CN207292410U - A kind of unmanned plane for air monitering - Google Patents
A kind of unmanned plane for air monitering Download PDFInfo
- Publication number
- CN207292410U CN207292410U CN201721384600.8U CN201721384600U CN207292410U CN 207292410 U CN207292410 U CN 207292410U CN 201721384600 U CN201721384600 U CN 201721384600U CN 207292410 U CN207292410 U CN 207292410U
- Authority
- CN
- China
- Prior art keywords
- cabinet
- syringe
- unmanned plane
- fuselage
- air
- 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
Landscapes
- Sampling And Sample Adjustment (AREA)
Abstract
The utility model discloses a kind of unmanned plane for air monitering, including fuselage, rotation axis is provided with above the fuselage, propeller is provided with the rotation axis, the bottom of the fuselage is provided with cabinet, and the surrounding of the cabinet is provided with supporting leg, and the inside of the cabinet sets air sampling case, controller and storage battery, the storage battery is connected by conducting wire with controller, and the air sampling case is internally provided with syringe.The beneficial effects of the utility model are：Mobility is good, and monitoring range is wide, is analyzed after being sampled to air sample, monitoring result is more accurate.
Description
Technical field
The utility model relates generally to unmanned air vehicle technique field, is specially a kind of unmanned plane for air monitering.
Background technology
Unmanned plane be using wireless remote control device (remote manipulator) and provide for oneself presetting apparatus manipulation it is not manned
Aircraft, or fully or intermittently independently operated by car-mounted computer, in recent years, Development of UAV is rapid, in police, city
The industry such as city's management, agricultural, geology, meteorology, electric power, rescue and relief work, video capture has a wide range of applications, and air monitering is often
Collection point is seriously polluted, and environment complexity is unfavorable for staff's collection in worksite, but existing unmanned plane is also deposited in use
In some problems：
1st, air quality monitoring is carried out using unmanned plane, unmanned plane can whenever and wherever possible take off, overcome fixed point monitoring and determine
Point drawback, makes the monitoring of air quality very flexible, although monitoring is flexible, sampling is relatively difficult, can not especially carry out more
Point, grab sampling.
2nd, unmanned plane is although small, it is easy to carry and for high-altitude detect air quality, but due to its volume compared with
It is small, its in high-altitude flight by being visually difficult to, when especially the place more in mountain area or trees carries out air monitering
Easily bump against barrier and damage.
Utility model content
To solve deficiency of the prior art, the utility model provides a kind of unmanned plane for air monitering, mobility
Good, monitoring range is wide, is analyzed after being sampled to air sample, monitoring result is more accurate.
The utility model to achieve the above object, is achieved through the following technical solutions：
A kind of unmanned plane for air monitering, including fuselage, are provided with rotation axis, the rotation above the fuselage
Propeller is provided with axis, the bottom of the fuselage is provided with cabinet, and the surrounding of the cabinet is provided with supporting leg, and the supporting leg is consolidated
It is scheduled on fuselage, the inside of the cabinet sets air sampling case, controller and storage battery, and the storage battery passes through conducting wire and control
Device connection processed, the air sampling case are internally provided with syringe, solenoid valve, institute are provided with the air inlet pipe of the syringe
Stating the end set of air inlet pipe has sampling head, and the sampling head is fixed on the bottom of cabinet, and the top of the syringe sets gas
Cylinder, the cylinder are fixed on the top of air sampling case, and the piston rod of the cylinder passes through the injection in connector sleeve and syringe
Device core bar connects, and the bottom of the cabinet is provided with receiver of remote-control sytem, and the propeller, solenoid valve and cylinder pass through conducting wire respectively
It is connected with controller, the controller is connected by conducting wire with receiver of remote-control sytem.
The syringe is provided with several altogether.
The left and right sides that the fuselage is located relatively at cabinet sets the support plate for being used for installing cabinet, and the enclosure top is set
Put first through hole, the left and right ends that the cabinet is located relatively at through hole are symmetrical arranged sliding block, be horizontally disposed with the support plate with
The sliding slot that sliding block is adapted, set in the support plate with matched second through hole of first through hole, further include screw rod, the spiral shell
Bar sequentially passes through first through hole, the second through hole and sets clamp nut at both ends.
The supporting leg is equipped with flash lamp.
The supporting leg is provided with four altogether, and four supporting leg rectangular in form are distributed in the bottom of fuselage.
The sampling head is funnel-form.
High-definition camera is set on the side wall of the cabinet.
Contrast and the prior art, the utility model beneficial effect are：
1st, the utility model is small, can whenever and wherever possible take off and destination air is sampled, mobility is good, to sky
Analyzed after gas sample, monitoring result is more accurate.
2nd, the utility model syringe is provided with several altogether, and the air in the more than enough certain area of energy carries out multi-point sampling,
Syringe takes back the air samples of different sampled points easy to detection, not only monitoring range it is wide and also can multi-point sampling be averaged
The accuracy of monitoring can be increased.
3rd, the utility model screw rod sequentially passes through first through hole, the second through hole and sets clamp nut at both ends, works as cabinet
After interior syringe sampling, cabinet can be replaced and continue to sample, further increase monitoring range.
4th, the utility model supporting leg is equipped with flash lamp, and flash lamp is connected by conducting wire with controller, can be in monitoring
Staff is facilitated to find the position of unmanned plane.
5th, four supporting leg rectangular in form of the utility model are distributed in the bottom of fuselage, and increase unmanned plane landing is contacted with ground
When stability.
The 6th, high-definition camera is set on the side wall of the utility model cabinet, high-definition camera is connected by conducting wire and controller
Connect, monitoring region can be shot, to understand the landforms in monitoring region.
Brief description of the drawings
Attached drawing 1 is the structure diagram one of the utility model.
Attached drawing 2 is the structure diagram two of the utility model.
Attached drawing 3 is the structure diagram of syringe.
Attached drawing 4 is enlarged drawing at the A of attached drawing 2.
Attached drawing 5 is this utility structure block diagram.
Label 1 shown in attached drawing, fuselage；2nd, cabinet；3rd, propeller；4th, supporting leg；5th, flash lamp；6th, high-definition camera；7、
Rotation axis；8th, storage battery；9th, controller；10th, sampling head；11st, air sampling case；12nd, receiver of remote-control sytem；13rd, solenoid valve；14、
Air inlet pipe；15th, syringe；16th, syringe core rod；17th, connector sleeve；18th, piston rod；19th, cylinder；20th, support plate；21st, sliding block；
22nd, sliding slot；23rd, screw rod；24th, clamp nut.
Embodiment
With reference to the drawings and specific embodiments, the utility model is described in further detail.It is to be understood that these embodiments are only used for
Illustrate the utility model rather than limitation the scope of the utility model.In addition, it should also be understood that, reading the utility model instruction
Content after, those skilled in the art can make various changes or modifications the utility model, and such equivalent forms equally fall
In scope defined herein.
A kind of unmanned plane for air monitering, including fuselage 1, the top of the fuselage 1 is provided with rotation axis 7, described
Propeller 3 is provided with rotation axis 7, the rotation axis 7 is provided with four altogether, and four 7 rectangular in form of rotation axis are distributed in
The top of fuselage 1.The bottom of the fuselage 1 is provided with cabinet 2, and cabinet 2 is hollow rectangular-shape.The surrounding of the cabinet 2
Supporting leg 4 is provided with, the supporting leg 4 is fixed on the fuselage 1, and unmanned plane is used to support unmanned plane when landing, and increases stability.It is described
Inside setting air sampling case 11, controller 9 and the storage battery 8 of cabinet 2, the use MDT20XX of controller 9 series monolithics,
EPSON monolithics or Intel MCS-51 series monolithics.It is preferred that solar panel, solar-electricity can be set in fuselage roof
Pond plate is electrically connected with storage battery.The storage battery 8 is connected by conducting wire with controller 9, is powered for unmanned plane.The air
Sampling box 11 is internally provided with syringe 15, and solenoid valve 13, the air inlet are provided with the air inlet pipe 14 of the syringe 15
The end set of pipe 14 has sampling head 10, and the sampling head 10 is fixed on the bottom of cabinet 2, and the top of the syringe 15 is set
Cylinder 19, the cylinder 19 are fixed on the top of air sampling case 11, the piston rod 18 of the cylinder 19 by connector sleeve 17 with
Syringe core rod 16 in syringe 15 connects, and the bottom of the cabinet 2 is provided with receiver of remote-control sytem 12, the propeller 3, electricity
Magnet valve 13 and cylinder 19 are connected by conducting wire with controller 9 respectively, and the controller 9 is connected by conducting wire and receiver of remote-control sytem 12
Connect.
Operation principle：In use, transmitting a signal to receiver of remote-control sytem 12 by remote manipulator, receiver of remote-control sytem 12 will be believed
Number pass to controller 9, controller 9 controls propeller 3 to start rotation to rise, to designated position after start to gather air, pass through
Controller 9 controls solenoid valve 13 to open, and controls 19 setting in motion of cylinder, first extracts air by the air displacement 3 in syringe 15
~5 times, then collection site air, then solenoid valve 1313 is closed, after collection, controls receiver of remote-control sytem 12 by unmanned plane
Withdraw, syringe 15 is taken back air sample and is detected, the sample in syringe 15 is analyzed.
The syringe 15 is provided with several altogether, and the cylinder 19 of the top of syringe 15 is connected by conducting wire and controller 9
Connect, controller 9 uses MDT20XX series monolithics, can control solenoid valve 13 in air sampling case 11 from left to right or from
A dextrad left side is opened successively, after being gathered in a certain position using syringe 15, change position using another syringe 15 after
It is continuous that to carrying out air acquisition, syringe 15 takes back the air samples of different sampled points easy to detection, not only monitoring range it is wide but also
Can multi-point sampling be averaged the accuracy that can increase monitoring.
The left and right sides that the fuselage 1 is located relatively at cabinet 2 sets the support plate 20 for being used for installing cabinet 2, the cabinet 2
Top sets first through hole, and the left and right ends that the cabinet 2 is located relatively at through hole are symmetrical arranged sliding block 21, in the support plate 20
The horizontally disposed sliding slot 22 being adapted with sliding block 21, set in the support plate 20 with matched second through hole of first through hole,
Screw rod 23 is further included, the screw rod 23 sequentially passes through first through hole, the second through hole and sets clamp nut 24 at both ends, works as cabinet
After syringe 15 in 2 samples, clamp nut 24, screw rod 23 can be removed successively, sliding block 21 is then skidded off into sliding slot
22, cabinet 2 is removed, replacement cabinet 2 reuses screw rod 23 and is fixed, continues to sample, further increase monitoring range.
The supporting leg 4 is equipped with flash lamp 5, and flash lamp 5 is connected by conducting wire with controller 9, can be convenient in monitoring
Staff finds the position of unmanned plane.
The supporting leg 4 is provided with four altogether, and four 4 rectangular in form of supporting leg are distributed in the bottom of fuselage 1, increase nobody
Stability when machine landing is contacted with ground.
The sampling head 10 is funnel-form, can facilitate 15 draw air of syringe.
High-definition camera 6 is set on the side wall of the cabinet 2, and high-definition camera 6 is connected by conducting wire with controller 9, is led to
Monitoring region can be shot by crossing setting high-definition camera 6, to understand the landforms in monitoring region.
Embodiment：
A kind of unmanned plane for air monitering, including fuselage 1, the top of the fuselage 1 is provided with rotation axis 7, described
Propeller 3 is provided with rotation axis 7, the rotation axis 7 is provided with four altogether, and four 7 rectangular in form of rotation axis are distributed in
The top of fuselage 1.The bottom of the fuselage 1 is provided with cabinet 2, and cabinet 2 is hollow rectangular-shape, the side wall of the cabinet 2
Upper setting high-definition camera 6.The left and right sides that the fuselage 1 is located relatively at cabinet 2 sets the support plate for being used for installing cabinet 2
20,2 top of cabinet sets first through hole, and the left and right ends that the cabinet 2 is located relatively at through hole are symmetrical arranged sliding block 21, institute
The sliding slot 22 for being horizontally disposed with support plate 20 and being adapted with sliding block 21 is stated, sets in the support plate 20 and is engaged with first through hole
The second through hole, further include screw rod 23, the screw rod 23 sequentially passes through first through hole, the second through hole and fastening spiral shell is set at both ends
Mother 24.The surrounding of the cabinet 2 is provided with supporting leg 4, and the supporting leg 4 is fixed on the fuselage 1, and the supporting leg 4 is provided with four altogether,
Four 4 rectangular in form of supporting leg are distributed in the bottom of fuselage 1, and the supporting leg 4 is equipped with flash lamp 5, and unmanned plane is used when landing
In support unmanned plane, increase stability.The inside of the cabinet 2 sets air sampling case 11, controller 9 and storage battery 8, described
Storage battery 8 is connected by conducting wire with controller 9, and the air sampling case 11 is internally provided with syringe 15, the syringe
15 are provided with several altogether.Solenoid valve 13 is provided with the air inlet pipe 14 of the syringe 15, the end of the air inlet pipe 14 is set
Sampling head 10 is equipped with, the sampling head 10 is fixed on the bottom of cabinet 2, and the sampling head 10 is funnel-form.The syringe 15
Top cylinder 19 is set, the cylinder 19 is fixed on the top of air sampling case 11, and the piston rod 18 of the cylinder 19 passes through
Connector sleeve 17 is connected with the syringe core rod 16 in syringe 15, and the bottom of the cabinet 2 is provided with receiver of remote-control sytem 12, described
Propeller 3, solenoid valve 13 and cylinder 19 are connected by conducting wire with controller 9 respectively, and the controller 9 is connect by conducting wire and remote control
Device 12 is received to connect.The beneficial effect of the present embodiment is：Syringe 15 is provided with several altogether, the sky in the more than enough certain area of energy
Gas carries out multi-point sampling, and syringe 15 takes back the air sample of different sampled points easy to detection, and not only monitoring range is wide but also energy
More than enough point sampling is averaged the accuracy that can increase monitoring；Screw rod 23 sequentially passes through first through hole, the second through hole and two
End sets clamp nut 24, after the syringe 15 in cabinet 2 samples, can replace cabinet 2 and continue to sample, into one
Step increase monitoring range.
Claims (7)
1. a kind of unmanned plane for air monitering, including fuselage (1), rotation axis (7) is provided with above the fuselage (1),
Propeller (3) is provided with the rotation axis (7), it is characterised in that：The bottom of the fuselage (1) is provided with cabinet (2), described
The surrounding of cabinet (2) is provided with supporting leg (4), and the supporting leg (4) is fixed on fuselage (1), and the inside of the cabinet (2) sets sky
Gas sampling box (11), controller (9) and storage battery (8), the storage battery (8) are connected by conducting wire with controller (9), the sky
Gas sampling box (11) is internally provided with syringe (15), and solenoid valve is provided with the air inlet pipe (14) of the syringe (15)
(13), the end set of the air inlet pipe (14) has sampling head (10), and the sampling head (10) is fixed on the bottom of cabinet (2),
The top of the syringe (15) sets cylinder (19), and the cylinder (19) is fixed on the top of air sampling case (11), described
The piston rod (18) of cylinder (19) is connected by connector sleeve (17) with the syringe core rod (16) in syringe (15), the cabinet
(2) bottom is provided with receiver of remote-control sytem (12), and the propeller (3), solenoid valve (13) and cylinder (19) pass through conducting wire respectively
It is connected with controller (9), the controller (9) is connected by conducting wire with receiver of remote-control sytem (12).
A kind of 2. unmanned plane for air monitering according to claim 1, it is characterised in that：The syringe (15) is altogether
It is provided with several.
A kind of 3. unmanned plane for air monitering according to claim 1 or 2, it is characterised in that：Fuselage (1) phase
The left and right sides for being pointed to cabinet (2) sets and is used to installing the support plates (20) of cabinet (2), and cabinet (2) top sets the
One through hole, the left and right ends that the cabinet (2) is located relatively at first through hole are symmetrical arranged sliding block (21), on the support plate (20)
The sliding slot (22) being adapted with sliding block (21) is horizontally disposed with, is set and first through hole matched second on the support plate (20)
Through hole, further includes screw rod (23), and the screw rod (23) sequentially passes through first through hole, the second through hole and sets clamp nut at both ends
(24)。
A kind of 4. unmanned plane for air monitering according to claim 1, it is characterised in that：Set on the supporting leg (4)
There is flash lamp (5).
A kind of 5. unmanned plane for air monitering according to claim 1, it is characterised in that：The supporting leg (4) sets altogether
Four are equipped with, four supporting leg (4) rectangular in form are distributed in the bottom of fuselage (1).
A kind of 6. unmanned plane for air monitering according to claim 1, it is characterised in that：During the cabinet (2) is
Empty rectangular-shape, the sampling head (10) is funnel-form.
A kind of 7. unmanned plane for air monitering according to claim 1, it is characterised in that：The side of the cabinet (2)
High-definition camera (6) is set on wall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721384600.8U CN207292410U (en) | 2017-10-23 | 2017-10-23 | A kind of unmanned plane for air monitering |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721384600.8U CN207292410U (en) | 2017-10-23 | 2017-10-23 | A kind of unmanned plane for air monitering |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207292410U true CN207292410U (en) | 2018-05-01 |
Family
ID=62273758
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721384600.8U Expired - Fee Related CN207292410U (en) | 2017-10-23 | 2017-10-23 | A kind of unmanned plane for air monitering |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207292410U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112046221A (en) * | 2020-09-21 | 2020-12-08 | 西南大学 | Dual-purpose unmanned aerial vehicle in air and ground |
| CN113514289A (en) * | 2020-04-09 | 2021-10-19 | 天津大学 | Unmanned aerial vehicle sampling device for mercury in different forms in atmosphere and using method thereof |
-
2017
- 2017-10-23 CN CN201721384600.8U patent/CN207292410U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113514289A (en) * | 2020-04-09 | 2021-10-19 | 天津大学 | Unmanned aerial vehicle sampling device for mercury in different forms in atmosphere and using method thereof |
| CN112046221A (en) * | 2020-09-21 | 2020-12-08 | 西南大学 | Dual-purpose unmanned aerial vehicle in air and ground |
| CN112046221B (en) * | 2020-09-21 | 2022-12-23 | 西南大学 | Dual-purpose unmanned aerial vehicle in air and ground |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207292410U (en) | A kind of unmanned plane for air monitering | |
| CN104198227A (en) | Catering source particulate matter and volatile organic compound sampling system | |
| CN103558066A (en) | On-line monitoring sampling system for sulfur hexafluoride gas | |
| CN104683759B (en) | Inner wall of stack corrosion condition wireless video monitoring apparatus and method for based on aircraft | |
| CN205378008U (en) | Big data acquisition and processing apparatus | |
| CN104677690B (en) | A kind of atmospheric aerosol automatic acquisition device | |
| CN103162992A (en) | Method and device for aircraft airborne environment gas automatic collection | |
| CN204064752U (en) | The comprehensive air sampler of a kind of six gas circuit | |
| CN208847535U (en) | Full gas circuit rinse atmosphere quality high-altitude gradient samples double light unmanned planes | |
| CN108146628A (en) | Carry the unmanned plane of aerosol sampling apparatus | |
| CN107571236A (en) | A kind of long-life, low maintenance rate crusing robot | |
| CN201673126U (en) | Tall building wall surface crack detection device | |
| CN201853960U (en) | Multifunctional photoelectric searching detector | |
| CN207215762U (en) | A kind of Gases Dissolved in Transformer Oil on-line monitoring system | |
| CN206114474U (en) | Atmospheric environment remote sensing monitoring mechanism | |
| CN111474317B (en) | Lake water quality monitoring system | |
| CN109001372A (en) | A kind of unmanned aerial vehicle onboard gas-detecting device remotely controlled | |
| CN208477011U (en) | Telescopic high-pressure acoustooptical electroscope | |
| CN114839003A (en) | Multichannel VOCs sampling and atmospheric pollutants detecting system based on unmanned aerial vehicle | |
| CN203758804U (en) | Air sample and inhalable particle sampler | |
| CN106774017A (en) | A kind of Unmanned Aerial Vehicle Data acquisition system | |
| CN205450178U (en) | Transmission line fault locating on -line monitoring device | |
| CN209044039U (en) | The easy adjustment type cylindrical lithium battery thermal runaway experiment porch of nested type | |
| CN204856870U (en) | Rotation type air monitoring appearance based on zigBee wireless communication | |
| CN107687962A (en) | A kind of individual well undisturbed sampler |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180501 Termination date: 20181023 |