CN105067780A - Air detection system with aerial photography system - Google Patents

Air detection system with aerial photography system Download PDF

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Publication number
CN105067780A
CN105067780A CN201510517229.7A CN201510517229A CN105067780A CN 105067780 A CN105067780 A CN 105067780A CN 201510517229 A CN201510517229 A CN 201510517229A CN 105067780 A CN105067780 A CN 105067780A
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CN
China
Prior art keywords
air
floating drum
detection system
fuselage
airduct
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Pending
Application number
CN201510517229.7A
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Chinese (zh)
Inventor
黄成城
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Chongqing Gusite Commercial Management Co Ltd
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Chongqing Gusite Commercial Management Co Ltd
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Publication date
Application filed by Chongqing Gusite Commercial Management Co Ltd filed Critical Chongqing Gusite Commercial Management Co Ltd
Priority to CN201510517229.7A priority Critical patent/CN105067780A/en
Publication of CN105067780A publication Critical patent/CN105067780A/en
Pending legal-status Critical Current

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Abstract

The invention provides an air detection system with an aerial photography system. The air detection system comprises a fuselage, a tail, a frame and a propeller. Floats are arranged on the two sides of the fuselage and provided with air inlets and air outlets. PM2.5 detectors are arranged in the floats. A video capture device is installed on the frame. A GPS clock control module, a PLC and a wireless communication module are arranged in the fuselage. The output end of the GPS clock control module is connected with the input end of the PLC, and the output end of the PLC is connected with the control ends of the PM2.5 detectors, the control end of the video capture device and the wireless communication module. The PM2.5 detectors, harmful gas detection sensors and the GPS clock control module are arranged on an aircraft, aerial monitoring data are collected based on a GPS reference clock, the data are transmitted through the wireless communication module via a wireless network, and therefore through continuous real-time data acquisition and instantaneous data transmission, haze early warning can be performed based on a data result.

Description

With the air detection system of the system of taking photo by plane
Technical field
The invention belongs to for coordinating with aircraft or installing to the equipment on aircraft; Flying suit; Parachute; The configuration of propulsion system or propulsion gearing or the technical field of installation, specifically relate to one with the air detection system of the system of taking photo by plane.
Background technology
Haze, also the dust in gray haze (mist and clouds in the twilight) air is claimed, sulfuric acid, nitric acid, the particles such as organic hydrocarbon compounds also can make air muddy, the visual field is fuzzy and cause visibility deterioration, if when horizontal visibility is less than ten thousand metres, the obstruction to vision that the aerosol systems that this non-water becomes thing to form causes is called haze (Haze) or gray haze (Dust-haze), Hong Kong Observatory claims mist and clouds in the twilight (Haze), when the difference of haze and mist is haze occurs, relative humidity is little, and the relative humidity in mist is saturated (when existing if any a large amount of nucleus of condensation, relative humidity not necessarily reach 100% just may occur saturated), the fuzzy visibility deterioration caused in the muddy visual field of air when general relative humidity is less than 80% is that haze causes, the fuzzy visibility deterioration caused in the muddy visual field of air when relative humidity is greater than 90% is that mist causes, the fuzzy visibility deterioration caused in the muddy visual field of air when relative humidity is between 80 ~ 90% is that the potpourri of haze and mist causes jointly, but its principal ingredient is haze, the Thickness Ratio of haze is thicker, 1 ~ 3 km can be reached, haze and mist, cloud is different, and there is no obvious border between clear sky district, the distribution of haze particle is more even, and the yardstick of gray haze particle is smaller, from 0.001 micron to 10 microns, mean diameter is greatly about 1 ~ 2 microns, be invisible to the naked eye the aerial particle floated.Due to molecular hazes of grain such as dust, sulfuric acid, nitric acid, the longer light ratio of its scattering wavelength is more, and thus haze seems in yellow or orange grey, existing haze early warning shows hysteresis quality, be all start to detect after haze is formed, there is no the function predicted.
Summary of the invention
In view of this, the object of the present invention is to provide one with the air detection system of the system of taking photo by plane, should with the air detection system of the system of taking photo by planeby being provided with PM2.5 detecting sensor, harmful gas detecting sensor and gps clock control module on board the aircraft, based on the aerial Monitoring Data of GPS reference clock collection, and adopt wireless communication module to carry out data transmission by wireless network, data continuous Real-time Obtaining, instantaneous transmission and can haze early warning be carried out based on data result.
In order to solve the problems of the technologies described above, the present invention is a kind of with the air detection system of the system of taking photo by plane, comprise unmanned vehicle, described unmanned vehicle comprises fuselage, tail, be arranged on the frame below fuselage and the screw propeller being arranged on body upper, described fuselage both sides are provided with floating drum, described floating drum is provided with air port, air outlet and the airduct be connected between air port and air outlet, PM2.5 detector is provided with in described floating drum, described frame is provided with video acquisition device, gps clock control module is provided with in described fuselage, PLC and wireless communication module, the output terminal of described gps clock control module is connected with PLC input end, described PLC control output end and described PM2.5 detector control end, video acquisition device control end is connected with wireless communication module.
Further, described frame is also provided with and is no less than 1 sensor, described sensor is used for detecting one or more harmful gases in CO, H2S, SO2, NO2, NO, CI2, HCN, HN3, PH3, CIO2, HCI, VOC respectively.
Further, described airduct is arranged on floating drum center, the valve for closing airduct is provided with in described airduct, the inwall that described airduct is positioned at valve nose is provided with fresh air inlet, described airduct inwall is provided with between floating drum outer wall the air channel being connected fresh air inlet, the end in described air channel is connected with air outlet opening, and described PM2.5 detector is arranged in air channel.
Further, described tail place is provided with pusher.
Further, described floating drum is set to pyramidal structure.
Further, described floating drum is made up of glass-reinforced plastic material.
Beneficial effect of the present invention is:
The present invention with the air detection system of the system of taking photo by planeby being provided with PM2.5 detecting sensor, harmful gas detecting sensor and gps clock control module on board the aircraft, based on the aerial Monitoring Data of GPS reference clock collection, and adopt wireless communication module to carry out data transmission by wireless network, data continuous Real-time Obtaining, instantaneous transmission and can haze early warning be carried out based on data result.
Accompanying drawing explanation
fig. 1for the present invention with the air detection system of the system of taking photo by planestructural representation figure;
fig. 2for the structural representation of floating drum on aircraft of the present invention figure.
accompanying drawingmark: 1-fuselage; 2-screw propeller; 3-tail; 4-frame; 5-floating drum; 6-air port; 7-air outlet; 8-airduct; 9-air channel; 10-PM2.5 detector; 11-valve; 12-fresh air inlet; 13-video acquisition device; 14-sensor; 15-PLC controller; 16-GPS clock control module; 17-wireless communication module.
Embodiment
Below in conjunction with accompanying drawingwith embodiment pair inventionbe described in further detail.
as Fig. 1be depicted as the present invention with the air detection system of the system of taking photo by planestructural representation figure, as Fig. 2be depicted as the structural representation of floating drum on aircraft of the present invention figure, the present invention is a kind of with the air detection system of the system of taking photo by plane, comprise unmanned vehicle, described unmanned vehicle comprises fuselage 1, tail 3, the screw propeller 2 being arranged on the frame 4 below fuselage 1 and being arranged on above fuselage 1, described fuselage 1 both sides are provided with floating drum 5, described floating drum 5 is provided with air port 6, air outlet 7 and the airduct 8 be connected between air port 6 and air outlet 7, PM2.5 detector 10 is provided with in described floating drum 5, described frame 4 is provided with video acquisition device 13, gps clock control module 16 is provided with in described fuselage, PLC 15 and wireless communication module 17, the output terminal of described gps clock control module 16 is connected with PLC 15 input end, described PLC control output end 16 and described PM2.5 detector 10 control end, video acquisition device 13 control end is connected with wireless communication module 17.
The present embodiment is by being provided with PM2.5 detecting sensor, harmful gas detecting sensor and gps clock control module on board the aircraft, based on the aerial Monitoring Data of GPS reference clock collection, and adopt wireless communication module to carry out data transmission by wireless network, data continuous Real-time Obtaining, instantaneous transmission and can haze early warning be carried out based on data result.
Further, described frame is also provided with and is no less than 1 sensor, described sensor is used for detecting one or more harmful gases in CO, H2S, SO2, NO2, NO, CI2, HCN, HN3, PH3, CIO2, HCI, VOC respectively, the present embodiment is by the content of the harmful gas such as sulfuric acid, nitric acid in monitoring air, not only can carry out prediction haze in advance, and other objectionable constituent of air can be detected, the healthy and safe and weather environmental improvement improving people provides foundation.
Further, preferred described airduct 8 is arranged on floating drum 5 center, the valve 11 for closing airduct 8 is provided with in described airduct 8, the inwall that described airduct 8 is positioned at valve 11 front end is provided with fresh air inlet 12, described airduct 8 inwall is provided with between floating drum 5 outer wall the air channel 9 being connected fresh air inlet 12, the end in described air channel 9 is connected with air outlet opening, described PM2.5 detector 10 is arranged in air channel 9, the preferred air outlet opening of the present embodiment is distributed on the surrounding of air outlet, this enforcement is by liking at all-rounder flying up and down and telling in flight course, open valve 11, air is circulated by airduct, the resistance of air can be reduced, do not carry out the quality detecting air, its reason is that now the data accuracy that detects of PM2.5 detector 10 pairs of air is poor, time aloft slowly flight or stopping are in fashion, valve-off 11, air is by fresh air inlet 12, enter air channel, discharge from air channel air outlet opening, now wind speed is in nature gustiness, be conducive to PM2.5 detector 10 pairs of air to detect, the air quality data accuracy of this detection is good, be conducive to the accuracy rate improving haze prediction.
Further, described tail 3 place is provided with pusher, and this structure is conducive to advance and the flight of all-rounder.
Further, preferred described floating drum 5 is set to pyramidal structure, and air intake opening end is arranged on the little one end of floating drum 5 diameter, and this structure is conducive to, in all-rounder is in fashion, reducing windage.
Further, preferred described floating drum 5 is made up of glass-reinforced plastic material, and this structure is conducive to, when reducing floating drum 5 weight, improving the intensity of floating drum 5.
What finally illustrate is, above embodiment is only in order to illustrate technical scheme of the present invention and unrestricted, although with reference to preferred embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that, can modify to technical scheme of the present invention or equivalent replacement, and not departing from aim and the scope of technical solution of the present invention, it all should be encompassed in the middle of right of the present invention.

Claims (6)

1. the air detection system with the system of taking photo by plane, comprise unmanned vehicle, described unmanned vehicle comprises fuselage, tail, be arranged on the frame below fuselage and the screw propeller being arranged on body upper, it is characterized in that: described fuselage both sides are provided with floating drum, described floating drum is provided with air port, air outlet and the airduct be connected between air port and air outlet, PM2.5 detector is provided with in described floating drum, described frame is provided with video acquisition device, gps clock control module is provided with in described fuselage, PLC and wireless communication module, the output terminal of described gps clock control module is connected with PLC input end, described PLC control output end and described PM2.5 detector control end, video acquisition device control end is connected with wireless communication module.
2. according to the air detection system with the system of taking photo by plane shown in claim 1, it is characterized in that: described frame is also provided with and is no less than 1 sensor, described sensor is used for detecting one or more harmful gases in CO, H2S, SO2, NO2, NO, CI2, HCN, HN3, PH3, CIO2, HCI, VOC respectively.
3. according to the air detection system with the system of taking photo by plane shown in claim 1, it is characterized in that: described airduct is arranged on floating drum center, the valve for closing airduct is provided with in described airduct, the inwall that described airduct is positioned at valve nose is provided with fresh air inlet, described airduct inwall is provided with between floating drum outer wall the air channel being connected fresh air inlet, the end in described air channel is connected with air outlet opening, and described PM2.5 detector is arranged in air channel.
4. according to the air detection system with the system of taking photo by plane shown in claim 1, it is characterized in that: described tail place is provided with pusher.
5. according to the air detection system with the system of taking photo by plane shown in claim 1, it is characterized in that: described floating drum is set to pyramidal structure.
6. according to the air detection system with the system of taking photo by plane shown in claim 1, it is characterized in that: described floating drum is made up of glass-reinforced plastic material.
CN201510517229.7A 2015-08-21 2015-08-21 Air detection system with aerial photography system Pending CN105067780A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510517229.7A CN105067780A (en) 2015-08-21 2015-08-21 Air detection system with aerial photography system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510517229.7A CN105067780A (en) 2015-08-21 2015-08-21 Air detection system with aerial photography system

Publications (1)

Publication Number Publication Date
CN105067780A true CN105067780A (en) 2015-11-18

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CN201510517229.7A Pending CN105067780A (en) 2015-08-21 2015-08-21 Air detection system with aerial photography system

Country Status (1)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106226208A (en) * 2016-06-30 2016-12-14 桂林理工大学 Lower atmosphere PM2.5 remote monitoring device
CN106442892A (en) * 2016-11-02 2017-02-22 安徽锦坤电子科技有限公司 Monitoring system for air quality
CN106546646A (en) * 2016-10-20 2017-03-29 浙江中烟工业有限责任公司 A kind of low-concentration hydrogen phosphide concentration on-line monitoring method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106226208A (en) * 2016-06-30 2016-12-14 桂林理工大学 Lower atmosphere PM2.5 remote monitoring device
CN106546646A (en) * 2016-10-20 2017-03-29 浙江中烟工业有限责任公司 A kind of low-concentration hydrogen phosphide concentration on-line monitoring method
CN106546646B (en) * 2016-10-20 2019-10-29 浙江中烟工业有限责任公司 A kind of low-concentration hydrogen phosphide concentration on-line monitoring method
CN106442892A (en) * 2016-11-02 2017-02-22 安徽锦坤电子科技有限公司 Monitoring system for air quality

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Application publication date: 20151118

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