Electroplating device for aerospace parts
By designing a limit device and a swing mechanism, the electroplating device for aerospace parts has solved the problem of parts falling off during the electroplating process, achieving efficient electroplating and reducing workload.
Patent Information
- Application Number
- CN202520349919.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-03
- Publication Date
- 2026-02-13
- Estimated Expiration
- 2035-03-03
AI Technical Summary
During the electroplating process, suspended parts may fall off, resulting in poor electroplating results and increasing the workload of workers in retrieving them.
An electroplating device for aerospace components was designed, comprising a base, a swing mechanism, and a drive mechanism. The device prevents components from falling off by a limiting device and promotes the flow of electroplating solution by the swing mechanism to improve electroplating efficiency.
It effectively prevents parts from falling off, ensures the electroplating effect, reduces the retrieval burden on workers, and improves electroplating efficiency.
Smart Images
Figure CN223906979U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the technical field of parts electroplating, especially to an aerospace parts electroplating device. BACKGROUND
[0002] The aerospace industry is a technology-intensive industry, and the performance requirements for parts are extremely high. In order to improve the corrosion resistance and wear resistance of parts, electroplating devices are needed for electroplating treatment of the surface of parts during the processing of parts.
[0003] Currently, when electroplating treatment is performed on parts, the parts are usually first hung on hooks, and then placed in an electroplating solution. In order to further improve the electroplating efficiency, some electroplating devices are equipped with a swing mechanism to drive the parts to move back and forth in the electroplating solution, thereby accelerating the flow of the electroplating solution and speeding up the electroplating process. However, when the swing mechanism drives the parts to move, the parts may fall off the hooks, and the fallen parts may not achieve the expected electroplating effect. In addition, the workers need to spend extra time to salvage these fallen parts, thereby increasing the workload. SUMMARY
[0004] The utility model aims to at least solve one of the technical problems in the related art to some extent.
[0005] To this end, the utility model provides an aerospace parts electroplating device, which can limit the suspension of parts during electroplating treatment, avoid falling off, ensure the electroplating effect of parts, eliminate the process of workers salvaging fallen parts, and reduce the burden on workers.
[0006] To achieve the above-mentioned purpose, the utility model provides an aerospace parts electroplating device, which comprises a base, a swing mechanism, a driving mechanism, and an electroplating tank. The top surface of the base is provided with a stand on both sides, and the top ends of the two stands are connected with a top plate. The bottom surface of the top plate is provided with a gas cylinder, the piston end of the gas cylinder is connected with a mounting bracket, the mounting bracket is provided with a swing plate, the swing mechanism is arranged on the mounting bracket and connected with the swing plate, the bottom surface of the swing plate is provided with a plurality of mounting columns, the bottom end of the mounting column is provided with a hook, one side of the mounting column is provided with a support plate, one side of the support plate is rotatably connected with a rotating shaft, the rotating shaft is connected with a baffle, the baffle abuts against the hook, the driving mechanism is arranged on the swing plate and connected with a plurality of rotating shafts, and the electroplating tank is arranged on the base.
[0007] The aerospace part electroplating device can limit the suspended parts during the electroplating treatment process, avoids the parts from falling off, guarantees the electroplating effect of the parts, eliminates the process of fishing the fallen parts, and reduces the burden of workers.
[0008] In addition, the aerospace part electroplating device according to the application can have the following additional technical features:
[0009] Specifically, the swinging mechanism comprises a fixing frame, two rotating plates, a driver, a mounting shaft, a moving rod, a connecting rod, a swinging plate and two swinging shafts, the fixing frame is connected with the mounting frame, the two rotating plates are arranged in the fixing frame respectively, the driver is arranged on the fixing frame and connected with the rotating plates, one end of the mounting shaft is connected with one of the rotating plates, and the other end is rotatably connected with the fixing frame, the moving rod penetrates through the two rotating plates respectively and is connected with the connecting rod, the moving rod is slidably connected with the rotating plates, the swinging plate is connected with the connecting rod, the two swinging shafts are connected with the two sides of the swinging plate respectively, the two swinging shafts are rotatably connected with the mounting frame respectively, and the swinging shafts are connected with the swinging plate through the mounting frame.
[0010] Specifically, the driving mechanism comprises a support plate, an electric push rod, a rack, a plurality of gears and a support assembly, the support plate is arranged on the swinging plate, the electric push rod is arranged on the support plate, the rack is connected with the piston end of the electric push rod, the plurality of gears are arranged on the plurality of rotating shafts respectively and are engaged with the rack respectively, and the support assembly is arranged on the swinging plate, and the rack is slidably connected with the support assembly.
[0011] Specifically, the support assembly comprises a T-shaped sliding groove and a T-shaped sliding plate, the T-shaped sliding groove is arranged on the swinging plate, the T-shaped sliding plate is connected with the rack and slidably connected with the T-shaped sliding groove.
[0012] Specifically, the electroplating tank is provided with an observation window.
[0013] The additional aspects and advantages of the present application will be partially given in the following description, partially will become obvious from the following description, or will be understood by the practice of the present application. BRIEF DESCRIPTION OF DRAWINGS
[0014] The above and / or additional aspects and advantages of the present application will become apparent and more readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings:
[0015] Figure 1 FIG. 1 is a structural schematic view of an aerospace part electroplating device according to the present application.
[0016] Figure 2 For Figure 1 Amplification structure schematic view in A area;
[0017] Figure 3 For Figure 1 Amplification structure schematic view in B area;
[0018] Figure 4 The utility model discloses aerospace parts electroplating device's T type sliding groove side view.
[0019] As shown in the figure: 10, base; 11, vertical plate; 12, top plate; 20, air cylinder; 21, mounting bracket; 22, swing board; 30, swing mechanism; 31, fixed frame; 32, rotating plate; 33, driver; 34, mounting shaft; 35, moving rod; 36, connecting rod; 37, swing board; 38, swing axle; 41, mounting column; 42, hook; 43, support plate; 44, rotating shaft; 45, baffle; 50, driving mechanism; 51, support plate; 52, electric push rod; 53, rack; 54, gear; 55, support assembly; 551, T type sliding groove; 552, T type sliding plate; 60, electroplating tank; 61, observation window. DETAILED DESCRIPTION
[0020] The embodiments of the utility model are described in detail below, and the examples of the embodiments are shown in the drawings, wherein the same or similar reference signs represent the same or similar elements or elements with the same or similar functions throughout. The embodiments described below by referring to the drawings are exemplary and are intended to explain the utility model, and cannot be understood as limiting the utility model. On the contrary, the embodiments of the utility model include all changes, modifications and equivalents falling within the spirit and scope of the appended claims.
[0021] The aerospace parts electroplating device of the embodiments of the utility model is described below in combination with the drawings.
[0022] As Figures 1-3 shown, the aerospace parts electroplating device of the embodiments of the utility model can include base 10, swing mechanism 30, driving mechanism 50 and electroplating tank 60.
[0023] Among them, the top surface of base 10 both sides are equipped with vertical plate 11, and the top end of two vertical plates 11 is connected with top plate 12, and the bottom surface of top plate 12 is equipped with air cylinder 20, and the piston end of air cylinder 20 is connected with mounting bracket 21, and mounting bracket 21 is equipped with swing board 22, and swing mechanism 30 is arranged on mounting bracket 21, and is connected with swing board 22.
[0024] The bottom surface of the swing plate 22 is provided with a plurality of mounting columns 41, the bottom end of the mounting column 41 is provided with a hook 42, one side of the mounting column 41 is provided with a supporting plate 43, one side of the supporting plate 43 is rotationally connected with a rotating shaft 44, the rotating shaft 44 is connected with a baffle plate 45, the baffle plate 45 abuts against the hook 42, and the driving mechanism 50 is arranged on the swing plate 22 and connected with the plurality of rotating shafts 44.
[0025] The electroplating tank 60 is arranged on the base 10.
[0026] Specifically, the staff first pours electroplating solution into the electroplating tank 60, and then starts the driving mechanism 50 to drive the plurality of rotating shafts 44 to rotate counterclockwise, thereby moving away the baffle plate 45, and then the holes on each part to be electroplated are threaded through each hook 42 for hanging, and then the driving mechanism 50 is started again to drive the plurality of rotating shafts 44 to rotate clockwise, so that the baffle plate 45 abuts against the hook 42 to limit the part, preventing the part from falling off.
[0027] The cylinder 20 is started to drive the mounting bracket 21 and the part to descend, so that the part enters the electroplating tank 60 for electroplating treatment, and then the swing mechanism 30 is started to drive the swing plate 22 to swing, so that the part moves in the electroplating solution, promotes the solution to flow, accelerates the speed of fresh electroplating solution reaching the surface of the part, helps to provide the required metal ions faster, and thus improves the electroplating efficiency.
[0028] The aerospace part electroplating device can limit the suspended part during the electroplating treatment process, avoid the part from falling off, not only ensure the electroplating effect of the part, but also eliminate the step of the staff fishing the fallen part, and reduce the burden of the staff.
[0029] In an embodiment of the utility model, as shown in Figure 2 The swing mechanism 30 can include a fixing frame 31, two rotating plates 32, a driver 33, a mounting shaft 34, a moving rod 35, a connecting rod 36, a swing plate 37 and two swing shafts 38.
[0030] The fixing frame 31 is connected with the mounting bracket 21, the two rotating plates 32 are arranged in the fixing frame 31 respectively, the driver 33 is arranged on the fixing frame 31 and connected with the rotating plate 32, one end of the mounting shaft 34 is connected with the other rotating plate 32, the other end is rotationally connected with the fixing frame 31, the moving rod 35 penetrates through the two rotating plates 32 respectively and is connected with the connecting rod 36, the moving rod 35 is slidingly connected with the rotating plate 32, the swing plate 37 is connected with the connecting rod 36, the two swing shafts 38 are connected with the two sides of the swing plate 22 respectively, the two swing shafts 38 are rotationally connected with the mounting bracket 21 respectively, and the swing shaft 38 penetrates through the mounting bracket 21 and is connected with the swing plate 37.
[0031] It should be noted that the driver 33 described in this embodiment can be selected by the motor, which can drive the rotating plate 32 to rotate, and the rotating plate 32 can drive another rotating plate 32 to rotate through the moving rod 35, thereby driving the moving rod 35 and the connecting rod 36 to move, and the moving rod 35 will slide in the rotating plate 32, and under the cooperation of the swing shaft 38, the connecting rod 36 will drive the swing plate 37 to swing, and the swing of the swing plate 22 is completed.
[0032] In an embodiment of the present application, as shown in Figure 3 The driving mechanism 50 can include a support plate 51, an electric push rod 52, a rack 53, a plurality of gears 54, and a support assembly 55, wherein the support plate 51 is arranged on the swing plate 22, the electric push rod 52 is arranged on the support plate 51, the rack 53 is connected with the piston end of the electric push rod 52, the plurality of gears 54 are arranged on the plurality of rotating shafts 44 respectively and are engaged with the rack 53 respectively, the support assembly 55 is arranged on the swing plate 22, and the rack 53 is in sliding connection with the support assembly 55.
[0033] It should be noted that the piston end of the electric push rod 52 can be controlled to stretch and retract to drive the rack 53 to move, thereby driving the plurality of gears 54 to rotate, so as to drive the rotating shaft 44 to rotate by a certain angle, thereby adjusting the angle of the baffle 45, and in this process, the support assembly 55 provides support and guiding effect for the rack 53.
[0034] In an embodiment of the present application, as shown in Figure 4 The support assembly 55 includes a T-shaped sliding groove 551 and a T-shaped sliding plate 552, wherein the T-shaped sliding groove 551 is arranged on the swing plate 22, and the T-shaped sliding plate 552 is connected with the rack 53 and is in sliding connection with the T-shaped sliding groove 551.
[0035] It should be noted that the two ends of the T-shaped sliding groove 551 are in an open state, and in the process of moving the rack 53, the T-shaped sliding plate 552 will move in the T-shaped sliding groove 551 to guide the rack 53.
[0036] In an embodiment of the present application, as shown in Figure 1 The electroplating tank 60 is provided with an observation window 61.
[0037] It can be understood that the observation window 61 is arranged to facilitate the staff to observe the electroplating condition of the parts in the electroplating tank 60.
[0038] In summary, the aerospace part electroplating device can limit the suspended parts during the electroplating process, avoid falling off, ensure the electroplating effect of the parts, eliminate the process of fishing the fallen parts, and reduce the burden of the staff.
[0039] In the description of the present application, the terms "first", "second" are only for the purpose of description, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined with "first", "second" can explicitly or implicitly include at least one of the features. In the description of the present application, the meaning of "a plurality of" is at least two, for example, two, three, etc., unless otherwise specifically limited.
[0040] In the description of the present application, the description of the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" means that the specific features, structures, materials or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the present application. In the present application, the illustrative description of the above terms is not necessarily for the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner. In addition, those skilled in the art can combine and combine the different embodiments or examples described in the present application and the features of the different embodiments or examples without contradiction.
[0041] Although the embodiments of the present application have been shown and described above, it can be understood that the above embodiments are exemplary and cannot be understood as limiting the present application, and those skilled in the art can change, modify, replace and deform the above embodiments within the scope of the present application.
Claims
1. An aerospace part electroplating apparatus, comprising: Including base, swing mechanism, drive mechanism and electroplating tank, wherein, Both sides of the top surface of the base are provided with vertical plates, and the top ends of the two vertical plates are connected with a top plate; The bottom surface of the top plate is provided with an air cylinder, and the piston end of the air cylinder is connected with a mounting bracket; The mounting bracket is provided with a swing plate, the swing mechanism is arranged on the mounting bracket and connected with the swing plate; The bottom surface of the swing plate is provided with a plurality of mounting columns, the bottom end of the mounting column is provided with a hook, one side of the mounting column is provided with a support plate, one side of the support plate is rotatably connected with a rotating shaft, the rotating shaft is connected with a baffle, and the baffle abuts against the hook; The drive mechanism is arranged on the swing plate and connected with a plurality of rotating shafts respectively; The electroplating tank is arranged on the base.
2. The aerospace part electroplating apparatus of claim 1, wherein, The swing mechanism comprises a fixing frame, two rotating plates, a driver, a mounting shaft, a moving rod, a connecting rod, a swing plate and two swing shafts, wherein, The fixing frame is connected with the mounting bracket, the two rotating plates are arranged in the fixing frame respectively, the driver is arranged on the fixing frame and connected with the rotating plates, one end of the mounting shaft is connected with one of the rotating plates, and the other end is rotatably connected with the fixing frame; The moving rod penetrates through the two rotating plates and is connected with the connecting rod, the moving rod is slidably connected with the rotating plates, the swing plate is connected with the connecting rod, and the two swing shafts are connected with the two sides of the swing plate respectively, the two swing shafts are rotatably connected with the mounting bracket respectively, and the swing shafts are connected with the swing plate through the mounting bracket.
3. The aerospace part electroplating apparatus of claim 1, wherein, The drive mechanism comprises a support plate, an electric push rod, a rack, a plurality of gears and a support assembly, wherein, The support plate is arranged on the swing plate, the electric push rod is arranged on the support plate, the rack is connected with the piston end of the electric push rod, a plurality of gears are arranged on a plurality of rotating shafts respectively and engaged with the rack respectively, the support assembly is arranged on the swing plate, and the rack is slidably connected with the support assembly.
4. The aerospace part electroplating apparatus of claim 3, wherein, The support assembly comprises a T-shaped sliding groove and a T-shaped sliding plate, wherein, The T-shaped sliding groove is arranged on the swing plate, the T-shaped sliding plate is connected with the rack and slidably connected with the T-shaped sliding groove.
5. The aerospace part electroplating apparatus of claim 1, wherein, An observation window is arranged on the electroplating tank.