CN205499370U - Environmental protection sampling aircraft - Google Patents
Environmental protection sampling aircraft Download PDFInfo
- Publication number
- CN205499370U CN205499370U CN201620309910.2U CN201620309910U CN205499370U CN 205499370 U CN205499370 U CN 205499370U CN 201620309910 U CN201620309910 U CN 201620309910U CN 205499370 U CN205499370 U CN 205499370U
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- environmental protection
- sampling
- control system
- aircraft
- joint
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Abstract
The utility model discloses an environmental protection sampling aircraft. This environmental protection sampling aircraft includes: the organism is provided with control system and wireless receiving device in, the wireless receiving device links to each other with control system, the motor, it is continuous with the control system of organism, the rotor, its pivot links to each other with the output shaft of motor, sampling mechanism installs in the organism, the remote controller, it is provided with wireless transmitting device, wireless transmitting device and wireless receiving device signal connection. The utility model provides an environmental protection sampling aircraft can accomplish the high altitude sampling automatically, and work efficiency is high, operating personnel only need the ground control can, need not to ascend a height, effectively ensured operating personnel's personal safety. In addition, sampling gas purity is high.
Description
Technical field
This utility model relates to environmental protection Sampling techniques field, particularly relates to a kind of environmental protection sampling aircraft.
Background technology
Along with industrialized continuous propelling, environment runs down, and the dynamics of environment monitoring is constantly strengthened by China.It is the important means realizing environment monitoring that gas carries out sampling monitoring.Then the operating mode of environmental protection sampling is the most severe, particularly samples high air body, during as sampled the discharge gas of chimney, needs operator to climb up high chimney.In work process, the safety of operator not only can not be guaranteed, and also wastes time and energy, and work efficiency is extremely low.
Utility model content
In order to solve above technical problem, this utility model provides a kind of environmental protection sampling aircraft.
This utility model provides a kind of environmental protection sampling aircraft, including:
Body, is provided with control system and radio receiver in described body；Described radio receiver is connected with described control system；
Motor, is connected with the control system of described body；
Rotor, its rotating shaft is connected with the output shaft of described motor；
Sampling mechanism, is installed on described body；Described sampling mechanism includes: asepwirator pump, air inlet pipe, the gentle capsule of connection pipeline；
Described asepwirator pump is connected with described control system, and its air inlet is connected with one end of described air inlet pipe；Air vent is connected with described one end being connected pipeline, the other end of described connection pipeline and described airbags；
It is provided with switch valve on described connection pipeline；Described switch valve is connected with described control system；Described switch valve has two kinds of duties, and in the first operative state, described air vent connects with described air bag；In a second operative state, described air vent connects with ambient atmosphere；
Remote controller, it is provided with wireless launcher, and described wireless launcher is connected with described radio receiver signal.
Further, described body being provided with connecting rod, described motor is installed on described connecting rod.
Further, the number of described rotor is multiple, and the circumference along described body is evenly arranged.
Further, the number of described rotor is 6.
Further, also include:
Connecting flexible pipe, its one end is connected with the other end of described air inlet pipe；
First joint, it is arranged at the other end of described connection flexible pipe；
Exhaust tube, its one end is arranged at sample area；
Second joint, is arranged at the other end of described exhaust tube；Described first joint is suitable with described second joint.
Further, described first joint being provided with electric magnet, described second joint is metal joint.
Further, also include the first photographic head, be installed on the top of described body.
Further, also include that support, described support are arranged at the bottom surface of described body.
Further, also include second camera, be installed on described support.
This utility model provides a kind of environmental protection sampling aircraft, when needs carry out high-altitude sampling, inputs flight directive to remote controller, and control system controls electric machine rotation, and electric machine rotation drives rotor wing rotation, and rotor wing rotation produces lift, environmental protection sampling aircraft takeoff；By adjusting the rotating speed of motor, the rotating speed of each rotor can be adjusted, so realize VTOL neatly, hovering, the flat of different directions fly and the motion such as rolling；Control environmental protection sampling aircraft and move to sample area, when needs are sampled, control system controls asepwirator pump work, control switch valve simultaneously and be in the second duty, the gas that now asepwirator pump sucks is first passed through after air inlet pipe enters and is discharged by air vent, realize the emptying of internal gas, to improve the purity of sample gas；After a period of time, after 20s, control system controls switch valve and is in the first duty, now, the gas that asepwirator pump sucks enters in air bag by air inlet pipe, when, after airbag aeration a period of time, control system controls asepwirator pump and quits work, control motor action makes environmental protection sampling aircraft fly back bottom surface simultaneously, completes sampling work.The environmental protection sampling aircraft that this utility model provides can be automatically performed high-altitude sampling, and work efficiency is high；Operator only need to control on ground, it is not necessary to ascends a height, the effective guarantee personal safety of operator.It addition, sample gas purity is high.
Accompanying drawing explanation
The front view of the environmental protection sampling aircraft that Fig. 1 provides for this utility model embodiment；
The top view of the environmental protection sampling aircraft that Fig. 2 provides for this utility model embodiment.
Description of reference numerals:
| 1 | Body | 11 | Air inlet pipe |
| 2 | Rotor | 12 | Connect flexible pipe |
| 3 | Motor | 13 | First joint |
| 4 | Connecting rod | 14 | Electric magnet |
| 5 | Support | 15 | First photographic head |
| 6 | Air bag | 16 | Second camera |
| 7 | Switch valve | 17 | Second joint |
| 8 | Connect pipeline | 18 | Exhaust tube |
| 9 | Asepwirator pump | 19 | Chimney |
| 10 | Air vent |
Detailed description of the invention
In order to make those skilled in the art be more fully understood that this utility model scheme, the utility model is described in further detail with detailed description of the invention below in conjunction with the accompanying drawings.
Refer to Fig. 1 and Fig. 2, the figure shows the environmental protection sampling aircraft that this utility model embodiment provides, it specifically includes:
Body 1, is provided with control system and radio receiver (not shown) in body 1；Radio receiver is connected with control system；
Motor 3, is connected with the control system of body 1；I.e. control system controls the duty of motor 3；
Rotor 2, its rotating shaft is connected with the output shaft of motor 3；
Sampling mechanism, is installed on body 1；Sampling mechanism specifically includes: asepwirator pump 9, air inlet pipe 11, connection pipeline 8 and air bag 6；
Asepwirator pump 9 is connected with control system, i.e. control system controls the duty of asepwirator pump 9；
The air inlet of asepwirator pump 9 is connected with one end of air inlet pipe 11；
The air vent 10 of asepwirator pump 9 is connected with the one end being connected pipeline 8, and the other end connecting pipeline 8 is connected with air bag 6；
Connecting and be provided with switch valve 7 on pipeline 8, this switch valve 7 is connected with control system, i.e. control system controls the duty of this switch valve 7；
This switch valve 7 has two kinds of duties, and in the first operative state, air vent 10 connects with air bag 6；In a second operative state, air vent 10 connects with ambient atmosphere；
Remote controller, it is provided with wireless launcher, and wireless launcher is connected with radio receiver signal.
The operation principle of the environmental protection sampling aircraft that the present embodiment provides is as follows:
The instruction of remote controller is sent to radio receiver by wireless launcher, and this instruction is transferred to control system by radio receiver again, and control system controls motor 3, asepwirator pump 9 and the duty of switch valve 7 according to control instruction system；
When needs carry out high-altitude sampling, inputting flight directive to remote controller, control system controls motor 3 and rotates, and motor 3 rotates and drives rotor 2 to rotate, and rotor 2 rotates and produces lift, environmental protection sampling aircraft takeoff；By adjusting the rotating speed of motor 3, the rotating speed of each rotor 2 can be adjusted, so realize VTOL neatly, hovering, the flat of different directions fly and the motion such as rolling；
Control environmental protection sampling aircraft and move to sample area, when needs are sampled, control system controls asepwirator pump 9 and works, control switch valve 7 simultaneously and be in the second duty, the gas that now asepwirator pump 9 sucks is first passed through after air inlet pipe 11 enters and is discharged by air vent 10, realize the emptying of internal gas, to improve the purity of sample gas；After a period of time, after 20s, control system controls switch valve 7 and is in the first duty, now, the gas that asepwirator pump 9 sucks enters in air bag 6 by air inlet pipe 11, and after a period of time inflated by air bag 6, control system controls asepwirator pump 9 and quits work, control motor 3 action makes environmental protection sampling aircraft fly back bottom surface simultaneously, completes sampling work.
Further, installing motor 3 for convenience, above-mentioned body 1 is further preferably provided with connecting rod 4, motor 3 is installed on connecting rod 4.
In order to ensure this environmental protection sampling aircraft stationarity in flight course and motility, the number of rotor 2 is preferably several, and the circumference along body 1 is evenly arranged.It will be understood by those skilled in the art that the number of now connecting rod 4 is the most accordingly for multiple.Further, the number of rotor 2 can be 6.
As the preferred version of the present embodiment, this environmental protection sampling aircraft further preferably includes that support 5, support 5 are arranged at the bottom surface of body 1.This support 5 is used for supporting body 1 parts such as grade, it is to avoid above-mentioned parts directly contact with ground.
For the ease of observing operating mode residing for aircraft, above-mentioned environmental protection sampling aircraft further preferably includes the first photographic head 15, and it is installed on the top of body 1.It is, of course, also possible to include second camera 16, it is installed on above-mentioned support 5.Above-mentioned first photographic head 15 and/or second camera 16 preferably can be provided with monitor with the high-definition camera of multi-directional rotation on ground simultaneously, and then are easy to staff and observe position and the working condition of environmental protection sampling aircraft flight.
Further, in order to improve sampling efficiency and sample purity, referring to Fig. 1 and Fig. 2, above-mentioned environmental protection sampling aircraft further preferably includes:
Connecting flexible pipe 12, its one end is connected with the other end of air inlet pipe 11；
First joint 13, it is arranged at the other end connecting flexible pipe 12；
Exhaust tube 18, its one end is arranged at sample area, at the exhaust opening of chimney 19；
Second joint 17, is arranged at the other end of exhaust tube 18；First joint 13 is suitable with the second joint 17.
During operation, by adjusting the position of aircraft, make the first joint 13 and the second joint 17 be connected, be achieved in directly sampling from sample area.Further, above-mentioned first joint 13 is preferably provided with electric magnet 14(Fig. 2), the second joint 17 is metal joint.This electric magnet 14 can be connected with control system, the control system magnetic by control system of switching on or off electricity electric magnet 14, when needs are sampled, makes electric magnet 14 be energized so that the first joint 13 and the second joint 17 exact contact, is connected firmly；When stopping sampling, make electric magnet 14 dead electricity lose magnetism, facilitate the first union joint to leave the second union joint, it is ensured that the fly back operation of bottom surface of environmental protection sampling aircraft is unobstructed.
In sum, the environmental protection sampling aircraft that this utility model embodiment provides can be automatically performed high-altitude sampling, and work efficiency is high；Operator only need to control on ground, it is not necessary to ascends a height, the effective guarantee personal safety of operator.It addition, sample gas purity is high.
Above environmental protection provided by the utility model sampling aircraft is described in detail.Principle of the present utility model and embodiment are set forth by specific case used herein, and the explanation of above example is only intended to help to understand method of the present utility model and core concept thereof.Should be understood that; for those skilled in the art; on the premise of without departing from this utility model principle, it is also possible to this utility model is carried out some improvement and modification, these improve and modification also falls in this utility model scope of the claims.
Claims (9)
1. an environmental protection sampling aircraft, it is characterised in that including:
Body, is provided with control system and radio receiver in described body；Described radio receiver is connected with described control system；
Motor, is connected with the control system of described body；
Rotor, its rotating shaft is connected with the output shaft of described motor；
Sampling mechanism, is installed on described body；Described sampling mechanism includes: asepwirator pump, air inlet pipe, the gentle capsule of connection pipeline；
Described asepwirator pump is connected with described control system, and its air inlet is connected with one end of described air inlet pipe；Air vent is connected with described one end being connected pipeline, the other end of described connection pipeline and described airbags；
It is provided with switch valve on described connection pipeline；Described switch valve is connected with described control system；Described switch valve has two kinds of duties, and in the first operative state, described air vent connects with described air bag；In a second operative state, described air vent connects with ambient atmosphere；
Remote controller, it is provided with wireless launcher, and described wireless launcher is connected with described radio receiver signal.
Environmental protection the most according to claim 1 sampling aircraft, it is characterised in that being provided with connecting rod on described body, described motor is installed on described connecting rod.
Environmental protection the most according to claim 1 sampling aircraft, it is characterised in that the number of described rotor is multiple, and the circumference along described body is evenly arranged.
Environmental protection the most according to claim 3 sampling aircraft, it is characterised in that the number of described rotor is 6.
Environmental protection the most according to claim 1 sampling aircraft, it is characterised in that also include:
Connecting flexible pipe, its one end is connected with the other end of described air inlet pipe；
First joint, it is arranged at the other end of described connection flexible pipe；
Exhaust tube, its one end is arranged at sample area；
Second joint, is arranged at the other end of described exhaust tube；Described first joint is suitable with described second joint.
Environmental protection the most according to claim 5 sampling aircraft, it is characterised in that being provided with electric magnet on described first joint, described second joint is metal joint.
Environmental protection the most according to claim 1 sampling aircraft, it is characterised in that also include the first photographic head, be installed on the top of described body.
Environmental protection the most according to claim 1 sampling aircraft, it is characterised in that also include that support, described support are arranged at the bottom surface of described body.
Environmental protection the most according to claim 8 sampling aircraft, it is characterised in that also include second camera, be installed on described support.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620309910.2U CN205499370U (en) | 2016-04-14 | 2016-04-14 | Environmental protection sampling aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620309910.2U CN205499370U (en) | 2016-04-14 | 2016-04-14 | Environmental protection sampling aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205499370U true CN205499370U (en) | 2016-08-24 |
Family
ID=56715282
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620309910.2U Withdrawn - After Issue CN205499370U (en) | 2016-04-14 | 2016-04-14 | Environmental protection sampling aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205499370U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105775134A (en) * | 2016-04-14 | 2016-07-20 | 内蒙古包钢钢联股份有限公司 | Environment-friendly sampling air vehicle |
-
2016
- 2016-04-14 CN CN201620309910.2U patent/CN205499370U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105775134A (en) * | 2016-04-14 | 2016-07-20 | 内蒙古包钢钢联股份有限公司 | Environment-friendly sampling air vehicle |
| CN105775134B (en) * | 2016-04-14 | 2018-12-25 | 内蒙古包钢钢联股份有限公司 | A kind of environmental protection sampling aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160824 Effective date of abandoning: 20181225 |
|
| AV01 | Patent right actively abandoned |