CN106976563A - Pesticide spraying unmanned plane - Google Patents
Pesticide spraying unmanned plane Download PDFInfo
- Publication number
- CN106976563A CN106976563A CN201710285392.4A CN201710285392A CN106976563A CN 106976563 A CN106976563 A CN 106976563A CN 201710285392 A CN201710285392 A CN 201710285392A CN 106976563 A CN106976563 A CN 106976563A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- unmanned plane
- pesticide spraying
- spraying unmanned
- plane according
- 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.)
- Pending
Links
- 239000000575 pesticide Substances 0.000 title claims abstract description 20
- 238000005507 spraying Methods 0.000 title claims abstract description 20
- 239000007788 liquid Substances 0.000 claims abstract description 34
- 238000009434 installation Methods 0.000 claims abstract description 13
- 239000007921 spray Substances 0.000 claims abstract description 9
- 239000000126 substance Substances 0.000 claims abstract description 4
- 210000002683 foot Anatomy 0.000 claims description 22
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 6
- 239000000741 silica gel Substances 0.000 claims description 6
- 229910002027 silica gel Inorganic materials 0.000 claims description 6
- 238000010276 construction Methods 0.000 abstract description 3
- 238000005265 energy consumption Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 3
- 239000003905 agrochemical Substances 0.000 description 2
- 239000003814 drug Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 208000010086 Hypertelorism Diseases 0.000 description 1
- 206010020771 Hypertelorism of orbit Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M7/00—Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Mechanical Engineering (AREA)
- Insects & Arthropods (AREA)
- Wood Science & Technology (AREA)
- Zoology (AREA)
- Environmental Sciences (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a kind of pesticide spraying unmanned plane, including fuselage and rotor, liquid reserve tank is provided with fuselage, fuselage bottom is provided with sprinkler head, and sprinkler head is connected by pipeline with liquid reserve tank, farm chemical spray pump is installed on pipeline, the fuselage is the ellipsoid being vertically arranged, and is provided with installation cavity in fuselage roof, ejection mechanism and parachute are provided with installation cavity, parachute coordinates with ejection mechanism, and there is installation cavity ejection to cover.The present invention is simple in construction, reasonable in design, is conducive to reducing the windage being subject in flight course, reduces energy consumption；Aircraft is out of control fall when, parachute can be ejected, so that unmanned plane slowly falls, it is to avoid occur personnel casualty accidentses.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, more particularly to a kind of pesticide spraying unmanned plane.
Background technology
At present due to the limitation of various factors, China is in agricultural using upper aircraft still with fixed wing aircraft and helicopter
Based on manned aircraft, SUAV, also in the primary research stage, is mainly gone back in research agriculturally and application
In the presence of following weak point：
First, unmanned plane form construction design is unreasonable, and the windage being subject in flight course is excessive, causes power consumption larger；
Second, unmanned plane typically all uses Remote, when there is situation out of control, and unmanned plane holds directly from falling from high altitude
Casualty accident is easily caused, and during hypertelorism, it is not easy to recover unmanned plane；
3rd, during night work, it is difficult to judge unmanned plane position；
4th, during unmanned plane during flying, the liquid in its liquid reserve tank is easily rocked, and then influences the flight of unmanned plane；
5th, pesticide spraying is uneven to leave dead angle, and it is serious to cause that the utilization rate of agricultural chemicals is low, Residual Pesticides in Farm Produce is exceeded etc.
Harm.
Therefore, how to solve the defect of above-mentioned prior art presence becomes the direction of art personnel effort.
The content of the invention
It is an object of the invention to provide a kind of pesticide spraying unmanned plane, can be fully solved above-mentioned the deficiencies in the prior art it
Place.
The purpose of the present invention is realized by following technical proposals：
A kind of pesticide spraying unmanned plane, including fuselage and rotor, are provided with liquid reserve tank in fuselage, and fuselage bottom is provided with sprinkling
Head, sprinkler head is connected by pipeline with liquid reserve tank, and farm chemical spray pump is provided with pipeline, and the fuselage is the ellipse being vertically arranged
Body, is provided with installation cavity in fuselage roof, ejection mechanism and parachute is provided with installation cavity, parachute is matched somebody with somebody with ejection mechanism
Close, there is installation cavity ejection to cover.
Using said structure, ellipsoidal fuselage can effectively reduce the windage being subject to during flight, and parachute can lead to
Cross ejection mechanism, unmanned plane is out of control fall when eject, unmanned plane is slowly fallen, it is to avoid unmanned plane, which falls, injures road by a crashing object
People.
Preferably, being nested with guard ring outside the fuselage, guard ring is centrally located on the major axis of fuselage, in fuselage with preventing
Uniformly connected between guard ring and rotor motor is installed in the middle part of three linking arms, linking arm, rotor is arranged on the rotary shaft of rotor motor
On.
The setting of guard ring can play a protective role to rotor and fuselage, if awing unmanned plane collides other things
Body, guard ring can absorb, shift impulsive force.
Preferably, the outer wall and inwall of the guard ring are the arcwall face of evagination.
The design of this structure can further reduce the windage being subject to during unmanned plane during flying, be conducive to unmanned plane during flying and
Reduce energy consumption.
Preferably, the protection ring outer wall is provided with silica gel energy-absorbing circle.
Silica gel energy-absorbing circle can effectively absorb collision impact, when crashing, further protection rotor and machine
Body, and be conducive to extending the service life of guard ring.
Preferably, at least one dividing plate is provided with the liquid reserve tank, between the top of the dividing plate and liquid reserve tank inner top surface
There is gap, have gap between the bottom of dividing plate and liquid reserve tank inner bottom surface.
The design of this structure can play cut-off effect to the liquid in liquid reserve tank, be multistage by liquid separation, so that
Liquid sloshing amplitude is reduced, influence of the liquid sloshing to unmanned plane is reduced.
Preferably, the sprinkler head is rotary sprinkler.
The design of this structure can uniformly be sprayed decoction, and scope is wide and uniform.
The storage tank matched with support feet is opened up preferably, being circumferentially uniformly provided with along fuselage on three support feets, fuselage,
Support feet is placed in the storage tank, and the bottom of support feet is hinged on accommodating trench bottom, and hydraulic stem, liquid are provided with storage tank
One end of depression bar is hinged in storage tank, and the other end is hinged in support feet.
The design of this structure, can be such that support feet is packed up in unmanned plane during flying, windage be reduced, in UAV Landing
Put down, unmanned plane is supported.
Preferably, the rotor is obliquely installed to fuselage direction.
The design of this structure, the rotor wind-force that rotation is produced at a high speed can make medicine liquid spray evenly, be conducive to simultaneously
Expand medicine liquid spray scope, improve the operating efficiency of unmanned plane.
Preferably, the fuselage is provided with light-emitting device.
The design of this structure, favourable unmanned plane night work helps operator to judge unmanned plane position.
Preferably, being provided with buzzer and GPS positioning device in the fuselage.
The design of this structure, can help operator quickly to recover unmanned plane when unmanned plane falls.
Compared with prior art, the beneficial effects of the present invention are：
1. it is simple in construction, it is reasonable in design, be conducive to reducing the windage being subject in flight course, reduce energy consumption；
2. aircraft is out of control fall when, parachute can be ejected, so that unmanned plane slowly falls, it is to avoid occur casualties
Accident, and provided with buzzer and GPS positioning device, facilitate operator to recover the unmanned plane fallen；
3. the setting of guard ring and silica gel energy-absorbing circle, can effectively shift and absorb the impulsive force produced during collision, to unmanned plane
Fuselage and rotor play a protective role；
4. the setting of liquid reserve tank internal partition can be played a part of avoiding its interior liquid from acutely rocking；
5. pesticide spraying is uniform, scope is big, and the utilization rate of agricultural chemicals is high.
Brief description of the drawings
Fig. 1 is the structural representation that support feet of the present invention is in rounding state；
Fig. 2 is the structural representation that support feet of the present invention is in open configuration；
Fig. 3 is the cross-sectional view of fuselage of the present invention；
Fig. 4 is the top view of the present invention；
Fig. 5 is the A-A cross-sectional views in Fig. 4.
Embodiment
With reference to specific embodiments and the drawings, the present invention is further illustrated.
As shown in Figures 1 to 5, a kind of pesticide spraying unmanned plane, including fuselage 1 and rotor 2, are provided with liquid storage in fuselage 1
Case 3, the bottom of fuselage 1 is provided with rotary sprinkler 4, and sprinkler head 4 is connected by pipeline with liquid reserve tank 3, and spray is provided with pipeline
Teat pipette 5, the fuselage 1 is the ellipsoid being vertically arranged, and is provided with installation cavity 6 at the top of fuselage 1, bullet is provided with installation cavity 6
Mechanism 7 and parachute 8 are penetrated, parachute 8 coordinates with ejection mechanism 7, installation cavity 6 has ejection lid 9.
Further say, the fuselage 1 is made up of top cover and sub-body, it is ellipse that top cover is arranged on sub-body top composition
The fuselage 1 of circle, forms installation cavity 6, top cover is above-mentioned ejection lid 9 between top cover and sub-body.
In order to be protected to rotor 2 and fuselage 1, it is nested with outside the fuselage 1 outside guard ring 10, the guard ring 10
Wall and inwall are the arcwall face of evagination, and guard ring 10 is centrally located on the major axis of fuselage 1, fuselage 1 and guard ring 10 it
Between uniform three linking arms 11 of connection, the middle part of linking arm 11 installs rotor motor 12, and rotor 2 is arranged on the rotation of rotor motor 12
On axle.Moreover, rotor motor 12 is obliquely installed to fuselage side so that the rotor 2 is also tilted to fuselage direction.It is preferred that,
The outer wall of guard ring 12 is provided with silica gel energy-absorbing circle 13.
One dividing plate 14 is laterally set in the liquid reserve tank 3, between having between the top of the dividing plate 14 and liquid reserve tank inner top surface
Gap, has gap between the bottom of dividing plate 14 and liquid reserve tank inner bottom surface.
The storage tank matched with support feet 15 is opened up along circumferential be uniformly provided with three support feets 15, fuselage 1 of fuselage 1, is propped up
Spike 15 is placed in the storage tank, and the bottom of support feet 15 is hinged on accommodating trench bottom, and hydraulic stem is provided with storage tank
16, one end of hydraulic stem 16 is hinged in storage tank, and the other end is hinged in support feet 15.When support feet 15 is drawn in storage tank
After interior, the outer surface of support feet 15 is flushed with the outer surface of fuselage 1, and the outer surface of support feet 15 constitutes the one of the outer surface of ellipsoid fuselage 1
Part.
The fuselage 1 is provided with light-emitting device.The light-emitting device can be in some mutually flat of the outer surface of fuselage 1 setting
Capable fluorescent ring 17 or the LED installed in the surface of fuselage 1.
Buzzer is also equipped with the fuselage 1（It is not drawn into figure）And GPS positioning device（It is not drawn into figure）.
In unmanned plane during flying, because it has the fuselage 1 of oval shape, and the outer wall and inwall of guard ring 10 are
The arcwall face of evagination, therefore the windage being subject to during unmanned plane during flying can be reduced.In addition, guard ring 10 and silica gel energy-absorbing circle 13
Set, the impulsive force produced when unmanned plane is collided can be effectively reduced, and protection is played to unmanned aerial vehicle body 1 and rotor 2
Effect.When unmanned plane is fallen due to out of control or collision, ejection lid 9 is ejected, and parachute 8 is ejected by catapult-launching gear 7, and unmanned plane exists
Slowly fall in the presence of parachute 8, it is to avoid occur personnel casualty accidentses, while buzzer and GPS positioning device are started working,
The position location shown on the sound and remote control that operator is sent by buzzer judges that unmanned plane falls position, so as to
The unmanned plane fallen with conveniently recovering.During unmanned plane night work, operator can be clear accurate by light-emitting device
Judgement unmanned plane position.
During unmanned plane during flying, the dividing plate 14 in liquid reserve tank 3 plays cut-off effect to decoction, is two by liquid separation
Part, so as to reduce liquid sloshing amplitude, reduces influence of the liquid sloshing to unmanned plane.
When unmanned plane spray insecticide operation, farm chemical spray pump 5 pumps out the decoction in liquid reserve tank 3, is sprayed by rotating
First 4 are sprayed, and the rotation of rotary sprinkler 4 can uniformly be sprayed to surrounding, and scope is big, meanwhile, it is obliquely installed
Rotor 2 rotate the air-flow produced to fuselage lower outer direction at a high speed, air-flow can be such that decoction spills laterally, further expand
Big spraying range, and spray evenly, it is to avoid local decoction is excessive, improves the operating efficiency of unmanned plane.
In UAV Landing, hydraulic stem 16 is stretched out so that three support feets 15 are turned down, and unmanned plane is smoothly supported on ground
On face, after unmanned plane takes off, hydraulic stem 16 shrinks, and support feet 15 collapses to the oval shape of composition fuselage 1 in storage tank
Outer wall, reduces flight resistance.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
Any modifications, equivalent substitutions and improvements made within refreshing and principle etc., should be included in the scope of the protection.
Claims (10)
1. a kind of pesticide spraying unmanned plane, including fuselage and rotor, are provided with liquid reserve tank in fuselage, fuselage bottom is provided with sprinkling
Head, sprinkler head is connected by pipeline with liquid reserve tank, and farm chemical spray pump is provided with pipeline, it is characterised in that：The fuselage is vertical
The ellipsoid of setting, is provided with installation cavity in fuselage roof, ejection mechanism and parachute, parachute and bullet is provided with installation cavity
Mechanism cooperation is penetrated, there is installation cavity ejection to cover.
2. pesticide spraying unmanned plane according to claim 1, it is characterised in that：Guard ring is nested with outside the fuselage, is protected
Circle is centrally located on the major axis of fuselage, is uniformly connected in the middle part of three linking arms, linking arm and is installed between fuselage and guard ring
Rotor motor, rotor is arranged in the rotary shaft of rotor motor.
3. pesticide spraying unmanned plane according to claim 2, it is characterised in that：The outer wall and inwall of the guard ring be
The arcwall face of evagination.
4. pesticide spraying unmanned plane according to claim 3, it is characterised in that：The protection ring outer wall is provided with silica gel energy-absorbing
Circle.
5. pesticide spraying unmanned plane according to claim 4, it is characterised in that：In the liquid reserve tank provided with least one every
Plate, has gap, has gap between the bottom of dividing plate and liquid reserve tank inner bottom surface between the top of the dividing plate and liquid reserve tank inner top surface.
6. pesticide spraying unmanned plane according to claim 5, it is characterised in that：The sprinkler head is rotary sprinkler.
7. the pesticide spraying unmanned plane according to claim any one of 1-6, it is characterised in that：Circumferentially it is uniformly provided with along fuselage
The storage tank matched with support feet is opened up on three support feets, fuselage, support feet is placed in the storage tank, and the bottom of support feet
Accommodating trench bottom is hinged on, hydraulic stem is installed in storage tank, one end of hydraulic stem is hinged in storage tank, and the other end is hinged
In support feet.
8. pesticide spraying unmanned plane according to claim 7, it is characterised in that：The rotor is tilted to fuselage direction and set
Put.
9. pesticide spraying unmanned plane according to claim 7, it is characterised in that：The fuselage is provided with light-emitting device.
10. pesticide spraying unmanned plane according to claim 7, it is characterised in that：Be provided with the fuselage buzzer and
GPS positioning device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710285392.4A CN106976563A (en) | 2017-04-27 | 2017-04-27 | Pesticide spraying unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710285392.4A CN106976563A (en) | 2017-04-27 | 2017-04-27 | Pesticide spraying unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106976563A true CN106976563A (en) | 2017-07-25 |
Family
ID=59342047
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710285392.4A Pending CN106976563A (en) | 2017-04-27 | 2017-04-27 | Pesticide spraying unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106976563A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109896016A (en) * | 2019-02-24 | 2019-06-18 | 张康康 | A kind of unmanned plane with sprinkling mould group |
Citations (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103003148A (en) * | 2010-06-08 | 2013-03-27 | 威尔海德救援公司 | Life-saving vehicle |
| CN103935522A (en) * | 2014-03-03 | 2014-07-23 | 浙江大学 | Protection device and method for out-of-control crash of rotary-wing-type unmanned aerial vehicle |
| CN104443411A (en) * | 2014-10-27 | 2015-03-25 | 成都好飞机器人科技有限公司 | Quad-rotor unmanned aerial vehicle with anti-collision protective device |
| CN204674832U (en) * | 2014-12-11 | 2015-09-30 | 南京尊龙生物科学有限公司 | A kind of herbal sprinkling unmanned plane |
| CN104986339A (en) * | 2015-06-10 | 2015-10-21 | 浙江空行飞行器技术有限公司 | Unmanned aerial vehicle capable of being prevented from being crashed |
| CN105253303A (en) * | 2015-10-23 | 2016-01-20 | 杨珊珊 | Device and method for regulating unmanned aerial vehicle spray range |
| CN105292487A (en) * | 2015-11-23 | 2016-02-03 | 天津玉敏机械科技有限公司 | Unmanned aerial vehicle for multi-angle pesticide spraying |
| CN105292489A (en) * | 2015-11-23 | 2016-02-03 | 天津玉敏机械科技有限公司 | Unmanned aerial vehicle having pesticide spraying function |
| CN105329444A (en) * | 2015-11-23 | 2016-02-17 | 天津玉敏机械科技有限公司 | Agricultural spraying unmanned aerial vehicle having spraying cover guiding function |
| CN205221114U (en) * | 2015-10-23 | 2016-05-11 | 杨珊珊 | Unmanned aerial vehicle sprays scope adjusting device and unmanned aerial vehicle thereof |
| CN205221115U (en) * | 2015-11-23 | 2016-05-11 | 天津玉敏机械科技有限公司 | Unmanned aerial vehicle with multi -angle function of spraying insecticide |
| CN205418100U (en) * | 2015-12-19 | 2016-08-03 | 云南熙祥航空科技有限公司 | Plant protection unmanned plane |
| CN105857612A (en) * | 2016-04-01 | 2016-08-17 | 南充驭云创新科技有限公司 | Rotor wing agricultural unmanned aerial vehicle for plant protection |
| CN105882985A (en) * | 2014-12-26 | 2016-08-24 | 郑州中电新能源汽车有限公司 | Dual-rotor-wing coaxial safe anti-collision power-driven unmanned plant protection machine |
| CN205589475U (en) * | 2016-05-12 | 2016-09-21 | 江西兴航智控航空工业有限公司 | Novel pesticide spray unmanned aerial vehicle |
| CN105947217A (en) * | 2016-05-23 | 2016-09-21 | 中山市捷信科技服务有限公司 | A remote-controlled agricultural spraying aircraft |
| CN106039625A (en) * | 2016-06-21 | 2016-10-26 | 山东创能机械科技有限公司 | Water extinguishing agent and extinguishing method combing water extinguishing agent and fire-fighting unmanned aerial vehicle |
| CN205707370U (en) * | 2016-05-25 | 2016-11-23 | 江西科技学院 | Portable and collapsible unmanned plane |
| CN106143886A (en) * | 2015-03-25 | 2016-11-23 | 北京天翼合创科技发展有限公司 | One can be disintegrated formula multi-rotor aerocraft |
| US20160355258A1 (en) * | 2015-06-08 | 2016-12-08 | Vadient Optics, LLC. | Aerial Fluid Delivery System |
| CN205891224U (en) * | 2016-07-02 | 2017-01-18 | 江西联博科技有限公司 | Agricultural unmanned aerial vehicle |
| CN206087325U (en) * | 2016-10-17 | 2017-04-12 | 湖南博航无人机技术有限公司 | Extreme low -altitude remote control flight plant protection of four electronic rotors machine |
| CN206734633U (en) * | 2017-04-27 | 2017-12-12 | 峨眉山市博派乐无人机科技有限公司 | Pesticide spraying unmanned plane |
-
2017
- 2017-04-27 CN CN201710285392.4A patent/CN106976563A/en active Pending
Patent Citations (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103003148A (en) * | 2010-06-08 | 2013-03-27 | 威尔海德救援公司 | Life-saving vehicle |
| CN103935522A (en) * | 2014-03-03 | 2014-07-23 | 浙江大学 | Protection device and method for out-of-control crash of rotary-wing-type unmanned aerial vehicle |
| CN104443411A (en) * | 2014-10-27 | 2015-03-25 | 成都好飞机器人科技有限公司 | Quad-rotor unmanned aerial vehicle with anti-collision protective device |
| CN204674832U (en) * | 2014-12-11 | 2015-09-30 | 南京尊龙生物科学有限公司 | A kind of herbal sprinkling unmanned plane |
| CN105882985A (en) * | 2014-12-26 | 2016-08-24 | 郑州中电新能源汽车有限公司 | Dual-rotor-wing coaxial safe anti-collision power-driven unmanned plant protection machine |
| CN106143886A (en) * | 2015-03-25 | 2016-11-23 | 北京天翼合创科技发展有限公司 | One can be disintegrated formula multi-rotor aerocraft |
| US20160355258A1 (en) * | 2015-06-08 | 2016-12-08 | Vadient Optics, LLC. | Aerial Fluid Delivery System |
| CN104986339A (en) * | 2015-06-10 | 2015-10-21 | 浙江空行飞行器技术有限公司 | Unmanned aerial vehicle capable of being prevented from being crashed |
| CN105253303A (en) * | 2015-10-23 | 2016-01-20 | 杨珊珊 | Device and method for regulating unmanned aerial vehicle spray range |
| CN205221114U (en) * | 2015-10-23 | 2016-05-11 | 杨珊珊 | Unmanned aerial vehicle sprays scope adjusting device and unmanned aerial vehicle thereof |
| CN205221115U (en) * | 2015-11-23 | 2016-05-11 | 天津玉敏机械科技有限公司 | Unmanned aerial vehicle with multi -angle function of spraying insecticide |
| CN105329444A (en) * | 2015-11-23 | 2016-02-17 | 天津玉敏机械科技有限公司 | Agricultural spraying unmanned aerial vehicle having spraying cover guiding function |
| CN105292489A (en) * | 2015-11-23 | 2016-02-03 | 天津玉敏机械科技有限公司 | Unmanned aerial vehicle having pesticide spraying function |
| CN105292487A (en) * | 2015-11-23 | 2016-02-03 | 天津玉敏机械科技有限公司 | Unmanned aerial vehicle for multi-angle pesticide spraying |
| CN205418100U (en) * | 2015-12-19 | 2016-08-03 | 云南熙祥航空科技有限公司 | Plant protection unmanned plane |
| CN105857612A (en) * | 2016-04-01 | 2016-08-17 | 南充驭云创新科技有限公司 | Rotor wing agricultural unmanned aerial vehicle for plant protection |
| CN205589475U (en) * | 2016-05-12 | 2016-09-21 | 江西兴航智控航空工业有限公司 | Novel pesticide spray unmanned aerial vehicle |
| CN105947217A (en) * | 2016-05-23 | 2016-09-21 | 中山市捷信科技服务有限公司 | A remote-controlled agricultural spraying aircraft |
| CN205707370U (en) * | 2016-05-25 | 2016-11-23 | 江西科技学院 | Portable and collapsible unmanned plane |
| CN106039625A (en) * | 2016-06-21 | 2016-10-26 | 山东创能机械科技有限公司 | Water extinguishing agent and extinguishing method combing water extinguishing agent and fire-fighting unmanned aerial vehicle |
| CN205891224U (en) * | 2016-07-02 | 2017-01-18 | 江西联博科技有限公司 | Agricultural unmanned aerial vehicle |
| CN206087325U (en) * | 2016-10-17 | 2017-04-12 | 湖南博航无人机技术有限公司 | Extreme low -altitude remote control flight plant protection of four electronic rotors machine |
| CN206734633U (en) * | 2017-04-27 | 2017-12-12 | 峨眉山市博派乐无人机科技有限公司 | Pesticide spraying unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109896016A (en) * | 2019-02-24 | 2019-06-18 | 张康康 | A kind of unmanned plane with sprinkling mould group |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105882985B (en) | A kind of electronic unmanned fog machine of DCB Specimen close coupled type anticollision | |
| CN104554726A (en) | Special intelligent unmanned aerial vehicle for agriculture and forestry | |
| CN204279950U (en) | Seeding apparatus | |
| CN206734633U (en) | Pesticide spraying unmanned plane | |
| CN108341045B (en) | Unmanned aerial vehicle protection device that falls | |
| CN113071681A (en) | Intelligent unmanned aerial vehicle | |
| CN106976563A (en) | Pesticide spraying unmanned plane | |
| CN104401492B (en) | Agricultural depopulated helicopter | |
| CN204846380U (en) | Agricultural plant protection unmanned aerial vehicle takes precautions against earthquakes and swings medical kit | |
| CN206846972U (en) | A kind of indoor purifying unmanned plane | |
| CN112591099A (en) | Atomized pesticide sprays unmanned aerial vehicle with automatic protect function drops in outage | |
| CN206068161U (en) | A kind of agricultural spraying unmanned plane | |
| CN205891255U (en) | Pesticide sprays unmanned aerial vehicle | |
| CN107771777A (en) | A kind of multi-functional scarecrow device on outdoor box transformer | |
| CN207791162U (en) | A kind of unmanned plane of agricultural sprayable pesticide | |
| CN204279936U (en) | The rotor driver of agricultural depopulated helicopter | |
| CN1117667C (en) | Flying dish capable of submerging under water | |
| CN204937494U (en) | A kind of remote control plant protection aircraft | |
| CN216581035U (en) | Air-assisted pesticide spraying device based on unmanned aerial vehicle | |
| CN104303667B (en) | The application process of fertilizer solution | |
| CN104316718A (en) | Wind speed measurement device | |
| CN204228737U (en) | The wind speed measuring device of agricultural depopulated helicopter | |
| CN210846822U (en) | Spraying device, spraying system and plant protection equipment | |
| CN112154997B (en) | Agricultural plant protection unmanned aerial vehicle | |
| CN104304222B (en) | Spray equipment |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170725 |