CN201707324U - Poisonous and harmful gas emergency monitoring UAV (unmanned aerial vehicle) system - Google Patents
Poisonous and harmful gas emergency monitoring UAV (unmanned aerial vehicle) system Download PDFInfo
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- CN201707324U CN201707324U CN2010202351550U CN201020235155U CN201707324U CN 201707324 U CN201707324 U CN 201707324U CN 2010202351550 U CN2010202351550 U CN 2010202351550U CN 201020235155 U CN201020235155 U CN 201020235155U CN 201707324 U CN201707324 U CN 201707324U
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Abstract
The utility model discloses a poisonous and harmful gas emergency monitoring UAV (unmanned aerial vehicle) system, which comprises a UAV, wherein the UAV comprises a gas detection sensor, and a meteorologic parameter detector for detecting meteorologic parameters, wherein the gas detector and the meteorologic parameter detector transmit the acquired data to an onboard flight controller connected thereof, the onboard flight controller transmits the flight parameter, the data of the gas concentration, the meteorologic parameter thereof through a transmitter connected thereof, a ground information processing and flight control center comprises a receiver for receiving the data of the UAV, wherein the receiver is connected with a flight control system and a monitoring information processing system, the flight control system generates the position coordinates displayed by GIS through the received flight parameter, the monitoring information processing system processes the data of the gas concentration and the meteorologic parameter, establishes the corresponding relationship of the result after processing and the position coordinates, and can provide evidence for the atmospheric pollution incident emergency response.
Description
Technical field
The utility model relates to the environmental emergency field, is meant a kind of toxic and harmful emergency monitoring UAS especially.
Background technology
Unmanned plane is that unmanned spacecraft (Unmanned Aerial Vehicle) is called for short UAV.It has had more than 80 year history so far since 20 beginnings of the century were born.Particularly under the promotion of electronics and aeronautical technology develop rapidly, the development of unmanned plane has been subjected to the attention of various countries.
Unmanned plane obtains paying attention in the application of civil area day by day in recent years, and correlation technique is day by day ripe.The civil area unmanned plane is mainly to carry video transmission and digital camera two kind equipments.Video transmission can be used for monitoring fields such as forest protection, air patrol, traffic monitoring, and its outstanding advantage is the data transmission real-time high-efficiency; Digital camera is taken and to be mainly used in mappings among a small circle such as cities and towns, development area, factories and miness, residential quarter, and its advantage is that the highly low weather effect that is subjected to is little and precision is high.In addition, also be widely used at the platform of scientific research field unmanned plane as a kind of low-altitude detection.Common have a weather monitoring unmanned plane, by carrying the flight of meteorologic parameter sensor, realizes the measurement to differing heights place meteorologic parameter.
Unmanned plane mainly concentrates on aspect two in the application of environmental area at present.Adopt unmanned plane that pollution range, landscape pattern's evolution etc. is carried out the large tracts of land investigation.Just a kind of expansion that video transmission and the function of taking photo by plane are applied, technology is maturation relatively; But adopt the method for taking, can only show the pollution of gas, can't monitor and forecast the parameter of the harmful gas of each position in certain zone by photo and image.
The utility model content
In view of this, the utility model is to provide a kind of toxic and harmful emergency monitoring UAS, when leaking suddenly to solve toxic and harmful, and the problem that can't monitor and forecast the parameter of the harmful gas of each position in certain zone.
For addressing the above problem, the utility model provides a kind of toxic and harmful emergency monitoring UAS, comprising: unmanned plane, mission payload, terrestrial information are handled and are flown the control center;
Described unmanned plane is fixed-wing unmanned plane or depopulated helicopter.
Described mission payload comprises:
Detect the gas detecting instrument of toxic and harmful concentration;
Detect the meteorologic parameter monitor of meteorologic parameter;
To the airborne flight controller that is connected, described airborne flight controller is with self flight parameter and the transmitter transmission by connection of the data of described gas concentration, meteorologic parameter with the data transmission of gathering for described gas detecting instrument and described meteorologic parameter monitor;
Described terrestrial information is handled and is flown the control center and comprises:
Reception is from the receiver of described unmanned plane data, and described receiver connects flight control system and monitoring information disposal system;
The described flight parameter of described flight control system by receiving is created on the position coordinates that Geographic Information System GIS shows;
Described monitoring information disposal system is handled the data and the meteorologic parameter of described gas concentration, the result after foundation is handled and the corresponding relation of described position coordinates.
Further, the described gas detecting instrument gas detection sensor that can be equipped with comprises:
CO sensor, H
2S sensor, SO
2Sensor, NO
2Sensor, NO sensor, CI
2Sensor, HCN sensor, NH
3Sensor, PH
3Sensor, CIO
2At least a sensor in sensor, HCI sensor and the VOC sensor etc.
Further, described meteorologic parameter monitor comprises:
Detect the thermistor of temperature, the humicap that detects humidity, the silicon baroceptor of detected air pressure, described thermistor, humicap and silicon baroceptor generate relevant parameters through the metering circuit that is connected, and described metering circuit is controlled by the single-chip microcomputer of connection.
After the signal that the utility model collects by gas detecting instrument and meteorological parameter monitoring instrument is handled, handle and fly the control center by airborne flight controller through the terrestrial information that transmitter sends to ground, terrestrial information is handled and is flown the flight parameter of control center according to aircraft, on generalized information system, show corresponding coordinate, and demonstration and corresponding gas concentration data of coordinate and meteorologic parameter.Thereby count the distribution of gas situation of each coordinate position accurately.
At sudden environment event scene, can realize the monitoring of quick-speed large-scale, remedy the deficiency that existing environmental emergency monitoring system emergency monitoring car and manpower under the complex-terrain environment are difficult to arrive.Simultaneously, gas detection data of gathering and meteorological parameter monitoring data send to the terrestrial information processing by the UAV Flight Control data link and carry out analysis-by-synthesis with flight control system, the trend that can be the defining of the detection of toxic and harmful and differentiation, pollution range and hazardous location, Pollutants Diffusion is judged provides valid data, for the environmental emergency decision support provides foundation.
Description of drawings
Fig. 1 is the systematic schematic diagram of utility model;
Fig. 2 is the system construction drawing of embodiment.
Embodiment
For clearly demonstrating the technical scheme in the utility model, provide preferred embodiment below and be described with reference to the accompanying drawings.
Referring to system architecture schematic diagram shown in Figure 1, the unmanned plane during flying device can adopt fixed-wing unmanned plane/depopulated helicopter.
The mission payload of unmanned plane disposes gas detecting instrument and meteorological parameter monitoring instrument, is installed on the aircraft.
Gas detecting instrument can once carry the multiple gases detecting sensor simultaneously, for example: carry 4 kinds of gas detection sensors, by gas detection sensor select the detection that can realize flexibly for use to multiple toxic and harmful, comprising: CO sensor, H
2S sensor, SO
2Sensor, NO
2Sensor, NO sensor, CI
2Sensor, HCN sensor, NH
3Sensor, PH
3Sensor, CIO
2At least a sensor in sensor, HCI sensor and the VOC sensor etc.By the gas detection sensor that connects, thereby after detecting toxic and harmful, gas detecting instrument is measured the concentration of these gases, sends by data-interface.
The meteorologic parameter monitor is made up of temperature, air pressure, humidity sensor, data processing unit and transmission interface.Adopt thermistor temperature detecting, humicap (Honeywell) hygrometric, silicon baroceptor to measure air pressure.With the measured value that collects through single-chip microcomputer and and after metering circuit handles, finish data acquisition, processing, send by data-interface at last.
Below by embodiment system architecture of the present utility model is described, referring to system construction drawing shown in Figure 2, in this embodiment, gas detecting instrument is connected airborne flight controller respectively with meteorological parameter monitoring instrument, airborne flight controller after receiving signal from receiver, according to the sign of signal with signal forwarding to gas detecting instrument or meteorologic parameter monitor; The signal that gas detecting instrument and meteorological parameter monitoring instrument are sent sends by transmitter.
Receiver And Transmitter all adopts the radio frequency requirement of aircraft air communications, handles and the transceiver wireless connections that fly the center of controlling by radiofrequency signal and terrestrial information.
Terrestrial information is handled and is flown the control center, be based on Geographic Information System (GIS, Geographic Information System) platform is developed, and it is integrated to have realized that flight control and Monitoring Data are handled, and can show temperature, pressure, wet and gas detection data in real time based on GIS in fact.Thereby demonstrate the air concentration in each geographic position and the concentration of airborne poisonous, harmful its gas etc. in real time.Wherein, flight control system is used to handle the flight parameter of aircraft, thereby realize corresponding flight control, and obtain flight path according to flight parameter, flight path is corresponding with generalized information system, the particular location coordinate that promptly on generalized information system, shows aircraft flight, by the monitoring information disposal system gas concentration data and the meteorologic parameter of gas detecting instrument and the collection of meteorological parameter monitoring instrument are handled, the result who handles is corresponding with corresponding position coordinates, show gas concentration data and the meteorologic parameter that aircraft is gathered on each position coordinates thereby be implemented in.
The following describes the preferred parameter of each parts of the present utility model:
1, unmanned plane during flying device
(1) fixed-wing unmanned plane: Standard Task load＞5kg, landing wind loading rating＞5 grade, takeoff distance＜30m, max level speed 150km/h, normal cruise speed 110km/h, ceiling 5000m, flying radius 70km, communication distance (non-relay) can reach 20km above (nothing is blocked), be with maximum mission payload cruising time＞2h, landing run＜60m.
(2) depopulated helicopter: ceiling altitude can reach 2500m, maximum load 15Kg, maximum airborne period＞1.5h.
2, gas detection sensor
Weight＜3kg restrains (containing battery), battery working time＞8 continuous throughout the twenty-four hour24s, and sampling pump is built-in, flow velocity 400cc/min, temperature-10～+ 40 ℃, working relative humidity 0%～95% relative humidity (frozen-free).
Range: CO 0-500ppm, H
2S 0-100ppm, SO
20-20ppm, NO
20-20ppm, NO 0-250ppm, CI
2O-10ppm, HCN 0-100ppm, NH
30-50ppm, PH
30-5ppm, CIO
20-1ppm, HCL 0-10ppm, VOC 1ppb-10000ppm.
3, meteorologic parameter monitoring sensor
Temperature measurement range-90 ℃～50 ℃; Measuring accuracy is less than being 0.3 ℃; The moisture measurement scope is 0～100%; Measuring accuracy is less than being 5%; The barometric surveying scope is 500～1050hPa; Measuring accuracy is less than being 0.5hPa.
Can make system of the present utility model reach best performance by above-mentioned preferred parameter.
After the signal that the utility model collects by gas detecting instrument and meteorological parameter monitoring instrument is handled, handle and fly the control center by airborne flight controller through the terrestrial information that transmitter sends to ground, terrestrial information is handled and is flown the flight parameter of control center according to aircraft, on generalized information system, show corresponding coordinate, and demonstration and corresponding gas concentration data of coordinate and meteorologic parameter.Thereby count the distribution of gas situation of each coordinate position accurately, accurate data is provided when toxic and harmful leaks, for emergency command provides foundation.
For the system that is set forth among each embodiment of the utility model, all within spirit of the present utility model and principle, any modification of being done, be equal to replacement, improvement etc., all should be included within the protection domain of the present utility model.
Claims (4)
1. a toxic and harmful emergency monitoring UAS is characterized in that, comprising: unmanned plane, terrestrial information are handled and are flown the control center;
Described unmanned plane comprises:
Detect and discern the gas detection sensor of gas, the gas detecting instrument of described gas detection sensor joint detection gas concentration;
Detect the meteorologic parameter monitor of meteorologic parameter;
To the airborne flight controller that is connected, described airborne flight controller is with self flight parameter and the transmitter transmission by connection of the data of described gas concentration, meteorologic parameter with the data transmission of gathering for described gas detecting instrument and described meteorologic parameter monitor;
Described terrestrial information is handled and is flown the control center and comprises:
Reception is from the receiver of described unmanned plane data, and described receiver connects flight control system and monitoring information disposal system;
The described flight parameter of described flight control system by receiving is created on the position coordinates that Geographic Information System GIS shows;
Described monitoring information disposal system is handled the data and the meteorologic parameter of described gas concentration, the result after foundation is handled and the corresponding relation of described position coordinates.
2. system according to claim 1 is characterized in that, described gas detection sensor comprises:
CO sensor, H
2S sensor, SO
2Sensor, NO
2Sensor, NO sensor, CI
2Sensor, HCN sensor, NH
3Sensor, PH
3Sensor, CIO
2At least a sensor in sensor, HCI sensor and the VOC sensor etc.
3. system according to claim 1, described meteorologic parameter monitor comprises:
Detect the thermistor of temperature, the humicap that detects humidity, the silicon baroceptor of detected air pressure, described thermistor, humicap and silicon baroceptor generate relevant parameters through the metering circuit that is connected, and described metering circuit is controlled by the single-chip microcomputer of connection.
4. system according to claim 1 is characterized in that, described unmanned plane is fixed-wing unmanned plane or depopulated helicopter.
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| CN2010202351550U CN201707324U (en) | 2010-06-24 | 2010-06-24 | Poisonous and harmful gas emergency monitoring UAV (unmanned aerial vehicle) system |
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