CN112455719A - Micro-nano bubble water cleaning system for airplane cleaning - Google Patents
Micro-nano bubble water cleaning system for airplane cleaning Download PDFInfo
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- CN112455719A CN112455719A CN202011124685.2A CN202011124685A CN112455719A CN 112455719 A CN112455719 A CN 112455719A CN 202011124685 A CN202011124685 A CN 202011124685A CN 112455719 A CN112455719 A CN 112455719A
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 162
- 238000004140 cleaning Methods 0.000 title claims abstract description 117
- 239000002101 nanobubble Substances 0.000 title claims abstract description 30
- 238000005406 washing Methods 0.000 claims abstract description 35
- 239000007788 liquid Substances 0.000 claims abstract description 16
- 239000003599 detergent Substances 0.000 claims abstract description 10
- 230000006698 induction Effects 0.000 claims abstract description 9
- 238000002156 mixing Methods 0.000 claims abstract description 9
- 239000012459 cleaning agent Substances 0.000 claims abstract description 7
- 239000010865 sewage Substances 0.000 claims description 14
- 238000004062 sedimentation Methods 0.000 claims description 12
- 238000001914 filtration Methods 0.000 claims description 8
- 238000011084 recovery Methods 0.000 claims description 8
- 239000007921 spray Substances 0.000 claims description 8
- 238000007599 discharging Methods 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 15
- 239000002351 wastewater Substances 0.000 description 8
- 230000006378 damage Effects 0.000 description 5
- 238000004064 recycling Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- 239000002689 soil Substances 0.000 description 4
- 238000009833 condensation Methods 0.000 description 2
- 230000005494 condensation Effects 0.000 description 2
- 239000003981 vehicle Substances 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000003796 beauty Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000013505 freshwater Substances 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 150000002894 organic compounds Chemical class 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/30—Cleaning aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D36/00—Filter circuits or combinations of filters with other separating devices
- B01D36/04—Combinations of filters with settling tanks
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Cleaning By Liquid Or Steam (AREA)
Abstract
The invention relates to the technical field of cleaning equipment, in particular to a micro-nano bubble water cleaning system for cleaning an airplane, which comprises: the device comprises a cleaning platform, a radar induction control device, a cleaning unit, a clear water cleaning unit, a detergent mixing device, a micro-nano bubble water generating device and a central controller; the radar induction control device comprises a starting radar inductor and a stopping radar inductor; the cleaning and washing unit and the clear water cleaning unit are respectively arranged at the upper machine port and the lower machine port of the cleaning platform, and both comprise: a first cavitation water storage tank, a cavitation pump and a high pressure nozzle; the detergent mixing device includes: the cleaning agent storage tank and the liquid dispensing pump are arranged, and the micro-nano bubble water generating devices are arranged in two groups and are symmetrically arranged on two sides of the cleaning platform. This micro-nano bubble water cleaning system improves the cleaning efficiency of aircraft, and water economy resource and cleaning cost, and the control and the management of cleaning process are convenient for to the modular equipment.
Description
Technical Field
The invention relates to the technical field of cleaning equipment, in particular to a micro-nano bubble water cleaning system for cleaning an airplane.
Background
The airplane is affected by the environment in the flying process to cause body pollution, which not only affects the beauty, but also can cause corrosion to the airplane body to cause accidents. Particularly, when an airplane flying in a marine environment continuously operates in a high-humidity and high-salt environment for a long time, pollution caused by accumulation of floating pollutants in the atmosphere due to condensation of water films capable of dissolving electrolytes such as organic salt and the like formed by condensation and magnetic field static electricity and various pollution generated in the operation process of equipment greatly damage the airplane and airborne equipment, seriously affect the service life of the airplane, affect the fighting capacity of the airplane and even lead various accidents of the airplane to happen.
At present, the airplane is cleaned in the form of manual cleaning and airplane washing vehicles at home, the manual cleaning has high labor intensity and long time, the surface of the airplane is easy to damage due to the fact that a common high-pressure cleaning machine is washed by high-pressure water, particularly, the airplane with a special coating is greatly damaged, and the airplane washing vehicles are directly washed by high-pressure continuous flow, so that the airplane washing equipment is poor in dirt removing capability, high in fresh water consumption and high in cleaning cost, and therefore, safe, reliable and quick airplane cleaning equipment is quite needed. In view of this, we propose a micro-nano bubble water cleaning system for aircraft cleaning.
Disclosure of Invention
The invention aims to provide a micro-nano bubble water cleaning system for cleaning an airplane, and aims to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme:
a micro-nano bubble water cleaning system for aircraft cleaning, includes: the device comprises a cleaning platform, a radar induction control device, a cleaning unit, a clear water cleaning unit, a detergent mixing device, a micro-nano bubble water generating device and a central controller;
the radar induction control device includes: the system comprises a starting-up radar sensor and a stopping radar sensor, wherein the starting-up radar sensor and the stopping radar sensor are respectively used for sensing the entrance and exit of an airplane to and from the cleaning platform;
the cleaning and washing unit and the clear water cleaning unit are respectively arranged at the upper machine port and the lower machine port of the cleaning platform, and both comprise: a first cavitation water storage tank, a cavitation pump and a high pressure nozzle;
the first cavitation water storage tank is communicated with a water inlet of the cavitation pump through a pipeline, a plurality of high-pressure spray heads are arranged, and the high-pressure spray heads are communicated with a water outlet of the cavitation pump through a pipeline;
the detergent mixing device includes: the cleaning device comprises a cleaning agent storage tank and a liquid dispensing pump, wherein the cleaning agent storage tank is communicated with a water inlet of the liquid dispensing pump through a pipeline, and a water outlet of the liquid dispensing pump is communicated with a first cavitation water storage tank on the cleaning and washing unit through a pipeline;
micro-nano bubble water generating device is provided with two sets ofly, and symmetrical arrangement is in wash platform's both sides include: the second cavitation water storage tank is communicated with a water inlet of the water cannon pump through a pipeline, and a water inlet of the high-pressure cavitation water cannon is communicated with a water outlet of the water cannon pump through a pipeline;
the starting radar sensor, the stopping radar sensor, the cavitation pump and the water cannon pump are all electrically connected with the central controller and used for controlling starting and stopping of the equipment through PLC programming.
Preferably, the device also comprises a recovery filtering device, wherein the recovery filtering device consists of a circulating pool, a sedimentation pool, a laminated filter, a filtering pump and a sewage pump;
the circulation tank is communicated with the sedimentation tank;
a water inlet of the filter pump is communicated with the first cavitation water storage tank and the second cavitation water storage tank through a pipeline, and a water outlet of the filter pump is communicated with the circulation tank through the laminated filter;
and a water inlet of the sewage pump is communicated with the sedimentation tank through a pipeline.
Preferably, the water inlet of the filter pump with all install the solenoid valve on the pipeline of first cavitation water holding vessel and second cavitation water holding vessel intercommunication, just the solenoid valve with central controller electric connection.
Preferably, still include the level gauge, all install on first cavitation water holding vessel, sanitizer storage tank and the second cavitation water holding vessel the level gauge, just the level gauge with central controller electric connection.
Preferably, the jet orifice of the high-pressure nozzle is vertically arranged upwards and hidden in the cleaning platform.
Preferably, the included angle between the water outlet angle of the high-pressure cavitation water cannon and the horizontal plane is adjusted to be 30-60 degrees.
Preferably, the cleaning platform is also provided with a plurality of drainage grooves which are distributed transversely and longitudinally, and the drainage grooves are used for sewage drainage and pipeline arrangement.
Compared with the prior art, the invention has the beneficial effects that:
1. this a micro-nano bubble water cleaning system for aircraft washing, the aircraft need not to stop at abluent in-process, drives over the in-process completion washing operation of washing platform, and whole cleaning process only needs the minute time of controlling from the beginning to the end, improves the cleaning efficiency greatly, and clear waste water can directly discharge, can not cause the injury to soil.
2. This be used for abluent micro-nano bubble water cleaning system of aircraft, retrieve cleaning wastewater through the recovery filter equipment who sets up and be used for recycling, water economy resource and washing cost.
3. This be used for abluent micro-nano bubble water cleaning system of aircraft, whole cleaning system modularization sets up, is convenient for to the control and the management of each washing link, and installation on the spot with arrange simply, reduction equipment cost.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic block diagram of the overall architecture of the present invention;
FIG. 3 is a block diagram of the cleaning and washing units and the clear water washing unit according to the present invention;
FIG. 4 is a structural schematic block diagram of the micro-nano bubble water generating device in the invention;
FIG. 5 is a schematic block diagram of the construction of the recovery filter apparatus of the present invention.
In the figure: 1. cleaning the platform; 11. a water discharge tank; 2. a radar sensing device; 21. starting up a radar sensor; 22. a shutdown radar sensor; 3. cleaning the unit; 31. a first cavitation water storage tank; 32. a cavitation pump; 33. a high pressure spray head; 4. cleaning the unit with clear water; 5. a detergent mixing device; 51. a detergent storage tank; 52. liquid dispensing pump; 6. a micro-nano bubble water generating device; 61. a second cavitation water storage tank; 62. a water cannon pump; 63. high-pressure cavitation water cannon; 7. a central controller; 8. a recovery filtration device; 81. a circulation tank; 82. a sedimentation tank; 83. a lamination filter; 84. a filter pump; 85. a sewage pump; 9. an electromagnetic valve; 10. a liquid level meter.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1-5, a technical solution provided by the present invention is:
a micro-nano bubble water cleaning system for aircraft cleaning, includes: the system comprises a cleaning platform 1, a radar induction control device 2, a cleaning unit 3, a clear water cleaning unit 4, a detergent mixing device 5, a micro-nano bubble water generation device 6 and a central controller 7;
the radar induction control device 2 includes: the system comprises a starting-up radar sensor 21 and a stopping radar sensor 22, wherein the starting-up radar sensor 21 and the stopping radar sensor 22 are respectively used for sensing the entering and exiting of the airplane to the cleaning platform 1, the starting-up radar sensor 21 is installed at one end of the airplane entering the cleaning platform 1, the stopping radar sensor 22 is installed at one end of the airplane exiting the cleaning platform 1, whether the airplane entering the cleaning platform 1 is a large airplane or a small airplane can be distinguished according to the distance between a front wheel and a rear wheel of the airplane, and the cleaning time and the water spraying amount are set according to the body type of the airplane;
the cleaning and washing unit 3 and the clean water cleaning unit 4 are respectively arranged at the upper machine port and the output machine port of the cleaning platform 1, and the cleaning and washing unit 3 and the clean water cleaning unit 4 are separated by 20m, and the cleaning and washing unit 3 and the clean water cleaning unit 4 respectively comprise: a first cavitation water storage tank 31, a cavitation pump 32, and a high pressure nozzle 33;
the first cavitation water storage tank 31 is communicated with a water inlet of the cavitation pump 32 through a pipeline, a plurality of high-pressure nozzles 33 are arranged, in the embodiment, 18 high-pressure nozzles 33 are arranged, and the high-pressure nozzles 33 are communicated with a water outlet of the cavitation pump 32 through a pipeline;
the detergent mixing device 5 includes: the cleaning agent storage tank 51 is communicated with a water inlet of the liquid dispensing pump 52 through a pipeline, a water outlet of the liquid dispensing pump 52 is communicated with the first cavitation water storage tank 31 on the cleaning and cleaning unit 3 through a pipeline and is used for adding cleaning liquid to the first cavitation water storage tank 31 on the cleaning and cleaning unit 3, the cleaning liquid is a water-based cleaning agent in the embodiment, and the cleaning liquid belongs to organic compounds and can be directly discharged without affecting soil;
micro-nano bubble water generating device 6 is provided with two sets ofly, and the symmetrical arrangement includes in the both sides of cleaning platform 1: the second cavitation water storage tank 61 is communicated with a water inlet of the water cannon pump 62 through a pipeline, and a water inlet of the high-pressure cavitation water cannon 63 is communicated with a water outlet of the water cannon pump 62 through a pipeline;
start radar sensor 21, shut down radar sensor 22, cavitation pump 32, water cannon pump 62 all with central controller 7 electric connection for start-stop through PLC programming control equipment is specific: on the washing platform 1 was sailed into to the aircraft, can drive into through radar induction control device 2 auto-induction aircraft to utilize central controller 7 controlgear to start, also can manually carry out the start-up of equipment, the cleaning process divide into three stage, and the first stage is: 18 high-pressure nozzles 33 of the cleaning and washing unit 3 spray mixed water containing cleaning liquid for washing; the second stage is as follows: the high-pressure cavitation water cannons 63 arranged on the two sides of the cleaning platform 1 are remotely and crossly sprayed with pure clean water for washing; the third stage is as follows: the 18 high pressure nozzles 33 of the clear water cleaning unit 4 spray pure clear water to wash, the airplane does not need to stay in the cleaning process, the cleaning operation is completed in the process of driving over the cleaning platform 1, the whole cleaning process only needs about 3 minutes from the beginning to the end, the cleaning efficiency is greatly improved, and the clean waste water can be directly discharged without causing damage to the soil.
In this embodiment, the recycling filter device 8 is further included, and the recycling filter device 8 is composed of a circulation tank 81, a sedimentation tank 82, a laminated filter 83, a filter pump 84 and a sewage pump 85;
the circulation tank 81 and the sedimentation tank 82 are communicated with each other;
the water inlet of the filter pump 84 is communicated with the first cavitation water storage tank 31 and the second cavitation water storage tank 61 through pipelines, and the water outlet of the filter pump 84 is communicated with the circulating tank 81 through the laminated filter 83;
the water inlet of the sewage pump 85 is communicated with the sedimentation tank 82 through a pipeline, the waste water sprayed in the second stage and the waste water sprayed in the third stage are precipitated through the sedimentation tank 82, clear water obtained after precipitation is filtered by the laminated filter 83 and then is conveyed to the first cavitation water storage tank 31 and the second cavitation water storage tank 61 again through the filter pump 84 for recycling, and sewage obtained after precipitation is discharged through the sewage pump 85, so that water resources and cleaning cost are saved.
Further, all install solenoid valve 9 on the water inlet of filter pump 84 and the pipeline of first cavitation water storage tank 31 and second cavitation water storage tank 61 intercommunication, and solenoid valve 9 and central controller 7 electric connection are convenient for utilize opening and close of solenoid valve 9 control pipeline, make the volume of recovered water in first cavitation water storage tank 31 and the second cavitation water storage tank 61 maintain in suitable scope.
It is worth explaining, still include level gauge 10, all install level gauge 10 on first cavitation water storage tank 31, sanitizer storage tank 51 and the second cavitation water storage tank 61, and level gauge 10 and central controller 7 electric connection, be convenient for utilize the water gauge 10 to monitor the water storage capacity in first cavitation water storage tank 31, sanitizer storage tank 51 and the second cavitation water storage tank 61 to whether need add water to the jar body according to the water storage capacity decision.
In addition, the jet orifice of the high-pressure nozzle 33 is vertically arranged upwards and hidden in the cleaning platform 1, so that the nozzle is prevented from being damaged in the sliding process of the airplane.
Specifically, the included angle between the water outlet angle of the high-pressure cavitation water cannon 63 and the horizontal plane is adjusted to be 30-60 degrees, so that the water outlet angle of the high-pressure cavitation water cannon 63 can be conveniently adjusted, and the high-pressure cavitation water cannon is suitable for airplanes of different body types.
Furthermore, the washing platform 1 is provided with a plurality of drainage channels 11 distributed transversely and longitudinally, and the drainage channels 11 are used for sewage drainage and pipeline arrangement.
The micro-nano bubble water cleaning system for aircraft cleaning of this embodiment is when using, and on the washing platform 1 was sailed into to the aircraft, can be through 2 auto-induction aircraft's of radar induction control device sailing into to utilize 7 controlgear of central controller to start, also can manually carry out the start-up of equipment, the cleaning process divide into three stage, and the first stage is: 18 high-pressure nozzles 33 of the cleaning and washing unit 3 spray mixed water containing cleaning liquid for washing; the second stage is as follows: the high-pressure cavitation water cannons 63 arranged on the two sides of the cleaning platform 1 are remotely and crossly sprayed with pure clean water for washing; the third stage is as follows: the 18 high-pressure nozzles 33 of the clear water cleaning unit 4 spray pure clear water for washing, the airplane does not need to stay in the cleaning process, the cleaning operation is completed in the process of driving through the cleaning platform 1, the whole cleaning process only needs about 3 minutes from the beginning to the end, the cleaning efficiency is greatly improved, and clean waste water can be directly discharged without causing damage to soil;
in addition, the recovery filtering device 8 is used for recovering wastewater, the wastewater sprayed in the second stage and the third stage is precipitated through the sedimentation tank 82, clear water obtained after precipitation is filtered by the laminated filter 83 and then is conveyed to the first cavitation water storage tank 31 and the second cavitation water storage tank 61 again through the filter pump 84 for recycling, and sewage obtained after precipitation is discharged through the sewage discharge pump 85, so that water resources and cleaning cost are saved, and the popularization and the promotion are facilitated.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (7)
1. A micro-nano bubble system for aircraft cleaning, comprising: the device comprises a cleaning platform (1), a radar induction control device (2), a cleaning and cleaning unit (3), a clear water cleaning unit (4), a detergent mixing device (5), a micro-nano bubble water generating device (6) and a central controller (7);
the radar sensing control device (2) comprises: the system comprises a starting-up radar sensor (21) and a stopping radar sensor (22), wherein the starting-up radar sensor (21) and the stopping radar sensor (22) are respectively used for sensing the entrance and exit of an airplane to and from the cleaning platform (1);
the cleaning and washing unit (3) and the clear water cleaning unit (4) are respectively arranged at an upper machine port and a lower machine port of the washing platform (1) and respectively comprise: a first cavitation water storage tank (31), a cavitation pump (32) and a high pressure nozzle (33);
the first cavitation water storage tank (31) is communicated with a water inlet of the cavitation pump (32) through a pipeline, a plurality of high-pressure nozzles (33) are arranged, and the high-pressure nozzles (33) are communicated with a water outlet of the cavitation pump (32) through a pipeline;
the detergent mixing device (5) comprises: the cleaning device comprises a cleaning agent storage tank (51) and a liquid dispensing pump (52), wherein the cleaning agent storage tank (51) is communicated with a water inlet of the liquid dispensing pump (52) through a pipeline, and a water outlet of the liquid dispensing pump (52) is communicated with a first cavitation water storage tank (31) on the cleaning and washing unit (3) through a pipeline;
micro-nano bubble water generating device (6) are provided with two sets ofly, and symmetrical arrangement is in the both sides of cleaning platform (1) include: the device comprises a second cavitation water storage tank (61), a water cannon pump (62) and a high-pressure cavitation water cannon (63), wherein the second cavitation water storage tank (61) is communicated with a water inlet of the water cannon pump (62) through a pipeline, and a water inlet of the high-pressure cavitation water cannon (63) is communicated with a water outlet of the water cannon pump (62) through a pipeline;
the starting radar sensor (21), the stopping radar sensor (22), the cavitation pump (32) and the water cannon pump (62) are electrically connected with the central controller (7) and used for controlling starting and stopping of equipment through PLC programming.
2. The micro-nano bubble system for aircraft washing of claim 1, wherein: the device also comprises a recovery filtering device (8), wherein the recovery filtering device (8) consists of a circulating pool (81), a sedimentation pool (82), a laminated filter (83), a filtering pump (84) and a sewage pump (85);
the circulating tank (81) is communicated with the sedimentation tank (82);
the water inlet of the filter pump (84) is communicated with the first cavitation water storage tank (31) and the second cavitation water storage tank (61) through a pipeline, and the water outlet of the filter pump (84) is communicated with the circulating pool (81) through the laminated filter (83);
the water inlet of the sewage pump (85) is communicated with the sedimentation tank (82) through a pipeline.
3. The micro-nano bubble system for aircraft washing of claim 2, wherein: the water inlet of filter pump (84) with all install solenoid valve (9) on the pipeline of first cavitation water holding vessel (31) and second cavitation water holding vessel (61) intercommunication, just solenoid valve (9) with central controller (7) electric connection.
4. The micro-nano bubble system for aircraft washing of claim 1, wherein: still include level gauge (10), all install on first cavitation water storage tank (31), sanitizer storage tank (51) and second cavitation water storage tank (61) level gauge (10), just level gauge (10) with central controller (7) electric connection.
5. The micro-nano bubble system for aircraft washing of claim 1, wherein: and the jet orifice of the high-pressure spray head (33) is vertically arranged upwards and is hidden in the cleaning platform (1).
6. The micro-nano bubble system for aircraft washing of claim 1, wherein: the included angle between the water outlet angle of the high-pressure cavitation water cannon (63) and the horizontal plane is adjusted to be 30-60 degrees.
7. The micro-nano bubble system for aircraft washing of claim 1, wherein: the cleaning platform (1) is also provided with a plurality of drainage grooves (11) which are transversely and longitudinally distributed, and the drainage grooves (11) are used for discharging sewage and arranging pipelines.
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CN202011124685.2A CN112455719A (en) | 2020-10-20 | 2020-10-20 | Micro-nano bubble water cleaning system for airplane cleaning |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN113857124A (en) * | 2021-09-29 | 2021-12-31 | 安徽鲸洋生物科技有限公司 | Water body cavitation equipment and water body cavitation method |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020002989A1 (en) * | 2000-05-08 | 2002-01-10 | Jones Allen S. | Vehicle wash system including a variable speed single pumping unit |
US20030141257A1 (en) * | 2001-09-14 | 2003-07-31 | Hammond Scot M. | Water recycling system and method |
US20060219269A1 (en) * | 2005-04-04 | 2006-10-05 | United Technologies Corporation | Mobile on-wing engine washing and water reclamation system |
DE102008023261A1 (en) * | 2008-05-13 | 2009-11-19 | Peter Lichtinghagen | Washer system for cleaning vehicles, particularly passenger motor vehicles, aircrafts, buses, rail cars and water crafts, has supporting frame, at which spray device is held for transferring washing medium for cleaning vehicle outer surface |
CN203391742U (en) * | 2013-08-17 | 2014-01-15 | 赖秉洪 | Water-saving non-pollution system for automatically cleaning automobile by using air |
JP2017154615A (en) * | 2016-03-02 | 2017-09-07 | 井上鋼材株式会社 | Vehicle mud cleaning device |
CN206528459U (en) * | 2017-02-24 | 2017-09-29 | 四川建筑职业技术学院 | A kind of construction site exports automatic car washing device |
CN109982932A (en) * | 2016-10-03 | 2019-07-05 | Msg产品公司 | For by aircraft washing and deicing system and method |
CN209617106U (en) * | 2019-03-24 | 2019-11-12 | 漳州市龙文区健达电子科技有限公司 | A kind of self-service car carwash with microbubble function |
CN211281520U (en) * | 2019-12-29 | 2020-08-18 | 济宁新云智控科技有限公司 | Aircraft spray device |
CN214296510U (en) * | 2020-10-20 | 2021-09-28 | 上海航翼高新技术发展研究院有限公司 | Micro-nano bubble water cleaning system for airplane cleaning |
-
2020
- 2020-10-20 CN CN202011124685.2A patent/CN112455719A/en active Pending
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020002989A1 (en) * | 2000-05-08 | 2002-01-10 | Jones Allen S. | Vehicle wash system including a variable speed single pumping unit |
US20030141257A1 (en) * | 2001-09-14 | 2003-07-31 | Hammond Scot M. | Water recycling system and method |
US20060219269A1 (en) * | 2005-04-04 | 2006-10-05 | United Technologies Corporation | Mobile on-wing engine washing and water reclamation system |
DE102008023261A1 (en) * | 2008-05-13 | 2009-11-19 | Peter Lichtinghagen | Washer system for cleaning vehicles, particularly passenger motor vehicles, aircrafts, buses, rail cars and water crafts, has supporting frame, at which spray device is held for transferring washing medium for cleaning vehicle outer surface |
CN203391742U (en) * | 2013-08-17 | 2014-01-15 | 赖秉洪 | Water-saving non-pollution system for automatically cleaning automobile by using air |
JP2017154615A (en) * | 2016-03-02 | 2017-09-07 | 井上鋼材株式会社 | Vehicle mud cleaning device |
CN109982932A (en) * | 2016-10-03 | 2019-07-05 | Msg产品公司 | For by aircraft washing and deicing system and method |
CN206528459U (en) * | 2017-02-24 | 2017-09-29 | 四川建筑职业技术学院 | A kind of construction site exports automatic car washing device |
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