CN206479513U - Unmanned aerial vehicle onboard gas detecting instrument - Google Patents
Unmanned aerial vehicle onboard gas detecting instrument Download PDFInfo
- Publication number
- CN206479513U CN206479513U CN201720106502.1U CN201720106502U CN206479513U CN 206479513 U CN206479513 U CN 206479513U CN 201720106502 U CN201720106502 U CN 201720106502U CN 206479513 U CN206479513 U CN 206479513U
- Authority
- CN
- China
- Prior art keywords
- housing
- pcb board
- aerial vehicle
- unmanned aerial
- detecting instrument
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000002245 particle Substances 0.000 claims abstract description 12
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims abstract description 11
- 238000013016 damping Methods 0.000 claims abstract description 8
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 11
- 239000013618 particulate matter Substances 0.000 claims description 2
- 238000000034 method Methods 0.000 description 6
- 238000001514 detection method Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
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- Testing Or Calibration Of Command Recording Devices (AREA)
Abstract
The utility model discloses a kind of unmanned aerial vehicle onboard gas detecting instrument, including housing, pcb board is provided with housing, leg is welded with pcb board, also it is installed with pcb board on sheet tin, sheet tin and is installed with gas particles thing sensor, asepwirator pump is provided with immediately below gas particles thing sensor, the side of asepwirator pump is fixedly connected with air intake duct, and the bottom of air intake duct is connected to the bottom of housing.The utility model is by setting pcb board, air intake window and damping spring, gas sensor, gas particles thing sensor, asepwirator pump, temperature sensor and GPS module are integrated on pcb board by the unmanned aerial vehicle onboard gas detecting instrument, greatly save the volume of detector, and by setting asepwirator pump and air intake duct, high aerial gas can be sucked in detector, it is easy to gather gas sample, pcb board is used with battery case and is symmetrical arranged, the space in housing is set reasonably to be distributed and utilized, the structure of enclosure interior is also simplify simultaneously, is easy to carry.
Description
Technical field
The utility model is related to atmospheric environment detection technique field, specially a kind of unmanned aerial vehicle onboard gas detecting instrument.
Background technology
With going from bad to worse for environment in recent years, particularly atmosphere pollution, the haze degree of China is increasingly severe, various countries
Government and tissue are all being actively working to the detection of environment and are improving work, make every effort to make our environment obtain larger improvement.
Atmospheric environment detection common at present, the typically all detection under the environment of low latitude, for the big of some high-altitudes
Gas environmental aspect, then had no way of doing it, with the development of science and technology, unmanned plane is born, environment measuring can be carried using unmanned plane
Device, is detected to the environment in high-altitude, but is due to unmanned plane small volume, and bearing capacity is poor, and existing environment measuring
The volume of device is larger, and internal structure is complicated, and weight is larger, and general UAV flight not, therefore constrains high altitude environment
That detects carries out the work.
Utility model content
(1) technical problem solved
In view of the shortcomings of the prior art, the utility model provides a kind of unmanned aerial vehicle onboard gas detecting instrument, solves existing
There is the problem of big unmanned plane airborne gas detector volume and complicated and inconvenient carrying.
(2) technical scheme
To achieve the above object, the utility model provides following technical scheme：A kind of unmanned aerial vehicle onboard gas detecting instrument, bag
Include housing, it is characterised in that：It is provided with the housing on pcb board, the pcb board and is welded with leg, it is fixed on the leg
It is provided with gas sensor, the pcb board and is also installed with sheet tin, gas particles thing biography is installed with the sheet tin
Asepwirator pump is provided with immediately below sensor, the gas particles thing sensor, the side of the asepwirator pump is fixedly connected with air-breathing
Pipe, the bottom of the air intake duct is connected to the bottom of housing, and the bottom of the pcb board side is installed with TEMP respectively
Also it is installed with device and GPS module, the housing in battery case, the battery case and is connected with battery, the one of the battery
Side is electrically connected with the side of pcb board, and the top of the battery case is fixedly connected with wireless data transmitter, wireless data transmitter
Top be provided with antenna pedestal, the antenna pedestal one end is through housing and extends to outside it, the antenna pedestal outside the housing
One end is socketed with wireless antenna, and the side of the housing offers charging inlet, and the side of the housing is also installed with electricity
Source switch, and power switch is located at the bottom of charging inlet.
It is preferred that, it is installed with wireless data transmitter on the battery.
It is preferred that, offer air intake window at the top of the housing.
It is preferred that, the bottom of the housing is fixedly connected with support column, and the bottom of the support column is fixedly connected with installation
Screwed hole is offered in seat, the mounting seat.
It is preferred that, the mounting seat is fixedly connected on the bottom of housing by the damping spring at the top of it.
It is preferred that, it is provided with the top and bottom of the pcb board on fixed block, the fixed block and is threaded with fastening
Screw.
(3) beneficial effect
The utility model provides a kind of unmanned aerial vehicle onboard gas detecting instrument.Possesses following beneficial effect：
(1), the utility model is by setting pcb board, leg, sheet tin, asepwirator pump, air intake duct, GPS module, battery case, electricity
Pond, air intake window and damping spring, the unmanned aerial vehicle onboard gas detecting instrument by gas sensor, gas particles thing sensor, asepwirator pump,
Temperature sensor and GPS module are integrated on pcb board, greatly save the volume of detector, and by set asepwirator pump and
Air intake duct, high aerial gas can be sucked in detector, be easy to gather gas sample, set battery, be that pcb board is powered,
The endurance of detector is substantially increased, pcb board, using being symmetrical arranged, makes the space in housing obtain reasonably with battery case
Distribution and utilization, while also simplify the structure of enclosure interior, are easy to carry, the unmanned aerial vehicle onboard gas detecting instrument is relative to biography
The detector of system, volume can reduce 30-45%, and weight can mitigate 30-40%, and compact conformation is easy to UAV flight, improved
The scope of application of detector.
Brief description of the drawings
Fig. 1 is the utility model structural profile schematic diagram；
Fig. 2 is the utility model shell structure side view；
Fig. 3 is the utility model shell structure upward view.
In figure：1 housing, 2PCB plates, 3 legs, 4 gas sensors, 5 gas particles thing sensors, 6 sheet tins, 7 asepwirator pumps, 8
Air intake duct, 9 temperature sensors, 10GPS modules, 11 battery cases, 12 batteries, 13 antenna pedestals, 14 wireless antennas, 15 power switches,
16 charging inlets, 17 wireless data transmitters, 18 air intake windows, 19 support columns, 20 mounting seats, 21 screwed holes, 22 damping springs, 23 are consolidated
Determine block, 24 trip bolts.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
As Figure 1-3, the utility model provides a kind of technical scheme：A kind of unmanned aerial vehicle onboard gas detecting instrument, including
Housing 1, the bottom of housing 1 is fixedly connected with support column 19, and the bottom of support column 19 is fixedly connected with mounting seat 20, mounting seat 20
On offer screwed hole 21, mounting seat 20 and screwed hole 21 are set, are easy to detector being mounted on unmanned plane, mounting seat 20 is led to
The damping spring 22 crossed at the top of it is fixedly connected on the bottom of housing 1, sets damping spring 22, can prevent unmanned plane from acutely shaking
When, the stationarity to detector is impacted, and pcb board 2 is provided with housing 1, and the top and bottom of pcb board 2 are provided with admittedly
Determine to be threaded with trip bolt 24 on block 23, fixed block 23, by trip bolt 24, it can be prevented with fix tightly pcb board 2
Come off, be welded with pcb board 2 on leg 3, leg 3 and be installed with gas sensor 4, tin is also installed with pcb board 2
Gas particles thing sensor 5 is installed with plate 6, sheet tin 6, the underface of gas particles thing sensor 5 is provided with asepwirator pump
7, the side of asepwirator pump 7 is fixedly connected with air intake duct 8, and the bottom of air intake duct 8 is connected to the bottom of housing 1, and the top of housing 1 is opened
Provided with air intake window 18, air intake window 18 is set, is easy to the entrance of air, the bottom of the side of pcb board 2 is installed with temperature respectively
Sensor 9 and GPS module 10, the unmanned aerial vehicle onboard gas detecting instrument is by gas sensor 4, gas particles thing sensor 5, air-breathing
Pump 7, temperature sensor 9 and GPS module 10 are integrated on pcb board 2, are examined by gas sensor 4 and gas particulate matter sensors 5
The pollutant index surveyed in gas, the temperature of air can be detected by temperature sensor 9, can be detected by GPS module 10
The position of unmanned plane, greatlys save the volume of detector, and by setting asepwirator pump 7 and air intake duct 8, can will be high aerial
Gas suction detector in, be easy to gather gas sample, be also installed with housing 1 in battery case 11, battery case 11 and block
Battery 12 is connected to, the side of battery 12 is electrically connected with the side of pcb board 2, and the top of battery case 11 is fixedly connected with wireless data
Transmitter 17, sets battery 12, is that pcb board 2 is powered, and substantially increases the endurance of detector, pcb board 2 and battery case 11
Using being symmetrical arranged, the space in housing 1 is set reasonably to be distributed and utilized, while the structure inside housing 1 is also simplify,
It is easy to carry, the unmanned aerial vehicle onboard gas detecting instrument is relative to traditional detector, and volume can reduce 30-45%, and weight can subtract
Light 30-40%, compact conformation is easy to UAV flight, improves the scope of application of detector, the top of wireless data transmitter 17
Portion is provided with antenna pedestal 13, and one end of antenna pedestal 13 is run through housing 1 and extended to outside it, one end of the antenna pedestal 13 outside housing 1
Wireless antenna 14 is socketed with, the side of housing 1 offers charging inlet 16, and the side of housing 1 is also installed with power switch
15, and power switch 15 is located at the bottom of charging inlet 16, by charging inlet 16, can be charged to battery 12.
In use, the unmanned aerial vehicle onboard gas detecting instrument by gas sensor 4, gas particles thing sensor 5, asepwirator pump 7,
Temperature sensor 9 and GPS module 10 are integrated on pcb board 2, greatly save the volume of detector, and by setting air-breathing
Pump 7 and air intake duct 8, high aerial gas can be sucked in detector, be easy to gather gas sample, set battery 12, be PCB
Plate 2 is powered, and substantially increases the endurance of detector, and pcb board 2, using being symmetrical arranged, makes the sky in housing 1 with battery case 11
Between reasonably distributed and utilized, while also simplify the structure inside housing 1, be easy to carry, the unmanned aerial vehicle onboard gas
Detector is relative to traditional detector, and volume can reduce 30-45%, and compact conformation is easy to UAV flight, improves detection
The scope of application of instrument.
It can to sum up obtain, the unmanned aerial vehicle onboard gas detecting instrument, by setting pcb board 2, leg 3, sheet tin 6, asepwirator pump 7, suction
Tracheae 8, GPS module 10, battery case 11, battery 12, air intake window 18 and damping spring 22, solve existing unmanned aerial vehicle onboard gas inspection
Survey the problem of big instrument volume and complicated and inconvenient carrying.
It should be noted that the electric elements occurred in this article are electrically connected with extraneous main controller and 220V civil powers, and
And main controller can play the conventionally known equipment of control for computer etc., (electric elements not with external connection, be one independent
System, power supply is by internal battery powers) herein, such as first and second or the like relational terms are used merely to one
Individual entity or operation make a distinction with another entity or operation, and not necessarily require or imply these entities or operate it
Between there is any this actual relation or order.Moreover, term " comprising ", "comprising" or its any other variant are intended to
Cover including for nonexcludability, so that process, method, article or equipment including a series of key elements not only include those
Key element, but also other key elements including being not expressly set out, or also include for this process, method, article or set
Standby intrinsic key element.In the absence of more restrictions, the key element limited by sentence "including a ...", it is not excluded that
Also there is other identical element in the process including the key element, method, article or equipment.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out in the case where not departing from principle of the present utility model and spirit a variety of changes, repaiies
Change, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. unmanned aerial vehicle onboard gas detecting instrument, including housing (1), it is characterised in that：Pcb board is provided with the housing (1)
(2), it is welded with the pcb board (2) on leg (3), the leg (3) and is installed with gas sensor (4), the PCB
Also it is installed with plate (2) on sheet tin (6), the sheet tin (6) and is installed with gas particles thing sensor (5), the gas
Asepwirator pump (7) is provided with immediately below body particulate matter sensors (5), the side of the asepwirator pump (7) is fixedly connected with air intake duct
(8), the bottom of the air intake duct (8) is connected to the bottom of housing (1), and the bottom of pcb board (2) side is fixedly mounted respectively
Have in temperature sensor (9) and GPS module (10), the housing (1) and be also installed with battery case (11), the battery case
(11) battery (12) is connected with, the side of the battery (12) is electrically connected with the side of pcb board (2), the battery case (11)
Top be fixedly connected with the top of wireless data transmitter (17), the wireless data transmitter (17) and be provided with antenna pedestal
(13), one end of the antenna pedestal (13) is through housing (1) and extends to outside it, the antenna pedestal (13) of the housing (1) outside
One end is socketed with wireless antenna (14), and the side of the housing (1) offers charging inlet (16), the side of the housing (1)
Power switch (15) is also installed with, and power switch (15) is located at the bottom of charging inlet (16).
2. unmanned aerial vehicle onboard gas detecting instrument according to claim 1, it is characterised in that：Fixed peace on the battery (12)
Equipped with wireless data transmitter (17).
3. unmanned aerial vehicle onboard gas detecting instrument according to claim 1, it is characterised in that：Opened at the top of the housing (1)
Provided with air intake window (18).
4. unmanned aerial vehicle onboard gas detecting instrument according to claim 1, it is characterised in that：The bottom of the housing (1) is consolidated
Surely support column (19) is connected with, the bottom of the support column (19) is fixedly connected with mounting seat (20), the mounting seat (20)
Offer screwed hole (21).
5. unmanned aerial vehicle onboard gas detecting instrument according to claim 4, it is characterised in that：The mounting seat (20) passes through it
The damping spring (22) at top is fixedly connected on the bottom of housing (1).
6. unmanned aerial vehicle onboard gas detecting instrument according to claim 1, it is characterised in that：The top of the pcb board (2) and
Bottom is provided with fixed block (23), the fixed block (23) and is threaded with trip bolt (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720106502.1U CN206479513U (en) | 2017-01-10 | 2017-01-10 | Unmanned aerial vehicle onboard gas detecting instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720106502.1U CN206479513U (en) | 2017-01-10 | 2017-01-10 | Unmanned aerial vehicle onboard gas detecting instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206479513U true CN206479513U (en) | 2017-09-08 |
Family
ID=59754353
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720106502.1U Expired - Fee Related CN206479513U (en) | 2017-01-10 | 2017-01-10 | Unmanned aerial vehicle onboard gas detecting instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206479513U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108535188A (en) * | 2018-05-23 | 2018-09-14 | 广东容祺智能科技有限公司 | A kind of the unmanned plane gas detecting system and its detection method of single line laser |
| CN108810460A (en) * | 2018-05-03 | 2018-11-13 | 南安市创培电子科技有限公司 | A kind of method of unmanned plane overhead welding and cutting |
| CN111781302A (en) * | 2019-04-03 | 2020-10-16 | 上海霍亨环保科技有限公司 | Pod for detecting atmospheric pollution and monitoring method thereof |
| CN113008488A (en) * | 2021-02-24 | 2021-06-22 | 陈盈 | Combined industrial hazardous gas leakage detector suitable for different occasions |
-
2017
- 2017-01-10 CN CN201720106502.1U patent/CN206479513U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108810460A (en) * | 2018-05-03 | 2018-11-13 | 南安市创培电子科技有限公司 | A kind of method of unmanned plane overhead welding and cutting |
| CN108535188A (en) * | 2018-05-23 | 2018-09-14 | 广东容祺智能科技有限公司 | A kind of the unmanned plane gas detecting system and its detection method of single line laser |
| CN111781302A (en) * | 2019-04-03 | 2020-10-16 | 上海霍亨环保科技有限公司 | Pod for detecting atmospheric pollution and monitoring method thereof |
| CN113008488A (en) * | 2021-02-24 | 2021-06-22 | 陈盈 | Combined industrial hazardous gas leakage detector suitable for different occasions |
| CN113008488B (en) * | 2021-02-24 | 2023-01-13 | 陈盈 | Combined industrial hazardous gas leakage detector suitable for different occasions |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170908 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |