CN210534107U - Atmospheric monitoring device - Google Patents
Atmospheric monitoring device Download PDFInfo
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- CN210534107U CN210534107U CN201921452627.5U CN201921452627U CN210534107U CN 210534107 U CN210534107 U CN 210534107U CN 201921452627 U CN201921452627 U CN 201921452627U CN 210534107 U CN210534107 U CN 210534107U
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Abstract
The utility model relates to an atmospheric analysis and monitoring technology field specifically are an atmospheric monitoring device, including the base, be provided with on the base with the fixed mating holes of outside aircraft cooperation, and the inside of base has the mounting bracket through bolt fixed mounting, and the rear end integrated into one piece of mounting bracket has five at least cooperation section of thick bamboos, and installs collection device in the cooperation section of thick bamboo, has negative pressure pump and air pump through bolt fixed mounting on the mounting bracket, and has the flow distribution box through bolt fixed mounting in the mounting bracket. The beneficial effects are that: this atmosphere monitoring devices can realize the real-time supervision to each regional corresponding composition in the atmosphere with the aircraft cooperation, and the realization that simultaneously can also be convenient is to the sample of the corresponding regional air sample in atmosphere to replace traditional artifical mode of taking a sample in the air, the effectual security, the efficiency that have improved atmosphere monitoring have reduced the cost that detects, and the device uses easy operation, and the sample can not be contaminated, the precision of the follow-up detection of improvement that can be great.
Description
Technical Field
The utility model relates to an atmospheric analysis and monitoring technology field specifically are an atmospheric monitoring device.
Background
Atmospheric quality monitoring means that the content of the main pollutant in the atmosphere etc. monitors, the tradition is monitored near the earth atmosphere and is mainly carried out with ground equipment, and the higher atmosphere of height then adopts the aircraft to carry monitoring facilities and monitors, but because monitoring facilities's detection capability is limited, consequently need carry sampling equipment and sample so that carry out accurate analysis on ground, but the sampling of a plurality of regions is difficult to realize to current sampling equipment and the sample leaks easily and is polluted, it can only adopt artifical sampling to have caused to need accurate sampling.
The novel atmosphere monitoring equipment capable of accurately sampling air can effectively solve the problems, so that an atmosphere monitoring device can be provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an atmosphere monitoring device to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an atmosphere monitoring device comprises a base, wherein a matching hole matched and fixed with an external aircraft is formed in the base, a mounting frame is fixedly mounted in the base through bolts, at least five matching cylinders are integrally formed at the rear end of the mounting frame, a collecting device is mounted in the matching cylinders, a negative pressure pump and an air pump are fixedly mounted on the mounting frame through bolts, a flow distribution box is fixedly mounted in the mounting frame through bolts, the rear end of the flow distribution box is inserted and mounted with the collecting device through insertion pipes, and a first electromagnetic valve is mounted on each insertion pipe;
the negative pressure pump is connected with the flow distribution box through an exhaust pipe, a second electromagnetic valve is installed on the exhaust pipe, the air pump is connected with the flow distribution box through an inflation pipe, a third electromagnetic valve is fixedly installed on the inflation pipe, a supporting seat is fixedly installed at the bottom of the base through a bolt, a rotating motor is fixedly installed on the supporting seat through a bolt, a connecting seat is driven by the output end of the rotating motor, an adjusting motor is fixedly installed on the connecting seat through a bolt, and a mounting seat is driven by the output end of the adjusting motor;
removable formula built-in power source is installed in the grafting on the supporting seat, and fixed mounting has the controller that passes through cable junction with the main control system of outside aircraft on the supporting seat, there is the charging seat of being convenient for with the installation of external power source grafting through bolt fixed mounting on the supporting seat, and the charging seat passes through charging electrode and built-in power source electric connection, there are camera and monitoring facilities through spiral shell button fixed mounting on the mounting seat, and the controller passes through cable first solenoid valve of difference electric connection, second solenoid valve, third solenoid valve, rotating electrical machines, adjustment motor, air pump, negative pressure pump, built-in power source, monitoring facilities and camera.
Preferably, collection device includes the collecting pipe, and the rear end of collecting pipe installs the pull handle, the front end spiro union of collecting pipe is installed and is sealed the cap, seal the cap the front end install with insert tube complex spring check valve, integrated into one piece has the cooperation arch on the collecting pipe, and the protruding outside of cooperation passes through screw thread and the installation of cooperation section of thick bamboo spiro union.
Preferably, the mounting frame is provided with a sealing door at the outer side corresponding to the collecting device, and the sealing door is fixedly mounted with the mounting frame through a fixing screw button.
Preferably, the rotating motor and the adjusting motor are both stepping motors, and the controller is a stm32 series single chip microcomputer.
Preferably, the built-in power supply is a lithium battery, and the monitoring device is an atmospheric environment monitor.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses an atmosphere monitoring device can realize the real-time supervision to each regional corresponding composition in the atmosphere with the aircraft cooperation, the realization that simultaneously can also be convenient is to the sample of the corresponding regional air sample in atmosphere to replace the mode of traditional manual work in the aerial sample, the effectual security that has improved atmosphere monitoring, efficiency and reduced the cost that detects, and the device uses easy operation, the sample can not be contaminated, the precision of the follow-up detection of improvement that can be great, consequently, very high practical value has.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is an assembly schematic view of the collecting device and the mounting rack of the present invention;
fig. 3 is a schematic structural diagram of the collecting device of the present invention.
In the figure: the device comprises a base 1, a collecting device 2, a spring one-way valve 201, a sealing cap 202, a collecting pipe 203, a matching bulge 204, a pull handle 205, a fixed screw button 3, a matching hole 4, a mounting rack 5, a charging seat 6, a rotating motor 7, a connecting seat 8, a monitoring device 9, a camera 10, a matching barrel 11, a first electromagnetic valve 12, a second electromagnetic valve 13, an exhaust pipe 14, a negative pressure pump 15, an air pump 16, an inflation pipe 17, a third electromagnetic valve 18, a flow distribution box 19, an insertion pipe 20, a sealing door 21, a built-in power supply 22, an adjusting motor 23 and a mounting seat 24.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the technical scheme in the utility model, all other embodiments that ordinary skilled person in the art obtained under the prerequisite of not making the creative work all belong to the scope of the utility model protection.
Referring to fig. 1 to 3, the present invention provides a technical solution: an atmosphere monitoring device comprises a base 1, wherein a matching hole 4 matched and fixed with an external aircraft is formed in the base 1, a mounting frame 5 is fixedly mounted in the base 1 through bolts, at least five matching cylinders 11 are integrally formed at the rear end of the mounting frame 5, a collecting device 2 is mounted in each matching cylinder 11, a negative pressure pump 15 and an air pump 16 are fixedly mounted on the mounting frame 5 through bolts, a flow distribution box 19 is fixedly mounted in the mounting frame 5 through bolts, the rear end of the flow distribution box 19 is inserted and mounted with the collecting device 2 through insertion pipes 20, and a first electromagnetic valve 12 is mounted on each insertion pipe 20;
the negative pressure pump 15 is connected with the flow distribution box 19 through an exhaust pipe 14, the exhaust pipe 14 is provided with a second electromagnetic valve 13, the air pump 16 is connected with the flow distribution box 19 through an inflation pipe 17, the inflation pipe 17 is fixedly provided with a third electromagnetic valve 18, the bottom of the base 1 is fixedly provided with a supporting seat 26 through a bolt, the supporting seat 26 is fixedly provided with a rotating motor 7 through a bolt, the output end of the rotating motor 7 drives a connecting seat 8, the connecting seat 8 is fixedly provided with an adjusting motor 23 through a bolt, and the output end of the adjusting motor 23 drives an installation seat 24;
a replaceable built-in power supply 22 is inserted and mounted on a supporting seat 26, a controller 25 which is connected with a main control system of an external aircraft through a cable is fixedly mounted on the supporting seat 25, a charging seat 6 which is convenient to be inserted and mounted with the external power supply is fixedly mounted on the supporting seat 26 through a bolt, the charging seat 6 is electrically connected with the built-in power supply 22 through a charging electrode, a camera 10 and a monitoring device 9 are fixedly mounted on a mounting seat 24 through a screw button, and the controller 25 is respectively electrically connected with a first electromagnetic valve 12, a second electromagnetic valve 13, a third electromagnetic valve 18, a rotating motor 7, an adjusting motor 23, an air pump 16, a negative pressure pump 15, the built-in power supply 22, the monitoring device 9 and the camera 10 through cables;
The working principle is as follows: when the device works, the base 1 is firstly fixed on an external aircraft, and then the controller 25 of the device is connected with a main control system on the external aircraft, so that communication equipment on the main control system of the external aircraft is utilized to communicate with ground personnel, the internal power supply 22 of the device is detachable, is convenient to directly replace, and can also be directly charged by utilizing the charging seat 6. When in use, firstly, the cleaned collecting device 2 is correctly inserted and installed in the matching barrel 11, so that each insertion pipe 20 can jack up the corresponding spring one-way valve, at the moment, the negative pressure pump 15, the second electromagnetic valve 13 and the first electromagnetic valve 12 are opened to vacuumize each collecting pipe 203, then, the negative pressure pump 15, the second electromagnetic valve 13 and the first electromagnetic valve 12 are closed again, the flying posture of the aircraft can be conveniently controlled by using the camera 10 in the monitoring process, meanwhile, the angle of the mounting seat 24 can be adjusted by using the rotating motor 7 and the adjusting motor 23, the monitoring equipment 9 is used for realizing specific atmospheric parameter monitoring, oxygen content, dust content and the like are utilized, when an atmospheric component sample in a certain area needs to be collected, only the air pump 16 and the third electromagnetic valve 18 need to be opened, then, the first electromagnetic valve 12 corresponding to the corresponding collecting device 2 is opened, and the sample can be sent into the collecting device 2, then the air pump 16, the third electromagnetic valve 18 and the corresponding first electromagnetic valve 12 are closed, the second electromagnetic valve 13 and the negative pressure pump 15 are opened again to pump out the residual gas in the distribution box 19, and after the pumping-out is finished, the second electromagnetic valve 13 and the negative pressure pump 15 are closed again, and the distribution box 19 of the device is actually a box which directly communicates the inflation pipe 17, the suction pipe 13 and each insertion pipe 20 by using an inner cavity. When the sampled air sample needs to be taken out, only the closing door 21 needs to be opened, then the collecting pipe 203 is rotated by the pull handle 205 to enable the matching protrusion 204 to be separated from the matching barrel 11 in a threaded matching state, at the moment, the corresponding collecting device 2 can be pulled out backwards, meanwhile, the spring type one-way valve 201 can also correctly seal the collecting pipe 203 after being separated from the inserting pipe 20, internal gas leakage is avoided, and then the internal gas can be discharged only by taking off the closing cap 202 after the use is finished. The device can realize the real-time supervision to the corresponding composition in each region in the atmosphere with the aircraft cooperation, the realization that simultaneously can also be convenient is to the sample of the corresponding regional air sample in atmosphere to replace traditional artifical mode of taking a sample in the air, the effectual security, the efficiency that have improved atmosphere monitoring has reduced the cost that detects, and the device uses easy operation, and the sample can not be contaminated, the follow-up precision that detects of improvement that can be great, consequently, has very high practical value.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. An atmosphere monitoring device, includes base (1), its characterized in that: the aircraft air distribution system is characterized in that a matching hole (4) matched and fixed with an external aircraft is formed in the base (1), a mounting frame (5) is fixedly mounted inside the base (1) through bolts, at least five matching cylinders (11) are integrally formed at the rear end of the mounting frame (5), a collecting device (2) is mounted in each matching cylinder (11), a negative pressure pump (15) and an air pump (16) are fixedly mounted on the mounting frame (5) through bolts, a flow distribution box (19) is fixedly mounted in the mounting frame (5) through bolts, the rear end of each flow distribution box (19) is connected with the collecting device (2) through an insertion pipe (20) in an inserting mode, and a first electromagnetic valve (12) is mounted on each insertion pipe (20);
the negative pressure pump (15) is connected with the flow distribution box (19) through an exhaust pipe (14), a second electromagnetic valve (13) is installed on the exhaust pipe (14), the air pump (16) is connected with the flow distribution box (19) through an inflation pipe (17), a third electromagnetic valve (18) is fixedly installed on the inflation pipe (17), a supporting seat (26) is fixedly installed at the bottom of the base (1) through bolts, a rotating motor (7) is fixedly installed on the supporting seat (26) through bolts, the output end of the rotating motor (7) drives a connecting seat (8), an adjusting motor (23) is fixedly installed on the connecting seat (8) through bolts, and the output end of the adjusting motor (23) drives an installation seat (24);
the support seat (26) is provided with a replaceable built-in power supply (22) in an inserted manner, the support seat (26) is fixedly provided with a controller (25) which is connected with a main control system of an external aircraft through a cable, a charging seat (6) which is convenient to be inserted and installed with an external power supply is fixedly installed on the supporting seat (26) through a bolt, the charging seat (6) is electrically connected with the built-in power supply (22) through a charging electrode, the mounting seat (24) is fixedly provided with a camera (10) and a monitoring device (9) through a screw button, and the controller (25) is respectively and electrically connected with the first electromagnetic valve (12), the second electromagnetic valve (13), the third electromagnetic valve (18), the rotating motor (7), the adjusting motor (23), the air pump (16), the negative pressure pump (15), the built-in power supply (22), the monitoring equipment (9) and the camera (10) through cables.
2. An atmosphere monitoring device according to claim 1, wherein: collection device (2) include collecting pipe (203), and the rear end of collecting pipe (203) installs pull handle (205), the front end spiro union of collecting pipe (203) is installed and is sealed cap (202), the front end of sealing cap (202) is installed and is gone up integrated into one piece and have cooperation arch (204) with insert tube (20) complex spring check valve (201), and the outside of cooperation arch (204) is passed through the screw and is installed with cooperation section of thick bamboo (11) spiro union on collecting pipe (203).
3. An atmosphere monitoring device according to claim 1, wherein: mounting bracket (5) are in the outside department that corresponds collection device (2) and install closed door (21), and closed door (21) are through fixed knob (3) and mounting bracket (5) fixed mounting.
4. An atmosphere monitoring device according to claim 1, wherein: the rotating motor (7) and the adjusting motor (23) are both stepping motors, and the controller (25) is a stm32 series single chip microcomputer.
5. An atmosphere monitoring device according to claim 1, wherein: the built-in power supply (22) is a lithium battery, and the monitoring equipment (9) is an atmospheric environment monitor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921452627.5U CN210534107U (en) | 2019-09-03 | 2019-09-03 | Atmospheric monitoring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921452627.5U CN210534107U (en) | 2019-09-03 | 2019-09-03 | Atmospheric monitoring device |
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| Publication Number | Publication Date |
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| CN210534107U true CN210534107U (en) | 2020-05-15 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921452627.5U Active CN210534107U (en) | 2019-09-03 | 2019-09-03 | Atmospheric monitoring device |
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| CN (1) | CN210534107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111812275A (en) * | 2020-07-24 | 2020-10-23 | 马小杰 | Atmospheric environment acid mist analysis monitoring devices |
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2019
- 2019-09-03 CN CN201921452627.5U patent/CN210534107U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111812275A (en) * | 2020-07-24 | 2020-10-23 | 马小杰 | Atmospheric environment acid mist analysis monitoring devices |
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