CN203558205U - Electrostatic multi-shaft flying plant protector - Google Patents
Electrostatic multi-shaft flying plant protector Download PDFInfo
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- CN203558205U CN203558205U CN201320734976.2U CN201320734976U CN203558205U CN 203558205 U CN203558205 U CN 203558205U CN 201320734976 U CN201320734976 U CN 201320734976U CN 203558205 U CN203558205 U CN 203558205U
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Abstract
The utility model discloses an electrostatic multi-shaft flying plant protector which comprises a multi-shaft flying machine and an electrostatic spraying mechanism. The electrostatic multi-shaft flying plant protector is characterized in that by rotation of each propeller of the multi-shaft flying machine, a rising force and a flying force are provided for the electrostatic multi-shaft flying plant protector; an electrostatic spraying mechanism control system is used for controlling the operation of a diaphragm pump and automatic extension of a spray rod, and an electrostatic metal ground wire is grounded in a suspension manner by a wire so as to realize electrostatic spraying. Due to adoption of the structure, the force borne by a main rotor wing of a traditional unmanned helicopter plant-protection flying machine is dispersed onto four rotor wings, so that the noise is reduced and the stability is improved; meanwhile, the electrostatic multi-shaft flying plant protector is different from a multi-rotor wing unmanned plant protector, and the structural form is changed due to decrease of the rotor wings, thus the load capacity is increased and the number of the dosing times is reduced; simultaneously, due to adoption of an electrostatic technology, medicine liquor is relatively easy to be adsorbed on the surfaces of crops, and the operation effect is improved.
Description
Technical field
The utility model relates to a kind of unmanned fog machine, especially has the multiaxis flight static fog machine of multiple rotors.
Background technology
Current unmanned fog machine adds chemical spraying device by rotary wind type aircraft and forms; one is depopulated helicopter plant protection; mainly the humidifier by the helicopter at one or two rotors of center arrangement and in the middle of being placed on forms; by the speed governing rotation of rotor; the power and the heading that provide aircraft to rise are sprayed simultaneously.Another kind is the unmanned fog machines of many rotors, mainly by arranging the unmanned plane of more than eight rotor in surrounding and being placed on middle humidifier, forms, and by the speed governing rotation of many rotors, the power and the heading that provide aircraft to rise are sprayed simultaneously.Depopulated helicopter plant protection aircraft principle of work is that rotary wind type aircraft engine drives rotor that lift is provided, rotor craft is lifted to holder aloft, sustainer, main engine simultaneously also outputting power to the minor spiral oar of afterbody, the airbone gyro instrument detects rotor craft degreeof turn and also feeds back to tail-rotor, offsets the antagonistic force under the different rotating speeds of king bolt oar by adjusting the pitch of minor spiral oar.By " tilting frame " mechanism, change the blade angle of rotary wind type aircraft rotor, the lift that changes rotor wing rotation plane diverse location with this is realized the flight attitude that changes rotary wind type aircraft, with lift direction, change change of flight direction again, thereby control rising and the decline of rotary wind type aircraft and take off vertically and land.The unmanned fog machine aircraft of many rotors principle of work is recently to provide power and rising and the decline of advancing by the rotating of many rotors and friction speed.
The unmanned fog machine flight theory of more than introducing has determined that their bodies can not do greatly, and chemical feeding quantity is limited, and fluid loss is serious, is difficult for crops and absorbs, and has again the weak points such as technical requirements is high, and cost is large, and noise is large, and stability is inadequate simultaneously.
Summary of the invention
The purpose of this utility model is to provide a kind of multiaxis flight static fog machine; by changing up hill and dale rotary-wing flight structure, chemical feeding quantity and the crops of improving rotary wind type aircraft absorb liquid effect, reduce technical requirements and cost simultaneously; noise decrease, improves stability.
In order to solve the problems of the technologies described above, technical scheme that the utility model is taked is: a kind of multiaxis flight static fog machine, is comprised of Multi-axis aircraft, electrostatic spray mechanism.By Multi-axis aircraft, provide lift and flight, by electrostatic spray mechanism, carry out spraying operation, mainly by control system control membrane pump, turned round, membrane pump inlet is connected with water tank liquid outlet, membrane pump liquid outlet is connected with flexible pipe, and flexible pipe is connected with spray boom, and spray boom is sprayed outward by control system auto-extending machine, static metal wool and membrane pump join simultaneously, and other end grounding jumper is suspended to ground by wire.
Multi-axis aircraft is comprised of upper left rotor, upper right rotor, lower-left rotor, bottom right rotor, Multi-axis aircraft fuselage, is characterized in that each screw propeller and Multi-axis aircraft fuselage are in same plane and fuselage has an angle of inclination.
Electrostatic spray mechanism comprises electrostatic spray mechanism fuselage (dosing tank, control system, storage battery, membrane pump, electrostatic generator, flexible pipe), spray boom, wire, alighting gear.Be characterized in that static metal grounding jumper is to hang ground connection, described spray boom can also can close in machine by automatic telescopic.
Adopt after said structure; compare with the unmanned fog machine of many rotors with depopulated helicopter plant protection: the one, aircraft is become at fuselage and arranges four rotors at one or two rotors of center arrangement, the power that main rotor is born is distributed on four rotors, has reduced noise; improved stability; the 2nd, by reducing rotor, change structure form, thus promoted load carrying ability; reduce dosing number of times; the 3rd, adopted electrostatic technique, make liquid more easily be adsorbed on crops surface, improved operation effectiveness.
Accompanying drawing explanation
Fig. 1 is the plan structure figure of the utility model multiaxis flight static fog machine.
Fig. 2 is the side-looking constructional drawing of the utility model multiaxis flight static fog machine.
The specific embodiment
Fig. 1, the multiaxis of the utility model shown in Fig. 2 flight static fog machine [comprises upper left rotor 1 by Multi-axis aircraft, upper right rotor 2, lower-left rotor 3, bottom right rotor 4, Multi-axis aircraft fuselage 5] and electrostatic spray mechanism [the fuselage 6(of electrostatic spray mechanism dosing tank, control system, storage battery, membrane pump, electrostatic generator, flexible pipe), spray boom 7, wire 8, alighting gear 9] composition, the High Rotation Speed of Multi-axis aircraft by each rotor provides lift and flight for multiaxis flight static fog machine, Multi-axis aircraft fuselage 5 is mounted with battery, control system, and various sensors.Electrostatic spray mechanism mainly turns round by control system control membrane pump, membrane pump inlet is connected with water tank liquid outlet, membrane pump liquid outlet is connected with flexible pipe, flexible pipe is connected with spray boom, spray boom 7 is sprayed outward by control system auto-extending machine, static metal wool and membrane pump join simultaneously, and static metal grounding jumper is hanging to ground by wire 8.
Upper left rotor 1, upper right rotor 2, lower-left rotor 3, bottom right rotor 4, each screw propeller and the Multi-axis aircraft fuselage 5 of the multiaxis of the utility model shown in Fig. 2 flight static fog machine is in same plane and fuselage 5 has an angle of inclination, so that each rotor also provides the power of the utility model multiaxis flight static fog machine to all directions motion when raising force is provided.Static metal grounding jumper is hanging to ground by wire 8.
Claims (4)
1. a multiaxis flight static fog machine; it is characterized in that: Multi-axis aircraft and the combination of electrostatic spray mechanism; electrostatic spray mechanism mainly turns round by control system control membrane pump; membrane pump inlet is connected with water tank liquid outlet; membrane pump liquid outlet is connected with flexible pipe, and flexible pipe is connected with spray boom, and spray boom is by outside control system auto-extending machine; static metal wool and membrane pump join simultaneously, and static metal grounding jumper is hanging to ground by wire.
2. multiaxis flight static fog machine according to claim 1, its Multi-axis aircraft is characterised in that: upper left rotor 1, upper right rotor 2, lower-left rotor 3, bottom right rotor 4, each screw propeller and Multi-axis aircraft fuselage 5 are in same plane and fuselage 5 has an angle of inclination.
3. multiaxis flight static fog machine according to claim 1, its electrostatic spray mechanism is characterised in that: static metal grounding jumper is to hang ground connection by wire.
4. multiaxis flight static fog machine according to claim 1, its electrostatic spray mechanism is characterised in that: spray boom can automatic telescopic.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320734976.2U CN203558205U (en) | 2013-11-20 | 2013-11-20 | Electrostatic multi-shaft flying plant protector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320734976.2U CN203558205U (en) | 2013-11-20 | 2013-11-20 | Electrostatic multi-shaft flying plant protector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203558205U true CN203558205U (en) | 2014-04-23 |
Family
ID=50507940
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320734976.2U Expired - Fee Related CN203558205U (en) | 2013-11-20 | 2013-11-20 | Electrostatic multi-shaft flying plant protector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203558205U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104192310A (en) * | 2014-09-02 | 2014-12-10 | 太仓市金港植保器械科技有限公司 | Electrostatic spraying device, aerial electrostatic spraying device and electrostatic spraying method |
| CN105035328A (en) * | 2015-08-19 | 2015-11-11 | 张旭超 | Hybrid-power flight vehicle |
| CN106823620A (en) * | 2016-02-01 | 2017-06-13 | 滑黎明 | Haze device is removed in the air |
| CN111526946A (en) * | 2017-12-29 | 2020-08-11 | 株式会社创意科技 | Air cleaner |
-
2013
- 2013-11-20 CN CN201320734976.2U patent/CN203558205U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104192310A (en) * | 2014-09-02 | 2014-12-10 | 太仓市金港植保器械科技有限公司 | Electrostatic spraying device, aerial electrostatic spraying device and electrostatic spraying method |
| CN105035328A (en) * | 2015-08-19 | 2015-11-11 | 张旭超 | Hybrid-power flight vehicle |
| CN106823620A (en) * | 2016-02-01 | 2017-06-13 | 滑黎明 | Haze device is removed in the air |
| CN111526946A (en) * | 2017-12-29 | 2020-08-11 | 株式会社创意科技 | Air cleaner |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140423 Termination date: 20141120 |
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| EXPY | Termination of patent right or utility model |