CN108514785A - A kind of automatic air deduster in open air - Google Patents
A kind of automatic air deduster in open air Download PDFInfo
- Publication number
- CN108514785A CN108514785A CN201810420582.7A CN201810420582A CN108514785A CN 108514785 A CN108514785 A CN 108514785A CN 201810420582 A CN201810420582 A CN 201810420582A CN 108514785 A CN108514785 A CN 108514785A
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- Prior art keywords
- cavity
- sliding
- shaft
- fuselage
- drive
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D47/00—Separating dispersed particles from gases, air or vapours by liquid as separating agent
- B01D47/06—Spray cleaning
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D2247/00—Details relating to the separation of dispersed particles from gases, air or vapours by liquid as separating agent
- B01D2247/08—Means for controlling the separation process
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- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Special Spraying Apparatus (AREA)
Abstract
The invention discloses a kind of automatic air dedusters in open air, including fuselage, the first drive cavity for being arranged in the fuselage and the lighting device for being set to the front fuselage, first drive cavity bottom is provided with and communicated with the first sliding cavity of opening upwards, it is rotatably provided with the axle sleeve extended up and down in first drive cavity, the sleeve outer surface is fixedly connected with first gear, perforative second sliding cavity up and down is provided in the axle sleeve, it can slide up and down in second sliding cavity and be provided with sliding bar, the sliding bar extends upward the external fuselage；The device structure of the present invention is simple, and conveniently moving realizes equipment multi-angle regulation using mechanical structure, equipment dedusting range is expanded, improves dust removing effects using high-pressure atomization equipment dedusting, and this equipment uses automation control using process, manpower is saved, device practical performance is improved.
Description
Technical field
Field of environment protection of the present invention, specifically a kind of automatic air deduster in open air.
Background technology
With the development of society, air pollution problems inherent is increasingly prominent, and the major pollutants of air pollution are to swim in sky
Dust in gas always exists a relatively difficult technical problem during air cleaning, is exactly that cleaner can only be single
One direction is sprayed, and inconvenience is adjusted, and overall mass is heavier, and mobile inconvenient, not only efficiency is low but also quality during use
Effect is general, this device efficiently solves the problems, such as this.
Invention content
Technical problem to be solved by the invention is to provide a kind of automatic air dedusters in open air, can solve
State the problems in present technology.
The present invention is achieved through the following technical solutions：A kind of automatic air deduster in open air of the present invention,
Including fuselage, the first drive cavity being arranged in the fuselage and the lighting device for being set to the front fuselage, described
One drive cavity bottom is provided with and communicated with the first sliding cavity of opening upwards, is rotatably provided in first drive cavity up and down
The axle sleeve of extension, the sleeve outer surface are fixedly connected with first gear, are provided in the axle sleeve and perforative second slide up and down
Chamber is moved, can slide up and down in second sliding cavity and be provided with sliding bar, the sliding bar extends upward outside the fuselage
The sliding bar top end in portion, the external fuselage is fixedly installed rotating disc, and the sliding bar extends down into described
First sliding cavity, the sliding bar is interior to be equipped with the third sliding cavity that Open Side Down, and first sliding cavity is symmetrical set out
Mouthful the 4th inside sliding cavity, is slidably provided with the first sliding shoe in the 4th sliding cavity, in first sliding shoe
Equipped with threaded hole up and down, the threaded hole screw-internal thread fit has the threaded rod extended up and down, the threaded rod to prolong upwards
It stretches into the third sliding cavity, the threaded rod extends down into first sliding cavity and end and is fixed at institute
The first motor be connected by power in the first sliding cavity bottom wall is stated, the first rotating shaft extended up and down is equipped on the left of the axle sleeve, it is described
First rotating shaft bottom end is rotationally connected in the first drive cavity lower end wall, and the first rotating shaft top end is set with fixation
The the second motor power connection being placed in the first drive cavity upper end wall, the first rotating shaft outer surface is installed with and institute
The second gear of first gear engagement is stated, the fuselage is symmetrical and front and back is symmetrically arranged with wheel, the wheel of rear side
It is inside symmetrically arranged with the first inside cavity of opening, the second cavity of left and right perforation, institute are provided with below first drive cavity
The wheel carrier for being rotatably provided through second cavity in two the first cavitys is stated, the second transmission is equipped in the wheel carrier
Chamber, is rotatably provided with the second shaft that left and right extends in second drive cavity, second shaft to both sides extend with
The first cavity outer end wall is fixedly connected, and second shaft outer surface is installed with first bevel gear, and described second
Rotation is provided with the front and back third shaft extended in end wall on rear side of drive cavity, and the third shaft stretches into forward described second
In drive cavity, the third shaft front side end in second drive cavity is fixedly connected with to be engaged with the first bevel gear
Second bevel gear, the third shaft, which extends back, stretches into second cavity, the third in second cavity turn
End is hingedly connected with the 4th shaft on rear side of axis, and the 4th shaft extends back and the second cavity rear side end is fixedly installed
Third motor power connection in face, the external fuselage are provided with spraying device, the spraying device include spray tank and
Flabellum.
Preferably technical solution, is equipped with the third cavity of opening upwards in the spray tank, in the third cavity
The flabellum main shaft connect with the 4th motor power being fixed in the third cavity bottom wall, in the third cavity
Equipped with annular atomizer, the atomizer is provided with and communicated with flexible communicating pipe, the spray tank bottom right with described turn
Articulated connection on the right side of Moving plate, the spray tank bottom left are hingedly connected with cylinder, and the cylinder extends downwardly articulated connection institute
State rotating disc.
Preferably technical solution, it is symmetrical in second cavity inner wall and symmetrical above and below to be provided with opening inside
Spring cavity, be slidably provided with the second sliding shoe extended up and down in the spring cavity, at the top of the second sliding shoe with
Elasticity is provided with top pressure spring in the spring cavity outer wall, and the second sliding shoe, which extends internally, is fixedly connected with the wheel carrier.
Preferably technical solution, the fuselage roof end face right side are equipped with liquid storage cylinder, the liquid storage cylinder and the company
Siphunculus phase communications and liaison, pressurized equipment is fixedly installed on the communicating pipe.
Preferably technical solution, the lighting device include being set in the front fuselage face to be fixedly connected with photograph
The front end of bright fixed plate, the illumination fixed plate is fixedly connected with headlamp, can be opened in the case where light is gloomy described
Headlamp makes device continue trouble free service.
The beneficial effects of the invention are as follows：The equipment of the present invention in the initial state, the first motor, the second motor, the
Three motors and the 4th motor are in stationary state, and the pressurized equipment is in halted state, and the sliding bar is located at described
First sliding cavity bottom, the spray tank are horizontal.
When being run with the equipment of the present invention, start the first motor, the first motor rotation drives the screw thread
Bar rotates, and the threaded rod rotation drives first sliding shoe to rise, and first sliding shoe, which rises, pushes the sliding bar
Rise, the sliding bar, which rises, drives the rotating disc to rise, and the rotating disc, which rises, drives the spraying device to rise, and works as institute
It states spraying device and rises to suitable position, stop the first motor and start second motor, second motor rotates band
The dynamic second gear rotation, the second gear rotation drive the first gear rotation, the first gear rotation to drive
The axle sleeve rotation, the axle sleeve rotation drive the sliding bar rotation, the sliding bar rotation to drive the turn disc,
The turn disc drives the spraying device rotation, when the spraying device goes to suitable position, starts the cylinder and pushes away
The spray tank is moved to swing up and down.
When the spraying device is in suitable position, start the pressurized equipment, the pressurized equipment is by the liquid storage
Intracavity liquid is pressed into the communicating pipe, and then the liquid is atomized by the atomizer and is sprayed, and starts the described 4th at this time
Motor, the 4th motor drive the flabellum rotation, the flabellum to blow to the fog after atomization in the air, the fog and sky
Minute dust contact in gas, falls to the ground, to reach air cleaning purpose.
When the equipment of the present invention needs mobile, start the third motor, the motor rotation drives described 4th turn
Shaft rotation is dynamic, and the 4th shaft rotation drives the third shaft, the third shaft rotation that the first bevel gear is driven to turn
Dynamic, the first bevel gear rotation drives the second bevel gear rotation, the second bevel gear rotation to drive described second turn
Shaft rotation is dynamic, and the second shaft rotation drives the vehicle wheel rotation, to realize the movement of equipment.
The device structure of the present invention is simple, and conveniently moving realizes equipment multi-angle regulation using mechanical structure, expands
Equipment dedusting range improves dust removing effects using high-pressure atomization equipment dedusting, and this equipment is controlled using process using automation
System, saves manpower, improves device practical performance.
Description of the drawings
The present invention is described in detail by following specific embodiment and attached drawing for ease of explanation,.
Fig. 1 is a kind of outdoor automatically air deduster overall structure diagram of the present invention；
Fig. 2 is the structural schematic diagram of A in Fig. 1.
Specific implementation mode
As Figure 1-Figure 2, a kind of automatic air deduster in open air of the invention, including fuselage 100, setting are in institute
The lighting device stated the first drive cavity 122 in fuselage 100 and be set to 100 front end of the fuselage, first drive cavity
122 bottoms are provided with and communicated with the first sliding cavity 103 of opening upwards, are rotatably provided in first drive cavity 122
The axle sleeve 110 of lower extension, 110 outer surface of the axle sleeve are fixedly connected with first gear 109, are provided in the axle sleeve 110
Under perforative second sliding cavity 121, can slide up and down in second sliding cavity 121 and be provided with sliding bar 135, the sliding
Bar 135 extends upward outside the fuselage 100,135 top end of the sliding bar fixed setting outside the fuselage 100
There are rotating disc 120, the sliding bar 135 to extend down into first sliding cavity 103, opening is equipped in the sliding bar 135
Downward third sliding cavity 108, first sliding cavity 103 is symmetrical set the 4th inside sliding cavity 140 of opening, described
It is slidably provided with the first sliding shoe 139 in 4th sliding cavity 140, is equipped with up and down in first sliding shoe 139
Threaded hole 126,126 screw-internal thread fit of the threaded hole have the threaded rod 102 extended up and down, the threaded rod 102 to upwardly extend
Enter in the third sliding cavity 108, the threaded rod 102 extends down into first sliding cavity 103 and end and fixation
107 be connected by power of first motor in 103 bottom wall of the first sliding cavity is set, and 110 left side of the axle sleeve is equipped with upper downward
The first rotating shaft 101 stretched, 101 bottom end of the first rotating shaft are rotationally connected in 122 lower end wall of the first drive cavity, institute
136 power of the second motor stated 101 top end of first rotating shaft and be fixedly installed in 122 upper end wall of the first drive cavity connects
It connects, 101 outer surface of the first rotating shaft is installed with the second gear 137 engaged with the first gear 109, the fuselage
100 it is symmetrical and it is front and back be symmetrically arranged with wheel 123, be symmetrically arranged in the wheel 123 of rear side opening it is inside the
One cavity 128, first drive cavity, 122 lower section are provided with the second cavity 106 of left and right perforation, described two first cavitys
It is rotatably provided through the wheel carrier 127 of second cavity 106 in 128, the second drive cavity is equipped in the wheel carrier 127
130, be rotatably provided with the second shaft 125 that left and right extends in second drive cavity 130, second shaft 125 to
Both sides extend to be fixedly connected with 128 outer end wall of the first cavity, and 125 outer surface of the second shaft is installed with first
Bevel gear 129, the interior rotation of second drive cavity, 130 rear side end wall are provided with the front and back third shaft 134 extended, the third
Shaft 134 stretches into forward in second drive cavity 130, before the third shaft 134 in second drive cavity 130
Side end is fixedly connected with the second bevel gear 131 engaged with the first bevel gear 129, and the third shaft 134 is prolonged backward
Second cavity 106 is stretched into, the 134 rear side end of the third shaft in second cavity 106 is hingedly connected with
Four shafts 133, the 4th shaft 133 extend back and the third electricity in fixed setting 106 back end surface of the second cavity
132 be connected by power of machine is provided with spraying device outside the fuselage 100, and the spraying device includes spray tank 116 and flabellum
117。
Valuably, the third cavity 114 of opening upwards, the institute in the third cavity 114 are equipped in the spray tank 116
118 be connected by power of the 4th motor stated 117 main shaft of flabellum and be fixed in 114 bottom wall of third cavity, the third
Annular atomizer 115 is equipped in cavity 114, the atomizer 115 is provided with and communicated with flexible communicating pipe 113, the spraying
116 bottom right of case is articulated and connected with 120 right side of the rotating disc, and 116 bottom left of the spray tank is hingedly connected with cylinder
119, the cylinder 119 extends downwardly the articulated connection rotating disc 120, is convenient for equipment adjustable spraying angle, and it is suitable to improve equipment
The property used.
Valuably, symmetrical in 106 inner wall of the second cavity and symmetrical above and below be provided with the inside spring cavity of being open
105, the second sliding shoe 138 extended up and down is slidably provided in the spring cavity 105, the second sliding shoe 138 pushes up
Portion is provided with top pressure spring 104 with elasticity in 105 outer wall of the spring cavity, and the second sliding shoe 138 extends internally fixed connect
The wheel carrier 127 is connect, convenient for reducing the vibrations in vehicle traveling, improves vehicle comfort.
Valuably, liquid storage cylinder 111, the liquid storage cylinder 111 and the communicating pipe are equipped on the right side of 100 top end surface of the fuselage
113 phase communications and liaison, are fixedly installed pressurized equipment 112 on the communicating pipe 113, generate vaporization water mist convenient for equipment, improve equipment
Dust removal performance.
Valuably, the lighting device includes being set in 100 front end face of the fuselage to be fixedly connected with illumination fixed plate
200, the front end of the illumination fixed plate 200 is fixedly connected with headlamp 201, can be opened in the case where light is gloomy described
Headlamp 200 makes device continue trouble free service.
The present invention equipment in the initial state, the first motor 107, the second motor 136, third motor 132 and
4th motor 118 is in stationary state, and the pressurized equipment 112 is in halted state, and the sliding bar 135 is located at described the
One sliding cavity, 103 bottom, the spray tank 116 are horizontal.
When being run with the equipment of the present invention, start the first motor 107, the rotation of the first motor 107 drives institute
The rotation of threaded rod 102 is stated, the threaded rod rotation drives first sliding shoe 139 to rise, and first sliding shoe 139 rises
The sliding bar 135 is pushed to rise, the sliding bar 135, which rises, drives the rotating disc 120 to rise, on the rotating disc 120
It rises and the spraying device is driven to rise, when the spraying device rises to suitable position, stop the first motor 107 and start institute
The second motor 136 is stated, the rotation of the second motor 136 drives the second gear 137 to rotate, and the second gear 137 rotates
The first gear 109 is driven to rotate, the rotation of the first gear 109 drives the axle sleeve 110 to rotate, 110 turns of the axle sleeve
Dynamic that the sliding bar 135 is driven to rotate, the rotation of the sliding bar 135 drives the rotating disc 120 to rotate, the rotating disc 120
Rotation drives spraying device rotation, when the spraying device goes to suitable position, starts the cylinder 119 and pushes the spray
Fog chamber 116 is swung up and down.
When the spraying device is in suitable position, start the pressurized equipment 112, the pressurized equipment 112 is by institute
It states liquid in liquid storage cylinder 111 and is pressed into the communicating pipe 113, then the liquid is atomized by the atomizer 115 and is sprayed, this
4th motor 118 described in Shi Qidong, the 4th motor 118 drive the flabellum 117 to rotate, after the flabellum 117 will be atomized
Fog blow in the air, the fog is contacted with the minute dust in air, is fallen to the ground, to reach air cleaning purpose.
When the equipment of the present invention needs mobile, start the third motor 132, the motor 132 rotates described in drive
4th shaft 133 rotates, and the 4th shaft 133 rotation drives the third shaft 134, the third shaft 134 to rotate band
The dynamic first bevel gear 129 rotates, and the rotation of the first bevel gear 129 drives the second bevel gear 131 to rotate, and described the
The rotation of two bevel gears 131 drives second shaft 125 to rotate, and the rotation of the second shaft 125 drives 123 turns of the wheel
It is dynamic, to realize the movement of equipment.
The beneficial effects of the invention are as follows：The equipment of the present invention in the initial state, the first motor, the second motor, the
Three motors and the 4th motor are in stationary state, and the pressurized equipment is in halted state, and the sliding bar is located at described
First sliding cavity bottom, the spray tank are horizontal.
When being run with the equipment of the present invention, start the first motor, the first motor rotation drives the screw thread
Bar rotates, and the threaded rod rotation drives first sliding shoe to rise, and first sliding shoe, which rises, pushes the sliding bar
Rise, the sliding bar, which rises, drives the rotating disc to rise, and the rotating disc, which rises, drives the spraying device to rise, and works as institute
It states spraying device and rises to suitable position, stop the first motor and start second motor, second motor rotates band
The dynamic second gear rotation, the second gear rotation drive the first gear rotation, the first gear rotation to drive
The axle sleeve rotation, the axle sleeve rotation drive the sliding bar rotation, the sliding bar rotation to drive the turn disc,
The turn disc drives the spraying device rotation, when the spraying device goes to suitable position, starts the cylinder and pushes away
The spray tank is moved to swing up and down.
When the spraying device is in suitable position, start the pressurized equipment, the pressurized equipment is by the liquid storage
Intracavity liquid is pressed into the communicating pipe, and then the liquid is atomized by the atomizer and is sprayed, and starts the described 4th at this time
Motor, the 4th motor drive the flabellum rotation, the flabellum to blow to the fog after atomization in the air, the fog and sky
Minute dust contact in gas, falls to the ground, to reach air cleaning purpose.
When the equipment of the present invention needs mobile, start the third motor, the motor rotation drives described 4th turn
Shaft rotation is dynamic, and the 4th shaft rotation drives the third shaft, the third shaft rotation that the first bevel gear is driven to turn
Dynamic, the first bevel gear rotation drives the second bevel gear rotation, the second bevel gear rotation to drive described second turn
Shaft rotation is dynamic, and the second shaft rotation drives the vehicle wheel rotation, to realize the movement of equipment.
The device structure of the present invention is simple, and conveniently moving realizes equipment multi-angle regulation using mechanical structure, expands
Equipment dedusting range improves dust removing effects using high-pressure atomization equipment dedusting, and this equipment is controlled using process using automation
System, saves manpower, improves device practical performance.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention
Protection domain should be determined by the scope of protection defined in the claims.
Claims (5)
1. the present invention a kind of automatic air deduster in open air, including fuselage, be arranged in the fuselage first be driven
Chamber and the lighting device for being set to the front fuselage, the first drive cavity bottom are provided with and communicated with the first of opening upwards
Sliding cavity is rotatably provided with the axle sleeve extended up and down in first drive cavity, and the sleeve outer surface is fixedly connected with
First gear is provided with perforative second sliding cavity up and down in the axle sleeve, can slide up and down and set in second sliding cavity
It is equipped with sliding bar, the sliding bar extends upward the external fuselage, the sliding bar top end of the external fuselage
It is fixedly installed rotating disc, the sliding bar extends down into first sliding cavity, and the sliding bar is interior equipped with Open Side Down
Third sliding cavity, first sliding cavity is symmetrical set the 4th inside sliding cavity of opening, in the 4th sliding cavity
It is slidable to be provided with the first sliding shoe, it is equipped with threaded hole up and down in first sliding shoe, spiral shell in the threaded hole
Line is combined with the threaded rod extended up and down, and the threaded rod extends upwardly into the third sliding cavity, and the threaded rod is downward
The first motor power for extending into first sliding cavity and end and being fixed in the first sliding cavity bottom wall connects
It connects, the first rotating shaft extended up and down is equipped on the left of the axle sleeve, the first rotating shaft bottom end is rotationally connected with described first
In drive cavity lower end wall, the first rotating shaft top end and the second electricity being fixedly installed in the first drive cavity upper end wall
Mechanomotive force connects, and the first rotating shaft outer surface is installed with the second gear engaged with the first gear, the fuselage
It is symmetrical and it is front and back be symmetrically arranged with wheel, the first inside cavity of opening, institute are symmetrically arranged in the wheel of rear side
The second cavity for being provided with left and right perforation below the first drive cavity is stated, is rotatably provided through in described two first cavitys
The wheel carrier of second cavity, the wheel carrier is interior to be equipped with the second drive cavity, and a left side is rotatably provided in second drive cavity
Second shaft of right extension, second shaft extends to both sides to be fixedly connected with the first cavity outer end wall, and described the
Two shaft outer surfaces are installed with first bevel gear, and interior rotate of end wall is provided with front and back extension on rear side of second drive cavity
Third shaft, the third shaft stretch into forward in second drive cavity, the third in second drive cavity
Shaft front side end is fixedly connected with the second bevel gear engaged with the first bevel gear, and the third shaft, which extends back, stretches
Entering second cavity, end is hingedly connected with the 4th shaft on rear side of the third shaft in second cavity, and described the
Four shafts extend back to be connect with the third motor power being fixedly installed in the second cavity back end surface, the external fuselage
It is provided with spraying device, the spraying device includes spray tank and flabellum.
2. a kind of automatic air deduster in open air according to claim 1, it is characterised in that：It is set in the spray tank
There is the third cavity of opening upwards, the flabellum main shaft in the third cavity and is fixed at the third cavity bottom wall
Interior the 4th motor power connection, the third cavity is interior to be equipped with annular atomizer, and the atomizer, which is provided with and communicated with, scratches
Property communicating pipe, be articulated and connected on the right side of the spray tank bottom right and the rotating disc, the spray tank bottom left hingedly connects
It is connected to cylinder, the cylinder extends downwardly the articulated connection rotating disc.
3. a kind of automatic air deduster in open air according to claim 1, it is characterised in that：In second cavity
In wall it is symmetrical and it is symmetrical above and below be provided with the inside spring cavity of being open, be slidably provided in the spring cavity downward
The second sliding shoe stretched, is provided with top pressure spring at the top of the second sliding shoe with elasticity in the spring cavity outer wall, and described the
Two sliding shoes, which extend internally, is fixedly connected with the wheel carrier.
4. a kind of automatic air deduster in open air according to claim 1, it is characterised in that：The fuselage roof end
Right side of face is equipped with liquid storage cylinder, the liquid storage cylinder and the communicating pipe phase communications and liaison, and pressurized equipment is fixedly installed on the communicating pipe.
5. a kind of automatic air deduster in open air according to claim 1, it is characterised in that：The lighting device packet
It includes to be set in the front fuselage face and is fixedly connected with illumination fixed plate, the front end of the illumination fixed plate is fixedly connected with photograph
Bright lamp, the headlamp can be opened in the case where light is gloomy makes device continue trouble free service.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810420582.7A CN108514785A (en) | 2018-05-04 | 2018-05-04 | A kind of automatic air deduster in open air |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810420582.7A CN108514785A (en) | 2018-05-04 | 2018-05-04 | A kind of automatic air deduster in open air |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108514785A true CN108514785A (en) | 2018-09-11 |
Family
ID=63430441
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810420582.7A Withdrawn CN108514785A (en) | 2018-05-04 | 2018-05-04 | A kind of automatic air deduster in open air |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108514785A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112460707A (en) * | 2020-11-30 | 2021-03-09 | 东南大学扬州研究院 | Dustless workshop temperature and humidity control system based on intelligent control of Internet of things |
-
2018
- 2018-05-04 CN CN201810420582.7A patent/CN108514785A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112460707A (en) * | 2020-11-30 | 2021-03-09 | 东南大学扬州研究院 | Dustless workshop temperature and humidity control system based on intelligent control of Internet of things |
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| PB01 | Publication | ||
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| WW01 | Invention patent application withdrawn after publication | ||
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Application publication date: 20180911 |