CN204415743U - A kind of patrol monitoring unmanned vehicle system - Google Patents
A kind of patrol monitoring unmanned vehicle system Download PDFInfo
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- CN204415743U CN204415743U CN201520063872.2U CN201520063872U CN204415743U CN 204415743 U CN204415743 U CN 204415743U CN 201520063872 U CN201520063872 U CN 201520063872U CN 204415743 U CN204415743 U CN 204415743U
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 29
- 238000004891 communication Methods 0.000 claims abstract description 8
- 239000000725 suspension Substances 0.000 claims description 3
- 238000004804 winding Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 230000007123 defense Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 241000269799 Perca fluviatilis Species 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
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Abstract
The utility model discloses a kind of patrol monitoring unmanned vehicle system, belong to unmanned vehicle technical field.Unmanned vehicle of the present utility model is connected with the electric power system on unmanned vehicle by cable, the base of this unmanned vehicle is connected with slip ring motor, the output shaft of slip ring motor connects watch-dog, the auxiliary rotor of unmanned vehicle is connected with main rotor by horn, the bottom of horn is provided with rotating machine, this rotating machine drives horn to rotate in the horizontal direction, and the both sides, top of unmanned vehicle casing are provided with cover plate, and the track that cover plate is laid along casing top closes or opens; The headstock portion of car body is provided with camera, is provided with power supply and communication means between headstock and casing.The utility model utilizes cross-country unmanned vehicle-mounted unmanned aerial vehicle, and the electric power system on unmanned vehicle by cable directly for aircraft is powered, make aircraft by the restriction of load capacity of cell, have the sufficient time to perform low latitude monitor task.
Description
Technical field
The utility model relates to unmanned vehicle technical field, more particularly, relates to a kind of patrol monitoring unmanned vehicle system.
Background technology
Compared with autogyro, dirigible, small-sized multi-rotor aerocraft has maneuverability, cheap advantage.Use small aircraft as the carrier of watch-dog, obstructed to ground such as road, to cause traffic jam because of on-the-spot confusion, make because of environmental pollution, nuclear leakage and anti-terrorism danger operating personnel cannot near etc. situation monitor, have also been obtained more and more general application.
But, the monitoring aircraft of current use adopts lithium cell etc. to power usually, due to the comparatively large so power consumption of aircraft energy consumption quickly, cause the cruise duration of aircraft short, generally can only continue 5 ~ 10 minutes, although carry high capacity cell can extend the flight time, reduce causing the capacity weight of aircraft.How to improve the cruise duration of monitoring aircraft, capacity weight and transmission image quality, become association area urgent problem.
In addition, China has vast in territory, border, land line length, seashore line length, the features such as marine site is vast, and island are numerous, in order to maintain the long-term stability of country, need to drop into a large amount of manpower and materials, in the whole nation, formation is set up, the safety of patrol defendance border and coast defence in the border area of each provinces and regions, coastline and defence area, island.Security protection drops into huge, and in the inspection of actual border and hazardous location monitoring work, and by heat and the impact of food supply in severe winter, the patrol condition of border personnel is very arduous.At present, the border security protection measure based on people's air defense more and more can not practical requirement.
Through retrieval, Chinese Patent Application No. 201410456009.3, the applying date is on September 10th, 2014, invention and created name is: a kind of unmanned plane mooring system, this application case is made up of ground HVDC voltage-stabilizing system, wire dispenser, synchronizing wire winding wheel, mooring cable, aerial Voltage stabilizing module and emergency battery, HVDC voltage-stabilizing system and synchronizing wire winding wheel are arranged on wire dispenser, and mooring cable is connected with Voltage stabilizing module and emergency battery.The unmanned plane of this application case can infinitely time overhead monitor, and pass vision signal back command van, be large-scale activity, the security of rally provides interim lofty perch to monitor.But this application case can only be monitored in fixed location, maneuverability is not high, still needs further improvement.
China Patent No. ZL 201220596561.9, authorized announcement date is on May 29th, 2013, invention and created name is: a kind of electric drive lifting unmanned flight platform, this application case comprises electric drive lifting unmanned plane, described unmanned plane is connected with floor power supply device by feeder cable, by floor power supply device for electric drive.Described floor power supply device is the confession electric car with vehicle power.This application case carries out continued power by ground power supply to electric drive lifting unmanned plane, and make the power of powering and time length have guarantee, the lift by screw propeller can be sling weight.But this application case is mainly used in weight lifting transport, can not promote the use of patrol monitoring.
Summary of the invention
1. the utility model technical matters that will solve
The purpose of this utility model is to overcome to be existed in prior art: 1) to monitor that aircraft cruise duration is short, capacity weight is low; 2) border security protection is based on people's air defense, the deficiency that patrol condition is arduous, provides a kind of patrol monitoring unmanned vehicle system; The utility model utilizes cross-country unmanned vehicle-mounted unmanned aerial vehicle, and the electric power system on unmanned vehicle by cable directly for aircraft is powered, make aircraft not by the restriction of load capacity of cell, considerably increase the cruise duration of aircraft, can ensure that aircraft has the sufficient time to perform low latitude monitor task; In addition, patrol personnel can go on patrol at headquarters' remotely-piloted vehicle, not only increase patrol range of observation, and it also avoid the risk that danger that beat may exist causes personnel, patrol monitoring condition and efficiency obtain obvious improvement.
2. technical scheme
For achieving the above object, the technical scheme that the utility model provides is:
One patrol monitoring unmanned vehicle system of the present utility model, comprise unmanned vehicle, slip ring motor, watch-dog and unmanned vehicle, described unmanned vehicle is connected with the electric power system on unmanned vehicle by cable, base is provided with bottom this unmanned vehicle, this base is connected with slip ring motor, and the output shaft of described slip ring motor connects watch-dog.
Further, described unmanned vehicle comprises main rotor and auxiliary rotor, and described main rotor is coaxial double-rotary wing structure, and auxiliary rotor is connected with main rotor by horn; The bottom of described horn is provided with rotating machine, and this rotating machine drives horn to rotate in the horizontal direction.
Further, described unmanned vehicle comprises car body and casing, and casing is arranged on car body, and the both sides, top of this casing are provided with cover plate, and the track that cover plate is laid along casing top closes or opens; The headstock portion of described car body is provided with camera, and between headstock and casing, be provided with power supply and communication means, this power supply and communication means comprise electric power system and telecommunications base station.
Further, described watch-dog adopts magnetic suspension camera.
3. beneficial effect
The technical scheme adopting the utility model to provide, compared with existing known technology, has following beneficial effect:
(1) one patrol monitoring unmanned vehicle system of the present utility model, its unmanned vehicle adopts the main rotor of coaxial double-rotary wing structure, and with four auxiliary rotors, and power is greatly and more economize the energy; In addition, this unmanned vehicle uses the electric power system on unmanned vehicle to power, compared with the battery-mounted scheme of flying of powering of existing unmanned vehicle, its cruise duration is not by the restriction of load capacity of cell, once can go out to treat empty 9 hours through measuring and calculating, can ensure that aircraft has the sufficient time to perform patrol monitor task;
(2) one patrol monitoring unmanned vehicle system of the present utility model, four auxiliary rotors of its unmanned vehicle can be contracted to bottom main rotor automatically, its unmanned vehicle casing can open and close automatically, unmanned vehicle can accurately fall in unmanned vehicle casing, or go up to the air fast in unmanned vehicle casing, whole aerocraft system maneuverability, can devote oneself to work fast;
(3) one patrol monitoring unmanned vehicle system of the present utility model, it utilizes cross-country unmanned vehicle-mounted unmanned aerial vehicle, unmanned vehicle is equipped with watch-dog, patrol personnel can carry out border patrol monitoring at headquarters' remotely pilotless aircraft, and patrol monitoring condition obtains and greatly improves.
Accompanying drawing explanation
Fig. 1 is a kind of structural representation going on patrol monitoring unmanned vehicle system of the present utility model;
Fig. 2 is the schematic diagram that in the utility model, unmanned vehicle is positioned at unmanned vehicle casing.
Label declaration in schematic diagram:
11, main rotor; 121, horn; 122, rotating machine; 123, auxiliary rotor; 13, base; 21, slip ring motor; 22, watch-dog; 3, cable; 41, car body; 42, casing; 421, cover plate; 422, track; 43, power supply and communication means; 44, camera.
Detailed description of the invention
For understanding content of the present utility model further, in conjunction with the accompanying drawings and embodiments the utility model is described in detail.
Embodiment 1
With reference to figure 1, the one patrol monitoring unmanned vehicle system of the present embodiment, comprises unmanned vehicle, slip ring motor 21, watch-dog 22 and unmanned vehicle.Be provided with base 13 bottom described unmanned vehicle, this base 13 is connected with slip ring motor 21, and the output shaft of described slip ring motor 21 connects watch-dog 22.In the present embodiment, watch-dog 22 adopts magnetic suspension camera, and camera lens is floated by repulsive force by such camera, has excellent stabilization shockproof properties, and then can ensure the clear of monitored picture to the full extent, be convenient to the observation of ground staff.
Described unmanned vehicle possesses cross-country function, can meet the transportation request of Special section.This unmanned vehicle comprises car body 41 and casing 42, casing 42 is arranged on car body 41, the both sides, top of this casing 42 are provided with cover plate 421, the two ends of cover plate 421 are provided with chute, both sides of the edge corresponding with chute, casing 42 top are equipped with track 422, cover plate 421 can move along track 422, realizes the closed of casing 42 or opens.The built-in GPS location of described car body 41 and personal vehicle system, the headstock portion of car body 41 is provided with camera 44, this camera 44 is miniature high-precision camera, it is equivalent to " eyes " of whole unmanned vehicle system, the controllers of headquarters can by the track route of the picture planning unmanned vehicle of this camera 44 shooting, and observe periphery situation, to reach patrol object.
Be provided with between headstock and casing 42 and power and communication means 43, this power supply and communication means 43 comprise electric power system and telecommunications base station, and described telecommunications base station is used for providing Signal transmissions for headquarters.Described electric power system comprises source of AC and voltage transformer, and this electric power system provides power supply for the operation of unmanned vehicle and unmanned vehicle.
Electric power system in the present embodiment on unmanned vehicle by cable 3 directly for unmanned vehicle is powered, conveying power quality is high and avoid the aircraft that traditional battery-mounted power supply plan exists and limit by load capacity of cell cruise duration, execute the task time short problem in overhead, once can go out to treat empty 9 hours through measuring and calculating, can ensure that aircraft has the sufficient time to perform patrol monitor task.And consider relative to the battery-mounted power supply plan of tradition, namely the present embodiment inevitable defect is the storage problem of cable 3.Although aircraft performs low-flying patrol operation, generally also need the cable 3 of tens meters, as well very big inconvenience can not be brought by giving the use of aircraft by management cable 3.In order to solve the problem, the present embodiment is provided with a wire spool (for illustrating in figure) in casing 42, cable 3 is coiled on wire spool, and be provided with by monolithic processor controlled follow-up motor in one end of wire spool, this follow-up motor can respond to the flying height of aircraft automatically, controls wire spool forward or reverse.So, aircraft no matter overhead execute the task or finish the work after landing, all need not worried cable 3 winding, reclaim problem, greatly facilitate the use of aircraft.
Described unmanned vehicle comprises main rotor 11 and four auxiliary rotors 123, and this unmanned vehicle adopts Absorbable rod radio material, has evading radar monitoring effect, can perform special duty at Special Areas.Described main rotor 11 adopts coaxial double-rotary wing structure (referring to Fig. 2), by using positive and negative two blades on same axle, turning to of two blades is contrary, and the moment of torsion of generation cancels each other, main rotor 11 is made to have power large, effective and that usefulness degree of utilization is high advantage of hovering.Described four auxiliary rotors 123 are connected with main rotor 11 by horn 121, and the bottom of horn 121 is provided with rotating machine 122, and this rotating machine 122 can drive horn 121 to rotate in the horizontal direction, realize Automatic-expanding and the contraction of auxiliary rotor 123.
The present embodiment is by designing four auxiliary rotor 123 Automatic-expandings and the contraction of unmanned vehicle, unmanned vehicle casing 42 automatically closes or opens, can ensure that unmanned vehicle is after completing patrol monitor task, landing is contracted in casing 42 automatically, carries fast return headquarters by unmanned vehicle.In like manner, also can carry unmanned vehicle by unmanned vehicle and arrive guarded region fast, open unmanned vehicle casing 42 again and discharge unmanned vehicle overhead execution monitor task, whole aerocraft system maneuverability, at utmost can utilize unmanned vehicle effective overhead monitoring period.
One patrol monitoring unmanned vehicle system described in embodiment 1, unmanned vehicle can after unmanned vehicle rises, according to patrol route and unmanned vehicle synchronizing moving, and can according to patrol monitoring requirement, unmanned vehicle flying height is adjusted, rise to effective strategic height, form stable monitoring aerial platform, improve the control efficiency to guarded region.The most important thing is, patrol personnel can carry out border patrol monitoring at headquarters' remotely pilotless aircraft, and patrol monitoring condition obtains and greatly improves.
Schematically above be described the utility model and embodiment thereof, this description does not have restricted, and also just one of the embodiment of the present utility model shown in accompanying drawing, actual structure is not limited thereto.So, if those of ordinary skill in the art enlightens by it, when not departing from the utility model and creating aim, design the frame mode similar to this technical scheme and embodiment without creationary, protection domain of the present utility model all should be belonged to.
Claims (4)
1. a patrol monitoring unmanned vehicle system, it is characterized in that: comprise unmanned vehicle, slip ring motor (21), watch-dog (22) and unmanned vehicle, described unmanned vehicle is connected with the electric power system on unmanned vehicle by cable (3), base (13) is provided with bottom this unmanned vehicle, this base (13) is connected with slip ring motor (21), and the output shaft of described slip ring motor (21) connects watch-dog (22).
2. one patrol monitoring unmanned vehicle system according to claim 1, it is characterized in that: described unmanned vehicle comprises main rotor (11) and auxiliary rotor (123), described main rotor (11) is coaxial double-rotary wing structure, and auxiliary rotor (123) is connected with main rotor (11) by horn (121); The bottom of described horn (121) is provided with rotating machine (122), and this rotating machine (122) drives horn (121) to rotate in the horizontal direction.
3. one patrol monitoring unmanned vehicle system according to claim 1, it is characterized in that: described unmanned vehicle comprises car body (41) and casing (42), casing (42) is arranged on car body (41), the both sides, top of this casing (42) are provided with cover plate (421), and the track (422) that cover plate (421) is laid along casing (42) top closes or opens; The headstock portion of described car body (41) is provided with camera (44), be provided with between headstock and casing (42) and power and communication means (43), this power supply and communication means (43) comprise electric power system and telecommunications base station.
4. the one patrol monitoring unmanned vehicle system according to Claims 2 or 3, is characterized in that: described watch-dog (22) adopts magnetic suspension camera.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520063872.2U CN204415743U (en) | 2015-01-29 | 2015-01-29 | A kind of patrol monitoring unmanned vehicle system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520063872.2U CN204415743U (en) | 2015-01-29 | 2015-01-29 | A kind of patrol monitoring unmanned vehicle system |
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Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105109704A (en) * | 2015-09-02 | 2015-12-02 | 南京国业科技有限公司 | Mooring system based on multi-rotor flight platform |
| CN105187777A (en) * | 2015-08-05 | 2015-12-23 | 广州杰赛科技股份有限公司 | Detection ball, camera recovery method thereof and detection system |
| CN105323445A (en) * | 2015-09-21 | 2016-02-10 | 杭州卓壮科技有限公司 | Magnetic suspension video camera |
| CN106274617A (en) * | 2016-08-26 | 2017-01-04 | 湖南航天远望科技有限公司 | Ship, machine combination monitoring method and monitoring system |
| CN106394382A (en) * | 2015-07-29 | 2017-02-15 | 周坤友 | Intelligent supply base for vehicle-mounted unmanned aircraft |
| CN106892097A (en) * | 2017-03-08 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of vehicle-mounted unmanned aerial vehicle for road condition monitoring |
| CN108367813A (en) * | 2015-12-21 | 2018-08-03 | 艾尔斯考特有限责任公司 | Autonomous docking station for unmanned plane |
| CN109362228A (en) * | 2017-10-31 | 2019-02-19 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle base and unmanned aerial vehicle system |
| CN111292561A (en) * | 2019-12-30 | 2020-06-16 | 中电科芜湖通用航空产业技术研究院有限公司 | Container modularization aerial reconnaissance system |
| CN111650949A (en) * | 2020-06-30 | 2020-09-11 | 深圳高度创新技术有限公司 | Tethered UAV control system and method |
| JP2021181709A (en) * | 2020-05-19 | 2021-11-25 | マツダ株式会社 | Landing and takeoff base apparatus for on-vehicle flight device |
| US11348472B2 (en) | 2020-04-29 | 2022-05-31 | Honeywell International Inc. | System and method to automatically construct a flight plan from a data set for an aerial vehicle |
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2015
- 2015-01-29 CN CN201520063872.2U patent/CN204415743U/en not_active Expired - Fee Related
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106394382A (en) * | 2015-07-29 | 2017-02-15 | 周坤友 | Intelligent supply base for vehicle-mounted unmanned aircraft |
| CN105187777A (en) * | 2015-08-05 | 2015-12-23 | 广州杰赛科技股份有限公司 | Detection ball, camera recovery method thereof and detection system |
| CN105187777B (en) * | 2015-08-05 | 2018-10-19 | 广州杰赛科技股份有限公司 | A kind of detecting ball and its camera recovery method, detecting system |
| CN105109704B (en) * | 2015-09-02 | 2018-06-08 | 南京国业科技有限公司 | A kind of mooring system based on more rotor flying platforms |
| CN105109704A (en) * | 2015-09-02 | 2015-12-02 | 南京国业科技有限公司 | Mooring system based on multi-rotor flight platform |
| CN105323445B (en) * | 2015-09-21 | 2018-08-17 | 杭州觅睿科技有限公司 | Magnetic suspension video camera |
| CN105323445A (en) * | 2015-09-21 | 2016-02-10 | 杭州卓壮科技有限公司 | Magnetic suspension video camera |
| CN108367813A (en) * | 2015-12-21 | 2018-08-03 | 艾尔斯考特有限责任公司 | Autonomous docking station for unmanned plane |
| CN106274617A (en) * | 2016-08-26 | 2017-01-04 | 湖南航天远望科技有限公司 | Ship, machine combination monitoring method and monitoring system |
| CN106274617B (en) * | 2016-08-26 | 2019-01-22 | 湖南航天远望科技有限公司 | Ship, machine combination monitoring method and monitoring system |
| CN106892097A (en) * | 2017-03-08 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of vehicle-mounted unmanned aerial vehicle for road condition monitoring |
| CN106892097B (en) * | 2017-03-08 | 2019-04-30 | 深圳榕亨实业集团有限公司 | A kind of vehicle-mounted unmanned aerial vehicle for road condition monitoring |
| CN109362228A (en) * | 2017-10-31 | 2019-02-19 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle base and unmanned aerial vehicle system |
| CN111292561A (en) * | 2019-12-30 | 2020-06-16 | 中电科芜湖通用航空产业技术研究院有限公司 | Container modularization aerial reconnaissance system |
| US11348472B2 (en) | 2020-04-29 | 2022-05-31 | Honeywell International Inc. | System and method to automatically construct a flight plan from a data set for an aerial vehicle |
| JP2021181709A (en) * | 2020-05-19 | 2021-11-25 | マツダ株式会社 | Landing and takeoff base apparatus for on-vehicle flight device |
| JP7409225B2 (en) | 2020-05-19 | 2024-01-09 | マツダ株式会社 | Vehicle-mounted aircraft launch and landing platform device |
| CN111650949A (en) * | 2020-06-30 | 2020-09-11 | 深圳高度创新技术有限公司 | Tethered UAV control system and method |
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| C14 | Grant of patent or utility model | ||
| 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: 20150624 Termination date: 20170129 |