CN207374677U - A kind of agricultural plant protection unmanned plane - Google Patents
A kind of agricultural plant protection unmanned plane Download PDFInfo
- Publication number
- CN207374677U CN207374677U CN201721455198.8U CN201721455198U CN207374677U CN 207374677 U CN207374677 U CN 207374677U CN 201721455198 U CN201721455198 U CN 201721455198U CN 207374677 U CN207374677 U CN 207374677U
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- Prior art keywords
- host
- inner cavity
- control system
- nozzle
- undercarriage
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Abstract
The utility model is related to unmanned air vehicle technique fields, more particularly to a kind of agricultural plant protection unmanned plane, including host housing, dynamical system, flight control system and lifting support mechanism, dynamical system includes annular battery and propeller component, annular battery is circumferentially positioned at the side of flight control system, lifting support mechanism includes undercarriage and is arranged on the nozzle of undercarriage bottom, the surface of nozzle is coated with raised rubber pad, the nozzle of nozzle surface is connected with the through hole one-to-one corresponding on raised rubber pad surface, not only so that sprinkling is more uniform, and play the role of support in landing；The bottom of flight control system is provided with the heat dissipation tank that surface carries ventilation hole, enhance the air flow of host shell inner cavity, and the semiconductor refrigerating part that is embedded of cooperation host upper lid surface, refrigeration end is exposed in the inner cavity of host shell, can effectively radiate to host shell inner cavity.
Description
Technical field
The utility model is related to unmanned air vehicle technique fields, and in particular to a kind of agricultural plant protection unmanned plane.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft or fully or intermittently independently operated by car-mounted computer that presetting apparatus manipulates.
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle.Unmanned plane is actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition：Nobody
Fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, unmanned parasol
Deng, compared with manned aircraft, it have small, low cost, it is easy to use, to operational environment require low, battlefield survival
The advantages that stronger.Since UAV has great significance to Future Air Combat, each main military country of the world is all adding
The tight development work for carrying out UAV.In November, 2013, Civil Aviation Administration of China issue《Civilian unmanned aviation
Device system driver management temporary provisions》, it is responsible for the related management of civilian unmanned plane by Chinese AOPA associations.According to《Regulation》,
Inland of China unmanned plane operation can be divided into 11 kinds of situations according to type size, flying area, wherein only 116 kilograms or more of nothing
Man-machine and 4600 cubic metres or more dirigibles fly in fusion spatial domain to be managed by civil aviation authority, remaining situation, including increasingly prevalence
Other flights including miniature aerial photography aircraft, are managed by employer's organization or are voluntarily responsible for by manipulator.
Plant protection unmanned plane, as the term suggests be for agriculture and forestry plant protection operation UAV, the type unmanned aerial vehicle
By flying platform by：Fixed-wing, helicopter, Multi-axis aircraft, navigation fly control, a few part compositions of spraying mechanism, distant by ground
Control or navigation fly control, to realize spraying operation, can spray medicament, seed, pulvis etc..
The radiator that plant protection unmanned plane at this stage is taken is typically all radiating fin, using heat transfer in unmanned plane
Portion radiates, but often heat dissipation effect is poor for this radiating mode, and the undercarriage of plant protection unmanned plane often function compared with
To be single.
Utility model content
In view of the deficiencies of the prior art, the utility model discloses a kind of agricultural plant protection unmanned plane, for solving at this stage
The radiator taken of plant protection unmanned plane be typically all radiating fin, radiated using heat transfer to unmanned plane inside, but
It is that often heat dissipation effect is poor for this radiating mode, and the undercarriage of plant protection unmanned plane the problems such as often function is more single；
The utility model is achieved by the following technical programs：
A kind of agricultural plant protection unmanned plane, it is described including host housing, dynamical system, flight control system and lifting support mechanism
Dynamical system includes annular battery and propeller component, and the flight control system is arranged on the inner cavity of the host housing and described flies
The bottom of control system is fixedly connected with heat dissipation tank, and the ring-type battery is circumferentially positioned at the side of the flight control system, described to dissipate
The surrounded surface of hot tank is both provided with ventilation hole with lower surface, and the upper surface of the host housing offers opening and the opening
One side host upper cover is connected with by articulate, the array of interior cavities of the host upper cover is provided with semiconductor chilling plate and institute
It states semiconductor chilling plate and is electrically connected the flight control system, the semiconductor chilling plate includes refrigeration end and heating end, the refrigeration
End is embedded the lower surface and upper surface covered on the host respectively with the heating end；
The lifting support mechanism includes undercarriage and the nozzle for being connected to the undercarriage bottom, the undercarriage
Inside is connected for hollow and described undercarriage with the inner cavity of the nozzle, and the lower surface of the nozzle is coated with raised rubber
The surface of pad and the raised rubber pad is evenly arranged with through hole；
It is embedded on the surface of the host housing surrounding solid respectively on chemical tank and the opposite lateral wall of the chemical tank
Surely compression pump and the undercarriage are connected with, the inner cavity of the chemical tank is connected with the inner cavity of the undercarriage, the pressure
Pump is electrically connected the flight control system.
Preferably, the compression pump is arranged in the inner cavity of the host housing.
Preferably, the surface of the nozzle has been uniformly arranged spray orifice and the spray orifice pads the logical of surface with the raised rubber
Hole corresponds connection.
Preferably, the propeller component includes propeller and spiral rowlock and is arranged on the propeller frame end portion electricity
It adjusts and motor, the both ends that the electricity is adjusted is electrically connected the flight control system, the top of the motor is rotatablely connected the spiral
Paddle.
Preferably, the heating end and the refrigeration end distinguish the exposed outside covered on the host and host shell
Inner cavity.
Preferably, the heat dissipation tank is embedded in the lower surface of the host shell.
The beneficial effects of the utility model are：
Lifting support mechanism includes undercarriage and is arranged on the nozzle of undercarriage bottom, and the surface of nozzle is coated with convex
Rubber pad is played, the nozzle of nozzle surface is connected with the through hole one-to-one corresponding on raised rubber pad surface, not only so that sprinkling is more equal
It is even, and play the role of support in landing；The bottom of flight control system is provided with the heat dissipation tank that surface carries ventilation hole, increases
The strong air flow of host shell inner cavity, and the semiconductor refrigerating part that host upper lid surface is coordinated to be embedded, refrigeration end are naked
The inner cavity of host shell is exposed at, can effectively be radiated to host shell inner cavity.
Description of the drawings
It in order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor
Under, it can also be obtained according to these attached drawings other attached drawings.
Fig. 1 is the stereogram of the utility model；
Fig. 2 is the top view of the utility model；
Fig. 3 is the sectional side view of the utility model；
Fig. 4 is the structural scheme of mechanism of the utility model nozzle；
Fig. 5 is the electric connection figure of the utility model.
In figure：1st, host housing；2nd, annular battery；3rd, propeller component；301st, propeller；4th, flight control system；5th, radiate
Case；6th, host upper cover；7th, semiconductor chilling plate；8th, undercarriage；9th, nozzle；10th, raised rubber pad；11st, chemical tank；12nd, pressure
Pump.
Specific embodiment
It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model part of the embodiment, instead of all the embodiments.Based on the implementation in the utility model
Example, those of ordinary skill in the art's all other embodiments obtained without creative efforts, belongs to
The scope of the utility model protection.
A kind of agricultural plant protection unmanned plane including host housing 1, dynamical system, flight control system 4 and lifting support mechanism, moves
Force system includes annular battery 2 and propeller component 3, and flight control system 4 is arranged on the inner cavity of host housing 1 and flight control system 4
Bottom is fixedly connected with heat dissipation tank 5, annular battery ring 2 around the side for being arranged on flight control system 4, the surrounded surface of heat dissipation tank 5 with
Lower surface is both provided with ventilation hole, and the upper surface of host housing 1 offers opening and the one side of opening is connected by articulate
There is host upper cover 6, the array of interior cavities of host upper cover 6 is provided with semiconductor chilling plate 7 and the electrical connection of semiconductor chilling plate 7 flies control system
System 4, semiconductor chilling plate 7 include refrigeration end and heating end, and refrigeration end is embedded respectively with heating end in the lower surface of host upper cover 6
With upper surface；
Lifting support mechanism includes undercarriage 8 and is connected to the nozzle 9 of 8 bottom of undercarriage, during the inside of undercarriage 8 is
Empty and undercarriage 8 is connected with the inner cavity of nozzle 9, and the lower surface of nozzle 9 is coated with raised rubber pad 10 and raised rubber pad
10 surface is evenly arranged with through hole；
Fixed respectively on chemical tank 11 and the opposite lateral wall of chemical tank 11 connect is embedded on the surface of 1 surrounding of host housing
Compression pump 12 and undercarriage 8 are connected to, the inner cavity of chemical tank 11 is connected with the inner cavity of undercarriage 8, and the electrical connection of compression pump 12 flies control
System 4.
Specifically, compression pump 12 is arranged in the inner cavity of host housing 1, the surface of nozzle 9 has been uniformly arranged spray orifice and spray
The through hole one-to-one corresponding that hole and raised rubber pad 10 surfaces connect, propeller component 3 include propeller 301 and spiral rowlock and
Propeller frame end portion electricity tune and motor are arranged on, electricity, which is adjusted, is electrically connected flight control system 4, the top rotation connection propeller 301 of motor,
Heating end is exposed in the outside of host upper cover 6 and the inner cavity of host shell respectively with refrigeration end, and heat dissipation tank 5 is embedded in host shell
Lower surface.
Lifting support mechanism includes undercarriage 8 and is arranged on the nozzle 9 of 8 bottom of undercarriage, the surface cladding of nozzle 9
There is raised rubber pad 10, the through hole one-to-one corresponding on 10 surfaces of nozzle 9 and raised rubber pad on 9 surface of nozzle connects, chemical tank 11
Undercarriage 8 and compression pump 12 are connected on opposite two side respectively, compression pump 12, will under the control action of flight control system 4
Medicament in chemical tank 11 is squeezed to nozzle 9, not only so that sprinkling is more uniform, but also the work of support is played in landing
With.
The bottom of flight control system 4 is provided with the hollow heat dissipation tank 5 that surface carries ventilation hole, enhances host shell inner cavity
Air flow, and the semiconductor refrigerating part that 6 surface of host upper cover is coordinated to be embedded, refrigeration end are exposed in host shell
Chamber, the heating end of semiconductor refrigerating part is exposed in the outside of host shell, can be more convenient during unmanned plane during flying
Ground is radiated by cross-ventilation and heat transfer, and refrigeration end is in the inner cavity of supporing shell, by heat transfer to host shell
Inner cavity is radiated, and simple in structure and heat dissipation effect is preferable.
Above example is only to illustrate the technical solution of the utility model, rather than its limitations；Although with reference to foregoing reality
Example is applied the utility model is described in detail, it will be understood by those of ordinary skill in the art that：It still can be to preceding
The technical solution recorded in each embodiment is stated to modify or carry out equivalent substitution to which part technical characteristic；And these
Modification is replaced, and the essence of appropriate technical solution is not made to depart from the spirit and model of various embodiments of the utility model technical solution
It encloses.
Claims (6)
1. a kind of agricultural plant protection unmanned plane, described dynamic including host housing, dynamical system, flight control system and lifting support mechanism
Force system includes annular battery and propeller component, and the flight control system is arranged on the inner cavity of the host housing and the winged control
The bottom of system is fixedly connected with heat dissipation tank, and the ring-type battery is circumferentially positioned at the side of the flight control system, and feature exists
In：The surrounded surface of the heat dissipation tank is both provided with ventilation hole with lower surface, and the upper surface of the host housing offers opening
And the one side of the opening is connected with host upper cover by articulate, the array of interior cavities of the host upper cover is provided with semiconductor
Cooling piece and the semiconductor chilling plate are electrically connected the flight control system, and the semiconductor chilling plate includes refrigeration end and heating
End, the refrigeration end are embedded the lower surface and upper surface covered on the host respectively with the heating end；
The lifting support mechanism includes undercarriage and the nozzle for being connected to the undercarriage bottom, the inside of the undercarriage
Be connected for hollow and described undercarriage with the inner cavity of the nozzle, the lower surface of the nozzle be coated with raised rubber pad and
The surface of the raised rubber pad is evenly arranged with through hole；
Fixed respectively on chemical tank and the opposite lateral wall of the chemical tank connect is embedded on the surface of the host housing surrounding
Compression pump and the undercarriage are connected to, the inner cavity of the chemical tank is connected with the inner cavity of the undercarriage, the compression pump electricity
Connect the flight control system.
2. a kind of agricultural plant protection unmanned plane according to claim 1, it is characterised in that：The compression pump is arranged on the master
In the inner cavity of machine shell.
3. a kind of agricultural plant protection unmanned plane according to claim 1, it is characterised in that：The surface of the nozzle is uniformly arranged
The spray orifice and spray orifice is connected with the through hole one-to-one corresponding on raised rubber pad surface.
4. a kind of agricultural plant protection unmanned plane according to claim 1, it is characterised in that：The propeller component includes spiral
Paddle and spiral rowlock and it is arranged on that the propeller frame end portion electricity is adjusted and motor, the both ends that the electricity is adjusted are electrically connected described
Flight control system, the top of the motor are rotatablely connected the propeller.
5. a kind of agricultural plant protection unmanned plane according to claim 1, it is characterised in that：The heating end and the refrigeration end
The exposed outside covered on the host and the inner cavity of host shell respectively.
6. a kind of agricultural plant protection unmanned plane according to claim 1, it is characterised in that：The heat dissipation tank is embedded in the master
The lower surface of casing body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721455198.8U CN207374677U (en) | 2017-11-03 | 2017-11-03 | A kind of agricultural plant protection unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721455198.8U CN207374677U (en) | 2017-11-03 | 2017-11-03 | A kind of agricultural plant protection unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207374677U true CN207374677U (en) | 2018-05-18 |
Family
ID=62334045
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721455198.8U Expired - Fee Related CN207374677U (en) | 2017-11-03 | 2017-11-03 | A kind of agricultural plant protection unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207374677U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108812601A (en) * | 2018-06-17 | 2018-11-16 | 苏州迅联佰丰智能科技有限公司 | A kind of unmanned fog machine of multiple wing circulating type agricultural of double-purpose spray head |
| CN112224415A (en) * | 2020-10-19 | 2021-01-15 | 黄远杰 | Pollination unmanned aerial vehicle with cooling and anti-deterioration functions |
-
2017
- 2017-11-03 CN CN201721455198.8U patent/CN207374677U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108812601A (en) * | 2018-06-17 | 2018-11-16 | 苏州迅联佰丰智能科技有限公司 | A kind of unmanned fog machine of multiple wing circulating type agricultural of double-purpose spray head |
| CN112224415A (en) * | 2020-10-19 | 2021-01-15 | 黄远杰 | Pollination unmanned aerial vehicle with cooling and anti-deterioration functions |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180518 Termination date: 20211103 |