CN214296510U - 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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- CN214296510U CN214296510U CN202022337876.9U CN202022337876U CN214296510U CN 214296510 U CN214296510 U CN 214296510U CN 202022337876 U CN202022337876 U CN 202022337876U CN 214296510 U CN214296510 U CN 214296510U
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Abstract
The utility model relates to a cleaning equipment technical field specifically is a be used for abluent micro-nano bubble water cleaning system of aircraft, include: 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 utility model relates to a cleaning equipment technical field specifically is a be used for abluent micro-nano bubble water cleaning system of aircraft.
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.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a be used for abluent micro-nano bubble water cleaning system of aircraft to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a 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 beneficial effects of the utility model are 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 structure of the present invention;
FIG. 3 is a block diagram of the cleaning unit and the clear water cleaning unit of the present invention;
FIG. 4 is a structural schematic block diagram of the micro-nano bubble water generating device of the present invention;
fig. 5 is a schematic block diagram of the structure of the recycling 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 described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to 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", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, 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 limited otherwise.
Referring to fig. 1-5, the present invention provides a technical solution:
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 should be understood by those skilled in the art that the present invention is not limited by the above embodiments, and the description in the above embodiments and the description is only preferred examples of the present invention, and is not intended to limit the present invention, and that the present invention can have various changes and modifications without departing from the spirit and scope of the present invention, and these changes and modifications all fall into the scope of the claimed invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (7)
1. The utility model provides a micro-nano bubble water cleaning system for aircraft washing which characterized in that includes: 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 water cleaning system for aircraft cleaning according to 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 water cleaning system for aircraft cleaning according to 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 water cleaning system for aircraft cleaning according to 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 water cleaning system for aircraft cleaning according to 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 water cleaning system for aircraft cleaning according to 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 water cleaning system for aircraft cleaning according to 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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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022337876.9U CN214296510U (en) | 2020-10-20 | 2020-10-20 | Micro-nano bubble water cleaning system for airplane cleaning |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022337876.9U CN214296510U (en) | 2020-10-20 | 2020-10-20 | Micro-nano bubble water cleaning system for airplane cleaning |
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| CN214296510U true CN214296510U (en) | 2021-09-28 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455719A (en) * | 2020-10-20 | 2021-03-09 | 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 |
| CN114850122A (en) * | 2022-03-21 | 2022-08-05 | 任相广 | Non-contact flexible cleaning system for airplane |
-
2020
- 2020-10-20 CN CN202022337876.9U patent/CN214296510U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455719A (en) * | 2020-10-20 | 2021-03-09 | 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 |
| CN114850122A (en) * | 2022-03-21 | 2022-08-05 | 任相广 | Non-contact flexible cleaning system for airplane |
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