CN109436332A - Big-elevation is flat to fly two sections of unmanned fog machines of the wing - Google Patents
Big-elevation is flat to fly two sections of unmanned fog machines of the wing Download PDFInfo
- Publication number
- CN109436332A CN109436332A CN201910005634.9A CN201910005634A CN109436332A CN 109436332 A CN109436332 A CN 109436332A CN 201910005634 A CN201910005634 A CN 201910005634A CN 109436332 A CN109436332 A CN 109436332A
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- China
- Prior art keywords
- wing
- big
- sections
- fly
- flat
- 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.)
- Granted
Links
- 239000003814 drug Substances 0.000 claims description 21
- 239000007921 spray Substances 0.000 claims description 12
- 238000000926 separation method Methods 0.000 claims description 8
- 238000005507 spraying Methods 0.000 claims description 7
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 3
- 238000005192 partition Methods 0.000 claims description 3
- 239000000575 pesticide Substances 0.000 abstract description 14
- 238000005260 corrosion Methods 0.000 abstract description 2
- 230000007797 corrosion Effects 0.000 abstract description 2
- 239000002699 waste material Substances 0.000 abstract description 2
- 229940079593 drug Drugs 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 230000001133 acceleration Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 3
- 239000010914 pesticide waste Substances 0.000 description 2
- 230000001154 acute effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 239000007787 solid Substances 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Mechanical Engineering (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a kind of flat winged two sections of unmanned fog machines of the wing of big-elevation; including at least two power rails disposed in parallel, the undercarriage being fixed on power rail and it is fixed on wing perpendicular with power rail on undercarriage; the both ends of above-mentioned power rail are respectively and fixedly provided with motor; and the revolving speed of the motor at the power rail both ends, which has, makes it be in the speed difference of high-angle of attack flight; the angle of the big-elevation is 30~45 degree; above-mentioned wing is two-part wing; it is divided into top wing and lower section wing, above-mentioned top wing is connected with lower section wing by vertical fin.Unmanned fog machine in the present invention is tiltedly flown using big-elevation, and the air-flow of rotor obliquely, can be avoided pesticide and deflect on the propeller of rack, avoids the waste of pesticide corrosion propeller and pesticide.
Description
Technical field
The present invention relates to agricultural machinery technological fields, and in particular to a kind of big-elevation is flat to fly two sections of unmanned fog machines of the wing.
Background technique
In current unmanned fog machine technical field, the unmanned fog machine of quadrotor is mostly used greatly, for quadrotor
The wind field of unmanned fog machine, quadrotor can deflect into pesticide on propeller, be easy to cause the waste of pesticide.
Summary of the invention
The purpose of the present invention is to provide a kind of flat winged two sections of unmanned fog machines of the wing of big-elevation, solve current unmanned plant protection
Machine mostly uses greatly the unmanned fog machine of quadrotor, and the wind field of quadrotor can deflect into pesticide on propeller, be easy to cause pesticide rotten
The problem of losing propeller and pesticide waste.
In order to solve the above technical problems, the invention adopts the following technical scheme:
A kind of big-elevation is flat to fly two sections of unmanned fog machines of the wing, including at least two power rails disposed in parallel, is fixed on power rail
On undercarriage and be fixed on wing perpendicular with power rail on undercarriage, the both ends of above-mentioned power rail are respectively and fixedly provided with electricity
Machine, and the revolving speed of the motor at the power rail both ends has the speed difference for making it in high-angle of attack flight, the angle of the big-elevation
It is 30~45 degree, above-mentioned wing is two-part wing, is divided into top wing and lower section wing, above-mentioned top wing and lower section wing
It is connected by vertical fin.
Preferably, above-mentioned top wing is internally provided with battery, Spraying Control System and flight control system；Above-mentioned lower section
Wing is internally provided with medicine storehouse, and the lower end of above-mentioned lower section wing is arranged at intervals with multiple spray heads.
Preferably, the medicine storehouse in above-mentioned lower section wing is opened up to by partition along it and is given as multiple independent separation medicines
Storehouse, above-mentioned separation medicine storehouse are corresponding with spray head.
Preferably, the outlet in above-mentioned separation medicine storehouse for Teat pipette with spray head by being connected.
Preferably, the length ratio of above-mentioned top wing and lower section wing is greater than 1.
Preferably, above-mentioned undercarriage include at least four vertical lifting levers and at least four transverse direction lifting levers, above-mentioned four
The vertical lifting lever of root is arranged in parallel and is separately fixed at least two power rails disposed in parallel, and at least four above-mentioned transverse directions rise
The lower end that bar is sequentially fixed at vertical lifting lever is fallen, and above-mentioned vertical lifting lever and lateral lifting lever fixation form cube
Structure.
Preferably, above-mentioned power rail and being connected between the vertical lifting lever on the power rail and being fixed with brace.
Preferably, being connected separately with two fixed links, above-mentioned top wing and lower section on each above-mentioned vertical lifting lever
Nut is provided on wing, above-mentioned fixed link is fixed top wing and lower section wing by nut.
Preferably, being fixed with connecting rod between adjacent above-mentioned power rail.
Preferably, the upper end of above-mentioned top wing is arranged at intervals at least two buckles, the position of above-mentioned buckle with
Power rail is corresponding and is connected on power rail.
Compared with prior art, the beneficial effects of the present invention are:
The flat winged unmanned plant protection machine equipment of two sections of wings of big-elevation provided by the invention is compared traditional agricultural unmanned plane of quadrotor and is possessed more
There is unique spraying effect long cruise duration.Compared to quadrotor uprush, possess it is oblique after air-flow, air-flow is to crop
The influence of posture is smaller.It can be used for other crops easily to lodge.The wind field of quadrotor can deflect to pesticide on propeller, keep away
Exempt from pesticide corrosion propeller and pesticide waste, the present invention are tiltedly flown using big-elevation, the air-flow of rotor obliquely, can be to avoid this
One influences.Wing improves space utilization rate for filling pesticide.Using the unique airflow influence feature of two sections of wings, liter is improved
Power.Two sections of wings have bigger wing area compared with single-blade, while can be to second segment wing by the acceleration air-flow of first segment wing
Beneficial Effect is generated, plays the role of increasing lift.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
Referring to Fig. 1, a kind of big-elevation is flat to fly two sections of unmanned fog machines of the wing, including two power rails 1 disposed in parallel, fixed
In the undercarriage 2 on power rail 1 and the wing 3 perpendicular with power rail 1 is fixed on undercarriage 2, the two of above-mentioned power rail 1
End is respectively and fixedly provided with motor 4, and the motor of different rotating speeds is used before and after power rail 2, utilizes the difference of the motor in 2 front and back of power rail
Speed realizes entire rack, i.e. big-elevation is presented in power rail and horizontal direction, and the angle of the big-elevation is 30~45 degree；Wing is horizontal
Flight, is capable of providing maximum lift in this angle flight attitude lower wing.Above-mentioned wing 3 is two-part wing, is divided into top machine
The wing 31 and lower section wing 32, above-mentioned top wing 31 and lower section wing 32 are connected by vertical fin 35, and there are two the vertical fin 35 tools, i.e.,
Top wing 31 and lower section wing 32 pass through vertical fin 35 at the position at its both ends and connect.Shape between power rail and undercarriage
At the structure of similar square.
The flat winged unmanned plant protection machine equipment of two sections of wings of big-elevation provided by the invention is compared traditional agricultural unmanned plane of quadrotor and is gathered around
There is longer cruise duration, there is unique spraying effect.Compared to quadrotor uprush, possess it is oblique after air-flow, air-flow pair
The influence of crop posture is smaller.It can be used for other crops easily to lodge.Pesticide can be deflected to propeller by the wind field of quadrotor
On, we are tiltedly flown using big-elevation, and the air-flow of rotor obliquely, can be to avoid this influence.Wing is improved for filling pesticide
Space utilization rate.Using the unique airflow influence feature of two sections of wings, lift is improved.Two sections of wings have the bigger wing compared with single-blade
Area, while Beneficial Effect can be generated to second segment wing by the acceleration air-flow of first segment wing, play the work for increasing lift
With.
Top wing 31 is internally provided with battery, Spraying Control System and flight control system；Above-mentioned lower section wing 32 it is interior
Portion is provided with medicine storehouse, and the lower edge of above-mentioned lower section wing 32 is arranged at intervals with multiple spray heads 33.For the automatically controlled of the fog machine
System and pesticide spraying system are divided to two sections of wings to be provided separately, and on the one hand make have bigger wing area, on the other hand can be improved sky
Between utilization rate, improve whole pesticide supplying effect.The lower edge of spray head wing placed below can utilize top wing when spraying insecticide
Downwash flow be lower section wing upper surface carry out air-flow acceleration so that the air-flow separated on wing from below be medicine mist
Accelerate.
It is directed to the wing, the wing chord angle of top wing 31 and lower section wing 32 is acute angle, can be to lower section wing 32
Offer more has a strong effect power.
Medicine storehouse in above-mentioned lower section wing 32 is opened up to by partition along it and is given as multiple independent separation medicine storehouses, and above-mentioned point
It is corresponding with spray head 33 every medicine storehouse.Medicine storehouse is separated to be independent and separates medicine storehouse, medicine binning medicine can be made more convenient, while
Different drugs can be accommodated.The outlet in above-mentioned separation medicine storehouse for Teat pipette with spray head 33 by being connected.By for Teat pipette and spray
Head is attached, and provides enough power for spray.
The length ratio of above-mentioned top wing 31 and lower section wing 32 is greater than 1.I.e. the overall distribution of wing is trapezoidal, so that whole
A fog machine is more stable.
Above-mentioned undercarriage 2 includes four vertical lifting levers 21 and four lateral lifting levers 22, above-mentioned four vertical lifting levers
21 are arranged in parallel and are separately fixed at least two power rails 1 disposed in parallel, and four above-mentioned lateral lifting levers 22 are successively solid
It is scheduled on the lower end of vertical lifting lever 21, and above-mentioned vertical lifting lever 21 and the lateral fixation of lifting lever 22 form cube knot
Structure.Undercarriage be for wing to be fixed, while be conducive to fog machine Normal Takeoff and Landing, be mainly reflected in structural stability side
Face.
Brace 23 is fixed between above-mentioned power rail 1 and the vertical lifting lever 21 being connected on the power rail 1.In power rail
Brace is fixed between vertical lifting lever also for the stability of structure, so that reducing gas during fog machine rises and falls
Flow the impact force to integrally-built stability.
In order to carry out stablizing fixation to wing, two fixed links 24 are connected separately on each above-mentioned vertical lifting lever 21,
Nut is provided on above-mentioned top wing 31 and lower section wing 32, above-mentioned fixed link 24 passes through nut for top wing 31 and lower section
Wing 32 is fixed.
For the stability of structure, connecting rod 25 is fixed between adjacent above-mentioned power rail 1.
For the ease of fixation, the upper end of above-mentioned top wing 31 is arranged at intervals at least two buckles 34, above-mentioned buckle
34 position is corresponding with power rail 1 and is connected on power rail 1.
" one embodiment ", " another embodiment ", " embodiment ", " preferred implementation spoken of in the present specification
Example " etc., referring to combining specific features, structure or the feature of embodiment description includes describing extremely in the application generality
In few one embodiment.It is not centainly to refer to the same embodiment that statement of the same race, which occur, in multiple places in the description.Into one
For step, when describing a specific features, structure or feature in conjunction with any embodiment, what is advocated is to combine other implementations
Example realizes that this feature, structure or feature are also fallen within the scope of the present invention.
Although reference be made herein to invention has been described for multiple explanatory embodiments of the invention, however, it is to be understood that
Those skilled in the art can be designed that a lot of other modification and implementations, these modifications and implementations will fall in this Shen
It please be within disclosed scope and spirit.More specifically, disclose in the application, drawings and claims in the range of, can
With the building block and/or a variety of variations and modifications of layout progress to theme combination layout.In addition to building block and/or layout
Outside the modification and improvement of progress, to those skilled in the art, other purposes also be will be apparent.
Claims (10)
1. a kind of big-elevation is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: including at least two power rails disposed in parallel
(1), the undercarriage (2) that is fixed on power rail (1) and it is fixed on wing perpendicular with power rail (1) on undercarriage (2)
(3), the both ends of the power rail (1) are respectively and fixedly provided with motor (4), and the revolving speed tool of the motor (4) at the power rail (1) both ends
Having makes it be in the speed difference of high-angle of attack flight, and the angle of the big-elevation is 30~45 degree, and the wing (3) is two-part wing,
It is divided into top wing (31) and lower section wing (32), the top wing (31) and lower section wing (32) pass through vertical fin (35) phase
Even.
2. big-elevation according to claim 1 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the top wing
(31) be internally provided with battery, Spraying Control System and flight control system；The lower section wing (32) is internally provided with medicine storehouse,
And the lower end of the lower section wing (32) is arranged at intervals with multiple spray heads (33).
3. big-elevation according to claim 2 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the lower section wing
(32) the medicine storehouse in, which is opened up along it to by partition, to be given as multiple independent separation medicine storehouses, the separation medicine storehouse and spray head (33) phase
It is corresponding.
4. big-elevation according to claim 3 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the separation medicine storehouse
Outlet for Teat pipette with spray head (33) by being connected.
5. big-elevation according to claim 1 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the top wing
(31) it is greater than 1 with the length ratio of lower section wing (32).
6. big-elevation according to claim 1 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the undercarriage (2)
Including at least four vertical lifting levers (21) and at least four lateral lifting levers (22), described four vertical lifting levers (21) are parallel
It is arranged and is separately fixed at least two power rails (1) disposed in parallel, at least four lateral lifting levers (22) is successively
It is fixed on the lower end of vertical lifting lever (21), and the vertical lifting lever (21) and fixed formed of lateral lifting lever (22) stand
Cube structure.
7. big-elevation according to claim 6 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the power rail (1)
Be fixed with brace (23) between the vertical lifting lever (21) that is connected on the power rail (1).
8. big-elevation according to claim 6 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: each described vertical
It falls on bar (21) and is connected separately with two fixed links (24), be provided with spiral shell on the top wing (31) and lower section wing (32)
Mother, the fixed link (24) are fixed by top wing (31) and lower section wing (32) by nut.
9. big-elevation according to claim 1 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the adjacent power
Connecting rod (25) are fixed between bar (1).
10. big-elevation according to claim 1 is flat to fly two sections of unmanned fog machines of the wing, it is characterised in that: the top wing
(31) upper end is arranged at intervals at least two buckles (34), and the position of the buckle (34) is corresponding with power rail (1) simultaneously
It is connected on power rail (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910005634.9A CN109436332B (en) | 2019-01-03 | 2019-01-03 | Unmanned plant protection machine of big elevation angle flat flight two section wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910005634.9A CN109436332B (en) | 2019-01-03 | 2019-01-03 | Unmanned plant protection machine of big elevation angle flat flight two section wings |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109436332A true CN109436332A (en) | 2019-03-08 |
| CN109436332B CN109436332B (en) | 2024-06-04 |
Family
ID=65542764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910005634.9A Active CN109436332B (en) | 2019-01-03 | 2019-01-03 | Unmanned plant protection machine of big elevation angle flat flight two section wings |
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| Country | Link |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205602110U (en) * | 2016-04-12 | 2016-09-28 | 郑州郑航通用航空工业科技有限公司 | Unmanned plant protection of four rotors machine |
| WO2017016096A1 (en) * | 2015-07-27 | 2017-02-02 | 江阴市翔诺电子科技有限公司 | Novel vertical take-off and landing aircraft and control method therefor |
| CN206125421U (en) * | 2016-10-12 | 2017-04-26 | 曹萍 | VTOL unmanned vehicles |
| CN108382579A (en) * | 2018-05-06 | 2018-08-10 | 北京天宇新超航空科技有限公司 | A kind of new and effective tilting rotor unmanned vehicle |
| CN213594533U (en) * | 2019-01-03 | 2021-07-02 | 朱文武 | Large-elevation plane-flying two-section-wing unmanned plant protection machine |
-
2019
- 2019-01-03 CN CN201910005634.9A patent/CN109436332B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017016096A1 (en) * | 2015-07-27 | 2017-02-02 | 江阴市翔诺电子科技有限公司 | Novel vertical take-off and landing aircraft and control method therefor |
| CN205602110U (en) * | 2016-04-12 | 2016-09-28 | 郑州郑航通用航空工业科技有限公司 | Unmanned plant protection of four rotors machine |
| CN206125421U (en) * | 2016-10-12 | 2017-04-26 | 曹萍 | VTOL unmanned vehicles |
| CN108382579A (en) * | 2018-05-06 | 2018-08-10 | 北京天宇新超航空科技有限公司 | A kind of new and effective tilting rotor unmanned vehicle |
| CN213594533U (en) * | 2019-01-03 | 2021-07-02 | 朱文武 | Large-elevation plane-flying two-section-wing unmanned plant protection machine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109436332B (en) | 2024-06-04 |
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