanned helicopter |
| CN101445156A (en) * | 2008-05-15 | 2009-06-03 | 龚文基 | Technology for integrating intelligent aerial robotic system |
| CN102556359A (en) * | 2010-12-28 | 2012-07-11 | 中国科学院沈阳自动化研究所 | Airborne air-photo image-stabilizing cloud deck of unmanned aerial vehicle |
| CN103029834A (en) * | 2012-11-26 | 2013-04-10 | 北京兰亭华谊文化传媒有限责任公司 | Small electric unmanned helicopter aerial photography system based on front-end triaxial-type pan-tilt |
| CN203666995U (en) * | 2013-12-05 | 2014-06-25 | 张锦海 | Three-shaft aerial shooting holder |
| CN104507799A (en) * | 2014-04-28 | 2015-04-08 | 深圳市大疆创新科技有限公司 | Protection control method of air vehicle, device and air vehicle |
| CN104002963A (en) * | 2014-05-12 | 2014-08-27 | 国家电网公司 | Unmanned patrol aircraft for power transmission lines |
| CN104477399A (en) * | 2014-11-26 | 2015-04-01 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle (UAV) for searching and rescuing at night |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107000833A (en) * | 2016-12-26 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| WO2018119555A1 (en) * | 2016-12-26 | 2018-07-05 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN107000833B (en) * | 2016-12-26 | 2019-01-22 | 深圳市大疆创新科技有限公司 | Unmanned plane |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |
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| RJ01 | Rejection of invention patent application after publication |