CN208383194U - Atmospheric detection equipment for unmanned plane - Google Patents
Atmospheric detection equipment for unmanned plane Download PDFInfo
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- CN208383194U CN208383194U CN201821246121.4U CN201821246121U CN208383194U CN 208383194 U CN208383194 U CN 208383194U CN 201821246121 U CN201821246121 U CN 201821246121U CN 208383194 U CN208383194 U CN 208383194U
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- box body
- unmanned plane
- mcu controller
- circuit board
- electrically connected
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Abstract
The utility model provides a kind of atmospheric detection equipment for unmanned plane, including box body, control circuit board and gas sensor are respectively arranged in the box body, multiple ports are offered on the box body, antenna and the fast connection mechanism for connecting unmanned plane are also respectively provided on the box body, the control circuit board includes circuit board body and the MCU controller that is separately positioned in the circuit board body, storage unit, inserting groove, wireless communication unit and signal processing circuit, the inserting groove is for gas sensor described in grafting, the MCU controller is electrically connected the storage unit and the gas sensor, the MCU controller is also electrically connected the antenna by the signal processing circuit and the wireless communication unit.The utility model has the advantages that design science, practical, structure is simple, easy to use.
Description
Technical field
The utility model relates to a kind of atmospheric detection equipment for unmanned plane.
Background technique
Now with the development of science and technology, unmanned plane is no longer used only for military mission, applies model in civil field
Enclose also more wide, unmanned plane can complete camera shooting, detection in environment badly, even dangerous, scout, search and rescue an etc. system
The activity of column.Individual unmanned plane function is more single, it usually needs cooperates other plug-in devices to realize multiple functions, in unmanned plane
Upper carry atmospheric detection equipment is one way in which.Present patent application is intended to provide a kind of atmospheric detection for unmanned plane
Equipment facilitates carry out atmospheric detection by the cooperation with unmanned plane.
In order to solve the above problems, people are seeking always a kind of ideal technical solution.
Summary of the invention
The purpose of this utility model is in view of the deficiencies of the prior art, to provide a kind of design science, practical, knot
Structure is simple, the atmospheric detection equipment easy to use for unmanned plane.
To achieve the goals above, the technical scheme adopted by the utility model is a kind of atmosphere for unmanned plane is examined
Measurement equipment, including box body are respectively arranged with control circuit board and gas sensor in the box body, offer on the box body more
A port is also respectively provided with antenna and the fast connection mechanism for connecting unmanned plane, the control circuit board packet on the box body
MCU controller, storage unit, the inserting groove, wireless communication for including circuit board body and being separately positioned in the circuit board body
Unit and signal processing circuit, the inserting groove is for gas sensor described in grafting, described in the MCU controller is electrically connected
Storage unit and the gas sensor, the MCU controller are also single by the signal processing circuit and the wireless communication
Member is electrically connected the antenna.
Based on above-mentioned, further include gas production bag, air pump and solenoid valve, the gas production are respectively arranged at the gas production bag sack
The top of bag and the bottom of the box body are correspondingly arranged on bindiny mechanism, and the MCU controller is electrical by the bindiny mechanism
Connect the air pump and the solenoid valve.
Based on above-mentioned, the bindiny mechanism includes the plug being arranged on the gas production bag and is arranged on the box body
Slot, the plug includes the vertical pivot and the horizontal axis that the vertical pivot end is arranged in that one end is arranged on the gas production bag, described
It is respectively arranged with limit convex at the top of the both ends of horizontal axis, is provided with the first hard contact, first metal at the top of the limit convex
Contact is electrically connected the air pump and the solenoid valve；The slot includes the cavity being arranged on the box body, vertically arranged
In the cavity the spring of bottom, the sheet metal of the spring end is set and the corresponding horizontal axis is arranged in the cavity
The socket at top corresponds to the horizontal axis in the cavity top inner wall and the limit convex is provided with limiting slot, the limiting slot
It is inside provided with the second hard contact, second hard contact is electrically connected the MCU controller.
Based on above-mentioned, the fast connection mechanism includes frame body, the fastener being arranged at the top of the frame body and is arranged described
The sliding slot of frame body bottom, the frame body are fixed below unmanned plane by the fastener, and the box body is slidably arranged in described
In sliding slot, it is provided with semi-circular groove at the top of the box body, the frame body bottom corresponds to the semi-circular groove and is provided with spring
The frame body bottom setting is protruded in pin, the end of the spring catch.
The utility model has substantive features and progress compared with the prior art, and specifically, the utility model passes through fast
Box body is arranged below unmanned plane and is realized that fast assembling-disassembling, gas sensor detect big by the port on box body by connection mechanism
Gas, and the data of acquisition are back to user terminal by antenna, with design science, practical, structure is simple, uses
Convenient advantage.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the structural schematic diagram of the fast connection mechanism of the utility model.
Fig. 3 is the structural schematic diagram of the utility model cavity.
Fig. 4 is the structural schematic diagram of the utility model inside cavity.
Fig. 5 is the structural schematic diagram of the utility model cavity top inner wall.
Fig. 6 is the structural schematic diagram of the utility model plug.
In figure: 1. box bodys；2. port；3. antenna；4. spring catch；5. bolt hole；6. semi-circular groove；7. sliding slot；8. chamber
Body；9. socket；10. spring；11. sheet metal；12. limiting slot；13. vertical pivot；14. horizontal axis；15. limit convex；16. the first metal touches
Point.
Specific embodiment
Below by specific embodiment, the technical solution of the utility model is described in further detail.
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4, Fig. 5 and Fig. 6, a kind of atmospheric detection equipment for unmanned plane, including box body
1, control circuit board and gas sensor are respectively arranged in the box body 1, and multiple ports 2 are offered on the box body 1, it is described
Antenna 3 and the fast connection mechanism for connecting unmanned plane are also respectively provided on box body 1, the control circuit board includes circuit board sheet
Body and MCU controller, storage unit, inserting groove, wireless communication unit and the signal being separately positioned in the circuit board body
Processing circuit, the inserting groove for gas sensor described in grafting, the MCU controller be electrically connected the storage unit and
The gas sensor, the MCU controller are also electrically connected by the signal processing circuit and the wireless communication unit
The antenna 3.
In use, the gas sensor of needs is inserted into the inserting groove, the box body 1 is pacified by the fast connection mechanism
Below unmanned plane.Unmanned plane during flying is controlled to target area, air enters in the box body 1 from the port 2, described
While the detection data of the gas sensor is stored into the storage unit by MCU controller, also pass through the channel radio
Letter unit and the antenna 3 are sent to the user terminal.Signal processing circuit described in the present embodiment is conventional filter and amplification electricity
Road, the gas sensor include SO 2 sensor, NOx sensor, chlorination hydrogen sensor, hydrogen sulfide sensor,
Ammonia gas sensor, carbon monoxide transducer, cyaniding hydrogen sensor, fluorination hydrogen sensor, bromine gas sensor, chlorine sensor, first
Aldehyde sensor etc..
In practice, the fast connection mechanism includes frame body, the fastener being arranged at the top of the frame body and is arranged in the frame
The sliding slot 7 of body bottom, the frame body are fixed below unmanned plane by the fastener, and the box body 1 is slidably arranged in described
In sliding slot 7, semi-circular groove 6 is provided at the top of the box body 1, the frame body bottom corresponds to the semi-circular groove 6 and is provided with
The frame body bottom setting is protruded in spring 104, the end of the spring 104.Fastener described in the present embodiment is bolt and spiral shell
Keyhole 5.When dismounting the box body 1, only need to the box body 1 be inserted into or be skidded off out of described sliding slot 7, it is convenient and efficient to tear open
Dress；The mutual cooperation of the spring 104 and the semi-circular groove 6, plays the role of limit and fixing to the box body 1.
Preferably, which further includes gas production bag, described to adopt for acquiring gas sample
Air pump and solenoid valve are respectively arranged at airbag sack, the top of the gas production bag and the bottom of the box body 1 are correspondingly arranged on
Bindiny mechanism, the MCU controller are electrically connected the air pump and the solenoid valve by the bindiny mechanism.According to the gas
The gas data of body sensor acquisition, when needing to acquire gas sample, the MCU controller controls the solenoid valve and opens, and
It controls the air pump and is filled with air into the gas production bag, the MCU controller controls the gas according to the preset sampling time
Pump stops working and controls the solenoid valve and closes.
In the present embodiment, the bindiny mechanism includes the plug being arranged on the gas production bag and is arranged in the box body 1
On slot, the plug includes the vertical pivot 13 that is arranged on the gas production bag of one end and the cross that 13 end of vertical pivot is arranged in
The both ends top of axis 14, the horizontal axis 14 is respectively arranged with limit convex 15, and the touching of the first metal is provided at the top of the limit convex 15
Point 16, first hard contact 16 is electrically connected the air pump and the solenoid valve；The slot includes being arranged in the box
Cavity 8 on body 1 is vertically provided at the spring of bottom in the cavity 8, the sheet metal 11 of the spring end is arranged in and right
It answers the horizontal axis 14 that the socket 9 at 8 top of cavity is set, corresponds to the horizontal axis 14 and institute in 8 top inner wall of cavity
It states limit convex 15 and is provided with limiting slot 12, the second hard contact, the second hard contact electricity are provided in the limiting slot 12
Property the connection MCU controller.In use, the horizontal axis 14 is inserted into the socket 9 and is pressed to the direction of the cavity 8
Pressure, the horizontal axis 14 compresses the spring by the sheet metal 11, after the horizontal axis 14 enters in the cavity 8 described in rotation
After 14 90 degree of horizontal axis, the horizontal axis 14 is pressed into the limiting slot 12 under spring force effect, first gold medal
Belong to contact 16 and second hard contact is in electrical contact.When removing the gas production bag from the box body 1, to the box body 1
Direction presses 90 degree of counter-rotating simultaneously of the vertical pivot 13, and the horizontal axis 14 can be by the cross after being aligned with the socket 9
Axis 14 takes out out of described cavity 8, convenient for disassembly and assembly.
Finally it should be noted that: above embodiments are only to illustrate the technical solution of the utility model rather than limit it
System；Although the utility model has been described in detail with reference to the preferred embodiment, those of ordinary skill in the art should
Understand: specific implementation of the utility model can still be modified or is equally replaced to some technical characteristics
It changes；Without departing from the spirit of technical solutions of the utility model, should all cover in the claimed technical solution of the utility model
In range.
Claims (4)
1. a kind of atmospheric detection equipment for unmanned plane, it is characterised in that: including box body, control is respectively arranged in the box body
Circuit board and gas sensor processed offer multiple ports on the box body, are also respectively provided with antenna and use on the box body
In the fast connection mechanism of connection unmanned plane, the control circuit board includes circuit board body and is separately positioned on the circuit board body
On MCU controller, storage unit, inserting groove, wireless communication unit and signal processing circuit, the inserting groove be used for grafting institute
Gas sensor is stated, the MCU controller is electrically connected the storage unit and the gas sensor, the MCU controller
The antenna is also electrically connected by the signal processing circuit and the wireless communication unit.
2. the atmospheric detection equipment according to claim 1 for unmanned plane, it is characterised in that: further include gas production bag, institute
It states and is respectively arranged with air pump and solenoid valve at gas production bag sack, the top of the gas production bag and the bottom of the box body are correspondingly arranged
There is bindiny mechanism, the MCU controller is electrically connected the air pump and the solenoid valve by the bindiny mechanism.
3. the atmospheric detection equipment according to claim 2 for unmanned plane, it is characterised in that: the bindiny mechanism includes
The plug being arranged on the gas production bag and the slot being arranged on the box body, the plug include that one end setting is adopted described
Vertical pivot on airbag and the horizontal axis that the vertical pivot end is arranged in are respectively arranged with limit convex at the top of the both ends of the horizontal axis, institute
It states and is provided with the first hard contact at the top of limit convex, first hard contact is electrically connected the air pump and the solenoid valve；
The slot includes the cavity being arranged on the box body, the spring of vertically arranged bottom in the cavity, is arranged described
The socket at the top of the cavity is arranged in the sheet metal of spring end and the corresponding horizontal axis, corresponds in the cavity top inner wall
The horizontal axis and the limit convex are provided with limiting slot, and the second hard contact, second metal are provided in the limiting slot
Contact is electrically connected the MCU controller.
4. the atmospheric detection equipment according to claim 1 for unmanned plane, it is characterised in that: the fast connection mechanism includes
Frame body, the fastener being arranged at the top of the frame body and the sliding slot that the frame body bottom is arranged in, the frame body pass through described tight
Firmware is fixed below unmanned plane, and the box body is slidably arranged in the sliding slot, is provided at the top of the box body semi-circular recessed
Slot, the frame body bottom correspond to the semi-circular groove and are provided with spring catch, and the frame body bottom is protruded in the end of the spring catch
Portion's setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821246121.4U CN208383194U (en) | 2018-08-03 | 2018-08-03 | Atmospheric detection equipment for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821246121.4U CN208383194U (en) | 2018-08-03 | 2018-08-03 | Atmospheric detection equipment for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208383194U true CN208383194U (en) | 2019-01-15 |
Family
ID=64962280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821246121.4U Active CN208383194U (en) | 2018-08-03 | 2018-08-03 | Atmospheric detection equipment for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208383194U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111287797A (en) * | 2020-04-09 | 2020-06-16 | 李化玉 | Underground coal mine communication control device |
-
2018
- 2018-08-03 CN CN201821246121.4U patent/CN208383194U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111287797A (en) * | 2020-04-09 | 2020-06-16 | 李化玉 | Underground coal mine communication control device |
| CN111287797B (en) * | 2020-04-09 | 2021-09-17 | 安徽恒源煤电股份有限公司 | Underground coal mine communication control device |
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