CN205060018U - Unmanned aerial vehicle for environmental monitoring - Google Patents
Unmanned aerial vehicle for environmental monitoring Download PDFInfo
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- CN205060018U CN205060018U CN201520261147.6U CN201520261147U CN205060018U CN 205060018 U CN205060018 U CN 205060018U CN 201520261147 U CN201520261147 U CN 201520261147U CN 205060018 U CN205060018 U CN 205060018U
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- unmanned plane
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Abstract
The utility model provides an unmanned aerial vehicle for environmental monitoring which the structural feature is: connection frame in foot rest upper end is installed in and is flown accuse and power supply system, and the camera is installed to the frame lower extreme, and the upper end is connected the installation number and is passed the system, is schemed biography system and "Global position" device, four screws are connected through four brushless motor in the frame upper end, and the screw symmetry sets up on four angles of unmanned aerial vehicle, and gas analysis system installs at whole unmanned aerial vehicle lower extreme, through the foot rest erection joint, and the last power that is provided with of gas analysis system. The utility model has the advantages of this unmanned aerial vehicle can the VTOL, not restricted by the topography, and when taking place the toxic gas and leak, the transmission that the monitoring environment data are quick is come out in the core area of the arrival scene of the accident that can be very fast, can also replace the monitoring personnel to carry out the high altitude, and the collection of the atmosphere data in low latitude is not restricted by any topography. This unmanned aerial vehicle is particularly suitable for the high altitude, low latitude, environment that manual work under the poisonous environment can't be monitored in person.
Description
Technical field
The utility model belongs to unmanned plane field, relates to and can apply high-altitude, low latitude, the unmanned plane of a kind of monitoring of environmental of the environment manually cannot in person monitored under toxic environment.
Background technology
Along with the development of contemporary society's state-of-art, unmanned plane enters into civil area from military domain gradually, more affects our life.Existing environmental monitoring generally needs huge manpower, the support of material resources, and time span is large, sometimes even has danger.Unmanned plane then has huge advantage, its mobility strong, can monitor on a large scale at short notice, and can fixed point monitoring.
Summary of the invention
Manpower can only be relied on to overcome existing environmental monitoring, the utility model provides a kind of environmental monitoring unmanned plane, this unmanned plane people can not only complete all tasks of conventional environment monitoring, and independently can also perform the task given by ground staff aloft.
The utility model object is achieved in that a kind of environmental monitoring unmanned plane, mainly comprises; Screw propeller, camera, brushless motor, Data transfer system, image transmission system, foot rest, gas analysis system, frame, fly control and electric power system, global pick device and power supply; It is characterized in that: foot rest upper end connection frame, frame is provided with and flies control and electric power system, frame lower end is provided with camera, upper end connection Data transfer system, image transmission system and global pick device, described frame upper end connects four screw propellers by four brushless motors, and screw propeller is symmetricly set on four angles of unmanned plane, and gas analysis system is arranged on whole unmanned plane lower end, installed by foot rest and connect, gas analysis system is provided with power supply.
Described four screw propellers, drive its High Rotation Speed by brushless motor and produce power.
Described camera, for gather unmanned plane remove the image of environment, sound signal.
Described brushless motor, correspondingly with screw propeller is arranged, and is used for driving it to rotate and produces power.
Described Data transfer system, sends by the frequency range of 5.8GHZ with by data acquired on gas analysis system.
Described image transmission system, returns with the image gathered by high-definition camera and audio data transmission.
Described foot rest, with support unmanned plane.
Described gas analysis system, comes the gaseous species that exists in testing environment and concentration with gas sensor, carry out high-precision analysis, and Data transfer system is returned to ground controlling personnel to the air in current residing space.
Described frame, supports whole unmanned plane.
Describedly fly control and electric power system, with the whole unmanned plane of control, and provide the electric energy needed for unmanned plane.
Described global pick device, with reception GPS(global positioning system), to complete the real-time location of unmanned plane.
Described power supply, for the power supply of whole unmanned plane.
The beneficial effects of the utility model are: traditional environmental monitoring has many restrictions, such as danger point etc., and monitoring personnel can not go in person, also just can not the first hand data of Real-time Obtaining, and need to consume huge manpower and materials.This novel practical provides a kind of environmental monitoring unmanned plane, avoid above drawback completely, can complete monitoring task at short notice by an operating personal, and this unmanned plane can vertical takeoff and landing, does not limit by landform, when there is noxious gas and leaking, the core area of the arrival scene of the accident that can be very fast, transmits out monitoring of environmental data fast speed, and monitoring personnel can also be replaced to carry out high-altitude, the collection of the atmosphere data in low latitude, does not limit by any landform.This unmanned plane is particularly suitable for high-altitude, low latitude, the environment manually cannot in person monitored under toxic environment.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is upward view of the present utility model.
Fig. 3 is birds-eye view of the present utility model.
Fig. 4 is that of the present utility model flying is controlled and electric power system schematic diagram.
Fig. 5 is gas analysis system schematic diagram of the present utility model.
In the drawings, 1, screw propeller, 2, camera, 3, brushless motor, 4, Data transfer system, 5, image transmission system, 6, foot rest, 7, gas analysis system, 8, frame, 9, fly control and electric power system, 10, global pick device, 11, power supply.
Detailed description of the invention
A kind of environmental monitoring unmanned plane, mainly comprises; Screw propeller 1, camera 2, brushless motor 3, Data transfer system 4, image transmission system 5, foot rest 6, gas analysis system 7, frame 8, fly control and electric power system 9 and global pick device 10, power supply 11; It is characterized in that: foot rest 6 upper end connection frame 8, frame 8 is provided with and flies control and electric power system 9, frame 6 lower end is provided with camera 2, upper end connection Data transfer system 4, image transmission system 5 and global pick device 10, described frame 6 upper end connects four screw propellers 1 by four brushless motors 3, and screw propeller 1 is symmetricly set on four angles of unmanned plane, and gas analysis system 7 is arranged on whole unmanned plane lower end, installed by foot rest 6 and connect, gas analysis system 7 is provided with power supply 11.
Further, described flying is controlled and electric power system 9, it mainly comprises: fly control figure and to conduct electricity platform, GPS module, remote control receiver, fly to control central process unit, image acquisition device, four road electronic governors, weather gauge, altimeter, triaxial accelerometer, three-axis gyroscope, three axle magneto-meter (magnetic compass) and fly control power supply, remote control receiver controls central process unit by Signal transmissions to flying, fly control central process unit and connect four road electronic governors, four road electronic governors are connected with the motor of unmanned plane, GPS module, weather gauge, altimeter, triaxial accelerometer, three-axis gyroscope, three axle magneto-meter (magnetic compass) with fly control central process unit be connected, and controlled by it.
Principle of design of the present utility model, mainly comprises autopilot system and environmental monitoring system composition.Autopilot system is made up of sensor-based system, master control system, power system.Environmental monitoring system is made up of gas analysis system and image transmission system, Data transfer system, install with this unmanned plane below.Sensor-based system is made up of sensors such as gyroscope, accelerometer, weather gauge, turn meter, compass, GPS, obtains this unmanned plane course information and locus, velocity information etc.Master control system adopts STM32F102 to be that central core CPU and peripheral sensor circuit combine, and determines the flight attitude of unmanned plane, flight position and direction by the data gathered.The PWM ripple that power system is exported by main control chip controls four brushless motor carrying screws thus makes the skyborne movement of unmanned plane.Gas analysis system, by the gaseous species that utilizes gas sensor and come to exist in testing environment and concentration, has the characteristic of selective absorbing according to the infrared ray of different component gas to different wave length and works.Image transmission system is made up of the high-resolution camera below unmanned plane and figure biography, can pass necessary view data aloft when unmanned plane can be made to run in real time back.Data transfer system is made up of digital transmission module, and the real-time transmission of the data that gas analysis system can be obtained by 5.8GHZ frequency range is returned.Make this unmanned plane finally can reach environmental monitoring object.
Claims (2)
1. an environmental monitoring unmanned plane, mainly comprises; Screw propeller, camera, brushless motor, Data transfer system, image transmission system, foot rest, gas analysis system, frame, fly control and electric power system, global pick device and power supply; It is characterized in that: foot rest upper end connection frame, frame is provided with and flies control and electric power system, frame lower end is provided with camera, upper end connection Data transfer system, image transmission system and global pick device, described frame upper end connects four screw propellers by four brushless motors, and screw propeller is symmetricly set on four angles of unmanned plane, and gas analysis system is arranged on whole unmanned plane lower end, installed by foot rest and connect, gas analysis system is provided with power supply.
2. a kind of environmental monitoring unmanned plane according to claim 1, it is characterized in that: described in fly control and electric power system mainly comprise GPS module, remote control receiver, fly to control central process unit, four road electronic governors, weather gauge, altimeter, triaxial accelerometer, three-axis gyroscope and three axle magneto-meter, remote control receiver controls central process unit by Signal transmissions to flying, fly control central process unit and connect four road electronic governors, four road electronic governors are connected with the motor of unmanned plane, GPS module, weather gauge, altimeter, triaxial accelerometer, three-axis gyroscope, three axle magneto-meter with fly control central process unit be connected, and controlled by it.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520261147.6U CN205060018U (en) | 2015-04-28 | 2015-04-28 | Unmanned aerial vehicle for environmental monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520261147.6U CN205060018U (en) | 2015-04-28 | 2015-04-28 | Unmanned aerial vehicle for environmental monitoring |
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| Publication Number | Publication Date |
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| CN205060018U true CN205060018U (en) | 2016-03-02 |
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| CN201520261147.6U Expired - Fee Related CN205060018U (en) | 2015-04-28 | 2015-04-28 | Unmanned aerial vehicle for environmental monitoring |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105799923A (en) * | 2016-04-28 | 2016-07-27 | 南京信息工程大学 | Four-rotor aircraft-based carrying manipulator |
| CN105891908A (en) * | 2016-04-19 | 2016-08-24 | 华南农业大学 | Airborne weather station apparatus for unmanned plane, and application method thereof |
| CN105974934A (en) * | 2016-06-24 | 2016-09-28 | 天津理工大学 | Air quality intelligent monitoring quadrotor formation system based on pilotage-following method |
| CN106323244A (en) * | 2016-08-18 | 2017-01-11 | 广州地理研究所 | Reservoir capacity monitoring method and device based on unmanned aerial vehicle |
| CN106516095A (en) * | 2016-12-21 | 2017-03-22 | 南京信息工程大学 | Specialized unmanned aerial vehicle for measuring wind direction and speed |
| CN107389385A (en) * | 2017-07-14 | 2017-11-24 | 深圳市可飞科技有限公司 | High-altitude gas detecting system and detection method |
| CN107416204A (en) * | 2016-04-11 | 2017-12-01 | 白伟华 | A kind of unmanned plane for monitoring ice condition key element |
| WO2017219255A1 (en) * | 2016-06-21 | 2017-12-28 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicles with tilting propellers, and associated systems and methods |
| CN109239715A (en) * | 2018-09-20 | 2019-01-18 | 嘉兴河海中控信息科技有限公司 | Unmanned plane Doppler's current surveying device |
| CN109814470A (en) * | 2019-03-26 | 2019-05-28 | 河南小兵网络科技有限公司 | A kind of quadrotor drone monitoring comprehensive platform |
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2015
- 2015-04-28 CN CN201520261147.6U patent/CN205060018U/en not_active Expired - Fee Related
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107416204A (en) * | 2016-04-11 | 2017-12-01 | 白伟华 | A kind of unmanned plane for monitoring ice condition key element |
| CN105891908A (en) * | 2016-04-19 | 2016-08-24 | 华南农业大学 | Airborne weather station apparatus for unmanned plane, and application method thereof |
| CN105799923A (en) * | 2016-04-28 | 2016-07-27 | 南京信息工程大学 | Four-rotor aircraft-based carrying manipulator |
| CN109314452A (en) * | 2016-06-21 | 2019-02-05 | 深圳市大疆创新科技有限公司 | Unmanned plane and related system and method with tilting propeller |
| CN112838731A (en) * | 2016-06-21 | 2021-05-25 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle with inclined propellers and related systems and methods |
| WO2017219255A1 (en) * | 2016-06-21 | 2017-12-28 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicles with tilting propellers, and associated systems and methods |
| CN112758325A (en) * | 2016-06-21 | 2021-05-07 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle with inclined propellers and related systems and methods |
| CN109314452B (en) * | 2016-06-21 | 2021-02-19 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle with inclined propellers and related systems and methods |
| CN105974934A (en) * | 2016-06-24 | 2016-09-28 | 天津理工大学 | Air quality intelligent monitoring quadrotor formation system based on pilotage-following method |
| CN106323244A (en) * | 2016-08-18 | 2017-01-11 | 广州地理研究所 | Reservoir capacity monitoring method and device based on unmanned aerial vehicle |
| CN106516095A (en) * | 2016-12-21 | 2017-03-22 | 南京信息工程大学 | Specialized unmanned aerial vehicle for measuring wind direction and speed |
| CN106516095B (en) * | 2016-12-21 | 2018-09-28 | 南京信息工程大学 | One kind determines the wind direction wind speed dedicated unmanned machine |
| CN107389385A (en) * | 2017-07-14 | 2017-11-24 | 深圳市可飞科技有限公司 | High-altitude gas detecting system and detection method |
| CN107389385B (en) * | 2017-07-14 | 2024-05-07 | 深圳市可飞科技有限公司 | High-altitude air detection system and detection method |
| CN109239715A (en) * | 2018-09-20 | 2019-01-18 | 嘉兴河海中控信息科技有限公司 | Unmanned plane Doppler's current surveying device |
| CN109814470A (en) * | 2019-03-26 | 2019-05-28 | 河南小兵网络科技有限公司 | A kind of quadrotor drone monitoring comprehensive platform |
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| Date | Code | Title | Description |
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| 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: 20160302 Termination date: 20160428 |