Cleaning device for flight part production
By adopting a pneumatic gathering cleaning structure and brush drum auxiliary cleaning components in the flight parts cleaning device, the problem of debris hiding in the bristle gap is solved, achieving a more efficient cleaning effect and self-cleaning function.
Patent Information
- Application Number
- CN202420543093.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-03-20
- Publication Date
- 2025-04-15
- Estimated Expiration
- 2034-03-20
AI Technical Summary
During the cleaning process of existing flight parts cleaning devices, debris are easily hidden in the bristle gap, resulting in contamination of subsequent parts and affecting the cleaning effect.
A cleaning device for the production of flight parts is designed, using a pneumatic gathering cleaning structure and brush drum auxiliary cleaning components. The pneumatic system drives the brush drum to rotate and clean, and uses cleaning screen plates and electromagnets to realize the self-cleaning of the brush drum.
It effectively avoids debris hiding in the bristle gap, improves the cleaning effect, extends the service life of the cleaning device, and prevents secondary pollution.
Smart Images
Figure CN222753833U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of parts cleaning, in particular to a cleaning device for producing flight parts. Background Art
[0002] Aircraft parts usually require extremely high precision and reliability. Any tiny contaminants, such as dust, grease or other residues, may affect the performance of the parts and even cause failures. Cleaning ensures that the parts can operate normally under harsh flight conditions; and contaminants may cause corrosion on the metal surface, especially in high humidity or corrosive environments. Through thorough cleaning, substances that may cause corrosion can be removed and the service life of the parts can be extended. The method used to clean the debris on the surface of the parts is usually to use a rotating brush roller to clean the surface of the parts. During cleaning, the parts are conveyed forward by a conveyor belt. The debris on the surface of the parts is swept down when passing through the brush roller. Since the bristle layer of the brush roller is composed of several bristles evenly arranged, when cleaning the debris, some debris will hide in the gaps between adjacent bristles. As the number of cleaned parts increases, the debris hidden between the bristles will gradually increase. When cleaning the subsequent parts, the debris hidden between the bristles will fall on the subsequent cleaned parts, thereby affecting the effect of cleaning the debris on the surface of the parts. For example, "Utility Model CN218394868U When the bristles of a brush roller of a parts cleaning device rotate through a paddle plate, they are blocked by the paddle plate, causing the bristles to bend and deform. After rotating through the paddle plate, the bristles rebound, causing debris attached to the inside of the bristle layer of the brush roller to fall off. The comb teeth can be inserted into the inside of the bristle layer of the brush roller to comb the bristles to prevent the ends of the bristles from being intertwined and entangled, making it difficult for debris to fall off and affecting the cleaning effect of the debris. "Therefore, this case hopes to propose a cleaning device for flight parts to solve the above problems. For the above problems, there may already be technical means to solve them in the prior art, but this case wants to provide an alternative or replacement technical solution. Utility Model Content
[0003] To achieve the above objectives, the utility model is implemented through the following technical solutions: a cleaning device for flight parts production, comprising: a parts transport platform, a suspension structure bearing box and a laser parts sensor, wherein the laser parts sensor is installed in the suspension structure bearing box, and the laser parts sensor is directly above the parts transport platform, a pneumatic gathering cleaning structure is installed in the suspension structure bearing box, and a brush cylinder auxiliary cleaning component is installed in the suspension structure bearing box;
[0004] The pneumatic gathering cleaning structure comprises: a driving air pump, a plurality of through rod bases, a plurality of displacement through rods, a plurality of sliding through holes on the rods, a pair of coordinated auxiliary push blocks, a push block coupling slideway, a plurality of auxiliary traction connecting rods, a plurality of pull rod sliding columns, a pair of special-shaped displacement connecting rods, a core rotating rod, a plurality of brush cylinder connecting columns, a plurality of column internal cleaning motors and a plurality of cleaning brush cylinders;
[0005] The driving air pump is installed in the bearing box of the suspension structure, and the driving air pump is connected to the cooperative auxiliary push block, the push block coupling slide is installed in the bearing box of the suspension structure, a pair of the cooperative auxiliary push blocks are respectively installed on the push block coupling slide, a number of the through rod bases are respectively installed in the bearing box of the suspension structure, a number of the displacement through rods are respectively installed on a number of the through rod bases through rotating shafts, and a number of the displacement through rods are respectively provided with a number of the rod sliding through holes, a number of the auxiliary traction connecting rods are respectively installed on a pair of the cooperative auxiliary push blocks through rotating shafts, a number of the pull rod sliding columns are respectively installed on a number of the auxiliary traction connecting rods, And several of the pull rod sliding columns are respectively inserted into the sliding through holes on several of the rods, a pair of the special-shaped displacement connecting rods are respectively installed on a pair of the cooperative auxiliary push blocks through rotating shafts, and a pair of the special-shaped displacement connecting rods are respectively connected to the core rotating rod through rotating shafts, and the core rotating rod is installed in the suspension structure bearing box through a rotating shaft, and several sliding grooves are respectively opened under the suspension structure bearing box, several of the brush cylinder connecting columns are respectively installed on several of the displacement through rods through several of the sliding grooves, several of the in-column cleaning motors are respectively installed in several of the brush cylinder connecting columns, and several of the in-column cleaning motors are respectively connected to several of the cleaning brush cylinders.
[0006] It should be noted that, in the above, the flight parts are transported in a dispersed manner through the parts transport platform. When the flight parts run to the bottom of the suspension structure bearing box, the laser parts sensor in the suspension structure bearing box will sense the position of the flight parts. When it is at the appropriate position, the parts transport platform will be stopped, the driving air pump will be started, and the corresponding cooperative auxiliary push block will be pushed to slide along the push block coupling slideway. The special-shaped displacement connecting rod therefore drives the core rotating rod to rotate and displace, so that the opposite side is also driven, so that a pair of cooperative auxiliary push blocks move relative to each other, thereby pulling the auxiliary traction connecting rod to drive the pulling rod sliding column to slide in the sliding through hole on the corresponding rod, so that the four displacement through rods are rotated and displaced based on the four through rod bases, so that the four brush tube connecting columns and the four cleaning brush tubes are gathered or dispersed, so that the four cleaning brush tubes wrap or separate the flight parts, and then the corresponding cleaning motor in the column drives the corresponding cleaning brush tube to rotate to clean the flight parts.
[0007] Preferably, the brush cylinder auxiliary cleaning assembly comprises: a pair of cleaning screen plates, a plurality of screen holes on the plates, a plurality of connecting spring telescopic columns and a plurality of position-changing electromagnets;
[0008] A pair of the cleaning screen plates are respectively connected to a plurality of the connecting spring telescopic columns, a plurality of cylindrical placement grooves are arranged in the bearing box of the suspension structure, a plurality of the connecting spring telescopic columns are respectively installed in the bearing box of the suspension structure through a plurality of the cylindrical placement grooves, a plurality of the displacement electromagnets are respectively installed in a plurality of the connecting spring telescopic columns and a plurality of the cylindrical placement grooves, and a pair of the cleaning screen plates are respectively provided with a plurality of the plate sieve holes;
[0009] It should be noted that, in the above-mentioned, the cleaning bristles arranged on the cleaning brush cylinder often stick to various debris after cleaning the flight parts. After cleaning, the four cleaning brush cylinders expand outward until they are fitted with a pair of cleaning screen plates. When the four cleaning brush cylinders rotate, the cleaning bristles fit the sieve holes on the plates above them, and a number of bionic barbs arranged in the sieve holes on the plates will remove the debris adhered to the cleaning bristles. At the same time, a corresponding pair of position-changing electromagnets simultaneously and rapidly exchange magnetic forces, so that a pair of connecting spring telescopic columns drive the corresponding cleaning screen plates to shake rapidly, so that the sieve holes on the plates are continuously in contact with the cleaning bristles longitudinally, and the debris is quickly separated from them, thereby realizing self-cleaning of the cleaning brush cylinder. The anti-static material coating arranged on the cleaning screen plate can prevent dust and debris from adhering to the surface of the cleaning screen plate, so as to avoid subsequent static electricity adsorption of dust and debris, and then contaminating the cleaning screen plate.
[0010] Preferably, a maintenance access is provided on the suspension structure bearing box;
[0011] Preferably, the cleaning brush cylinder is provided with cleaning bristles;
[0012] Preferably, the cleaning screen plate is provided with an anti-static material coating;
[0013] Preferably, a plurality of bionic barbs are provided in the sieve holes on the plate. Beneficial Effects
[0014] The utility model provides a cleaning device for the production of flight parts. It has the following beneficial effects. Compared with the prior art, the cleaning device for the production of flight parts has the following advantages: the device uses a pneumatic gathering cleaning structure to make four cleaning brush cylinders wrap the flight parts on the parts transport platform and rotate to clean their surfaces. After cleaning, the brush cylinder assists the cleaning component to perform a self-cleaning operation on the cleaning brush cylinder. Compared with general cleaning equipment, long-term use will cause a decrease in cleaning power, and the debris and pollutants carried will cause secondary pollution to the flight parts, so the cleaning power and practicality are greatly improved. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 This is a schematic diagram of the front cross-sectional structure of a cleaning device for producing flight parts described in the utility model.
[0016] Figure 2 It is a side structural schematic diagram of a cleaning device for producing flight parts described in the utility model.
[0017] Figure 3 for Figure 2 A partial enlarged schematic diagram of "A" in the figure.
[0018] Figure 4 This is a schematic diagram of the structure of the suspension structure bearing box of a cleaning device for producing flight parts described in the utility model.
[0019] Figure 5 This is a schematic diagram of the cleaning screen plate structure of a cleaning device for producing flight parts described in the utility model.
[0020] In the figure: 1. component transport platform; 2. suspension structure bearing box; 3. laser component sensor; 4. driving air pump; 5. through rod base; 6. displacement through rod; 7. sliding through hole on the rod; 8. cooperative auxiliary push block; 9. push block coupling slide; 10. auxiliary traction connecting rod; 11. pull rod sliding column; 12. special-shaped displacement connecting rod; 13. core rotating rod; 14. brush cylinder connecting column; 15. cleaning motor in the column; 16. cleaning brush cylinder; 17. cleaning screen plate; 18. sieve holes on the plate; 19. connecting spring telescopic column; 20. displacement electromagnet. DETAILED DESCRIPTION
[0021] Based on the embodiments of the present utility model, all other embodiments obtained by ordinary technicians in the field without making any creative work shall fall within the scope of protection of the present utility model.
[0022] Through the personnel in this field, all the electrical components in this case are connected to their corresponding power supplies through wires, and appropriate controllers and encoders should be selected according to actual conditions to meet the control requirements. The specific connection and control sequence should refer to the following working principle, and the electrical connection between the electrical components is completed in the order of working in sequence. The detailed connection means are well-known technologies in this field. The following mainly introduces the working principles and processes, and no longer explains the electrical control. Example
[0023] The present invention will be described in detail below in conjunction with the accompanying drawings. Figure 1-5As shown, a cleaning device for the production of flight parts includes: a part transport platform 1, a suspension structure bearing box 2 and a laser part sensor 3, wherein the laser part sensor 3 is installed in the suspension structure bearing box 2, and the laser part sensor 3 is directly above the part transport platform 1, and a pneumatic gathering cleaning structure is installed in the suspension structure bearing box 2, and a brush cylinder auxiliary cleaning component is installed in the suspension structure bearing box 2; the pneumatic gathering cleaning structure includes: a driving air pump 4, a plurality of through rod bases 5, a plurality of displacement through rods 6, a plurality of sliding through holes 7 on the rod, a pair of cooperative auxiliary push blocks 8, and a push block coupling slide 9. , a plurality of auxiliary traction links 10, a plurality of pull rod slides 11, a pair of special-shaped displacement links 12, a core rotary rod 13, a plurality of brush tube connection columns 14, a plurality of column cleaning motors 15 and a plurality of cleaning brush tubes 16; the driving air pump 4 is installed in the suspension structure bearing box 2, and the driving air pump 4 is connected to the cooperative auxiliary push block 8, the push block coupling slide 9 is installed in the suspension structure bearing box 2, a pair of the cooperative auxiliary push blocks 8 are respectively installed on the push block coupling slide 9, a plurality of the through rod bases 5 are respectively installed in the suspension structure bearing box 2, and a plurality of the displacement through rods 6 are respectively connected to the through rod bases 5. The plurality of through-rod bases 5 are installed through a rotating shaft, and the plurality of displacement through-rods 6 are respectively provided with a plurality of rod sliding through holes 7, the plurality of auxiliary traction links 10 are respectively installed on a pair of the cooperative auxiliary push blocks 8 through a rotating shaft, the plurality of pull rod slide columns 11 are respectively installed on the plurality of auxiliary traction links 10, and the plurality of pull rod slide columns 11 are respectively inserted into the plurality of rod sliding through holes 7, a pair of the special-shaped displacement links 12 are respectively installed on a pair of the cooperative auxiliary push blocks 8 through a rotating shaft, and a pair of the special-shaped displacement links 12 are respectively connected to the core rotating rod 13 through a rotating shaft, and the core The central rotating rod 13 is installed in the suspension structure bearing box 2 through a rotating shaft, and a plurality of sliding grooves are respectively opened below the suspension structure bearing box 2, and a plurality of brush cylinder connecting columns 14 are respectively installed on a plurality of displacement rods 6 through a plurality of sliding grooves, and a plurality of column cleaning motors 15 are respectively installed in a plurality of brush cylinder connecting columns 14, and a plurality of column cleaning motors 15 are respectively connected to a plurality of cleaning brush cylinders 16; the brush cylinder auxiliary cleaning assembly includes: a pair of cleaning screen plates 17, a plurality of screen holes 18 on the plates, a plurality of connecting spring telescopic columns 19 and a plurality of displacement electromagnets 20;A pair of the cleaning screen plates 17 are respectively connected to a plurality of the connecting spring telescopic columns 19, a plurality of cylindrical placement grooves are provided in the suspension structure bearing box 2, a plurality of the connecting spring telescopic columns 19 are respectively installed in the suspension structure bearing box 2 through a plurality of the cylindrical placement grooves, a plurality of the displacement electromagnets 20 are respectively installed in a plurality of the connecting spring telescopic columns 19 and a plurality of the cylindrical placement grooves, and a pair of the cleaning screen plates 17 are respectively provided with a plurality of the plate sieve holes 18. ;
[0024] According to the attached Figure 1-5 It is concluded that the flying parts are transported in a dispersed manner through the part transport platform 1. When the flying parts run to the bottom of the suspension structure bearing box 2, the laser part sensor 3 in the suspension structure bearing box 2 will sense the position of the flying parts. When the flying parts are in the appropriate position, the part transport platform 1 will be stopped, and the driving air pump 4 will be started to push the corresponding cooperative auxiliary push block 8 to slide along the push block coupling slideway 9. The special-shaped displacement connecting rod 12 therefore drives the core rotating rod 13 to rotate and displace, so that the opposite side is also driven, so that a pair of cooperative auxiliary push blocks 8 move relative to each other, thereby pulling the auxiliary traction connecting rod 10 to drive the pulling rod sliding column 11 to slide in the corresponding sliding through hole 7 on the rod, so that the four displacement through rods 6 are rotated and displaced based on the four through rod bases 5, so that the four brush tube connecting columns 14 and the four cleaning brush tubes 16 are gathered or dispersed, so that the four cleaning brush tubes 16 wrap or separate the flying parts, and then the corresponding column cleaning motor 15 drives the corresponding cleaning brush The cylinder 16 rotates to clean the flying parts; the cleaning bristles arranged on the cleaning brush cylinder 16 often stick to various debris after cleaning the flying parts. After cleaning, the four cleaning brush cylinders 16 expand outward until they are in contact with a pair of cleaning screen plates 17. When the four cleaning brush cylinders 16 rotate, the cleaning bristles are in contact with the screen holes 18 on the plates thereon, and a number of bionic barbs arranged in the screen holes 18 on the plates will remove the debris adhered to the cleaning bristles. At the same time, the corresponding pair of variable position electromagnets 20 simultaneously and rapidly exchange magnetic forces, so that a pair of connecting spring telescopic columns 19 drive the corresponding cleaning screen plates 17 to shake rapidly, so that the screen holes 18 on the plates are continuously contacted with the cleaning bristles longitudinally, and the debris is quickly separated from them, thereby realizing the self-cleaning of the cleaning brush cylinder 16, and the anti-static material coating arranged on the cleaning screen plate 17 can prevent dust and debris from adhering to the surface of the cleaning screen plate 17, so as to avoid the subsequent electrostatic adsorption of dust and debris, thereby contaminating the cleaning screen plate 17.
[0025] Although the embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A cleaning device for producing flight parts, comprising: A component transport platform (1), a suspension structure bearing box (2), and a laser component sensor (3), characterized in that the laser component sensor (3) is installed in the suspension structure bearing box (2), and the laser component sensor (3) is directly above the component transport platform (1), a pneumatic gathering cleaning structure is installed in the suspension structure bearing box (2), and a brush cylinder auxiliary cleaning component is installed in the suspension structure bearing box (2); The pneumatic gathering cleaning structure comprises: a driving air pump (4), a plurality of through rod bases (5), a plurality of displacement through rods (6), a plurality of sliding through holes on the rods (7), a pair of coordinated auxiliary push blocks (8), a push block coupling slideway (9), a plurality of auxiliary traction connecting rods (10), a plurality of pull rod sliding columns (11), a pair of special-shaped displacement connecting rods (12), a core rotating rod (13), a plurality of brush cylinder connecting columns (14), a plurality of column internal cleaning motors (15) and a plurality of cleaning brush cylinders (16); The driving air pump (4) is installed in the suspension structure bearing box (2), and the driving air pump (4) is connected to the cooperative auxiliary push block (8), the push block coupling slideway (9) is installed in the suspension structure bearing box (2), a pair of the cooperative auxiliary push blocks (8) are respectively installed on the push block coupling slideway (9), a plurality of the through rod bases (5) are respectively installed in the suspension structure bearing box (2), a plurality of the displacement through rods (6) are respectively installed on a plurality of the through rod bases (5) through rotating shafts, and a plurality of the displacement through rods (6) are respectively provided with a plurality of the rod sliding through holes (7), a plurality of the auxiliary traction connecting rods (10) are respectively installed on a pair of the cooperative auxiliary push blocks (8) through rotating shafts, and a plurality of the pull rod sliding columns (11) are respectively installed on a plurality of the auxiliary traction connecting rods (10). , and a plurality of the pull rod sliding columns (11) are respectively inserted into the sliding through holes (7) on the plurality of the rods, a pair of the special-shaped displacement connecting rods (12) are respectively installed on a pair of the cooperative auxiliary push blocks (8) via rotating shafts, and a pair of the special-shaped displacement connecting rods (12) are respectively connected to the core rotating rod (13) via rotating shafts, and the core rotating rod (13) is installed in the suspension structure bearing box (2) via rotating shafts, and a plurality of sliding through grooves are respectively opened below the suspension structure bearing box (2), a plurality of the brush cylinder connecting columns (14) are respectively installed on the plurality of the displacement through rods (6) via the plurality of the sliding through grooves, a plurality of the column cleaning motors (15) are respectively installed in the plurality of the brush cylinder connecting columns (14), and a plurality of the column cleaning motors (15) are respectively connected to a plurality of the cleaning brush cylinders (16).
2. A cleaning device for flight parts production according to claim 1, characterized in that: The brush cylinder auxiliary cleaning assembly comprises: a pair of cleaning screen plates (17), a plurality of screen holes (18) on the plates, a plurality of connecting spring telescopic columns (19) and a plurality of position-changing electromagnets (20); A pair of the cleaning screen plates (17) are respectively connected to a plurality of the connecting spring telescopic columns (19); a plurality of cylindrical mounting grooves are provided in the suspension structure bearing box (2); a plurality of the connecting spring telescopic columns (19) are respectively installed in the suspension structure bearing box (2) through the plurality of cylindrical mounting grooves; a plurality of the displacement electromagnets (20) are respectively installed in the plurality of the connecting spring telescopic columns (19) and the plurality of cylindrical mounting grooves; and a pair of the cleaning screen plates (17) are respectively provided with a plurality of the plate sieve holes (18).
3. A cleaning device for producing flight parts according to claim 2, characterized in that: The suspension structure bearing box (2) is provided with a maintenance and inspection opening.
4. A cleaning device for producing flight parts according to claim 3, characterized in that: The cleaning brush cylinder (16) is provided with cleaning bristles.
5. A cleaning device for producing flight parts according to claim 4, characterized in that: The cleaning screen plate (17) is provided with an anti-static material coating.
6. A cleaning device for producing flight parts according to claim 5, characterized in that: A plurality of bionic barbs are arranged in the sieve holes (18) on the plate.