CN207292402U - With gas detection function unmanned plane - Google Patents
With gas detection function unmanned plane Download PDFInfo
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- CN207292402U CN207292402U CN201721018525.3U CN201721018525U CN207292402U CN 207292402 U CN207292402 U CN 207292402U CN 201721018525 U CN201721018525 U CN 201721018525U CN 207292402 U CN207292402 U CN 207292402U
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Abstract
Unmanned plane field is the utility model is related to, more particularly to a kind of unmanned plane with gas detection function, including unmanned plane body, the load platform that is arranged on unmanned plane body and the detection of gas module on load platform；Detection of gas module includes drive component, cable assembly, carry component and detection of gas component, and detection of gas module is installed on load platform by carry component；Drive component and carry component are installed on the shell of cable assembly, the output axis connection of the roller of cable assembly and the motor of drive component, are wound with hawser on roller, detection of gas component is connected on the tache motorice of hawser.The unmanned plane with gas detection function of the utility model, the topology layout of its whole detection of gas module is relatively simple, mobility is preferable, so as to which the dispensing of detection of gas component promptly and accurately is carried out gas-monitoring to appointed place, to achieve the purpose that to feed back testing result into disaster relief personnel in time.
Description
Technical field
Unmanned plane field is the utility model is related to, more particularly to a kind of unmanned plane with gas detection function.
Background technology
In all kinds of disaster accident scenes such as the energy, chemical industry or the attack of terrorism, disaster relief personnel need first to understand disaster field
Dangerous position information after, be only possible to than relatively safe performing the task of rescuing；Especially some are inflammable and explosive, chemical accident is existing
Field needs the long-range monitoring key parameter such as hazardous gas component and concentration, is taken appropriate measures according to testing result, kept away as far as possible
Exempt from dangerous generation, farthest reduce loss.
At present, gas-monitoring is carried out to disaster field using UAV flight's gas detecting instrument, is more feasible and safe
Long-range monitoring mode；But the gas detection module of existing unmanned plane, structure is complex, and mobility is poor, leads
Result of detection is caused accurately and timely to feed back to disaster relief personnel, it is possible to delay optimal rescue opportunity.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane with gas detection function, its detection of gas modular structure
It is relatively simple, and mobility is preferable, testing result timely and accurately can be fed back to disaster relief personnel.
To solve the above-mentioned problems, the utility model provides a kind of unmanned plane with gas detection function, including nothing
Man-machine body, the load platform being arranged on the unmanned plane body and the detection of gas mould on the load platform
Block；Wherein, the detection of gas module includes drive component, cable assembly, carry component and detection of gas component, the gas
Detecting module is installed on the load platform by the carry component；The driving component and carry component are installed in institute
State on the shell of cable assembly, the output axis connection of the roller of the cable assembly and the motor of the driving component, the rolling
Hawser is wound with wheel, the detection of gas component is connected on the tache motorice of the hawser.
Preferably, controller is further included, the controller is equipped with control unit and signal transmitting and receiving unit, the electricity
Machine is electrically connected with described control unit；The signal transmitting and receiving unit receives the control signal of unmanned aerial vehicle control system, and this is controlled
Signal processed feeds back to control unit, to control motor to work.
Preferably, the driving component includes protective shell and the motor, and the motor is installed on the protection
In shell, the protective shell is fixed on the shell of the cable assembly, and the output shaft of the motor is stretched out out of described protective shell
And it is connected with the roller of the cable assembly.
Preferably, the cable assembly includes the shell, the shaft being located in the shell and the roller
And be wrapped in the hawser on the roller, the roller is socketed in the shaft, the shaft by bearing with it is described outer
Shell is rotatablely connected, and the shaft and the output shaft of the motor are coaxially connected；The bottom of the shell is equipped with perforation, the hawser
Tache motorice be pierced by from the perforation and be connected with the detection of gas component.
Preferably, the carry component includes carry plate and linking arm, and one end of the linking arm is fixed
On the carry plate, the other end connection of the linking arm is on the housing；The carry plate is equipped with multiple connecting holes,
The carry plate is fastenedly connected on the load platform through the connecting hole by screw.
Preferably, the detection of gas component includes housing, the sensor assembly being arranged in the housing, passes
Sensor signal processing module, central control module, air-breathing pump module, GPS module, power module, memory module, be wirelessly transferred mould
Block, gas receiving module；Wherein, the sensor assembly, the sensor signal processing module, air-breathing pump module, GPS moulds
Block, power module, memory module, wireless transport module are electrically connected with central control module；The air-breathing pump module will absorb
To under test gas be transferred to the gas receiving module, the sensor assembly docks received under test gas and is detected.
Preferably, the detection of gas component further includes the anti-tumble mould being electrically connected with the central control module
Block and alarm module.
The unmanned plane with gas detection function of the utility model, its detection of gas module is by drive component and carry group
Part integrated installation drives the roller of cable assembly to rotate on the shell of cable assembly, and by the motor of drive component, realizes
The function of folding and unfolding detection of gas component, the topology layout of whole detection of gas module is relatively simple, and mobility is preferable, so as to
The dispensing of detection of gas component promptly and accurately is subjected to gas-monitoring to appointed place, is rescued with reaching in time to feed back testing result
The purpose of calamity personnel, is that disaster relief personnel can get hold of optimal rescue opportunity, farthest reduces loss.
Brief description of the drawings
Fig. 1 is the overall structure diagram of the unmanned plane with gas detection function of the preferred embodiment in the utility model；
Fig. 2 is the vertical of the detection of gas module of the unmanned plane with gas detection function of the preferred embodiment in the utility model
Body structure diagram；
Fig. 3 is the schematic cross-section of the detection of gas module shown in Fig. 2.
Wherein, 1, drive component；11st, protective shell；12nd, motor；13rd, output shaft；2nd, cable assembly；21st, shell；22nd, roll
Wheel；23rd, hawser；24th, shaft；25th, bearing；3rd, carry component；31st, carry plate；32nd, linking arm；4th, detection of gas component；41、
Housing；42nd, display screen；43rd, gas receiving terminal；10th, unmanned plane body；20th, detection of gas module；30th, load platform.
Embodiment
With reference to the accompanying drawings and examples, specific embodiment of the present utility model is described in further detail.Below
Embodiment is used to illustrate the utility model, but is not intended to limit the scope of the present invention.
As shown in Figure 1 to Figure 3, nobody with gas detection function of the utility model embodiment is schematically showed
Machine, it includes unmanned plane body 10, the load platform 30 being arranged on 10 lower part of unmanned plane body and installed in load platform
Detection of gas module 20 on 30；Wherein, detection of gas module 20 includes drive component 1, cable assembly 2, carry component 3 and gas
Body probe assembly 4, detection of gas module 20 are installed on load platform 30 by carry component 3；Wherein, drive component 1 and extension
Carry component 3 to be installed on the shell 21 of cable assembly 2, the output of the roller 22 of cable assembly 2 and the motor 12 of drive component 1
Axis 13 connects, and hawser 23 is wound with roller 22, and detection of gas component 4 is connected on the tache motorice of hawser 23.
The detection of gas module 20 of the unmanned plane with gas detection function of the utility model embodiment, due to that will drive
Component 1 and 3 integrated installation of carry component drive hawser on the shell 21 of cable assembly 2, and by the motor 12 of drive component 1
The roller 22 of component 2 rotates, and realizes the function of folding and unfolding detection of gas component 4, the topology layout of whole detection of gas module is more
Simply, mobility is preferable, so as to which the dispensing of detection of gas component 4 promptly and accurately is carried out gas-monitoring to appointed place,
It is that disaster relief personnel can get hold of optimal rescue opportunity, most to achieve the purpose that to feed back testing result into disaster relief personnel in time
Reduce loss to big degree.
The detection of gas module of the utility model embodiment further includes controller, and controller is equipped with control unit and signal is received
Bill member, motor 12 are electrically connected with control unit；Signal transmitting and receiving unit receives the control signal of unmanned aerial vehicle control system, and should
Control signal feeds back to control unit, to control motor 12 to work, to realize the mesh of control 12 folding and unfolding detection of gas component 4 of motor
's.
Please after with reference to shown in Fig. 1 and Fig. 2, drive component 1 includes protective shell 11 and the motor in protective shell 11
12, motor 12 is installed in protective shell 11, can prevent that motor 12 from being damaged be subject to the external world, and cisco unity malfunction, protection
Shell 11 is fixed on the shell 21 of cable assembly 2, so that more firm, the motor that drive component 1 can be connected with cable assembly 2
12 output shaft 13 is stretched out out of protective shell 11 and is connected with the roller 22 of cable assembly 2, can improve whole detection of gas module
Structural compactness.
Cable assembly 2 includes shell 21, the shaft 24 being located in shell 21 and roller 22 and is wrapped on roller 22
Hawser 24, roller 22 are socketed in shaft 24, and shaft 24 is rotatablely connected by bearing 25 and shell 21, shaft 24 and motor 12
Output shaft 13 is coaxially connected, and shell 21 can play a protective role roller 22, shaft 24 and bearing 25, prevent these components by
To external damage, and the compactedness of 2 structure of cable assembly can be improved；The bottom of shell 21 is equipped with perforation, the fortune of hawser 23
Moved end is pierced by from perforation to be connected with detection of gas component 4.
With reference to shown in Fig. 1 to Fig. 3, carry component 3 includes carry plate 31 and linking arm 32, and one end of linking arm 32 is fixed on
On carry plate 31, the other end of linking arm 32 is connected on shell 21；Carry plate 31 is equipped with multiple connecting holes, is worn by screw
Cross connecting hole carry plate 31 is fastenedly connected on unmanned plane body 10, to realize whole detection of gas module and unmanned plane sheet
Body 10 is reliably connected.
Detection of gas component 4 includes housing 41, the sensor assembly being arranged in housing 41, sensor signal processing mould
Block, central control module, air-breathing pump module, GPS module, power module, memory module, wireless transport module, gas receive mould
Block；Wherein, sensor assembly, sensor signal processing module, air-breathing pump module, GPS module, power module, memory module, nothing
Line transport module is electrically connected with central control module；Sensor component can detect the pernicious gas in disaster field in time
Component and concentration, the consequential signal of detection be sent to sensor signal processing module and carry out quick signal conversion and preliminary
Signal processing, and result is conveyed to central control module, so as to quick obtaining and analyzes the specific targets of pernicious gas；
Air-breathing pump module is electrically connected with central control module, to realize active inspiration detecting function, can quickly have been drawn
Evil gas, and the under test gas being absorbed to is transferred to gas receiving module, so that sensor assembly docks received gas to be measured
Body is detected.
In addition, detection of gas component 4 further includes the anti-tumble module being electrically connected with central control module and alarm module, when
When detection of gas module is surprisingly fallen, prompt message can be sent, and specific GPS geographical location information can be provided, and with searching
Rescue personnel searching；When the excessive concentration of pernicious gas, alarm module is started to work, and to search and rescue in a manner of flash of light or alarm
Personnel alarm, and can be when gas concentration exceedes investigative range, to remind central control module to stop detection operations.
The above is only the preferred embodiment of the utility model, it is noted that for the common skill of the art
For art personnel, on the premise of the utility model technical principle is not departed from, some improvement and replacement can also be made, these change
The scope of protection of the utility model is also should be regarded as into replacement.
Claims (7)
1. a kind of unmanned plane with gas detection function, it is characterised in that including unmanned plane body, be arranged on the unmanned plane
Load platform on body and the detection of gas module on the load platform；Wherein,
The detection of gas module includes drive component, cable assembly, carry component and detection of gas component, the detection of gas
Module is installed on the load platform by the carry component；
The driving component and carry component are installed on the shell of the cable assembly, the roller of the cable assembly and institute
The output axis connection of the motor of drive component is stated, hawser is wound with the roller, the detection of gas component is connected to described
On the tache motorice of hawser.
2. the unmanned plane according to claim 1 with gas detection function, it is characterised in that further include controller, institute
State controller and be equipped with control unit and signal transmitting and receiving unit, the motor is electrically connected with described control unit；The signal transmitting and receiving
Unit receives the control signal of unmanned aerial vehicle control system, and the control signal is fed back to control unit, to control motor to work.
3. the unmanned plane according to claim 1 with gas detection function, it is characterised in that the driving component includes
Protective shell and the motor, the motor are installed in the protective shell, and the protective shell is fixed on the outer of the cable assembly
On shell, the output shaft of the motor is stretched out out of described protective shell and is connected with the roller of the cable assembly.
4. the unmanned plane according to claim 1 with gas detection function, it is characterised in that the cable assembly includes
The shell, the shaft being located in the shell and the roller and the hawser being wrapped on the roller, the roller housing
It is connected in the shaft, the shaft is rotatablely connected by bearing and the shell, the shaft and the output shaft of the motor
It is coaxially connected；The bottom of the shell is equipped with perforation, and the tache motorice of the hawser is pierced by from the perforation to be visited with the gas
Survey component connection.
5. the unmanned plane according to claim 1 with gas detection function, it is characterised in that the carry component includes
Including carry plate and linking arm, one end of the linking arm is fixed on the carry plate, the other end connection of the linking arm
On the housing；The carry plate is equipped with multiple connecting holes, through the connecting hole that the carry plate is tight by screw
It is solidly connected on the load platform.
6. the unmanned plane according to claim 1 with gas detection function, it is characterised in that the detection of gas component
Including housing, the sensor assembly being arranged in the housing, sensor signal processing module, central control module, asepwirator pump
Module, GPS module, power module, memory module, wireless transport module, gas receiving module；Wherein, the sensor assembly,
The sensor signal processing module, air-breathing pump module, GPS module, power module, memory module, wireless transport module with
Central control module is electrically connected；The under test gas being absorbed to is transferred to the gas receiving module, institute by the air-breathing pump module
The received under test gas of sensor assembly docking is stated to be detected.
7. the unmanned plane according to claim 6 with gas detection function, it is characterised in that the detection of gas component
Further include the anti-tumble module being electrically connected with the central control module and alarm module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721018525.3U CN207292402U (en) | 2017-08-14 | 2017-08-14 | With gas detection function unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721018525.3U CN207292402U (en) | 2017-08-14 | 2017-08-14 | With gas detection function unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN207292402U true CN207292402U (en) | 2018-05-01 |
Family
ID=62444169
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201721018525.3U Active CN207292402U (en) | 2017-08-14 | 2017-08-14 | With gas detection function unmanned plane |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109204799A (en) * | 2018-09-30 | 2019-01-15 | 江苏省生态环境评估中心（江苏省排污权登记与交易管理中心） | The original place gas-dynamic monitoring device and its application method of reconnaissance are transported and visualized based on unmanned plane |
| CN109254122A (en) * | 2018-10-24 | 2019-01-22 | 阮斌 | A kind of multi-parameter gas detection device based on unmanned plane |
| CN109911229A (en) * | 2019-03-23 | 2019-06-21 | 佛山昊航科技有限公司 | A kind of environment monitoring unmanned vehicle |
-
2017
- 2017-08-14 CN CN201721018525.3U patent/CN207292402U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109204799A (en) * | 2018-09-30 | 2019-01-15 | 江苏省生态环境评估中心（江苏省排污权登记与交易管理中心） | The original place gas-dynamic monitoring device and its application method of reconnaissance are transported and visualized based on unmanned plane |
| CN109204799B (en) * | 2018-09-30 | 2023-11-10 | 生态环境部南京环境科学研究所 | Unmanned plane transportation and visual point selection-based in-situ gas dynamic monitoring device and application method thereof |
| CN109254122A (en) * | 2018-10-24 | 2019-01-22 | 阮斌 | A kind of multi-parameter gas detection device based on unmanned plane |
| CN109911229A (en) * | 2019-03-23 | 2019-06-21 | 佛山昊航科技有限公司 | A kind of environment monitoring unmanned vehicle |
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