CN220611464U - Oil removal cleaning equipment for aerospace parts - Google Patents
Oil removal cleaning equipment for aerospace parts Download PDFInfo
- Publication number
- CN220611464U CN220611464U CN202322241956.8U CN202322241956U CN220611464U CN 220611464 U CN220611464 U CN 220611464U CN 202322241956 U CN202322241956 U CN 202322241956U CN 220611464 U CN220611464 U CN 220611464U
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- China
- Prior art keywords
- cylinder
- cleaning
- water
- oil removal
- baffle
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- 238000004140 cleaning Methods 0.000 title claims abstract description 98
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 73
- 239000007788 liquid Substances 0.000 description 14
- 238000000034 method Methods 0.000 description 7
- 230000000694 effects Effects 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 230000006978 adaptation Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000005489 elastic deformation Effects 0.000 description 2
- 238000005406 washing Methods 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 230000001680 brushing effect Effects 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Cleaning By Liquid Or Steam (AREA)
Abstract
The utility model relates to the technical field of cleaning equipment, and particularly discloses oil removal cleaning equipment for aerospace parts, which comprises a support, wherein a cleaning cylinder is arranged in the middle of the support, support rods which are uniformly distributed are fixedly arranged on the side edges of the cleaning cylinder, a transverse plate is commonly arranged at the top ends of the support rods, symmetrical first air cylinders are fixedly arranged at the top parts of the transverse plate, a mounting plate is arranged below the transverse plate, connecting plates are fixedly arranged at two sides of the mounting plate, the end parts of output shafts of the first air cylinders are fixedly arranged with the connecting plates respectively, a motor is fixedly arranged at the top parts of the mounting plate, a baffle is arranged below the mounting plate, the end parts of output shafts of the motor are fixedly arranged at the top parts of the baffle, bristles which are uniformly distributed are arranged at the bottom parts are arranged.
Description
Technical Field
The utility model belongs to the technical field of cleaning equipment, and particularly relates to oil removal cleaning equipment for aerospace parts.
Background
The components of the aerospace vehicle are orderly assembled by parts, and oil removal treatment is needed in the processing or assembling process of the aerospace vehicle parts so as to reduce the influence of oil stains on the aerospace vehicle parts in the processing or assembling process, and further to influence the processing precision or the working state after the assembly.
However, the degreasing and cleaning device for the aerospace components in the prior art has poor cleaning effect on the aerospace components, and is not beneficial to subsequent processing of the aerospace components.
The utility model provides an existing patent (application number: CN 202111344016.0) deoiling cleaning equipment for aerospace spare part, through putting into the cleaning tank and pour into appropriate amount of deoiling liquid into the cleaning tank into, then can drive the roof through starting four electric telescopic handle and move downwards, make second bevel gear remove to when meshing with first bevel gear can close four electric telescopic handle, at this moment, two cleaning brushes all remove to the cleaning tank in, can start the motor immediately, through the meshing transmission of second gear and third gear, can drive first rotating shaft rotation, thereby can pass through the rolling contact of cam and baffle, and through the elastic deformation of spring, can drive rack reciprocal left and right movement, and then can drive the reciprocal rotation of first gear, thereby can drive the reciprocal rotation of cleaning tank through the support column, and can drive the rotation of third pivot through the meshing transmission of first bevel gear and second bevel gear, and can drive two cleaning brushes through the meshing transmission of two third bevel gears and belt, thereby can drive two cleaning brushes and can be convenient for take out the cleaning effect through the cleaning brush to the cleaning tank through the meshing transmission of two cleaning brushes, can be convenient for the cleaning position of two spare parts, can be to take out the clean the spare part through the elastic deformation of spring, and can be convenient for the cleaning position of the spare part, and take out the spare part through the reciprocal rotation of the support column, and can be used for the reciprocal rotation of cleaning the cleaning tank.
For above-mentioned problem, current patent has given the solution, but at in-service use's in-process device overall structure is comparatively complicated for spare part cleaning process is comparatively loaded down with trivial details, and the spare part is also comparatively inconvenient when getting and putting, and the practicality is not strong, need improve this.
Therefore, the oil removal cleaning equipment for the aerospace parts is provided.
Disclosure of Invention
The utility model aims to solve the technical problem of providing the oil removal cleaning equipment for the aerospace parts, which has the advantages of good cleaning effect, convenience in taking and placing parts and simple integral structure.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: the utility model provides an aerospace spare part is with deoiling cleaning equipment, includes the support, the support middle part is provided with the wash bowl, the support is located wash bowl side fixed mounting and has evenly distributed's bracing piece, the diaphragm is installed jointly on the bracing piece top, diaphragm top fixed mounting has symmetrical first cylinder, the diaphragm below is provided with the mounting panel, mounting panel both sides fixed mounting has the connecting plate, first cylinder output shaft tip respectively with connecting plate fixed mounting, mounting panel top fixed mounting has the motor, the mounting panel below is provided with the baffle, motor output shaft tip and baffle top fixed mounting, the baffle bottom is provided with evenly distributed's brush hair.
Preferably, the baffle is arranged in a round shape, the outer diameter size of the baffle is matched with the inner diameter size of the cleaning cylinder, and the length of the brush hair is matched with the height of the inner wall of the cleaning cylinder.
Preferably, the bottom of the cleaning cylinder is fixedly provided with a second air cylinder, and the bottom of the cleaning cylinder is provided with a lifting plate.
Preferably, the outer diameter of the lifting plate is matched with the inner diameter of the cleaning cylinder, and through holes which are uniformly distributed are formed in the lifting plate.
Preferably, the support is provided with a water supply part, and the water supply part comprises a water tank fixedly arranged on the support, a water pump fixedly arranged at the bottom of the water tank and a water delivery pipe arranged between the water pump and the cleaning cylinder.
Preferably, the water inlet of the water pump is communicated with the water tank, and two ends of the water delivery pipe are respectively communicated with the water outlet of the water pump and the cleaning cylinder.
Preferably, a water outlet pipe is arranged at the bottom side of the cleaning cylinder, and a switch valve is arranged on the water outlet pipe.
Preferably, the support is provided with a controller, and the controller is electrically connected with the first cylinder, the motor, the second cylinder and the water pump respectively.
In summary, compared with the prior art, the utility model has the following beneficial effects:
1. according to the utility model, through the cooperation work among the bracket, the cleaning barrel, the supporting rod, the transverse plate, the first cylinder, the mounting plate, the connecting plate, the motor, the baffle and the brush hair, aerospace parts can be automatically cleaned, the cleaning effect is good, cleaning liquid can not be splashed out in the cleaning process, the structure is simple, and the practicability is strong.
2. According to the utility model, through the cooperation among the second cylinder, the lifting plate and the through hole, the aerospace parts can be conveniently placed and taken, so that the labor and the trouble are saved, and the practicability is high.
3. According to the utility model, through the cooperation among the water tank, the water pump, the water delivery pipe, the water outlet pipe and the switch valve, cleaning liquid can be automatically supplied into the cleaning cylinder, and waste liquid can be automatically discharged from the cleaning cylinder, so that the practicability of the device is further improved.
Drawings
FIG. 1 is a perspective view of the present utility model;
FIG. 2 is a front plan view of the present utility model;
FIG. 3 is a block diagram of the upper elements of the cross plate of the present utility model;
FIG. 4 is a bottom view of the present utility model;
fig. 5 is a view showing the structure of the bottom inside of the cleaning cylinder according to the present utility model.
Legend description:
1. a bracket; 2. a cleaning cylinder; 3. a support rod; 4. a cross plate; 5. a first cylinder; 6. a mounting plate; 7. a connecting plate; 8. a motor; 9. a baffle; 10. brushing; 11. a second cylinder; 12. a lifting plate; 13. a through hole; 14. a water supply member; 141. a water tank; 142. a water pump; 143. a water pipe; 15. a water outlet pipe; 16. and (3) switching the valve.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, the present utility model provides a technical solution: the utility model provides an aerospace spare part is with deoiling cleaning equipment, includes support 1, support 1 middle part is provided with wash bowl 2, support 1 is located wash bowl 2 side fixed mounting and has evenly distributed's bracing piece 3, diaphragm 4 is installed jointly on bracing piece 3 top, diaphragm 4 top fixed mounting has symmetrical first cylinder 5, diaphragm 4 below is provided with mounting panel 6, mounting panel 6 both sides fixed mounting has connecting plate 7, first cylinder 5 output shaft tip respectively with connecting plate 7 fixed mounting, mounting panel 6 top fixed mounting has motor 8, mounting panel 6 below is provided with baffle 9, motor 8 output shaft tip and baffle 9 top fixed mounting, baffle 9 bottom is provided with evenly distributed's brush hair 10, baffle 9 set up to circular and baffle 9 external diameter size and wash bowl 2 internal diameter size looks adaptation, brush hair 10 length and wash bowl 2 inner wall height looks adaptation.
When the surface of aerospace spare part needs to be deoiled, pour into the washing liquid into in the wash bowl 2 to put into the wash bowl 2 with spare part, start the first cylinder 5 of diaphragm 4 top simultaneously, first cylinder 5 output shaft moves down and drives connecting plate 7 vertical downwardly moving, connecting plate 7 moves down and promotes baffle 9 motor 8 and brush hair 10 and move down simultaneously, make brush hair 10 get into in the wash bowl 2, baffle 9 just come in and go out wash bowl 2 inner wall nozzle department, later start motor 8 on mounting panel 6, motor 8 output shaft rotates and drives baffle 9 rotation, the rotating plate rotates and drives brush hair 10 and rotate in wash bowl 2, brush hair 10 rotates and deoils the surface of aerospace spare part simultaneously, can wash aerospace spare part with deoiling cleaning equipment voluntarily, cleaning effect is good, can not lead to the washing liquid to splash out in the cleaning process, and is simple structure, and the practicality is strong.
The bottom of the cleaning cylinder 2 is fixedly provided with a second air cylinder 11, the bottom in the cleaning cylinder 2 is provided with a lifting plate 12, the outer diameter size of the lifting plate 12 is matched with the inner diameter size of the cleaning cylinder 2, and the lifting plate 12 is provided with evenly distributed through holes 13; when the aerospace components are placed in the cleaning cylinder 2, the second air cylinder 11 at the bottom of the cleaning cylinder 2 is started, the second air cylinder 11 pushes the lifting plate 12 to move upwards in the cleaning cylinder 2, the components are placed on the lifting plate 12 when moving to the cylinder opening, the lifting plate 12 is driven to drive the components to move to the bottom of the cleaning cylinder 2 after the components are placed, the through holes 13 are formed, the water cleaning liquid in the cleaning cylinder 2 can be prevented from moving in the lifting process of the lifting plate 12, the aerospace components can be conveniently placed and taken, trouble and labor are saved, and the practicability is high.
The water supply device comprises a bracket 1, a water supply part 14 is arranged on the bracket 1, the water supply part 14 comprises a water tank 141 fixedly arranged on the bracket 1, a water pump 142 fixedly arranged at the bottom of the water tank 141 and a water delivery pipe 143 arranged between the water pump 142 and a cleaning cylinder 2, a water inlet of the water pump 142 is communicated with the water tank 141, two ends of the water delivery pipe 143 are respectively communicated with a water outlet of the water pump 142 and the cleaning cylinder 2, a water outlet pipe 15 is arranged at the bottom side of the cleaning cylinder 2, and a switch valve 16 is arranged on the water outlet pipe 15; injecting cleaning liquid into the water tank 141, starting the water pump 142 at the bottom of the water tank 141, conveying the cleaning liquid in the water tank 141 into the cleaning cylinder 2 through the water conveying pipe 143 by the water pump 142, opening the switch valve 16 on the water outlet pipe 15, and discharging waste liquid in the cleaning cylinder 2 from the water outlet pipe 15, thereby further increasing the practicability of the device.
The bracket 1 is provided with a controller which is respectively and electrically connected with the first air cylinder 5, the motor 8, the second air cylinder 11 and the water pump 142; the setting controller can realize automatic control of each element of the device.
Working principle: when the surface of the aerospace component needs to be deoiled, the water pump 142 at the bottom of the water tank 141 is started, the water pump 142 conveys cleaning liquid in the water tank 141 into the cleaning cylinder 2 through the water pipe 143, the second air cylinder 11 at the bottom of the cleaning cylinder 2 is started, the second air cylinder 11 pushes the lifting plate 12 to move upwards in the cleaning cylinder 2, the component is placed on the lifting plate 12 when moving to the cylinder opening, the lifting plate 12 is driven to drive the component to move to the bottom of the cleaning cylinder 2 after the placement, the first air cylinder 5 above the transverse plate 4 is started at the same time, the output shaft of the first air cylinder 5 moves downwards to drive the connecting plate 7 to move downwards, the motor 8 and the brush hair 10 move downwards at the same time, so that the brush hair 10 enters the cleaning cylinder 2, the baffle 9 just enters the inner wall opening of the cleaning cylinder 2, the motor 8 on the mounting plate 6 is started at the same time, the output shaft of the motor 8 drives the baffle 9 to rotate, the baffle 10 rotates in the cleaning cylinder 2, the surface of the aerospace component is deoiled at the same time when the rotating, the component is driven to be deoiled, the component is driven to move to the bottom the cleaning cylinder 2 through the lifting plate 12, the brush hair is driven to move downwards, the cleaning liquid is discharged from the cleaning liquid 15 through the lifting plate 2, and the water outlet pipe 15 is required to be repeatedly opened when the cleaning liquid is discharged from the cleaning cylinder 15, and the cleaning cylinder 15 is opened.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (8)
1. The utility model provides an aerospace spare part is with deoiling cleaning equipment, includes support (1), a serial communication port, support (1) middle part is provided with wash bowl (2), support (1) are located wash bowl (2) side fixed mounting and have evenly distributed's bracing piece (3), diaphragm (4) are installed jointly on bracing piece (3) top, diaphragm (4) top fixed mounting has symmetrical first cylinder (5), diaphragm (4) below is provided with mounting panel (6), mounting panel (6) both sides fixed mounting has connecting plate (7), first cylinder (5) output shaft tip respectively with connecting plate (7) fixed mounting, mounting panel (6) top fixed mounting has motor (8), mounting panel (6) below is provided with baffle (9), motor (8) output shaft tip and baffle (9) top fixed mounting, baffle (9) bottom is provided with evenly distributed's brush hair (10).
2. The oil removal cleaning device for aerospace parts according to claim 1, wherein the baffle (9) is circular, the outer diameter of the baffle (9) is matched with the inner diameter of the cleaning cylinder (2), and the length of the bristles (10) is matched with the height of the inner wall of the cleaning cylinder (2).
3. The oil removal cleaning device for aerospace parts according to claim 1, wherein a second cylinder (11) is fixedly arranged at the bottom of the cleaning cylinder (2), and a lifting plate (12) is arranged at the inner bottom of the cleaning cylinder (2).
4. An aerospace component oil removal cleaning device according to claim 3, wherein the outer diameter of the lifting plate (12) is matched with the inner diameter of the cleaning cylinder (2), and the lifting plate (12) is provided with evenly distributed through holes (13).
5. The oil removal cleaning device for aerospace parts according to claim 1, wherein the support (1) is provided with a water supply piece (14), and the water supply piece (14) comprises a water tank (141) fixedly installed on the support (1), a water pump (142) fixedly installed at the bottom of the water tank (141) and a water delivery pipe (143) arranged between the water pump (142) and the cleaning cylinder (2).
6. The oil removal cleaning device for aerospace parts according to claim 5, wherein the water inlet of the water pump (142) is communicated with the water tank (141), and two ends of the water delivery pipe (143) are respectively communicated with the water outlet of the water pump (142) and the cleaning cylinder (2).
7. The oil removal cleaning device for aerospace parts according to claim 1, wherein a water outlet pipe (15) is arranged at the bottom side of the cleaning cylinder (2), and a switch valve (16) is arranged on the water outlet pipe (15).
8. The oil removal cleaning device for aerospace parts according to claim 1, wherein a controller is arranged on the bracket (1), and the controller is electrically connected with the first air cylinder (5), the motor (8), the second air cylinder (11) and the water pump (142) respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322241956.8U CN220611464U (en) | 2023-08-21 | 2023-08-21 | Oil removal cleaning equipment for aerospace parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322241956.8U CN220611464U (en) | 2023-08-21 | 2023-08-21 | Oil removal cleaning equipment for aerospace parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220611464U true CN220611464U (en) | 2024-03-19 |
Family
ID=90232121
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322241956.8U Active CN220611464U (en) | 2023-08-21 | 2023-08-21 | Oil removal cleaning equipment for aerospace parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220611464U (en) |
-
2023
- 2023-08-21 CN CN202322241956.8U patent/CN220611464U/en active Active
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