CN107914876A - A kind of combined system of aerostatics unmanned plane - Google Patents
A kind of combined system of aerostatics unmanned plane Download PDFInfo
- Publication number
- CN107914876A CN107914876A CN201711245414.0A CN201711245414A CN107914876A CN 107914876 A CN107914876 A CN 107914876A CN 201711245414 A CN201711245414 A CN 201711245414A CN 107914876 A CN107914876 A CN 107914876A
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- China
- Prior art keywords
- unmanned plane
- gondola
- aerostatics
- connecting rod
- hose
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/022—Tethered aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The present invention provides a kind of aerostatics unmanned plane combined system, and aerostatics is parent, provides corresponding support in the air for operation unmanned plane.The power-supply system that unmanned plane electric system is carried by aerostatics provides, and power-supply system can allow rotor wing unmanned aerial vehicle to stop for a long time in the air.Aerostatics can also carry the equipment such as flow container according to job requirements.Unmanned plane performs pesticide spraying when task, and unmanned plane need not land dressing repeatedly.When flight is not required in unmanned plane, can reversely it be shut down in aerostatics airplane parking area, unmanned plane energy free consumption during shutdown.Whole system greatly improves the work capacity and operating efficiency of rotor wing unmanned aerial vehicle.
Description
Technical field
The invention belongs to vehicle technology field, and in particular to a kind of aerostatics unmanned plane.
Background technology
Rotor wing unmanned aerial vehicle lift fully relies on rotor motor and drives rotor blade to provide, and energy consumption is big, can not be competent at for a long time
Aerial work.Operation of either taking photo by plane still performs large area pesticide spraying, its activity duration is all shorter.
Most of current designing scheme for improving rotor wing unmanned aerial vehicle cruising ability is that what is relied on is the increase of battery capacity, but
It is that battery capacity increases so that the heavy burden of unmanned plane becomes larger, and use high energy efficiency high density battery, cost is added, and can
The effect and unobvious played.
Unmanned plane perform plant protection task when, for needs spray insecticide etc. work when, since its load is limited, take
Band dose is limited, therefore spraying range is smaller every time, many subjobs.
General rotor wing unmanned aerial vehicle completes all kinds of work, in addition to dead weight, it is also necessary to relevant device is carried, from working continuously
From the point of view of ability, no matter rotor wing unmanned aerial vehicle possesses great heavy burden ability, its weight of equipment carried has very big limitation, limits
The performance of its effect.
The content of the invention
The present invention solves the problems, such as be in the prior art for rotor wing unmanned aerial vehicle execution flight operation when cruising ability extremely
Limited, manipulator needs to carry polylith battery when working continuously, and unmanned plane needs landing to change battery；Unmanned plane carries medicine
Plant protection is carried out when task, its band dose is very low, and each job area is limited.
To solve the above problems, the present invention provides a kind of aerostatics unmanned plane combined system, the system can allow rotor nobody
Machine stops for a long time in the air, and the power-supply system that unmanned plane electric system is carried by aerostatics provides, and power-supply system is except on ground
Face can also utilize the solar panels of aerostatics upper surface to charge to storage battery full of outside.Except power-supply system, aerostatics may be used also
According to job requirements, to carry the equipment such as flow container, when unmanned plane performs pesticide spraying when task, unmanned plane need not land；
When flight is not required in rotor wing unmanned aerial vehicle, can reversely it be shut down in aerostatics airplane parking area, unmanned plane energy free consumption during shutdown.Nobody
Machine fuselage can not carry battery, by cable power supply, reduce flight dead weight, can carry more plug-in devices.Due to flow container not
On unmanned aerial vehicle body, so unmanned plane heavy burden is relatively low, and aerostatics can carry the flow container of weight bigger, and unmanned plane performs
It can work for a long time in a wider context during pesticide spraying task, whole system greatly improves the work of rotor wing unmanned aerial vehicle
Industry ability and operating efficiency.
The present invention is divided into five parts and forms, and is aerostat system, power control system, shutdown system, cable respectively
Storage system and plug-in flow container system.
Aerostat system includes utricule, lifting controller, propeller, flow container chamber, connecting rod, gondola, gondola and shuts down suction
Disk.
Further, utricule is connected with gondola by connecting rod, can be connected up inside connecting rod, it is right that lifting controller passes through
The control of balloonet air capacity inside utricule, changes buoyancy size, realizes the rising and landing of integral device, propeller is by installing
Multiple blades in utricule side form, and make aerostatics steadily hovering, and can change aerostatics hovering position, outside gondola
Shell lower surface installation gondola shuts down sucker.
Power control system includes solar panels, charging cable, power transmission cable, charging-discharging controller and storage battery.
Further, solar panels are installed on utricule upper surface, can convert the solar into electric energy；Charging cable is by connecting
Extension bar is connected with the storage battery in gondola；Storage battery is installed on gondola internal upper part, its output terminal connection power transmission cable；Power transmission cable
Stored by the cable collection drum of lower part in gondola, the cable other end is connected with unmanned plane, is directly provided for rotor wing unmanned aerial vehicle flight
Electric power, charging-discharging controller manage the input and output of electric energy.
Shutdown system includes unmanned plane and shuts down connecting rod, unmanned plane shutdown sucker.
Further, connecting rod boring is shut down, lower end is installed on unmanned plane block upper surface, and upper end installation unmanned plane stops
Machine sucker, after completing installation, small end exceeds unmanned plane rotor blade height, is higher than rotor blade position shutting down connecting rod side
Cable hole is installed, for line arrangements such as cable and liquid hoses；It is electromagnet that gondola, which shuts down sucker, and when energization, which produces, inhales
Power, it is ferromagnetism material that unmanned plane, which shuts down sucker, and when gondola shuts down sucker energization work, unmanned plane shuts down sucker can be with gondola
Shut down sucker to be attracted, unmanned plane shuts down sucker and shuts down sucker mating reaction with gondola, when enabling rotor wing unmanned aerial vehicle idle
It is enough to be shut down below gondola.
Cable storage system includes cable collection drum, hose collection drum, line concentration motor, shaft, storage controller.
Further, cable collection drum, hose collection drum are coaxially connected by shaft, and line concentration motor output end is another for shaft
One end, storage controller control motor steering and speed realize the draw-in and draw-off function to cable, cable collection drum, hose collection drum,
Line concentration motor, shaft and storage controller are installed on lower part in gondola.
Plug-in flow container system includes fluid reservoir, hose, decides whether to use according to the task that aerostatics unmanned plane performs.
Further, fluid reservoir is installed on the flow container intracavitary of aerostatics, hose one end connection fluid reservoir, and the other end passes through company
Extension bar wire location enters gondola, is stored by hose collection drum, and the cable hole access nothing on connecting rod is shut down by unmanned plane
Mouth spray on man-machine.
Unmanned plane is directly powered by power transmission cable, it is not necessary to carries battery, power transmission cable connection rotor motor, rotor motor
Rotor blade rotation is driven, lift and power is provided for unmanned plane, mouth spray is set below each rotor motor of unmanned plane, is performed
Connection flexible pipe during hydrojet task, the liquid such as spray insecticide, carries plug-in device below unmanned plane, can carry video camera etc. and takes photo by plane and sets
It is standby.
The present invention is described in further details below with reference to attached drawing.
Brief description of the drawings
Fig. 1 aerostatics unmanned plane combined system schematic diagrames.
Fig. 2 power control system schematic diagrames.
Fig. 3 gondolas airplane parking area schematic diagram.
Fig. 4 unmanned plane schematic diagrames.
Fig. 5 unmanned planes reversely shut down schematic diagram in the air.
Fig. 6 line outlet line concentration schematic diagrams.
Embodiment
A kind of combined system by aerostatics, the common cooperating of unmanned plane of present invention offer, reference view, including 1
Aerostatics, 2 power control systems, 3 shutdown systems, 4 cable storage systems, 5 plug-in flow container systems, 6 unmanned planes, 11 utricules, 12
Propeller, 13 flow container chambers, 14 gondolas, 15 gondolas shut down sucker, 16 lifting controllers, 17 connecting rods, 21 solar panels, 22 chargings
Cable, 23 power transmission cables, 24 charging-discharging controllers, 25 storage batteries, 31 unmanned planes shut down connecting rod, 32 unmanned planes shut down sucker, 33
Cable hole, 41 cable collection drums, 42 hose collection drums, 43 line concentration motors, 44 shafts, 45 storage controllers, 46, line outlet, 51
Fluid reservoir, 52 hoses, 61 rotors, 62 mouth sprays, 63 plug-in devices.
In specific implementation, aerostatics 1 includes utricule 11, propeller 12, flow container chamber 13, gondola 14, gondola shutdown suction
Disk 15, lifting controller 16, connecting rod 17, aerostatics 1 are used as parent, carry all devices lift-off and landing.11 main gas of utricule
Capsule is filled with inert gas helium, and balloonet is interior to control air capacity by air valve, and balloonet is filled with the change of air bag global density
Greatly, buoyancy reduces；Balloonet releases air bag global density and diminishes, buoyancy increase；Utricule passes through connecting rod 17 with gondola 14
Connection；Space is left inside connecting rod 17 to be connected up；Lifting controller 16 is installed in gondola, can be to 11 inside gas of utricule
The scale of construction is controlled, and then adjusts the size of lift, realizes the rising and landing of integral device；Propeller 12 is by installed in utricule
Multiple rotors composition of 11 sides, has an air-flow due to aerial, and the effect of propeller 12 is to provide opposite with aerial airflow direction
Power, prevents that aerostatics 1 is out of control in the air, and can change 1 hovering position of aerostatics；Flow container chamber 13 is installed in utricule 11
Center, it is ensured that overall stress balance, when task is sprayed insecticide in execution, flow container chamber 13 is stored in pesticide, by hose 52, soft
Pipe collection drum 42 is connected with unmanned plane mouth spray 62；14 shell lower surface of gondola installation gondola shuts down sucker 15, and gondola, which is shut down, to be inhaled
Disk 15 and unmanned plane shut down 32 mating reaction of sucker, realize that unmanned plane 6 is reversely shut down below gondola idle when.
Power control system 2 provides the electric power of all devices such as unmanned plane 6, cable storage system 4, propeller 12, including
Solar panels 21, charging cable 22, power transmission cable 23, charging-discharging controller 24, storage battery 25.Solar panels 21 are installed on capsule
11 upper surface of body, can convert the solar into electric energy, and electric energy is stored in storage battery 25 by charging cable 22；Charging electricity
Cable 22 is routed in inside connecting rod 17；Storage battery 25 is installed on 14 internal upper part of gondola, its output terminal connection power transmission cable 23；Transmission of electricity
Cable 23 is stored by the cable collection drum 41 of lower part in gondola 14, and 23 other end of power transmission cable is connected with unmanned plane 6, is unmanned plane
6 flights directly provide electric power；Charging-discharging controller 24 manages the input and output of electric energy；Remaining of the present invention needs electrical equipment
Powered by the output terminal of storage battery 25.
Shutdown system 3 includes unmanned plane and shuts down connecting rod 31, unmanned plane shutdown sucker 32, cable hole 33, and wherein gondola is shut down
The also mating reaction in shutdown system of sucker 15, it be electromagnet that gondola, which shuts down sucker 15, and when energization produces suction, unmanned plane shutdown
Sucker 32 is ferromagnetism material, and when gondola shuts down 15 energization work of sucker, unmanned plane, which is shut down sucker 32 and can be shut down with gondola, to be inhaled
Disk 15 is attracted；Unmanned plane is shut down connecting rod 31 and is installed on directly over the unmanned plane longitudinal axis, and one end is connected with unmanned aerial vehicle body, other end peace
Fill unmanned plane and shut down sucker 32, unmanned plane shuts down 31 boring of connecting rod, and shutting down 31 side of connecting rod in unmanned plane is higher than rotor 61
Position sets cable hole, and for power transmission cable 23 and the grade line arrangement of hose 52, after completing installation, small end exceeds unmanned plane
Rotor blade height；When unmanned plane 6 prepares aerial reversely shutdown, slowly fly to gondola to shut down near sucker 15 first, treat cable
After storage system 4 completes work, unmanned plane 6 flies to gondola to shut down immediately below sucker 15, and slowly rises, and shuts down and inhales when unmanned plane
After disk 32 is contacted with gondola shutdown sucker 15, gondola shuts down the energization of sucker 15 and produces suction, and unmanned plane is firmly inhaled in gondola 14
Lower section, completes shutdown action, and unmanned plane is without energy consumption during this state.
Cable storage system 4 includes cable collection drum 41, hose collection drum 42, line concentration motor 43, shaft 44, storage control
Device 45 processed, line outlet 46, as shown in Fig. 2, cable collection drum 41, hose collection drum 42, line concentration motor 43, shaft 44 and storage
Controller 45 is installed on lower part in gondola, and line outlet 46 is on gondola shell wall；Wherein cable collection drum 41, hose collection drum 42
It is co-axially mounted, line concentration motor 43 drives cable collection drum 41,42 synchronous rotary of hose collection drum by shaft 44, at line outlet 46
Equipped with hub, its line concentration mode by hose 52 and power transmission cable 23 by hub as shown in fig. 6, can be separately directed to hose
Collect on drum 42 and cable collection drum 41, and can weaken hose 52 at the same time and frictional resistance when power transmission cable 23 passes in and out gondola,
The storage control line concentration of controller 45 motor 43 turns to and speed, realizes the folding and unfolding action to cable and the control of folding and unfolding speed.
Plug-in flow container system 5 includes fluid reservoir 51, hose 52, is decided whether according to the task that aerostatics unmanned plane performs
Use.Fluid reservoir 51 is installed in the flow container chamber 13 of aerostatics, and 52 one end of hose connection fluid reservoir 13, the other end passes through connecting rod
17 enter gondola 14, are then stored by hose collection drum 42, and the cable on connecting rod 31 is shut down through line outlet 46 and unmanned plane
Hole 33, accesses mouth spray 62 finally by 6 internal wiring of unmanned plane, performs hydrojet task.
Unmanned plane 6 is directly powered by power transmission cable 23, it is not necessary to carries battery, power transmission cable 23 connects rotor motor, rotation
Wing motor drives rotor 61 to rotate, and provides lift and power for unmanned plane 6, mouth spray is set below each rotor motor of unmanned plane
62, connection flexible pipe 52 when performing hydrojet task, sprays insecticide and waits liquid, and carrying plug-in device 63, can carry and take the photograph below unmanned plane
Camera etc. is taken photo by plane equipment.
In specific implementation, the present invention is first on the ground near transport to the task of execution place, and bag is carried out on ground
Include the preparations such as storage battery charging, utricule inflation.
Further, during takeoff and landing of the present invention, unmanned plane 6 is reversely shut down below gondola 14, and propeller 12 starts
Work, when combined system is integrally transported to assignment task by aerostatics, and whole combined system is in stable state, nobody
Machine 6 is started shooting, and starts to perform inter-related task.
Further, when aerostatics 1 takes off, lifting controller 16 is by controlling air valve in balloonet to reduce the pair of utricule 11
Air capacity in air bag, balloonet extraction air, air bag global density diminish, buoyancy increase, when buoyancy is more than combined system
During overall weight, combined system rises；After reaching specified altitude assignment, lifting controller 16 is by controlling air valve in balloonet to increase
Air capacity in 11 balloonet of utricule, balloonet are filled with air, and air bag global density becomes larger, and buoyancy reduces, and combined system rises
When buoyancy is decreased to identical with combined system entirety gravity, combined system highly remains unchanged at this time；Since the difference in high-altitude is made
Industry ambient wind influences also to be not quite similar, and provides the power opposite with wind-force by propeller 12 at this time so that whole system dynamic
Stablize specified altitude assignment in the air, complete the take-off process of combined system at this time；When combined system needs to carry out displacement in the air,
Propeller 12 can provide power.
Further, when aerostatics 1 lands, lifting controller 16 is by controlling air valve in balloonet to increase the pair of utricule 11
Air capacity in air bag, balloonet are filled with air, and air bag global density becomes larger, and buoyancy reduces, when buoyancy is less than combined system
During overall gravity, combined system declines, and the air capacity of balloonet need to be slowly varying in utricule 11 during decline, it is ensured that combination system
System slowly declines, and at the same time, propeller 12 need to work at the same time, and combined system is in one and stablizes relatively during guarantee declines
Spatial domain, prevent decline when due to close propeller 12, wind-force produce negative effect it is excessive.
In specific implementation, if combined system performs generic task of taking photo by plane, aerostatics 1 need not carry plug-in flow container system 5, i.e.,
Fluid reservoir 51, hose 52 need not be carried, the overall circuit of combined system need to only arrange cable.The task of taking photo by plane starts from aerostatics
1 take-off process terminates, i.e., combined system stable suspersion is at designated flying zone.Charging-discharging controller 24 works at this time, storage battery 25
Powered by power transmission cable for unmanned plane 6,6 rotor 61 of unmanned plane starts, and when lift is close to unmanned plane self gravitation, gondola stops
Machine sucker 15 powers off, and suction disappears, and unmanned plane 6 departs from aerostatics gondola airplane parking area, and cable storage system 4 works at this time, stores
Controller 45 controls line concentration motor 43 to rotate forward, and cable collection drum 41 rotates forward, and promotes power transmission cable 23 to elongate, and coordinates nothing
Man-machine 6 fly away from aerostatics 1, and provide 6 flight electric power of unmanned plane and electric power of taking photo by plane, and unmanned plane 6 starts to perform various classes times of taking photo by plane
Business.
Further, unmanned plane 6 has performed task, or when need not temporarily perform task, it can be under gondola 14
Fang Fanxiang is shut down.When unmanned plane 6 need to be from working status convert to static state, first, unmanned plane 6 moves closer to aerostatics 1, this
When cable storage system 4 change working method, storage controller 45 controls line concentration motor 43 to reversely rotate, and cable collection drum 41 is anti-
To rotation, power transmission cable 23 is promoted to shorten；Afterwards, unmanned plane 6 flies to gondola and shuts down 32 position directly below of sucker, treats that cable is stored
After system 4 stores cable, unmanned plane 6 continues to rise, and unmanned plane is shut down sucker 32 and is contacted with gondola shutdown sucker 15,
Finally, sucker is powered, and produces suction, 6 reverse adsorption of unmanned plane is below gondola；Rotor 61 is shut down, at this time plug-in equipment of taking photo by plane
It can decide whether to work on as needed.
In specific implementation, if combined system performs fixed-area short period pesticide spraying generic task, aerostatics 1 need to be taken
With plug-in flow container system 5, i.e., fluid reservoir 51, hose 52 need to be carried, the overall circuit of combined system need to arrange cable and hose
52.Liquid in fluid reservoir 51 is transferred to unmanned plane mouth spray 62 by hose 52；Cable and solar panels 21 can not be arranged at this time,
Aerostatics 1 carries a small amount of storage battery and provides energy for propeller 12, each quasi-controller, electromagnet etc., and unmanned plane plug-in device is taken
Charged pool, there is provided electric power needed for itself flight, unmanned plane 6 fly away from aerostatics 1 using the mode identical with aforesaid way and perform spray
Spill task or reversely shut down close to gondola 14, because combined system is furnished with plug-in flow container system, unmanned plane 6 is without voluntarily carrying
Flow container, mitigates and bears a heavy burden, the long period can fly and spray insecticide for a long time.
In specific implementation, if combined system needs to perform pest and disease monitoring, preventing and controlling for a long time, both carrying was needed to take photo by plane
Monitoring of equipment crop growth situation, and need to spray insecticide to prevent pest and disease damage from spreading, or monitoring medication effect, at this time can be by electricity
Source control system 2 and plug-in flow container system 5 carry at the same time, aerostatics 1 take off landing working method it is same as described above, unmanned plane 6
Fly away from 1 execution task of aerostatics and 14 reverse halt mode of close gondola is same as described above, unmanned plane is performing related appoint
Video camera is installed at plug-in device 63 during business, mouth spray 62 is responsible for the sprinkling of the liquid such as pesticide.
In specific implementation, unmanned plane shuts down 31 height of connecting rod and obtains length decision, i.e. basis according to institute's band cable and hose
Its flying radius determines that unmanned plane shuts down connecting rod 31 and proper height is adjusted to before ground is taken off, it is ensured that line during unmanned plane during flying
Cable will not be touched with rotor blade.
Claims (7)
1. a kind of hydrojet combined system of aerostatics unmanned plane, it is characterised in that including aerostatics（1）, shutdown system（3）, cable
Line storage system（4）, plug-in flow container system（5）, unmanned plane（6）；Aerostatics（1）The lift of combined system, including utricule are provided
（11）, propeller（12）, gondola（14）, gondola shut down sucker（15）, lifting controller（16）, connecting rod（17）, utricule（11）
In main gasbag in be full of helium, the air valve of balloonet is by lifting controller（16）Control air disengaging, propeller（12）
Utricule side arrangement is installed, gondola（14）Pass through connecting rod（17）It is connected with utricule, connecting rod（17）It is internally provided with wiring space,
Gondola（14）Shell lower surface center installation gondola shuts down sucker（15）, gondola shutdown sucker（15）For electromagnet, it is powered
When sucker can to ferromagnetic material produce suction；Shutdown system（3）Realize unmanned plane（6）Reversely shut down, including unmanned plane is shut down
Connecting rod（31）, unmanned plane shut down sucker（32）, cable hole（33）, unmanned plane shutdown connecting rod（31）Installed in unmanned plane（6）The longitudinal axis
Surface, one end and unmanned plane（6）Fuselage is connected, and other end installation unmanned plane shuts down sucker（32）, unmanned plane shutdown connecting rod
（31）Side is higher than rotor（61）Position sets cable hole, and unmanned plane shuts down connecting rod（31）Upper end exceeds unmanned plane rotor blade height
Degree；Cable storage system（4）Control hose（52）Folding and unfolding length, including hose collection drum（42）, line concentration motor（43）, shaft
（44）, storage controller（45）, line outlet（46）, hub（47）, hose collection drum（42）, line concentration motor（43）, shaft
（44）With storage controller（45）Installed in gondola（14）Interior lower part, line outlet（46）On gondola shell wall, hub（47）
Installed in line outlet, line concentration motor（43）Pass through shaft（44）Drive hose collection drum（42）Rotation, to realize hose（52）
Folding and unfolding；Plug-in flow container system（5）Including fluid reservoir（51）, hose（52）, fluid reservoir（51）Installed in the flow container chamber of aerostatics
（13）It is interior, hose（52）One end connects fluid reservoir（13）, the other end passes through connecting rod（17）Into gondola（14）, then by soft
Pipe collection drum（42）Storage, through hub（47）Through line outlet（46）Then pass through cable hole（33）, finally by unmanned plane
（6）Internal wiring accesses mouth spray（62）, realize liquid spraying function；Unmanned plane（6）For rotor wing unmanned aerial vehicle, including rotor（61）, spray
Liquid mouth（62）And battery, mouth spray（62）Below unmanned plane rotor motor.
2. hydrojet combined system as claimed in claim 1, it is characterised in that unmanned plane shuts down sucker（32）For ferromagnetism material,
Including but not limited to iron, chromium or nickel.
3. hydrojet combined system as claimed in claim 1, it is characterised in that propeller（12）With utricule（11）Central symmetry is pacified
Dress, its quantity are 4,8,12 or 16.
4. hydrojet combined system as claimed in claim 1, it is characterised in that hose uses watertight plastic material.
5. hydrojet combined system as claimed in claim 1, it is characterised in that utricule（11）The number of middle balloonet is 1 or 2
It is a.
6. hydrojet combined system as claimed in claim 1, it is characterised in that gondola（14）For titanium-aluminium alloy material.
7. hydrojet combined system as claimed in claim 1, it is characterised in that the rotor number of unmanned plane is 4,6 or 8.
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| CN201711245414.0A CN107914876A (en) | 2017-12-01 | 2017-12-01 | A kind of combined system of aerostatics unmanned plane |
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| CN201711245414.0A CN107914876A (en) | 2017-12-01 | 2017-12-01 | A kind of combined system of aerostatics unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2788553C1 (en) * | 2022-10-28 | 2023-01-23 | Федеральное государственное казенное образовательное учреждение высшего образования "Московский пограничный институт Федеральной службы безопасности Российской Федерации" | Unmanned ground surface monitoring system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102897311A (en) * | 2012-10-29 | 2013-01-30 | 中国科学院光电研究院 | Overpressure dish-shaped buoyancy lifting integral aircraft |
| US20140021288A1 (en) * | 2012-07-20 | 2014-01-23 | Andrew Charles Elson | Unmanned aerial vehicle and method of launching |
| CN105539852A (en) * | 2016-02-19 | 2016-05-04 | 蒋引 | Multi-rotor UAV (unmanned aerial vehicle) as well as control system and method thereof |
| CN206012932U (en) * | 2016-08-02 | 2017-03-15 | 张莱 | The combination aircraft that a kind of dirigible and unmanned plane are combined |
| CN206351780U (en) * | 2016-12-02 | 2017-07-25 | 北京化工大学 | A kind of unmanned plane aircraft carrier based on earth station and helium balloon |
-
2017
- 2017-12-01 CN CN201711245414.0A patent/CN107914876A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140021288A1 (en) * | 2012-07-20 | 2014-01-23 | Andrew Charles Elson | Unmanned aerial vehicle and method of launching |
| CN102897311A (en) * | 2012-10-29 | 2013-01-30 | 中国科学院光电研究院 | Overpressure dish-shaped buoyancy lifting integral aircraft |
| CN105539852A (en) * | 2016-02-19 | 2016-05-04 | 蒋引 | Multi-rotor UAV (unmanned aerial vehicle) as well as control system and method thereof |
| CN206012932U (en) * | 2016-08-02 | 2017-03-15 | 张莱 | The combination aircraft that a kind of dirigible and unmanned plane are combined |
| CN206351780U (en) * | 2016-12-02 | 2017-07-25 | 北京化工大学 | A kind of unmanned plane aircraft carrier based on earth station and helium balloon |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| RU2788553C1 (en) * | 2022-10-28 | 2023-01-23 | Федеральное государственное казенное образовательное учреждение высшего образования "Московский пограничный институт Федеральной службы безопасности Российской Федерации" | Unmanned ground surface monitoring system |
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