CN205098479U - Aircraft sprays paint - Google Patents
Aircraft sprays paint Download PDFInfo
- Publication number
- CN205098479U CN205098479U CN201520907206.2U CN201520907206U CN205098479U CN 205098479 U CN205098479 U CN 205098479U CN 201520907206 U CN201520907206 U CN 201520907206U CN 205098479 U CN205098479 U CN 205098479U
- Authority
- CN
- China
- Prior art keywords
- paint
- aircraft
- cavity
- air
- pipeline
- 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
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Abstract
The utility model provides an aircraft sprays paint, including the aircraft, install the camera on the aircraft, be equipped with power and control module in the aircraft, one end at the bottle that sprays paint communicates in proper order and has spray tube and nozzle, be equipped with air cavity and paint cavity in the bottle that sprays paint, be equipped with air hose and fluid hose in the spray tube, the one end intercommunication of air hose and fluid hose is on the nozzle, still be equipped with first electromagnetism stop valve and second electromagnetism stop valve in the air cavity, first electromagnetism stop valve is installed on air conduit, the air cavity is linked together through pipeline and paint cavity, second electromagnetism stop valve intercommunication is on this pipeline, be equipped with the piston at the paint intracavity, first electromagnetism stop valve and second electromagnetism stop valve pass through the wire and are connected with control module, the utility model discloses spraying paint when marking to erectting aloft pipeline, need not the manual work and set up the scaffold and just can carry out the sign to the pipeline that erects aloft.
Description
Technical field
The utility model relates to a kind of aircraft, and feature relates to one and to spray paint aircraft.
Background technology
In the daily production in chemical plant, usually need to carry out mopping sign to pipeline, so that operating personal tracking wire, but some pipelines are but be erected at high-altitude, when carrying out spraying operation for the high-level pipeline of this kind of erection, be generally adopt manually to set up scaffold and spray, this spraying method not only cost of labor is high, and people easily drops from high-altitude and has an accident, so this problem must solve.
Summary of the invention
The technical problems to be solved in the utility model is to provide one and sprays paint aircraft, the high-level pipeline of erection is sprayed paint indicate time, just can identify setting up high-level pipeline without the need to manually setting up scaffold.
In order to solve this technical matters, the technical solution of the utility model is: one is sprayed paint aircraft, comprise aircraft, on board the aircraft camera is installed, power supply and control module is provided with in aircraft, in the below of aircraft, the bottle that sprays paint is installed, jet pipe and nozzle is communicated with successively in the one end of the bottle that sprays paint, air cavity and paint cavity is provided with spraying paint in bottle, air pipe and fluid hose is provided with in jet pipe, air cavity is connected with air pipe, paint cavity is connected with fluid hose, air pipe is communicated with on nozzle with one end of fluid hose, the first electromagnet cut off valve and the second electromagnet cut off valve is also provided with in air cavity, first electromagnet cut off valve is arranged on air duct, air cavity is connected with paint cavity by pipeline, second electromagnet cut off valve is communicated with on this pipeline, piston is provided with in paint chamber, first electromagnet cut off valve is connected with control module by wire with the second electromagnet cut off valve.
Further, one end of described fluid hose extends in paint chamber, and its end is positioned at the bottom in paint chamber.
The technique effect after this structure is adopted to be: before aircraft is flown to corresponding pipeline, pass through control module, open the first electromagnet cut off valve and the second electromagnet cut off valve, paint is sprayed in cavity, the effect of paint ejection can be observed by camera, not only do not need manually to scaffold erecting and pipeline sprayed, and simple to operate, safe ready.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is described further:
Fig. 1 is perspective view of the present utility model,
Fig. 2 is generalized section of the present utility model.
Detailed description of the invention
As shown in Fig. 1 to 2: a kind of based on aircraft 1 high-altitude sign paint spray equipment, comprise aircraft 1, aircraft 1 is provided with camera 14, power supply 10 and control module 9 is provided with in aircraft 1, in the below of aircraft 1, the bottle 3 that sprays paint is installed, the bottle 3 that sprays paint can be placed on the alighting gear of aircraft 1, jet pipe 7 and nozzle 8 is communicated with successively in the one end of the bottle 3 that sprays paint, air cavity 3 and paint cavity 4 is provided with spraying paint in bottle 3, air pipe 71 and fluid hose 72 is had in jet pipe 7, air cavity 3 is connected with air pipe 71, paint cavity 4 is connected with fluid hose 72, air pipe 71 is connected with nozzle 8 with fluid hose 72, the first electromagnet cut off valve 5 and the second electromagnet cut off valve 6 is also provided with in air cavity 3, first electromagnet cut off valve 5 is arranged on air pipe 71, air cavity 3 is connected with paint cavity 4 by pipeline 12, second electromagnet cut off valve 6 is communicated with on this pipeline 12, piston 11 is provided with in paint cavity 4, first electromagnet cut off valve 5 is connected with control module 9 by wire 13 with the second electromagnet cut off valve 6.
Further, one end of described fluid hose 72 extends in paint cavity 4, and its end is positioned at the bottom of paint cavity 4.
In paint cavity 4, be filled with paint, in air cavity 3, be filled with the pressurized air of 0.3 MPa,
Control module 9 is connected with power supply 10, the remote controller of wireless aircraft 1 is installed the manipulation button that may be used for start and stop first electromagnet cut off valve 5 and the second electromagnet cut off valve 6, when aircraft 1 flies near the chemical pipeline needing to spray paint, press manipulation button, control module 9 controls the first electromagnet cut off valve 5 and the second electromagnet cut off valve 6 is opened, and the pressurized air in air cavity 3 applies pressure to piston 11, promote piston 11 paint is extruded from nozzle 8, the paint extruded is dispelled atomization in the exit of nozzle 8 by the air in air chamber, the paint mist of atomization just can marked chemical pipeline.
Claims (2)
1. the aircraft that sprays paint, comprise aircraft (1), aircraft (1) is provided with camera (14), power supply (10) and control module (9) is provided with in aircraft (1), it is characterized in that, in the below of aircraft (1), the bottle that sprays paint (3) is installed, jet pipe (7) and nozzle (8) is communicated with successively in one end of the bottle that sprays paint (3), air cavity (3) and paint cavity (4) is provided with in the bottle that sprays paint (3), air pipe (71) and fluid hose (72) is provided with in jet pipe (7), air cavity (3) is connected with air pipe (71), paint cavity (4) is connected with fluid hose (72), air pipe (71) is communicated with on nozzle (8) with one end of fluid hose (72), the first electromagnet cut off valve (5) and the second electromagnet cut off valve (6) is also provided with in air cavity (3), first electromagnet cut off valve (5) is arranged on air pipe (71), air cavity (3) is connected with paint cavity (4) by pipeline (12), second electromagnet cut off valve (6) is communicated with on this pipeline (12), piston (11) is provided with in paint chamber, first electromagnet cut off valve (5) is connected with control module (9) by wire (13) with the second electromagnet cut off valve (6).
2. one according to claim 1 is sprayed paint aircraft, it is characterized in that: one end of described fluid hose (72) extends in paint cavity (4), and its end is positioned at the bottom of paint cavity (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520907206.2U CN205098479U (en) | 2015-11-16 | 2015-11-16 | Aircraft sprays paint |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520907206.2U CN205098479U (en) | 2015-11-16 | 2015-11-16 | Aircraft sprays paint |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205098479U true CN205098479U (en) | 2016-03-23 |
Family
ID=55514280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520907206.2U Expired - Fee Related CN205098479U (en) | 2015-11-16 | 2015-11-16 | Aircraft sprays paint |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205098479U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111670143A (en) * | 2018-02-15 | 2020-09-15 | 瓦格纳喷涂技术有限公司 | Aerial fluid spraying system |
| CN115999804A (en) * | 2022-12-20 | 2023-04-25 | 广东电网有限责任公司江门供电局 | Unmanned aerial vehicle sprays paint |
-
2015
- 2015-11-16 CN CN201520907206.2U patent/CN205098479U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111670143A (en) * | 2018-02-15 | 2020-09-15 | 瓦格纳喷涂技术有限公司 | Aerial fluid spraying system |
| CN111670143B (en) * | 2018-02-15 | 2024-02-02 | 瓦格纳喷涂技术有限公司 | Aerial fluid spray system |
| CN115999804A (en) * | 2022-12-20 | 2023-04-25 | 广东电网有限责任公司江门供电局 | Unmanned aerial vehicle sprays paint |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160323 Termination date: 20161116 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |