CN205589478U - Unmanned aerial vehicle with mosquito repellent function - Google Patents
Unmanned aerial vehicle with mosquito repellent function Download PDFInfo
- Publication number
- CN205589478U CN205589478U CN201620380650.8U CN201620380650U CN205589478U CN 205589478 U CN205589478 U CN 205589478U CN 201620380650 U CN201620380650 U CN 201620380650U CN 205589478 U CN205589478 U CN 205589478U
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- CN
- China
- Prior art keywords
- unmanned plane
- function
- driving mosquitoes
- thickness
- utility
- 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.)
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Links
- 239000000077 insect repellent Substances 0.000 title abstract 2
- 238000000576 coating method Methods 0.000 claims abstract description 18
- 239000011248 coating agent Substances 0.000 claims abstract description 10
- 241000255925 Diptera Species 0.000 claims description 14
- 125000005375 organosiloxane group Chemical group 0.000 claims description 8
- 230000002787 reinforcement Effects 0.000 claims description 7
- 239000011152 fibreglass Substances 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 6
- 241000238631 Hexapoda Species 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 3
- 229910052799 carbon Inorganic materials 0.000 claims description 3
- 239000000835 fiber Substances 0.000 claims description 3
- 238000003384 imaging method Methods 0.000 claims description 3
- 238000005259 measurement Methods 0.000 claims description 3
- 239000011521 glass Substances 0.000 claims 2
- KPUWHANPEXNPJT-UHFFFAOYSA-N disiloxane Chemical class [SiH3]O[SiH3] KPUWHANPEXNPJT-UHFFFAOYSA-N 0.000 claims 1
- 239000004744 fabric Substances 0.000 claims 1
- 239000000843 powder Substances 0.000 claims 1
- 239000003365 glass fiber Substances 0.000 abstract description 3
- 238000013461 design Methods 0.000 abstract description 2
- 125000000962 organic group Chemical group 0.000 abstract 1
- 244000045947 parasite Species 0.000 abstract 1
- 239000004447 silicone coating Substances 0.000 abstract 1
- 238000010276 construction Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 206010003399 Arthropod bite Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
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- Catching Or Destruction (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle with mosquito repellent function, including the fuselage, set up horn on the fuselage, set up rotation axis on the horn, set up at rotatory epaxial paddle, the surface of rotation axis is equipped with organo -silicone coating, glass fiber enhancement layer, 3M reflective film layer and fluorescent coating in proper order, the surface of unmanned aerial vehicle casing is equipped with a plurality of triangle -shaped recesses, it has ultrasonic wave expelling parasite ware to inlay in the triangle -shaped recess. The utility model discloses stability is good, and the reliability is high, and the modern design is easily promoted and is implemented.
Description
Technical field
This utility model relates to unmanned plane field, particularly relates to a kind of unmanned plane with function of driving mosquitoes.
Background technology
UAV, is called for short unmanned plane, has maneuverability, is swift in response, without artificial driving
The advantages such as low are required with operation.By carrying polytype sensor, it is possible to achieve image real-time Transmission,
The functions such as high-order area detection.Unmanned plane can be applicable to military affairs, scientific research, civilian three big fields, concrete body
Now electric power, communication, meteorology, environment, ocean, agricultural, explore, take precautions against natural calamities, the aspect such as public security.
At present, in the poor open air of environment or in the summer of heat, when operating and use unmanned plane,
Operator is easily by mosquito bite.
Utility model content
The purpose of this utility model is to overcome the deficiency of above-mentioned prior art to provide one to have anophelifuge merit
The unmanned plane of energy.
For achieving the above object, this utility model provides a kind of unmanned plane with function of driving mosquitoes, including machine
Body, the horn being arranged on fuselage, the rotary shaft being arranged on horn, setting blade on the rotary shaft,
The outer surface of described rotary shaft is sequentially provided with organosiloxanes coatings, fiberglass reinforcement layers, 3M reflective membrane
Layer and fluorescent coating, the surface of described unmanned plane housing is provided with some triangular grooves, described triangle
Ultrasonic insects expelling device it is inlaid with in groove.
Preferably, described fuselage also has cabin, loads accumulator, in described accumulator in described cabin
Connect and have residual capacity measurement module.
Preferably, imaging device and positioner also it are mounted with in described cabin.
Preferably, described fuselage is that carbon fibre material makes.
Preferably, the thickness of described organosiloxanes coatings is 0.02mm to 0.03mm.
Preferably, the thickness of described fiberglass reinforcement layers is 0.4mm to 0.5mm.
Preferably, the thickness of described 3M reflexed light film is 0.2mm to 0.3mm.
Preferably, the thickness of described fluorescent coating is 0.05mm to 0.08mm.
The beneficial effects of the utility model are: rotary shaft outer surface lay successively organosiloxanes coatings,
Fiberglass reinforcement layers, 3M reflexed light film and fluorescent coating, so that rotary shaft overall corrosion-resistant resisting should
Power performance effectively improves and can be effectively improved the identification of unmanned plane, on the surface of unmanned plane housing
It is provided with some triangular grooves, is inlaid with ultrasonic insects expelling device in triangular groove, so can effectively play
During unmanned plane near-earth flight, the space being positioned at around operator is not easy to there is the problem that mosquito assembles, from
And play the effect of protection operator.This utility model simple in construction, durability is high, low cost of manufacture.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram of this utility model one embodiment；
Fig. 2 is the structural representation on this utility model foot rest surface；
Reference:
Fuselage 10；
Horn 20；
Rotary shaft 30；
Organosiloxanes coatings 301；
Fiberglass reinforcement layers 302；
3M reflexed light film 303；
Fluorescent coating 304；
Blade 40；
Triangular groove 50.
The realization of this utility model purpose, functional characteristics and advantage will in conjunction with the embodiments, do referring to the drawings into
One step explanation.
Detailed description of the invention
Of the present utility model embodiment is described below in detail, and the example of described embodiment is shown in the drawings,
The most same or similar label represents same or similar element or has same or like merit
The element of energy.The embodiment described below with reference to accompanying drawing is exemplary, it is intended to be used for explaining this reality
With novel, and it is not intended that to restriction of the present utility model.
In description of the present utility model, it is to be understood that term " " center ", " longitudinally ", " horizontal stroke
To ", " length ", " width ", " thickness ", " on ", D score, "front", "rear",
"left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward ",
The orientation of the instruction such as " clockwise ", " counterclockwise " or position relationship be based on orientation shown in the drawings or
Position relationship, is for only for ease of description this utility model and simplifies description rather than instruction or hint institute
Refer to device or element must have specific orientation, with specific azimuth configuration and operation, therefore can not
It is interpreted as restriction of the present utility model.
In this utility model, unless otherwise clearly defined and limited, term " install ", " being connected ",
" connect ", the term such as " fixing " should be interpreted broadly, and connects for example, it may be fixing, it is also possible to
It is to removably connect, or is integrally connected；Can be to be mechanically connected, it is also possible to be electrical connection；Can be
It is joined directly together, it is also possible to be indirectly connected to by intermediary, can be the connection of two element internals.Right
For those of ordinary skill in the art, can understand that above-mentioned term is new in this practicality as the case may be
Concrete meaning in type.
Referring to figs. 1 through Fig. 2, a kind of unmanned plane with function of driving mosquitoes, including fuselage 10, it is arranged at machine
Horn 20 on body 10, the rotary shaft 30 being arranged on horn 20, the oar that is arranged in rotary shaft 30
Leaf 40, the outer surface of described rotary shaft 30 is sequentially provided with organosiloxanes coatings 301, glass fibre is strengthened
Layer 302,3M reflexed light film 303 and fluorescent coating 304, if the surface of described unmanned plane housing is provided with
Dry triangular groove 50, is inlaid with ultrasonic insects expelling device in described triangular groove 50.
Preferably, described fuselage 10 also has cabin, loads accumulator, described accumulator in described cabin
Upper connection has residual capacity measurement module.
Preferably, imaging device and positioner also it are mounted with in described cabin.
Preferably, described fuselage 10 makes for carbon fibre material.
Preferably, the thickness of described organosiloxanes coatings 301 is 0.02mm to 0.03mm.
Preferably, the thickness of described fiberglass reinforcement layers 302 is 0.4mm to 0.5mm.
Preferably, the thickness of described 3M reflexed light film 303 is 0.2mm to 0.3mm.
Preferably, the thickness of described fluorescent coating 304 is 0.05mm to 0.08mm.
In sum, organosiloxanes coatings 301, glass fibre are laid successively at rotary shaft 30 outer surface
Enhancement Layer 302,3M reflexed light film 303 and fluorescent coating 304, so that the overall corrosion resistant of rotary shaft 30
Erosion resistance to stress performance effectively improves and can be effectively improved the identification of unmanned plane, at unmanned plane housing
Surface be provided with some triangular grooves 50, be inlaid with ultrasonic insects expelling device in triangular groove 50, so
When can effectively play unmanned plane near-earth flight, the space being positioned at around operator is not easy to there is mosquito and assembles
Problem, thus play protection operator effect.This utility model simple in construction, durability is high, system
Making low cost, good stability, reliability is high, novel in design, it is easy to promotion and implementation.
In the description of this specification, reference term " embodiment ", " some embodiments ", " show
Example ", the description of " concrete example " or " some examples " etc. means to combine this embodiment or example is retouched
Specific features, structure, material or the feature stated be contained at least one embodiment of the present utility model or
In example.In this manual, the schematic representation to above-mentioned term is not necessarily referring to identical enforcement
Example or example.And, the specific features of description, structure, material or feature can be at any one
Or multiple embodiment or example combine in an appropriate manner.
Although above it has been shown and described that embodiment of the present utility model, it is to be understood that above-mentioned
Embodiment is exemplary, it is impossible to be interpreted as restriction of the present utility model, the ordinary skill people of this area
Member can be right in the range of this utility model in the case of without departing from principle of the present utility model and objective
Above-described embodiment is changed, revises, replaces and modification.
Claims (8)
1. a unmanned plane with function of driving mosquitoes, it is characterised in that include fuselage, be arranged on fuselage
Horn, the rotary shaft being arranged on horn, blade on the rotary shaft is set, outside described rotary shaft
Surface is sequentially provided with organosiloxanes coatings, fiberglass reinforcement layers, 3M reflexed light film and fluorescent material and is coated with
Layer, the surface of described unmanned plane housing is provided with some triangular grooves, is inlaid with in described triangular groove
Ultrasonic insects expelling device.
The unmanned plane with function of driving mosquitoes the most according to claim 1, it is characterised in that described machine
Body also has cabin, loads accumulator in described cabin, and described accumulator connects residual capacity measurement
Module.
The unmanned plane with function of driving mosquitoes the most according to claim 2, it is characterised in that described machine
Imaging device and positioner also it is mounted with in cabin.
The unmanned plane with function of driving mosquitoes the most according to claim 1, it is characterised in that described machine
Make as carbon fibre material.
The unmanned plane with function of driving mosquitoes the most according to claim 1, it is characterised in that described in have
The thickness of organic siloxane coating is 0.02mm to 0.03mm.
The unmanned plane with function of driving mosquitoes the most according to claim 1, it is characterised in that described glass
The thickness of glass fabric reinforcement is 0.4mm to 0.5mm.
The unmanned plane with function of driving mosquitoes the most according to claim 1, it is characterised in that described
The thickness of 3M reflexed light film is 0.2mm to 0.3mm.
The unmanned plane with function of driving mosquitoes the most according to claim 1, it is characterised in that described glimmering
The thickness of light powder coating is 0.05mm to 0.08mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620380650.8U CN205589478U (en) | 2016-04-29 | 2016-04-29 | Unmanned aerial vehicle with mosquito repellent function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620380650.8U CN205589478U (en) | 2016-04-29 | 2016-04-29 | Unmanned aerial vehicle with mosquito repellent function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205589478U true CN205589478U (en) | 2016-09-21 |
Family
ID=56933444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620380650.8U Expired - Fee Related CN205589478U (en) | 2016-04-29 | 2016-04-29 | Unmanned aerial vehicle with mosquito repellent function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205589478U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110291009A (en) * | 2016-12-13 | 2019-09-27 | Mu-G知识管理有限责任公司 | Insect elimination system and application thereof |
| CN110461147A (en) * | 2017-03-25 | 2019-11-15 | 余绍炽 | Multifunctional light electroacoustics ion unmanned plane |
-
2016
- 2016-04-29 CN CN201620380650.8U patent/CN205589478U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110291009A (en) * | 2016-12-13 | 2019-09-27 | Mu-G知识管理有限责任公司 | Insect elimination system and application thereof |
| CN110461147A (en) * | 2017-03-25 | 2019-11-15 | 余绍炽 | Multifunctional light electroacoustics ion unmanned plane |
| CN110461147B (en) * | 2017-03-25 | 2022-05-13 | 余绍炽 | Multifunctional photoelectric acoustic ion unmanned aerial vehicle |
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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: 20160921 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |