Aviation cleaning device
By designing an aviation cleaning device with detachable nozzles and inlets, the problem of existing technologies being unable to adapt to cleaning in different spatial locations has been solved, achieving flexible cleaning effects and high-quality cleaning.
Patent Information
- Application Number
- CN202520041546.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-08
- Publication Date
- 2026-01-16
- Estimated Expiration
- 2035-01-08
AI Technical Summary
Existing aviation cleaning equipment is difficult to adapt to cleaning operations in different spatial locations, especially the challenge of cleaning in confined spaces.
An aviation cleaning device was designed, comprising a cleaning tank, a nozzle, a spraying module, and an adsorption module. Through detachable nozzles and inlets, it can spray cleaning fluid with different flow rates and spray diameters to meet the cleaning needs of different space ranges, and is equipped with an adsorption module to adsorb grease and impurities.
It enables comprehensive cleaning of aviation equipment, improves cleaning quality and flexibility, adapts to cleaning needs in different spatial locations, and ensures cleaning effectiveness.
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Figure CN223801059U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to cleaning equipment technical field, concretely relates to an aviation cleaning device. BACKGROUND
[0002] The aviation aircraft maintenance refers to the maintenance and repair of aircraft and technical equipment thereon, ensures the safety of the aircraft, and the regular maintenance of the aviation aircraft is the prerequisite and necessary condition for ensuring the safe flight of the aircraft and is also an important component of the aviation industry.
[0003] The cleaning equipment disclosed by the document with publication number CN111056039A is provided with a cleaning gun fixedly installed at one end of the sound wave pipe away from the merging manifold, a nozzle fixedly installed at the top of the cleaning gun, a cleaning brush fixedly installed at the top of the cleaning gun and located around the nozzle, and a switch fixedly installed on the surface of the cleaning gun.
[0004] However, due to the limitation of the nozzle structure, the flow rate and the spraying diameter of the cleaning equipment are relatively fixed, and the flexibility is poor, so it can only adapt to cleaning operations in a certain large fixed space position, and it is difficult to perform cleaning operations in a narrow space position. UTILITY MODEL CONTENTS
[0005] The utility model aims at overcoming the above technical deficiencies, and provides an aviation cleaning device to solve the technical problem that the aviation cleaning device in the prior art is difficult to perform cleaning operations in different space positions.
[0006] To achieve the above technical purposes, the utility model adopts the following technical scheme:
[0007] In a first aspect, the utility model provides an aviation cleaning device, which comprises:
[0008] A cleaning box is provided with a cleaning liquid cavity, a first inlet port and a second inlet port, and the first inlet port and the second inlet port are communicated with the cleaning liquid cavity;
[0009] A gun head is detachably connected to the cleaning box and used for connecting the first inlet port or the second inlet port;
[0010] A spraying module comprises first and second nozzles with different calibers, and the first and second nozzles are respectively located on one side of the first and second inlet ports and are detachably connected to the gun head; and
[0011] An adsorption module is installed in the cleaning box and used for adsorbing grease and impurities.
[0012] In some embodiments, the cleaning tank is provided with an inner tank on the inner side of the cleaning tank, the inner tank is fixed on both sides of the cleaning tank by a fixing frame, and the cleaning liquid cavity is arranged in the inner tank.
[0013] In some embodiments, the cleaning tank is further provided with an outlet tank fixedly connected to the cleaning tank, the outlet tank is connected to the inner tank through a connecting pipe, and the first inlet and the second inlet communicate with the outlet tank.
[0014] In some embodiments, the cleaning tank is further provided with a filling port communicating with the cleaning tank, and the filling port is used for filling cleaning liquid into the cleaning liquid cavity.
[0015] In some embodiments, the side of the cleaning tank is fixed with a plug-in plate provided with a plug-in hole, and the gun head is inserted into the plug-in plate through the plug-in hole.
[0016] In some embodiments, the aviation cleaning device further comprises a storage frame fixed to the cleaning tank, and the storage frame is used for storing cleaning tools.
[0017] In some embodiments, the suction module comprises a machine box fixed to the inner side of the cleaning tank and a suction pipe connected to the machine box, and the suction pipe is used for sucking grease and impurities through the driving of the machine box.
[0018] In some embodiments, the aviation cleaning device further comprises a cleaning module fixed to the cleaning tank and connected to the machine box, and the cleaning module is used for cleaning the grease and impurities sucked by the suction pipe.
[0019] In some embodiments, the cleaning module comprises a cleaning tank fixed to the cleaning tank, an adsorption layer arranged in the cleaning tank, and a connecting pipe connected to the machine box and the adsorption layer, and the connecting pipe is used for passing the grease and impurities from the machine box into the adsorption layer.
[0020] In some embodiments, the cleaning tank is provided with a dismounting port provided with a cover, and the dismounting port is used for dismounting the adsorption layer.
[0021] Compared with the prior art, the aviation cleaning device provided by the utility model has the cleaning tank, the gun head, the spraying module and the adsorption module, the cleaning tank is provided with the cleaning liquid cavity, the first inlet and the second inlet, the gun head is detachably connected to the cleaning tank, the spraying module is provided with the first nozzle and the second nozzle with different calibers, when cleaning the aviation equipment, the gun head is detached from the cleaning tank and connected to the first inlet and the second inlet, then the first nozzle or the second nozzle is detached and connected to the gun head according to the requirement, the cleaning liquid can be sprayed through the first nozzle or the second nozzle to clean the aviation equipment, the adsorption module is arranged on the cleaning tank and can adsorb oil and impurities to assist the cleaning of the aviation equipment and ensure the cleaning quality of the aviation equipment, when cleaning, the first nozzle or the second nozzle can be arranged to spray, so that the spraying of the liquid with different flow rates and spraying diameters is realized, thereby adapting to the cleaning of the aviation equipment in different space ranges. BRIEF DESCRIPTION OF DRAWINGS
[0022] Figure 1 is the structure schematic view of the aviation cleaning device provided by the utility model embodiment;
[0023] Figure 2 is the front view of the aviation cleaning device provided by the utility model embodiment;
[0024] Figure 3 is the side view of the aviation cleaning device provided by the utility model embodiment.
[0025] Reference signs in the drawings:
[0026] 10 - cleaning tank 11 - cleaning liquid cavity 12 - first inlet
[0027] 13 - second inlet 14 - inner tank 15 - liquid outlet tank
[0028] 16 - filling port 17 - supply plugboard 20 - gun head
[0029] 30 - spraying module 31 - first nozzle 32 - first nozzle
[0030] 40 - adsorption module 41 - machine case 42 - suction pipe
[0031] 50 - storage frame 51 - clamping groove plate 52 - hook
[0032] 60 - cleaning module 61 - cleaning tank 62 - adsorption layer
[0033] 141 - fixing frame 142 - connecting pipe 611 - detaching port. DETAILED DESCRIPTION
[0034] In order to make the purpose, technical scheme and advantages of the utility model more clearly, the utility model will be further described in detail below in combination with the drawings and examples.
[0035] In order to solve the technical problem that the aviation cleaning device in the prior art is difficult to perform cleaning operation at different spatial positions, the utility model provides an aviation cleaning device, which can replace spray heads with different diameters to perform cleaning operation according to the spatial range of operation, thereby improving the application range of the aviation cleaning device.
[0036] It should be noted that the aviation cleaning device is used for but not limited to aircrafts and the like, in order to facilitate the description, in the utility model, only the aviation cleaning device applied to the aircraft is taken as an example to be described, and the principle of the aviation cleaning device applied to other types of equipment is substantially the same as that applied to the aircraft, which will not be described here.
[0037] The aviation cleaning device provided by the utility model comprises a cleaning box 10, a gun head 20, a spraying module 30 and a suction module 40. Figures 1-2 As shown in the figure, the aviation cleaning device comprises a cleaning box 10, a gun head 20, a spraying module 30 and a suction module 40, the cleaning box 10 is provided with a cleaning liquid cavity 11, a first inlet 12 and a second inlet 13, the first inlet 12 and the second inlet 13 are communicated with the cleaning liquid cavity 11, the gun head 20 is detachably connected to the cleaning box 10 and is used for connecting the first inlet 12 or the second inlet 13, the spraying module 30 comprises first spray heads 31 and second spray heads with different diameters, the first spray heads 31 and the second spray heads are respectively located at one side of the first inlet 12 and the second inlet 13 and are used for spraying spraying liquid with different diameters and flow rates through the connected gun head 20, and the suction module 40 is installed on the cleaning box 10 and is used for adsorbing grease and impurities.
[0038] Specifically, the aviation cleaning device is provided with a cleaning box 10, a gun head 20, a spraying module 30 and an adsorption module 40. The cleaning box 10 is provided with a cleaning liquid cavity 11, a first inlet 12 and a second inlet 13. The gun head 20 is detachably connected to the cleaning box 10. The spraying module 30 is provided with first and second nozzles with different diameters. When cleaning the aviation equipment, the gun head 20 is detached from the cleaning box 10 and connected to the first and second inlets 12 and 13. Then, according to the requirement, the first or second nozzle is detached and connected to the gun head 20. The cleaning liquid can be sprayed through the first or second nozzle to clean the aviation equipment. The adsorption module 40 is installed on the cleaning box 10 to adsorb oil and impurities, thereby assisting the cleaning of the aviation equipment and ensuring the cleaning quality of the aviation equipment. When cleaning, the first or second nozzle can be used for spraying, thereby realizing the spraying of the liquid with different flow rates and spraying diameters and adapting to the cleaning of different space ranges of the aviation equipment.
[0039] In one embodiment, as shown in Figure 2 The cleaning box 10 is provided with an inner box 14 on the inner side. The two sides of the inner box 14 are fixed to the cleaning box 10 through a fixing frame 141. The cleaning liquid cavity 11 is arranged in the inner box 14. Specifically, the inner box 14 is separately fixed in the cleaning box 10 to contain the cleaning liquid to be cleaned, thereby facilitating the cleaning of the cleaning liquid filling part by detaching the inner box 14.
[0040] In one embodiment, as shown in Figures 1-2 The cleaning box 10 is further provided with an outlet box 15 on the inner side. The outlet box 15 is fixedly connected to the cleaning box 10. The outlet box 15 is connected to the inner box 14 through a connecting pipe 142. The first and second inlets 12 and 13 are communicated with the outlet box 15. Specifically, the cleaning liquid in the cleaning box 10 enters the outlet box 15 through the connecting pipe 142 and then enters the first or second inlet 12 or 13 through the outlet box 15. Finally, under the pressure of the gun head 20, the cleaning liquid is sprayed outward. The outlet part can be easily cleaned by detaching the outlet box 15.
[0041] In one embodiment, as shown in Figures 1-3 The cleaning box 10 is further provided with a filling port 16. The filling port 16 is communicated with the cleaning box 10 and is used for filling the cleaning liquid into the cleaning liquid cavity 11.
[0042] In one embodiment, as shown in Figures 1-2 The cleaning box 10 is further provided with a supply plate 17 with a plug hole on the side. The gun head 20 is plugged into the supply plate 17. Specifically, the supply plate 17 is plugged with the gun head 20 to realize the detachable connection of the gun head 20 with the cleaning box. When the gun head 20 needs to be taken out, the gun head 20 can be pulled out of the supply plate 17.
[0043] In one embodiment, as shown in Figure 3 The cleaning device further comprises a storage frame 50 fixed to the cleaning box 10, which is used to store cleaning tools. Specifically, the storage frame 50 can store other cleaning tools, avoiding the mess of cleaning tools and facilitating the taking and placing of cleaning tools.
[0044] In this embodiment, as shown in Figure 3 The storage frame 50 is internally fixed with a clamping groove plate 51 and a hook 52. The storage frame 50 can insert and place tools through the clamping groove plate 51 and hang tools through the hook 52, so as to store cleaning tools.
[0045] In this embodiment, as shown in Figures 1-2 The first nozzle 31 and the second nozzle have different sizes. When the place to be sprayed with cleaning liquid is small, the gun head 20 is combined with the second nozzle, and then the gun head 20 is inserted into the second connecting port 13, so that the flow rate and the spraying diameter of the cleaning liquid are reduced. When the place to be sprayed with cleaning liquid is large, the gun head 20 is combined with the first nozzle 31, and then the gun head 20 is inserted into the first connecting port 12, so that the flow rate and the spraying diameter of the cleaning liquid are increased.
[0046] In one embodiment, as shown in Figures 1-2 The suction module 40 comprises a case 41 fixed to the inner side of the cleaning box 10 and a suction pipe 42 connected to the case 41, which is used to suck oil and impurities through the driving of the case 41. Specifically, the case 41 generates suction force acting on the suction pipe 42, so as to suck oil and impurities in the gap of the aviation equipment into the case 41, thereby removing the oil and impurities of the aviation equipment.
[0047] In this embodiment, the case 41 is internally provided with a vacuum pump connected to the suction pipe 42, which can suck external oil and impurities.
[0048] In one embodiment, as shown in Figures 1-3 The cleaning device further comprises a cleaning module 60 fixed to the cleaning box 10 and connected to the case 41, which is used to clean the oil and impurities sucked by the suction pipe 42. Specifically, the cleaning module 60 can store and clean the oil and impurities sucked by the suction module 40, thereby avoiding the return of the oil and impurities to the air and causing air pollution.
[0049] In one embodiment, as shown in Figures 2-3As shown, the cleaning module 60 comprises a cleaning box 61, a connecting pipe 142 and an adsorption layer 62, the cleaning box 61 is fixed to the cleaning box 10, the adsorption layer 62 is arranged in the interior of the cleaning box 61, the connecting pipe 142 is connected to the machine box 41 and the adsorption layer 62, and is used for passing the oil and impurities into the adsorption layer 62 through the machine box 41. Specifically, the oil and impurities adsorbed by the adsorption module 40 enter the adsorption layer 62 through the connecting pipe 142, and after being adsorbed by the adsorption layer 62, clean air is discharged from the exhaust port of the cleaning box 61, so as to realize the cleaning of the oil and impurities.
[0050] In the embodiment, the adsorption layer 62 can be any adsorption structure capable of adsorbing oil stains or dust impurities, such as sponge or activated carbon.
[0051] In one of the embodiments, as shown in Figure 1 and 3 As shown, the cleaning box 61 is provided with a dismounting port 611 for arranging a cover body, and the dismounting port 611 is used for dismounting the adsorption layer 62. Specifically, the adsorption layer 62 can be dismounted through the dismounting port 611, so as to provide convenience for the replacement of the adsorption layer 62.
[0052] In order to better understand the present application, the technical scheme of the present application will be described in detail below: In order to better understand the present application, the technical scheme of the present application will be described in detail below: Figures 1 to 3 The technical scheme of the present application is described in detail as follows: when the cleaning work of the aircraft is performed, first, the cleaning box 10 is connected to the power supply, then the machine box 41 is opened, at the same time, the suction pipe 42 starts to work and begins to absorb the oil and impurities in the gap, after the oil and impurities are absorbed, the gun head 20 is taken out of the plug-in plate, at this time, the gun head 20 is inserted into the first inlet port 12 or the second inlet port 13 of the operation plate according to the space requirement, and the corresponding first spray head 31 or second spray head is selected to be connected with the gun head 20, the cleaning liquid enters the gun head 20 and sprays the working area through the first spray head 31 or the second spray head, so as to realize the cleaning of the aircraft.
[0053] The specific implementation manner of the present application described above does not constitute a limitation on the protection scope of the present application. Any other corresponding changes and modifications made according to the technical concept of the present application should be included in the protection scope of the claims of the present application.
Claims
1. An aerial washing apparatus, characterised in that, The aviation cleaning device comprises: a cleaning box provided with a cleaning liquid cavity, a first inlet and a second inlet, the first inlet and the second inlet being communicated with the cleaning liquid cavity; a gun head detachably connected to the cleaning box for connecting the first inlet or the second inlet; a spraying module comprising first and second nozzles with different diameters, the first and second nozzles being respectively located on one side of the first inlet and the second inlet and detachably connected to the gun head; and an adsorption module installed in the cleaning box for adsorbing grease and impurities. The cleaning box is provided with an inner box on the inner side, the inner box being fixed on both sides of the cleaning box through a fixing frame, and the cleaning liquid cavity being arranged in the inner box.
2. An aerial washing apparatus as claimed in claim 1, wherein, The cleaning box is further provided with an outlet box fixedly connected to the cleaning box, the outlet box being connected to the inner box through a connecting pipe, and the first inlet and the second inlet being communicated with the outlet box.
3. An aerial washing apparatus as claimed in claim 2, wherein, The cleaning box is further provided with a filling port communicated with the cleaning box for filling cleaning liquid into the cleaning liquid cavity.
4. An aerial washing apparatus as claimed in claim 1, wherein, The gun head is inserted into the supply plate through the insertion hole.
5. An aerial washing apparatus as claimed in claim 1, wherein, The aviation cleaning device further comprises a storage frame fixed to the cleaning box, the storage frame being used for storing cleaning tools.
6. An aerial washing apparatus as claimed in any one of claims 1 to 5, wherein, The adsorption module comprises a case and a suction pipe, the case being fixed to the inner side of the cleaning box, and the suction pipe being connected to the case for sucking grease and impurities through the driving of the case.
7. An aerial washing apparatus as claimed in any one of claims 1 to 5, wherein, The aviation cleaning device further comprises a cleaning module fixed to the cleaning box and connected to the case for cleaning the grease and impurities adsorbed by the suction pipe.
8. An aerial washing apparatus as claimed in claim 7, characterised in that, The cleaning module comprises a cleaning box, a connecting pipe and an adsorption layer, the cleaning box being fixed to the cleaning box, the adsorption layer being arranged in the cleaning box, and the connecting pipe being connected to the case and the adsorption layer for passing the grease and impurities from the case to the adsorption layer.
9. An aerial washing apparatus as claimed in claim 8, wherein, The cleaning box is provided with a dismounting port provided with a cover for dismounting the adsorption layer.
10. An aerial washing apparatus as claimed in claim 9, wherein,
Citation Information
Patent Citations
Environment-friendly cleaning equipment convenient to clamp and fix for aviation equipment maintenance
CN111056039A