CN206087325U - Extreme low -altitude remote control flight plant protection of four electronic rotors machine - Google Patents
Extreme low -altitude remote control flight plant protection of four electronic rotors machine Download PDFInfo
- Publication number
- CN206087325U CN206087325U CN201621129446.5U CN201621129446U CN206087325U CN 206087325 U CN206087325 U CN 206087325U CN 201621129446 U CN201621129446 U CN 201621129446U CN 206087325 U CN206087325 U CN 206087325U
- Authority
- CN
- China
- Prior art keywords
- support
- medicine
- chest
- foot rest
- flight
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Catching Or Destruction (AREA)
Abstract
Extreme low -altitude remote control flight plant protection of four electronic rotors machine includes rotor, flight control computer, support, foot rest, motor, medical kit, receives formula spray lance, flight control box, battery to one side, its characterized in that, the support is cross distribution, the tip of support all is provided with the motor, there is the rotor on motor upper portion through the hub connection, the cross middle part that the support formed is provided with the flight control box, the inside flight control computer that is provided with of flight control box, flight control box lower part is provided with battery and medical kit, the battery is located between flight control box and the medical kit, the medical kit is the hemisphere, the foot rest is located the lower part of support, the tip at the support is fixed to the foot rest, the end fixing of receiving the formula spray lance to one side is on the foot rest, the battery is located the medical kit top, the support is fixed on the flight control box, the medical kit is fixed on the foot rest. The utility model relates to a safe, high -efficient, reliable, convenient operation's plant protection unmanned aerial vehicle.
Description
Technical field
This utility model belongs to a kind of aerial pesticide dispersal equipment, the extreme low-altitude remote control distributor plant protection of specially electronic four rotor
Machine.
Background technology
, when plant protection operation is carried out, often because equipment for plant protection volume is larger, transport is inconvenient for existing plant protection unmanned plane.Nobody
Machine flight control system is immature, causes to fall machine situation and happens occasionally, and causes loss of personal property.
Utility model content
The purpose of this utility model is to provide electronic four rotor extreme low-altitude remote control distributor fog machine, is solved in background technology
Problem.
This utility model employs the following technical solutions realization：
The extreme low-altitude remote control distributor fog machine of electronic four rotor, including rotor, flight-control computer, support, foot rest, electricity
Machine, tiltedly medicine-chest, receipts formula spray boom, flight control box, battery, the support is in cross distribution, and the end of the support is respectively provided with
There is motor, the motor top is connected with rotor by axle, and the cross middle part that the support is formed is provided with flight control box,
The flight control box is internally provided with flight-control computer, and the flight control box bottom is provided with battery and medicine-chest, institute
State battery to be located between flight control box and medicine-chest, the medicine-chest is hemispherical, the foot rest is located at the bottom of support, the foot
Frame is fixed on the end of support, and the end of the oblique receipts formula spray boom is fixed on foot rest, is provided with spray on the oblique receipts formula spray boom
Head, the number of the oblique receipts formula spray boom is two, and the oblique receipts formula spray boom is with medicine-chest by pipeline communication, the flight control meter
Calculation machine is electrically connected with motor, and the battery is electrically connected with flight-control computer, and the battery is located at the top of medicine-chest, the support
It is fixed in flight control box, the medicine-chest is fixed on foot rest.
In this utility model, the number of the rotor is four, and four rotors are located in same level, four rotors with
The distance of flight control box is equal, and the angle between adjacent stent is 90 °.
In this utility model, the material of the support and foot rest is contained within the ultralight carbon of high intensity of weight portion percentage ratio 65%
The high-strength engineering plastics of fibrous material, the aviation aluminum of weight portion percentage ratio 30% and weight portion percentage ratio 5%.
In this utility model, the junction of the support and foot rest is provided with Shockproof rubber pad.
In this utility model, the medicine-chest is internally provided with cross dividing plate, and the cross dividing plate is by medicine-chest interior part
Into four parts, on the cross dividing plate, aperture is provided with.
In this utility model, the battery is located in the air between medicine-chest and flight control box.
In this utility model, the oblique receipts formula spray boom is expansion link.
In this utility model, the foot rest is an entirety.
Beneficial effect：This utility model is a kind of safe efficient, reliable, easy to operate plant protection unmanned plane, and this practicality is newly
Type is that on existing market a kind of structure of various unmanned plane kind apoplexy due to endogenous wind is ripe, the four axle plant protection of many rotors of stable performance and convenient manipulation without
It is man-machine.This utility model compact：Spray boom is foldable, and body cantilever arm foldable, battery are directly placed on water tank；This practicality
Novel precision is efficient：Match when water tank flow velocity is with flight boat, manually can be finely adjusted, the spraying swath compared with free-standing nozzle-type type
It is bigger；The fixed high constant speed of this utility model：Plant protection unmanned plane can guarantee that to enter with constant altitude, constant speed by flight control system
Row plant protection operation, further ensures that uniform spray；This utility model is simple to operate, safe and intelligent：Can be advised using self-defined flight path
Flight is drawn, autonomous landing, autonomous flight, a key are maked a return voyage, the continuous spray of breakpoint significantly shortens the unmanned plane training on operation time.
Description of the drawings
Fig. 1 is front view of the present utility model；
Fig. 2 is side view of the present utility model；
Fig. 3 is axonometric chart of the present utility model；
Fig. 4 is top view of the present utility model.
Specific embodiment
In order that technological means, creation characteristic, reached purpose and effect that this utility model is realized are easy to understand, under
Face combines and is specifically illustrating, and this utility model is expanded on further.
Referring to Fig. 1, Fig. 2, Fig. 3, Fig. 4, the front view of the extreme low-altitude remote control distributor fog machine of electronic four rotor, electronic four rotor
The side view of extreme low-altitude remote control distributor fog machine, the axonometric chart of the extreme low-altitude remote control distributor fog machine of electronic four rotor, electronic four rotation
The top view of the extreme low-altitude remote control distributor fog machine of the wing, the extreme low-altitude remote control distributor fog machine of electronic four rotor, including rotor 1, flight
Control computer 2, support 3, foot rest 4, motor 5, medicine-chest 6, formula spray boom 7, flight control box 8, battery 9 are tiltedly received, the support 3 is in
Cross distribution, the end of the support 3 are provided with motor 5, and 5 top of the motor is connected with rotor 1 by axle, described
The cross middle part that frame 3 is formed is provided with flight control box 8, and the flight control box 8 is internally provided with flight-control computer
2,8 bottom of flight control box is provided with battery 9 and medicine-chest 6, and the battery 9 is located between flight control box 8 and medicine-chest 6,
The medicine-chest 6 is hemispherical, and the foot rest 4 is located at the bottom of support 3, and the foot rest 4 is fixed on the end of support 3, described oblique
The end of receipts formula spray boom 7 is fixed on foot rest 4, is provided with shower nozzle on the oblique receipts formula spray boom 7, the oblique receipts formula spray boom 7
Number is two, and with medicine-chest 6 by pipeline communication, the flight-control computer 2 is electrically connected the oblique receipts formula spray boom 7 with motor 5,
The battery 9 is electrically connected with flight-control computer 2, and the material of the support 3 and foot rest 4 is contained within weight portion percentage ratio 65%
The ultralight carbon fibre material of high intensity, the aviation aluminum of weight portion percentage ratio 30% and weight portion percentage ratio 5% high-strength engineering plastics,
The number of the rotor 1 is four, and four rotors 1 are located in same level, the distance of four rotors 1 and flight control box 8
Equal, the angle between adjacent stent 3 is 90 °, and the battery 9 is located at the top of medicine-chest 6, and the support 3 is fixed on flight control
On box 8, the junction of the support 3 and foot rest 4 is provided with Shockproof rubber pad, and the medicine-chest 6 is fixed on foot rest 4, the medicine
Case 6 is internally provided with cross dividing plate, and the cross dividing plate will be divided into four parts, the cross dividing plate inside medicine-chest 6
On be provided with aperture, the battery 9 is located in the air between medicine-chest 6 and flight control box 8, and the oblique receipts formula spray boom 7 is to stretch
Contracting bar, the foot rest 4 are an entirety.
In this utility model, the material 65% of support 3 and foot rest 4 adopts boat using the ultralight carbon fibre material of high intensity, 30%
Empty aluminum, 5% adopt high-strength engineering plastics, high intensity, the material of super light material to widely use and ensure that the safety of aircraft, stablize
Property and cruising time, meet low energy consumption, efficient operation or work standard.
In this utility model, rotor 1 is symmetrically distributed in the four direction around of body, and four rotors 1 are in same
Elevation plane, and the structure and radius of four rotors 1 are all identical, four motors 5 are symmetrically installed on the end of the support 3 of aircraft
Flight-control computer 2 and external equipment are put in portion, 3 intermediate space of support.
In this utility model, flight control is effectively prevented in special box body by flight-control computer 2 independently installed
Computer processed 2 is affected by bad external environment（Such as：Pesticide, magnetic field etc.）, safety during actual job is increased, is protected
Flight-control computer 2, greatly reduces maintenance cost, effectively avoid due to flight-control computer 2 be damaged it is out of control and
The accident for causing.
In this utility model, foot rest 4 is fabricated to into overall structure, is installed on four supports 3 of aircraft, that is, has dissipated by electricity
The vibrations that machine is produced, also increase aircraft overall construction intensity and stability, reduce due to falling machine to a certain extent and make
Damage into body, extend the service life of aircraft.In addition foot rest 4 is lined with Shockproof rubber pad with 3 junction of support, makes foot rest 4
Be connected with support 3 and more fasten, and play antihunt action, aircraft landing has been buffered instantaneously in the face of the impact of aircraft.
In this utility model, the medicine-chest 6 is fixed on foot rest 4, and 6 fixed form of medicine-chest of fog machine is crucial, aircraft
Main by weight concentrate on the load of medicine-chest 6 and the inside, the bearing capacity that mode can guarantee that aircraft is firmly fixed, can make again
The center of gravity of aircraft is at center all the time, reduces the power consumption produced to keep aircraft steady, extends cruising time.
In this utility model, 10 kilograms of operation medication in medicine-chest 6, is loaded with, shake can be produced in rocking for flight course Chinese medicine
It is dynamic, arrange in medicine-chest 6 and on cross partition, and dividing plate, be installed with several apertures, medicine-chest 6 is divided into into four parts, each several part
Between connected by aperture, be effectively prevented the vibrations of medicine, and can play a part of to strengthen 6 structural strength of medicine-chest.
In this utility model, the battery 9 is located at the top of medicine-chest 6, and battery 9 provides energy for aircraft, and itself can produce heat
Amount, battery 9 is placed on medicine-chest 6, makes battery 9 in air, and aircraft can produce wind in flight course, dissipate beneficial to battery 9
Heat；Using DC source, battery 9 can produce magnetic field in power supply process, using the structure, away from flight-control computer 2,
Interference of the magnetic field to flight-control computer 2 is prevented.
In this utility model, tiltedly receipts formula spray boom 7 is longer, and spraying swath is bigger, and working area is also wider, but long spray boom can increase
Plus the overall dimensions of aircraft be inconvenient to transport, also inconvenience farmland operation.Using formula structure is tiltedly received, aircraft is made to ensure that foot
Enough big spraying swaths, while spray boom is accepted rear aircraft overall dimensions reducing, facilitate transport.
In this utility model, flight-control computer 2 is the brain of aircraft, and adjustment flight attitude is played in flight course,
Make aircraft that horizontal level is automatically adjusted in flight course, even if the external environmental interferences such as crosswind are run in operation, also can
Keep stable to fly forward not having deflection.Make flight more controllable, it is safer.
This utility model have developed nobody that meet extreme low-altitude agricultural plant protection job requirements premised on agricultural plant protection application
Machine flight control system.Intend, based on inverse optimal theoretical, proposing the inverse optimal control method based on small-sized multi-rotor unmanned aerial vehicle.Design
Amplitude and speed saturation function, elimination amplitude bring hydraulic performance decline even wild effect with speed saturation to control system.Build
Vertical fault model, proposes ART network unknown failure information.Simultaneously in model uncertainty, extra interference, input saturation and
Under the failure condition of generation, based on Lyapunov functions proof system when these situations occur, remain to make system reach stably
Purpose.
Ultimate principle of the present utility model and principal character and advantage of the present utility model, one's own profession has been shown and described above
The technical staff of industry it should be appreciated that this utility model is not restricted to the described embodiments, described in above-described embodiment and description
Simply illustrate principle of the present utility model, on the premise of without departing from this utility model spirit and scope, this utility model is also
Various changes and modifications are had, these changes and improvements are both fallen within the range of claimed this utility model, this utility model
Claimed scope is by appending claims and its equivalent thereof.
Claims (8)
1. the extreme low-altitude remote control distributor fog machine of electronic four rotor, including rotor, flight-control computer, support, foot rest, motor,
Medicine-chest, tiltedly receive formula spray boom, flight control box, battery, it is characterised in that the support is in cross distribution, the end of the support
Portion is provided with motor, and the motor top is connected with rotor by axle, and the cross middle part that the support is formed is provided with winged
Row control box, the flight control box are internally provided with flight-control computer, and the flight control box bottom is provided with battery
And medicine-chest, positioned between flight control box and medicine-chest, the medicine-chest is hemispherical for the battery, and the foot rest is located under support
Portion, the foot rest are fixed on the end of support, and the end of the oblique receipts formula spray boom is fixed on foot rest, on the oblique receipts formula spray boom
Shower nozzle is provided with, the number of the oblique receipts formula spray boom is two, and the oblique receipts formula spray boom passes through pipeline communication with medicine-chest, described to fly
Row control computer is electrically connected with motor, and the battery is electrically connected with flight-control computer, and the battery is located at the top of medicine-chest,
The support is fixed in flight control box, and the medicine-chest is fixed on foot rest.
2. the extreme low-altitude remote control distributor fog machine of electronic four rotor according to claim 1, it is characterised in that the rotor
Number is four, and four rotors are located in same level, and four rotors are equal with the distance of flight control box, adjacent stent it
Between angle be 90 °.
3. the extreme low-altitude remote control distributor fog machine of electronic four rotor according to claim 1, it is characterised in that the support and
The material of foot rest is contained within the ultralight carbon fibre material of high intensity of weight portion percentage ratio 65%, the aviation aluminum of weight portion percentage ratio 30%
With the high-strength engineering plastics of weight portion percentage ratio 5%.
4. the extreme low-altitude remote control distributor fog machine of electronic four rotor according to claim 1, it is characterised in that the support and
The junction of foot rest is provided with Shockproof rubber pad.
5. the extreme low-altitude remote control distributor fog machine of electronic four rotor according to claim 1, it is characterised in that in the medicine-chest
Portion is provided with cross dividing plate, and the cross dividing plate will be divided into four parts inside medicine-chest, arranges on the cross dividing plate
There is aperture.
6. the extreme low-altitude remote control distributor fog machine of electronic four rotor according to claim 1, it is characterised in that the battery position
In air between medicine-chest and flight control box.
7. the extreme low-altitude remote control distributor fog machine of electronic four rotor according to claim 1, it is characterised in that the oblique receipts formula
Spray boom is expansion link.
8. the extreme low-altitude remote control distributor fog machine of electronic four rotor according to claim 1, it is characterised in that the foot rest is
One entirety.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621129446.5U CN206087325U (en) | 2016-10-17 | 2016-10-17 | Extreme low -altitude remote control flight plant protection of four electronic rotors machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621129446.5U CN206087325U (en) | 2016-10-17 | 2016-10-17 | Extreme low -altitude remote control flight plant protection of four electronic rotors machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206087325U true CN206087325U (en) | 2017-04-12 |
Family
ID=58483497
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621129446.5U Active CN206087325U (en) | 2016-10-17 | 2016-10-17 | Extreme low -altitude remote control flight plant protection of four electronic rotors machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206087325U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106976563A (en) * | 2017-04-27 | 2017-07-25 | 峨眉山市博派乐无人机科技有限公司 | Pesticide spraying unmanned plane |
| CN108094379A (en) * | 2017-12-26 | 2018-06-01 | 燕山大学 | A kind of fog machine and its paths planning method for being used to perform agriculture automatic spraying task |
-
2016
- 2016-10-17 CN CN201621129446.5U patent/CN206087325U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106976563A (en) * | 2017-04-27 | 2017-07-25 | 峨眉山市博派乐无人机科技有限公司 | Pesticide spraying unmanned plane |
| CN108094379A (en) * | 2017-12-26 | 2018-06-01 | 燕山大学 | A kind of fog machine and its paths planning method for being used to perform agriculture automatic spraying task |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103274042B (en) | A kind of floated driven helicopter | |
| CN203222114U (en) | Electric small-sized unmanned helicopter for spraying pesticide | |
| CN104986335A (en) | Long-endurance heavy-load oil-drive direct-driven agricultural plant protection unmanned aerial vehicle | |
| CN104875888A (en) | Detachable ring-pillar type hollow unmanned aerial vehicle and operation method thereof | |
| CN203612209U (en) | Agricultural aircraft | |
| CN206087325U (en) | Extreme low -altitude remote control flight plant protection of four electronic rotors machine | |
| CN104590555A (en) | Electrodynamic multi-rotor helicopter | |
| CN108284949B (en) | Foldable staggered six-rotor aircraft | |
| CN109896003A (en) | A kind of VTOL is verted three rotor wing unmanned aerial vehicles | |
| CN203544370U (en) | Agricultural multi-rotor unmanned helicopter | |
| CN202711065U (en) | Ducted fan unmanned plane | |
| CN207157497U (en) | A kind of agricultural plant protection controls culvert type unmanned plane with rudder face | |
| CN112722289A (en) | Self-rotary wing aircraft combined with multi-shaft rotor wing | |
| CN206087323U (en) | Many rotors plant protection unmanned aerial vehicle | |
| CN108583867A (en) | A kind of three ducted fan bionic Aircraft of torque self-balancing | |
| CN205239919U (en) | A explosive barrel combined type duct for having more unmanned plant protection of rotor machine | |
| CN111392030A (en) | Retractable angle-adjustable helicopter short wing | |
| CN207985205U (en) | A kind of six axis encircling types folding fog machine | |
| CN110714879A (en) | Liftable wind power generation device capable of automatically adjusting high altitude and keeping relative position | |
| CN202666408U (en) | Six-arm model aerial propeller | |
| CN209600800U (en) | A kind of VTOL is verted three rotor wing unmanned aerial vehicles | |
| CN105818970B (en) | A kind of unmanned paint spraying machine in high-altitude | |
| CN104843191A (en) | Non-contact type intelligent rainproof device for unmanned aerial vehicle | |
| CN201086824Y (en) | Dish shaped aircraft | |
| CN108557067A (en) | A kind of nothing is risen and fallen posture small drone |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |