CN205971848U - Novel primary and secondary unmanned aerial vehicle system - Google Patents
Novel primary and secondary unmanned aerial vehicle system Download PDFInfo
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- CN205971848U CN205971848U CN201620725319.5U CN201620725319U CN205971848U CN 205971848 U CN205971848 U CN 205971848U CN 201620725319 U CN201620725319 U CN 201620725319U CN 205971848 U CN205971848 U CN 205971848U
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- machine tool
- flight control
- control system
- handset
- shooting
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Abstract
The utility model discloses the technique relates to a novel primary and secondary unmanned aerial vehicle system, constitute including delivery machine tool, shooting parasite aircraft, machine year capstan winch system, ground satellite station, the delivery machine tool is received and wireless data transmission transfer message through the instruction with the ground satellite station, and the instruction is received and is connected with machine tool flight control system, and wireless data transmission links to each other with machine tool flight control system, machine tool driving system links to each other with machine tool flight control system, the machine tool power meets with machine tool flight control system, it is continuous through the quick -witted capstan winch system of carrying between delivery machine tool and shooting parasite aircraft, the machine carries capstan winch system one end and links to each other with the delivery machine tool, and the other end links to each other with parasite aircraft flight control system, it does not have the line chart biography to be equipped with parasite aircraft wireless data transmission and parasite aircraft in the parasite aircraft flight control system, parasite aircraft flight control system and cloud platform link to each other, and the cloud platform embeds image imaging system, parasite aircraft flight control system is equipped with servo steering wheel, parasite aircraft flight control system's electric energy is provided by the parasite aircraft power, servo steering wheel links to each other with parasite aircraft driving system.
Description
Technical field
The technology of the present invention belongs to electron electric power unmanned plane apparatus field, relates generally to a kind of new primary and secondary UAS.
Background technology
Unmanned plane is that one kind is dynamic, controllable, can carry multiple-task equipment, executes multiple-task, and can repeat to make
Unmanned aviation aircraft.One of important means as Spatial data capture, unmanned plane has maneuverability, quick
Reaction, unmanned flight, operation require low, carry multiclass sensor, image real-time Transmission, high-risk areas detect, comprehensive benefit is high
The advantages of, it is the strong supplement of satellite remote sensing and traditional air remote sensing mode.
Since first automatic pilot of invention, unmanned plane is paid attention to by more and more national, development rapidly in view of
Its exclusive advantage, the range of unmanned plane has widened military affairs, scientific research, civilian three big fields.Militarily can be used for detecing
Examine, monitor, the guidance of communication relay, electronic countermeasure, firepower, combat success assessment, harassing and wrecking, temptation, target simulation etc.；In scientific research
On, can be used for the test of atmospheric research, the sampling in core biochemical pollution area and monitoring, new technical equipment and new aircraft；Civilian
On, can be used for geodesic survey, meteorological observation, urban environment detection, earth resource exploration, forest fire protection etc..Because it possesses application
Widely characteristic, causes the research boom of global unmanned plane now, and is developed and push the new stage to.
Chinese unmanned plane research and development mainly rest in national army and scientific research institutions with production capacity.Enter the nineties in 20th century
Afterwards, domestic Development of UAV enter one " golden age ".Private enterprise is with sharp market sense of smell, quickly reaction energy
Power and educational advantages, emerge rapidly in unmanned plane market.2007, space flight star chart science and technology (Beijing) Co., Ltd was using autonomous
Core technology, successfully develops the multinomial software and hardware product based on unmanned air vehicle technique.Space flight star chart UAS is flat from flight
On platform, machine, system to terrestrial information integrated treatment has complete series from major product and core technology, be domestic collection unmanned plane application,
The multinomial service such as information processing and the integrated system of solution one.The starting point of space flight star chart unmanned plane system is research nothing
People's aircraft information characteristic processes (fast, ageing), unmanned vehicle information and space flight, the fusion of aviation information, unmanned flight
The application of device information.Set up general unmanned vehicle intelligence support system, form generalization, seriation, architecture, multiplexing
Property high unmanned vehicle informix process product.Set up based on Data-Link, unmanned vehicle platform, with machine with ground
Surface information is worked in coordination with and is processed as core, and on formation slave, data acquisition, fusion, target sieve subtract, position compression, be transferred to ground-based mission
Planning and monitoring, information processing and analysis, information Store and issue, the unmanned vehicle informix process assisting decision-making of holding a conference or consultation
Architectural framework.Put goods on the market at present have autonomous small-sized electric UAS, medium-sized oil move integrated UAS, autonomous in
SUAV flight control system, unmanned plane task grouping, Unmanned Aerial Vehicle Data processing system, unmanned aerial vehicle tracking telemetry and command station, no
Man-machine intelligence analysis system, unmanned aerial vehicle onboard processing system.
However, unmanned plane power industry apply due to high-voltage electric power circuit produce electromagnetic field can be to the winged control of unmanned plane
System interferes, and makes the flight control system of unmanned plane and GPS location function produce logical miss, affects normally flying of unmanned plane
OK, unmanned plane air crash out of control may be made, even more serious meeting threatens the safety of high-voltage electric power circuit and causes the damage of personal property
Lose.Additionally, current unmanned plane high-resolution, high-quality picture shooting are more difficult, its flight must be with distance within circuit holding 40m
More picture rich in detail could be shot, but hypotelorism needs the higher anti-interference equipment of configuration, if deposited using long zoom facility
Unmanned plane load increase cruising time and picture processing later stage, length time, costly the problems such as.
Content of the invention
In order to overcome the shortcomings of background technology, the invention provides a kind of possess independent power supply and dynamical system and shooting
Subsystem can be carried machine tool and is carried to transfer to by static(al) rope above electric power facility closely to be clapped near high-tension line
The new primary and secondary UAS taken the photograph.Mainly solve existing unmanned plane shooting at close range to be easily disturbed, wide-long shot picture
Definition low and deliver machine tool with shoot subsystem be difficult to independent work the problems such as.
Design of the present invention：A kind of new primary and secondary UAS is it is characterised in that include delivery mother
Machine, shooting handset, airborne capstan system 6, earth station 1 form, and described delivery machine tool passes through command reception 2 and mother with earth station 1
Wireless data sending 15 transmission information, described command reception 2 is connected with machine tool flight control system 3, and described mother's wireless data sending 15 is flown with machine tool
Control system 3 is connected, the power that described machine tool dynamical system 4 is connected with machine tool flight control system 3 needed for offer machine tool flight control system 3,
Electric energy, described delivery machine tool and bat that described machine tool power supply 5 is connected with machine tool flight control system 3 needed for offer machine tool flight control system 3
Take the photograph and pass through airborne capstan system 6 between handset and be connected, described airborne capstan system 6 one end is connected with delivery machine tool, the other end with sub
Machine flight control system 11 is connected, and is provided with sub- wireless data sending 7 and handset wireless image transmission 8, described handset in described handset flight control system 11
Flight control system 11 is connected with head 10, head 10 Built-in Image camera system 9, and described handset flight control system 11 is provided with servorudder
Machine 13, the electric energy of described handset flight control system 11 is provided by handset power supply 12, described Servo-controller 13 and handset dynamical system 14
It is connected.
According in a kind of design of new primary and secondary UAS, it is characterized in that, described delivery machine tool is by carbon fiber
Bar support, rotor, command reception 2, female wireless data sending 15, machine tool flight control system 3, machine tool dynamical system 4 and 5 groups of machine tool power supply
Become.
According in a kind of design of new primary and secondary UAS, it is characterized in that, described airborne capstan system 6 is by electricity
Motivation, reduction gear box, reel, static(al) rope and support composition.
According in a kind of design of new primary and secondary UAS, it is characterized in that, described Servo-controller 13 is provided with 4
Individual, it is respectively arranged in four corner locations shooting handset.
According in a kind of design of new primary and secondary UAS, it is characterized in that, described static(al) rope is shut out for high intensity
Nation's cord, and be wrapped on reel.
According in a kind of design of new primary and secondary UAS, it is characterized in that, the volume of described airborne capstan system 6
Cylinder edge is provided with intelligent counter, can read the distance that static(al) rope is put, received.
According in a kind of design of new primary and secondary UAS, described rotor has 4 and is designed as culvert type, keeps away
Exempt from rotor and be wound around static(al) rope, the Gravity support shooting handset is provided by static(al) rope, 4 ducts control the aerial statue of unmanned plane,
Held stationary, four duct oar faces are in that 45 degree of angles are installed, and 10 centimetres of each duct diameter simultaneously carries an independent Servo-controller
13, Servo-controller 13 controls duct can do the rotation of positive and negative 45 degree of angles, and four ducts provide lateral dynamics.
According in a kind of design of new primary and secondary UAS, it is provided between described delivery machine tool and shooting handset
Infrared locating calibration device.
According in a kind of design of new primary and secondary UAS, described infrared locating calibration device is delivery machine tool
When shooting handset is packed up, shooting handset is made accurately to enter position it is ensured that primary and secondary UAS, after the completion of task, makes a return voyage and landed
Cheng Zhong, shooting handset will not rock.
The technology of the present invention has the advantage that：
(1), in a kind of new primary and secondary UAS that the present invention provides, shoot handset and possess independent power supply and power
System and can be carried machine tool and be transferred to by static(al) rope and carry out shooting at close range near high-tension line, this mode reduces height
The interference to delivery machine tool for the line ball road, makes unmanned plane operate steadily, thus improving shooting picture clarity.
(2), in a kind of new primary and secondary UAS that the present invention provides, delivery machine tool and shooting subsystem can be carried out
Remote operation, operating personnel need not be accurately controlled to primary and secondary UAS, when undertaking task, only need to be by primary and secondary unmanned plane
System flight, to target overhead, delivers machine tool and passes through static(al) rope decentralization shooting subsystem to high-tension line, can approach fault hidden
Affected part, accurate failure judgement point, and timely expatriate personnel are rushed to repair it is ensured that safe operation of electric network.
(3) in a kind of new primary and secondary UAS that the present invention provides, delivery machine tool and shooting subsystem have data altogether
Enjoy function, improve the uniformity of primary and secondary UAS operation, shooting subsystem has independent flight control system can be with delivery
Carry out data transmission between machine tool, keep both positions relatively stable, reduce and difficulty is manipulated to primary and secondary UAS, reduce
The interference of picture shooting process.
Brief description
A kind of structural framing figure of new primary and secondary UAS of Fig. 1 present invention
Specific embodiment
Accompanying drawing below in conjunction with the technology of the present invention and specific design scheme, to the technical side in patent Example of the present invention
Case is clearly and completely described it is clear that described embodiment is only a part of embodiment of patent of the present invention, and not
It is whole embodiments.Based on the embodiment in patent of the present invention, those of ordinary skill in the art are not paying creative labor
The every other embodiment being obtained under the premise of dynamic, broadly falls into the scope of this patent protection.
Implement row 1
Shown in the structural framing figure of new primary and secondary UAS as a kind of in Fig. 1, a kind of described new primary and secondary unmanned plane system
System, forms including delivery machine tool, shooting handset, airborne capstan system 6, earth station 1, and described delivery machine tool is passed through with earth station 1
Command reception 2 and female wireless data sending 15 transmission information, described command reception 2 is connected with machine tool flight control system 3, described mother no line number
Pass 15 to be connected with machine tool flight control system 3, described machine tool dynamical system 4 is connected with machine tool flight control system 3 provides machine tool flight control system 3
Required power, the electric energy that described machine tool power supply 5 is connected with machine tool flight control system 3 needed for offer machine tool flight control system 3, described
Delivery machine tool and shoot handset between be connected by airborne capstan system 6, described airborne capstan system 6 one end and deliver machine tool phase
Even, the other end is connected with handset flight control system 11, is provided with sub- wireless data sending 7 and handset no line chart in described handset flight control system 11
Pass 8, described handset flight control system 11 is connected with head 10, head 10 Built-in Image camera system 9, described handset flight control system 11
It is provided with Servo-controller 13, the electric energy of described handset flight control system 11 is provided by handset power supply 13, described Servo-controller 13 and handset
Dynamical system 14 is connected.
Described delivery machine tool by carbon fiber bar support, rotor, command reception 2, female wireless data sending 15, machine tool flight control system 3,
Machine tool dynamical system 4 and machine tool power supply 5 form.
Described airborne capstan system 6 is made up of motor, reduction gear box, reel, static(al) rope and support.
Described Servo-controller 13 is provided with 4 and is installed on four corner locations shooting handset.
Described static(al) rope is high intensity Du Pont cord, and is wrapped on reel.
The reel edge of described airborne capstan system 6 is provided with intelligent counter, can read the distance that static(al) rope is put, received.
Described rotor has 4 and is designed as culvert type, it is to avoid rotor is wound around static(al) rope, and the Gravity support shooting handset is by quiet
Power rope provides, and 4 ducts control the aerial statue of unmanned plane, held stationary, and four duct oar faces are in 45 degree of installations, each duct
10 centimetres of diameter simultaneously carries an independent Servo-controller 14, and Servo-controller 14 control duct can do positive and negative 45 degree and rotate, and four
Individual duct provides lateral dynamics.
Between described delivery machine tool and shooting handset, infrared locating calibration device is installed.
When described infrared locating calibration device is that shooting handset is packed up by delivery machine tool, shooting handset is made accurately to enter position, really
Protect primary and secondary UAS after the completion of task, make a return voyage in descent, shooting handset will not rock.
During use, the contract type post of delivery machine tool lower end is inserted by infrared locating calibration device shoot handset fuselage first
On inward recess in, by three-point fox method fixing delivery machine tool and the relative position shooting handset, earth station 1 opens unmanned
Machine, the command reception 2 of delivery machine tool receives information, and transfers information to machine tool flight control system 3, and unmanned plane starts running winged
OK, open simultaneously shoot handset, transmit information to after shooting handset receive information shoot handset flight control system 11, deliver machine tool
Female wireless data sending 15 and handset sub- wireless data sending 7 can mutual receive information, according to the state of flight delivering machine tool, handset
Flight control system 11 controls Servo-controller 13 so that shooting handset is run with position with delivery machine tool, when finding that target needs to shoot, female
Machine flight control system 3, while sending information to infrared locating calibration device, is opened the insertion of delivery machine tool lower end and is shot on handset fuselage
Inward recess in contract type post, send instruction, the motor running of airborne capstan system 6, reel to airborne capstan system 6
Operating release static(al) rope, intelligent counter calculates the input distance of static(al) rope, shoots handset and approaches target shooting at close range.Work as bat
After the completion of taking the photograph, airborne capstan system 6 packs up static(al) rope, shoots handset and withdraws, infrared locating calibration device precisely shoots handset machine
Indent hole site with it makes it inject delivery machine tool lower end contract type post establishing shot handset.
Every technical staff's notice：Although the present invention describes according to above-mentioned specific embodiment, the present invention
Invention thought be not limited to that invention, the repacking of any utilization inventive concept, all will include this patent protection of the patent right
In the range of.
Claims (9)
1. a kind of new primary and secondary UAS is it is characterised in that including delivery machine tool, shooting handset, airborne capstan system
(6), earth station (1) composition, described delivery machine tool and earth station (1) pass through command reception (2) and female wireless data sending (15) transmission
Information, described command reception (2) is connected with machine tool flight control system (3), described mother wireless data sending (15) with machine tool flight control system (3)
It is connected, the power that described machine tool dynamical system (4) is connected with machine tool flight control system (3) needed for offer machine tool flight control system (3), institute
State the electric energy that machine tool power supply (5) is connected needed for offer machine tool flight control system (3), described delivery machine tool with machine tool flight control system (3)
It is connected by airborne capstan system (6) between handset with shooting, described airborne capstan system (6) one end is connected with delivery machine tool, separately
One end is connected with handset flight control system (11), is provided with sub- wireless data sending (7) and handset is wireless in described handset flight control system (11)
Figure passes (8), and described handset flight control system (11) is connected with head (10), head (10) Built-in Image camera system (9), described son
Machine flight control system (11) is provided with Servo-controller (13), and the electric energy of described handset flight control system (11) is provided by handset power supply (12),
Described Servo-controller (13) is connected with handset dynamical system (14).
2. a kind of new primary and secondary UAS according to claim 1, is characterized in that, described delivery machine tool is by carbon fiber
Bar support, rotor, command reception (2), female wireless data sending (15), machine tool flight control system (3), machine tool dynamical system (4) and machine tool
Power supply (5) forms.
3. a kind of new primary and secondary UAS according to claim 1, is characterized in that, described airborne capstan system (6)
It is made up of motor, reduction gear box, reel, static(al) rope and support.
4. a kind of new primary and secondary UAS according to claim 1, is characterized in that, described Servo-controller (13) is provided with
4, it is respectively arranged in four corner locations shooting handset.
5. a kind of new primary and secondary UAS according to claim 3, is characterized in that, described static(al) rope is shut out for high intensity
Nation's cord, and be wrapped on reel.
6. a kind of new primary and secondary UAS according to claim 1, is characterized in that, described airborne capstan system (6)
Reel edge be provided with intelligent counter, the distance that static(al) rope is put, received can be read.
7. a kind of new primary and secondary UAS according to claim 2, described rotor has 4 and is designed as culvert type,
Rotor is avoided to be wound around static(al) rope, the Gravity support shooting handset is provided by static(al) rope, 4 ducts control the aerial appearance of unmanned plane
State, held stationary, four duct oar faces are in 45 degree of installations, and 10 centimetres of each duct diameter simultaneously carries an independent Servo-controller
(13), Servo-controller (13) controls duct can do positive and negative 45 degree of rotations, and four ducts provide lateral dynamics.
8. a kind of new primary and secondary UAS according to claim 1, installs between described delivery machine tool and shooting handset
There is infrared locating calibration device.
9. a kind of new primary and secondary UAS according to claim 8, described infrared locating calibration device is that delivery is female
When shooting handset is packed up by machine, shooting handset is made accurately to enter position it is ensured that primary and secondary UAS is after the completion of task, landing of making a return voyage
During, shooting handset will not rock.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725319.5U CN205971848U (en) | 2016-07-05 | 2016-07-05 | Novel primary and secondary unmanned aerial vehicle system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620725319.5U CN205971848U (en) | 2016-07-05 | 2016-07-05 | Novel primary and secondary unmanned aerial vehicle system |
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| Publication Number | Publication Date |
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| CN205971848U true CN205971848U (en) | 2017-02-22 |
Family
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620725319.5U Withdrawn - After Issue CN205971848U (en) | 2016-07-05 | 2016-07-05 | Novel primary and secondary unmanned aerial vehicle system |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005410A (en) * | 2016-07-05 | 2016-10-12 | 国网浙江省电力公司衢州供电公司 | Novel son and mother unmanned aerial vehicle system |
| CN106850049A (en) * | 2017-03-21 | 2017-06-13 | 广东容祺智能科技有限公司 | A kind of unmanned plane communicates transferring system |
| CN106882383A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | Take off mode and its device of a kind of aircraft |
| CN107264769A (en) * | 2017-06-22 | 2017-10-20 | 北京信息科技大学 | A kind of rigid multi-rotor aerocraft combination system |
| CN107444642A (en) * | 2017-08-16 | 2017-12-08 | 广东容祺智能科技有限公司 | A kind of flight system of large-scale UAV flight's SUAV |
| CN107554786A (en) * | 2017-08-19 | 2018-01-09 | 中国矿业大学 | A kind of handset of mine detecting aircraft starts control device and control method |
| CN110290476A (en) * | 2019-06-10 | 2019-09-27 | 河南华讯方舟航空科技有限公司 | Unmanned plane cluster communication method and system |
-
2016
- 2016-07-05 CN CN201620725319.5U patent/CN205971848U/en not_active Withdrawn - After Issue
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005410A (en) * | 2016-07-05 | 2016-10-12 | 国网浙江省电力公司衢州供电公司 | Novel son and mother unmanned aerial vehicle system |
| CN106005410B (en) * | 2016-07-05 | 2019-05-24 | 国网浙江省电力有限公司衢州供电公司 | A kind of primary and secondary UAV system |
| CN106882383A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | Take off mode and its device of a kind of aircraft |
| CN106850049A (en) * | 2017-03-21 | 2017-06-13 | 广东容祺智能科技有限公司 | A kind of unmanned plane communicates transferring system |
| CN107264769A (en) * | 2017-06-22 | 2017-10-20 | 北京信息科技大学 | A kind of rigid multi-rotor aerocraft combination system |
| CN107264769B (en) * | 2017-06-22 | 2020-05-08 | 北京信息科技大学 | Rigid multi-rotor aircraft merging system |
| CN107444642A (en) * | 2017-08-16 | 2017-12-08 | 广东容祺智能科技有限公司 | A kind of flight system of large-scale UAV flight's SUAV |
| CN107554786A (en) * | 2017-08-19 | 2018-01-09 | 中国矿业大学 | A kind of handset of mine detecting aircraft starts control device and control method |
| CN110290476A (en) * | 2019-06-10 | 2019-09-27 | 河南华讯方舟航空科技有限公司 | Unmanned plane cluster communication method and system |
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Legal Events
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170222 Effective date of abandoning: 20181019 |