CN204642162U - Based on the atmosphere environment supervision space station of MWC four-axle aircraft - Google Patents
Based on the atmosphere environment supervision space station of MWC four-axle aircraft Download PDFInfo
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- CN204642162U CN204642162U CN201520278698.3U CN201520278698U CN204642162U CN 204642162 U CN204642162 U CN 204642162U CN 201520278698 U CN201520278698 U CN 201520278698U CN 204642162 U CN204642162 U CN 204642162U
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- atmosphere environment
- environment supervision
- axle aircraft
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- Y02B60/50—
Abstract
The utility model discloses a kind of atmosphere environment supervision space station based on MWC four-axle aircraft, comprise four-axle aircraft and atmosphere environment supervision module; Described four-axle aircraft comprises atmosphere environment supervision module described in fuselage and is arranged on fuselage, comprises STM nucleus module, wireless communication module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor and poly-lithium battery; Described wireless communication module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor are all connected with STM nucleus module; Described poly-lithium battery is that each several part is powered.The utility model solves a difficult problem for small space atmosphere environment supervision, and structure is simple, easy to use; Employ poly-lithium battery, more economize energy, be beneficial to environmental protection; Range of use is wide, has very large promotional value.
Description
Technical field
The utility model relates to data monitoring instrument field, is specifically related to a kind of atmosphere environment supervision space station based on MWC four-axle aircraft.
Background technology
Air environment information belongs to one of data very important in the data of environmental quality, all plays very important work in fields such as biology, medical science, storage production, agriculture and forestry.In the prior art, usually the method by placing multiple air environment measurer comes humiture, illuminance, the dust granules information of monitoring environment, but this needs to buy multiple atmosphere environment supervision device, increase financial cost, if monitored successively by artificial hand-held monitor, then time cost increases and very inconvenient, and the dangerous complexity of environment sometimes to be monitored, personal monitoring is difficult to realize.
Utility model content
In order to solve the problem, the utility model discloses a kind of atmosphere environment supervision space station based on MWC four-axle aircraft.
The technical solution of the utility model is as follows:
Based on the atmosphere environment supervision space station of MWC four-axle aircraft, comprise four-axle aircraft and atmosphere environment supervision module; Described four-axle aircraft comprises fuselage; In described fuselage, flight control modules is installed; Described fuselage surrounding is provided with in cross-shaped four mechanical arms, and intersecting angle is 90 °; The end of each mechanical arm is fixed with electronic governor and motor, and motor is provided with screw propeller; Described atmosphere environment supervision module is arranged on fuselage, comprises STM nucleus module, wireless communication module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor and poly-lithium battery; Described wireless communication module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor are all connected with STM nucleus module; Described poly-lithium battery is that each several part is powered.
Its further technical scheme is: in described four screw propellers, two screw propeller clickwises, two screw propeller left-hand revolutions; Two the screw propeller hand of rotation be on same straight line are identical.
Its further technical scheme is: described fuselage adopts glass fibre to make.
Its further technical scheme is: the flying of described flight control modules to be model be MultiWii SE v2.5 controls plate.
Its further technical scheme is: the model of described STM nucleus module is STM8S105K4.
Its further technical scheme is: the model of described wireless communication module is USR-WIFI232-TEVKV2.
Its further technical scheme is: the model of described Temperature Humidity Sensor is DHT11.
Its further technical scheme is: the model of described illuminance sensor is T5516.
Its further technical scheme is: the model of described dust granules sensor is GP2Y1050AU0F.
Advantageous Effects of the present utility model is:
The utility model solves a difficult problem for narrow and small ambient atmosphere environmental monitoring, can be applicable to the industry field that each needs to carry out atmosphere environment supervision, also can be used for the atmosphere environment supervision of civilian near-earth lower atmosphere.Generally, only needing precisely to control four-axle aircraft flight to detecting target area, the air environment information of target area can be obtained by intelligent mobile terminal.The utility model structure is simple, easy to use; Four-axle aircraft and atmosphere environment supervision module employ poly-lithium battery and power, more economize energy, be beneficial to environmental protection; The utility model range of use is wide, has very large promotional value.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of four-axle aircraft.
Fig. 2 is the schematic diagram that atmosphere environment supervision module is arranged on four-axle aircraft.
Detailed description of the invention
Fig. 1 is the schematic diagram of four-axle aircraft, and four-axle aircraft comprises fuselage, and fuselage is spliced by fuselage upper plate 1 and fuselage lower plate 2 and forms, and is provided with flight control modules in fuselage.Fuselage surrounding is provided with in cross-shaped four mechanical arms 8, and intersecting angle is 90 °, and the end of each mechanical arm 8 is fixed with motor 3 and electronic governor, and motor 3 is brushless motor, each motor 3 is provided with a screw propeller.In four screw propellers, two screw propeller clickwises, two screw propeller left-hand revolutions, two the screw propeller hand of rotation be on same straight line are identical.In the present embodiment, screw propeller 4 and screw propeller 7 rotate according to anticlockwise direction, and screw propeller 5 and screw propeller 6 rotate according to clockwise direction.
Fig. 2 is the schematic diagram that air environment module is arranged on four-axle aircraft.Atmosphere environment supervision module is arranged in fuselage, comprises STM nucleus module, wireless communication module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor and poly-lithium battery.STM nucleus module is a MCU (Microcontroller Unit, micro controller system) module, for establishment and the program of recording, to control the function of other modules.Temperature Humidity Sensor, illuminance sensor, dust granules sensor are used for recording the humiture in air, illuminance and dust granules situation respectively, and then the situation of monitoring air environment.Wireless communication module is used for transmitting data with intelligent mobile terminal.The battery that the utility model uses is poly-lithium battery, and battery is fixed in fuselage upper plate 1 and fuselage lower plate 2, for the various piece of atmosphere environment supervision module and four-axle aircraft module is powered.Measured monitoring data is sent on the intelligent mobile terminal such as mobile phone, panel computer by wireless communication module, and reads the information such as humiture, illuminance, dust granules of air environment by the dependent instruction that intelligent mobile terminal sends.
Each several part in atmosphere environment supervision module of the present utility model is commercial goods, can directly buy.In the present embodiment, in four-axle aircraft part, the flying of flight control modules to be model be MultiWii SE v2.5 controls plate, can be edited and burning dependent program by Arduino IDE software; The model of electronic governor is Xin Xida 30A; Motor 3 is brushless motor, and model is Xin Xida A2212; The model of screw propeller is 1045.Fuselage upper plate 1 and fuselage lower plate 2 adopt glass fibre to make.In atmosphere environment supervision module, the model of STM nucleus module is STM8S105K4, the WIFI module of wireless communication module to be model be USR-WIFI232-TEVKV2, the model of Temperature Humidity Sensor is DHT11, the model of illuminance sensor is T5516, and the model of dust granules sensor is GP2Y1050AU0F.The battery of powering for each several part is poly-lithium battery.
During use, first intelligent mobile terminal and atmosphere environment supervision module are carried out WIFI P2P successful matching, then under the prerequisite ensureing four-axle aircraft flying power, flight monitors space to predetermined.Pass through intelligent mobile terminal, such as Android phone, the command information reading atmospheric environmental parameters is sent to atmosphere environment supervision module, USR-WIFI232-TEVKV2 wireless data transmission module in atmosphere environment supervision module is transmitted to STM nucleus module after obtaining upper computer instruction, by the control of STM nucleus module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor records the humiture in air respectively, illuminance, the air environment information such as PM2.5, read the information of each sensor record in real time by STM nucleus module after, by wireless data transmission module, air environment information is forwarded back to intelligent mobile terminal, realize the function at air environment detection space station.
Above-described is only preferred implementation of the present utility model, and the utility model is not limited to above embodiment.Be appreciated that the oher improvements and changes that those skilled in the art directly derive or associate under the prerequisite not departing from spirit of the present utility model and design, all should think and be included within protection domain of the present utility model.
Claims (8)
1. based on an atmosphere environment supervision space station for MWC four-axle aircraft, it is characterized in that: comprise four-axle aircraft and atmosphere environment supervision module; Described four-axle aircraft comprises fuselage; In described fuselage, flight control modules is installed; Described fuselage surrounding is provided with in cross-shaped four mechanical arms, and intersecting angle is 90 °; The end of each mechanical arm is fixed with electronic governor and motor, and motor is provided with screw propeller; Described atmosphere environment supervision module is arranged on fuselage, comprises STM nucleus module, wireless communication module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor and poly-lithium battery; Described wireless communication module, Temperature Humidity Sensor, illuminance sensor, dust granules sensor are all connected with described STM nucleus module; Described poly-lithium battery is that each several part is powered.
2., as claimed in claim 1 based on the atmosphere environment supervision space station of MWC four-axle aircraft, it is characterized in that: in described four screw propellers, two screw propeller clickwises, two screw propeller left-hand revolutions; Two the screw propeller hand of rotation be on same straight line are identical.
3. as claimed in claim 1 based on the atmosphere environment supervision space station of MWC four-axle aircraft, it is characterized in that: the flying of described flight control modules to be model be MultiWii SE v2.5 controls plate.
4., as claimed in claim 1 based on the atmosphere environment supervision space station of MWC four-axle aircraft, it is characterized in that: the model of described STM nucleus module is STM8S105K4.
5., as claimed in claim 1 based on the atmosphere environment supervision space station of MWC four-axle aircraft, it is characterized in that: the model of described wireless communication module is USR-WIFI232-TEVKV2.
6., as claimed in claim 1 based on the atmosphere environment supervision space station of MWC four-axle aircraft, it is characterized in that: the model of described Temperature Humidity Sensor is DHT11.
7., as claimed in claim 1 based on the atmosphere environment supervision space station of MWC four-axle aircraft, it is characterized in that: the model of described illuminance sensor is T5516.
8., as claimed in claim 1 based on the atmosphere environment supervision space station of MWC four-axle aircraft, it is characterized in that: the model of described dust granules sensor is GP2Y1050AU0F.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520278698.3U CN204642162U (en) | 2015-04-30 | 2015-04-30 | Based on the atmosphere environment supervision space station of MWC four-axle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520278698.3U CN204642162U (en) | 2015-04-30 | 2015-04-30 | Based on the atmosphere environment supervision space station of MWC four-axle aircraft |
Publications (1)
| Publication Number | Publication Date |
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| CN204642162U true CN204642162U (en) | 2015-09-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520278698.3U Expired - Fee Related CN204642162U (en) | 2015-04-30 | 2015-04-30 | Based on the atmosphere environment supervision space station of MWC four-axle aircraft |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270645A (en) * | 2015-11-11 | 2016-01-27 | 惠州市东阳智能技术股份有限公司 | Aerial photographic aircraft |
| CN105387887A (en) * | 2015-12-03 | 2016-03-09 | 上海交通大学 | Aircraft atmosphere monitoring system based on printing sensor |
-
2015
- 2015-04-30 CN CN201520278698.3U patent/CN204642162U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270645A (en) * | 2015-11-11 | 2016-01-27 | 惠州市东阳智能技术股份有限公司 | Aerial photographic aircraft |
| CN105387887A (en) * | 2015-12-03 | 2016-03-09 | 上海交通大学 | Aircraft atmosphere monitoring system based on printing sensor |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150916 Termination date: 20200430 |