CN205168898U - Environmental monitoring unmanned aerial vehicle - Google Patents
Environmental monitoring unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205168898U CN205168898U CN201520768132.9U CN201520768132U CN205168898U CN 205168898 U CN205168898 U CN 205168898U CN 201520768132 U CN201520768132 U CN 201520768132U CN 205168898 U CN205168898 U CN 205168898U
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- CN
- China
- Prior art keywords
- fuselage
- rotor bar
- connects
- bias circuit
- rotary wings
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- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses an environmental monitoring unmanned aerial vehicle, including fuselage and meteorological monitoring system, the fuselage is outside be streamlined, and the front end top symmetry of fuselage is equipped with two preceding rotor mast, and the activity of preceding rotor mast sets up on the fuselage, the rotatory wing before preceding rotor mast end perpendicularly upwards is equipped with, and the side top of fuselage is equipped with the first recess with preceding rotor mast and preceding rotatory wing adaptation, and first recess is used for holding the fold up preceding rotor mast and the preceding rotatory wing, the rear end top symmetry of fuselage is equipped with two back rotor mast, and back rotor mast end is perpendicularly to having the rotatory wing in back, be equipped with the meteorological monitoring system in the fuselage, the meteorological monitoring system includes outside monitoring facilities, solar cell, LED drive circuit, LED device and bias circuit, the utility model discloses unmanned aerial vehicle more does benefit to and carries, simultaneously can be accurate, timely, the efficient knows the real -time meteorological state in the air.
Description
Technical field
The utility model relates to a kind of unmanned plane, specifically a kind of environmental monitoring unmanned plane.
Background technology
Visible ray wireless communication technology can realize merging with current wireless communication system.Visible ray radio communication develops the new frequency spectrum resource of visible ray, not by complicated electromagnetic interference influence, ubiquitous communication can be realized while illumination, not limited visible light spectrum resource can provide high-capacity communication service, on airport, medical monitoring, to have a extensive future under water with under the special screnes such as mine.Unmanned plane militarily can be used for scouting, supervision, trunking traffic, electronic countermeasure, firepower guidance, combat success assessment, harassing and wrecking, temptation, over the ground (sea) attack, target simulation and early warning etc.At civil area, can be used for geodesic measurement, meteorological watch, city environment detect, earth resources exploration and forest fire protection etc., existing nobody carry convenient not.
Utility model content
The purpose of this utility model is to provide a kind of environmental monitoring unmanned plane, to solve the problem proposed in above-mentioned background technology.
For achieving the above object, the utility model provides following technical scheme:
A kind of environmental monitoring unmanned plane, comprise fuselage and weather monitoring system, described external fuselage is stream line pattern, two front rotor bars are arranged with above the front end of fuselage, front rotor bar is movably arranged on fuselage, front rotor bar ending vertical is upwards provided with front rotary wings, is provided with the first groove with front rotor bar and front rotary wings adaptation above the side of fuselage, and the first groove is for holding rotor bar and front rotary wings before folding; Rotor bar after being arranged with two above the rear end of described fuselage, rear rotor bar ending vertical is to having rear rotary wings, be provided with the second groove with rear rotor bar and rear rotary wings adaptation below the side of fuselage, the second groove is for holding rotor bar and rear rotary wings after folding; Be provided with weather monitoring system in described fuselage, weather monitoring system comprises external monitoring devices, solar cell, LED drive circuit, LED component and bias circuit; Described external monitoring devices comprises pick up camera, heat indicator, humidity gauge and wind indicator, the mouth of external monitoring devices connects the input end of bias circuit, the mouth of LED drive circuit connects the input end of bias circuit, the mouth of bias circuit connects the input end of LED component, bias circuit connects LED component, LED component connects photoelectric detection module, the input end of the mouth connection signal amplifier of photoelectric detection module, the mouth of signal amplifier connects the input end of wireless module, and wireless module connects terminal backstage.
Further, described fuselage bottom is provided with feet.
Compared with prior art, external fuselage of the present utility model is stream line pattern, decreases windage, make to fly energy consumption that is more stable and that decrease in flight course, simultaneously front rotor bar and rear rotor bar stagger setting, and rotor bar folds more convenient, makes unmanned plane be more conducive to carry; The real-time weather state in air can be understood accurately, in time, efficiently simultaneously.
Accompanying drawing explanation
Fig. 1 is the structural representation of environmental monitoring unmanned plane.
Fig. 2 is the connection diagram of weather monitoring system in environmental monitoring unmanned plane.
Detailed description of the invention
Be described in more detail below in conjunction with the technical scheme of detailed description of the invention to this patent.
Refer to Fig. 1-2, a kind of environmental monitoring unmanned plane, comprise fuselage 1 and weather monitoring system, described fuselage 1 outside is stream line pattern, two front rotor bars 2 are arranged with above the front end of fuselage 1, front rotor bar 2 is movably arranged on fuselage 1, front rotor bar 2 ending vertical is upwards provided with front rotary wings 21, the first groove 11 with front rotor bar 2 and front rotary wings 21 adaptation is provided with above the side of fuselage 1, first groove 11, for holding rotor bar 2 and front rotary wings 21 before folding, is provided with feet 13 bottom fuselage 1, rotor bar 3 after being arranged with two above the rear end of described fuselage 1, rear rotor bar 3 ending vertical is to having rear rotary wings 31, be provided with below the side of fuselage 1 with the second groove 12, second groove 12 of rear rotor bar 3 and rear rotary wings 31 adaptation for holding rotor bar 3 and rear rotary wings 31 after folding, be provided with weather monitoring system in described fuselage 1, weather monitoring system comprises external monitoring devices 2, solar cell 3, LED drive circuit 4, LED component 5 and bias circuit 6, and solar cell 3 is powered for whole system, described external monitoring devices 2 comprises pick up camera, heat indicator, humidity gauge and wind indicator, the mouth of external monitoring devices 2 connects the input end of bias circuit 6, the environmental information monitored is transferred to bias circuit 6 by external monitoring devices 2 as electronic signals, the mouth of LED drive circuit 4 connects the input end of bias circuit 6, LED drive circuit 4 provides vdc to bias circuit 6, the vdc of above-said current signal and LED drive circuit 4 is carried out coupling processing by bias circuit 6, produce coupled electrical signal, the mouth of bias circuit 6 connects the input end of LED component 5, above-mentioned coupled electrical signal is transferred to LED component 5 by bias circuit 6, driving LED device 5 is luminous, LED component 5 converts coupled electrical signal to optical signal, by the mode of transmission over radio by optical signal transmission to photoelectric detection module, the input end of the mouth connection signal amplifier of described photoelectric detection module, photoelectric detection module receives above-mentioned optical signal, and transfer to signal amplifier after optical signal is converted to electric signal, the mouth of signal amplifier connects the input end of wireless module, above-said current signal is carried out power gain by signal amplifier, and by the electric signal transmission after power gain to wireless module, the electric signal after power gain is transferred to terminal backstage by the mode of transmission over radio by wireless module.
Above the better embodiment of this patent is explained in detail, but this patent is not limited to above-mentioned embodiment, in the ken that one skilled in the relevant art possesses, various change can also be made under the prerequisite not departing from this patent aim.
Claims (2)
1. an environmental monitoring unmanned plane, comprise fuselage and weather monitoring system, it is characterized in that, described external fuselage is stream line pattern, be arranged with two front rotor bars above the front end of fuselage, front rotor bar is movably arranged on fuselage, and front rotor bar ending vertical is upwards provided with front rotary wings, be provided with the first groove with front rotor bar and front rotary wings adaptation above the side of fuselage, the first groove is for holding rotor bar and front rotary wings before folding; Rotor bar after being arranged with two above the rear end of described fuselage, rear rotor bar ending vertical is to having rear rotary wings, be provided with the second groove with rear rotor bar and rear rotary wings adaptation below the side of fuselage, the second groove is for holding rotor bar and rear rotary wings after folding; Be provided with weather monitoring system in described fuselage, weather monitoring system comprises external monitoring devices, solar cell, LED drive circuit, LED component and bias circuit; Described external monitoring devices comprises pick up camera, heat indicator, humidity gauge and wind indicator, the mouth of external monitoring devices connects the input end of bias circuit, the mouth of LED drive circuit connects the input end of bias circuit, the mouth of bias circuit connects the input end of LED component, bias circuit connects LED component, LED component connects photoelectric detection module, the input end of the mouth connection signal amplifier of photoelectric detection module, the mouth of signal amplifier connects the input end of wireless module, and wireless module connects terminal backstage.
2. environmental monitoring unmanned plane according to claim 1, is characterized in that, described fuselage bottom is provided with feet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520768132.9U CN205168898U (en) | 2015-10-06 | 2015-10-06 | Environmental monitoring unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520768132.9U CN205168898U (en) | 2015-10-06 | 2015-10-06 | Environmental monitoring unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205168898U true CN205168898U (en) | 2016-04-20 |
Family
ID=55732915
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520768132.9U Expired - Fee Related CN205168898U (en) | 2015-10-06 | 2015-10-06 | Environmental monitoring unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205168898U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107389862A (en) * | 2017-07-17 | 2017-11-24 | 王金锁 | Can flight instruments in one kind detection air chamber |
| WO2018108148A1 (en) * | 2016-12-16 | 2018-06-21 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle |
-
2015
- 2015-10-06 CN CN201520768132.9U patent/CN205168898U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018108148A1 (en) * | 2016-12-16 | 2018-06-21 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle |
| CN107389862A (en) * | 2017-07-17 | 2017-11-24 | 王金锁 | Can flight instruments in one kind detection air chamber |
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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: 20160420 Termination date: 20171006 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |