CN215251307U

CN215251307U - Coating electroplating device for finish machining of aviation parts

Info

Publication number: CN215251307U
Application number: CN202121443175.1U
Authority: CN
Inventors: 吴林; 王延寿; 王会琼
Original assignee: Guizhou Xiangcheng Jiahe Machinery Manufacturing Co ltd
Current assignee: Guizhou Xiangcheng Jiahe Machinery Manufacturing Co ltd
Priority date: 2021-06-28
Filing date: 2021-06-28
Publication date: 2021-12-21
Anticipated expiration: 2031-06-28

Abstract

The utility model discloses an aviation spare part finish machining is with coating electroplating device, the on-line screen storage device comprises a base, the top fixed mounting of base has electroplating bath and clean water basin, and the top of electroplating bath and the top of clean water basin are the opening structure, and the top fixed mounting of base has four stands, and four stands are two bisymmetry settings, and the top fixed mounting of four stands has same fixed diaphragm, and the spout has been seted up to the bottom of fixed diaphragm, is provided with the lead screw in the spout, and the thread bush is equipped with the slide on the lead screw. The utility model relates to a rationally, the practicality is good, can carry out electroplating process to a plurality of aviation spare parts simultaneously, can carry out even electroplating treatment to a plurality of aviation spare part surfaces, improved the electroplating quality to aviation spare part to be convenient for carry out quick effectual washing and heat drying treatment to electroplating good aviation spare part surface, the simple operation has reduced staff's the amount of labour, has improved work efficiency.

Description

Coating electroplating device for finish machining of aviation parts

Technical Field

The utility model relates to an aviation spare part processing technology field specifically is an aviation spare part finish machining is with coating electroplating device.

Background

Electroplating refers to a process of plating a thin layer of other metals or alloys on the surface of some metals by using an electrolysis principle, and is a process of adhering a layer of metal film on the surface of a metal or other material workpiece by using an electrolysis effect.

However, in the prior art, when a common coating electroplating device for finish machining of aviation parts is used, electroplating processing cannot be simultaneously performed on a plurality of aviation parts, electroplating on the surfaces of the aviation parts is uneven, so that the electroplating quality of the aviation parts is poor, the electroplating device does not have the functions of cleaning, heating and drying the surfaces of the electroplated aviation parts, and workers are required to take down the electroplated aviation parts and then manually operate and clean the aviation parts, and then naturally dry the aviation parts, so that the labor capacity of the workers is increased, time is wasted, and the working efficiency is reduced.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model is not enough to prior art, the utility model provides an aviation spare part is coating electroplating device for finish machining, solved current aviation spare part is coating electroplating device for finish machining when using, can not electroplate simultaneously to a plurality of aviation spare parts and process, it is inhomogeneous to electroplate aviation spare part surface, lead to relatively poor to the electroplating quality of aviation spare part, and do not have the function of wasing and heat drying to electroplating good aviation spare part surface, still need the staff to carry out manual operation and wash and carry out nature sunning again dry, staff's the amount of labour has been increased, waste time, lead to the problem that work efficiency reduces.

(II) technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: a coating electroplating device for finish machining of aviation parts comprises a base, wherein an electroplating pool and a clean water pool are fixedly installed at the top of the base, the top of the electroplating pool and the top of the clean water pool are both of an open structure, four stand columns are fixedly installed at the top of the base and are arranged symmetrically in pairs, the top ends of the four stand columns are fixedly installed with a same fixed transverse plate, a sliding groove is formed in the bottom of the fixed transverse plate, a lead screw is arranged in the sliding groove, a sliding seat is sleeved on the lead screw in a threaded manner, a groove is formed in the inner wall of one side of the sliding groove, a first motor is fixedly installed in the groove, one end of the lead screw extends into the groove and is fixedly connected with an output shaft end of the first motor, a cylinder is fixedly installed at the bottom of the sliding seat and extends out of the sliding groove, a telescopic column is fixedly installed at the output shaft end of the cylinder, a connecting plate is fixedly installed at the bottom of the telescopic column, two vertical plates are fixedly installed at the bottom of the connecting plate, the bottom fixed mounting of two risers has same mounting panel, and the mounting hole has been seted up at the top of mounting panel, and the hollow shaft is installed in the mounting hole rotation, and outside the both ends of hollow shaft all extended to the mounting hole, the bottom fixed mounting of hollow shaft has the disc, and the bottom fixed mounting of disc has a plurality of rings, and a plurality of rings are the array and arrange, and the top of mounting panel is provided with drive assembly.

Preferably, the transmission assembly comprises a second motor, a driving straight gear and a driven straight gear, the second motor is fixedly installed at the top of the mounting plate, the driving straight gear is fixedly installed at the output shaft end of the second motor, the driven straight gear is fixedly sleeved on the hollow shaft and is located above the mounting plate, and the driven straight gear is meshed with the driving straight gear.

Preferably, a cavity is formed in the hanging ring, the hollow shaft is communicated with the cavity, a plurality of air outlet holes are formed in the inner wall of the bottom of the cavity at equal intervals, the heater unit is fixedly installed at the top of the installation plate, an air suction pipe is fixedly installed at the suction end of the heater unit, an exhaust pipe is fixedly installed at the exhaust end of the heater unit, and one end, away from the heater unit, of the exhaust pipe extends into the hollow shaft.

Preferably, a sealing ring is fixedly mounted on the inner wall of the hollow shaft, and the exhaust pipe is in rotary sealing fit with the hollow shaft through the sealing ring.

Preferably, a guide rod is fixedly installed in the sliding groove, the sliding seat is sleeved on the guide rod in a sliding mode, a bearing seat is fixedly installed on the inner wall of one side, away from the first motor, of the sliding groove, and one end, away from the first motor, of the screw rod is rotatably installed on the bearing seat.

Preferably, the hollow shaft is fixedly sleeved with a bearing, and an outer ring of the bearing is fixedly connected with the inner wall of the mounting hole.

(III) advantageous effects

The utility model provides a coating electroplating device for fine machining of aviation parts. The method has the following beneficial effects:

(1) this aviation spare part finish machining is with coating electroplating device, through setting up a plurality of rings, can hang a plurality of aviation spare parts that wait to plate on corresponding ring, through starting cylinder work, the vertical downstream of aviation spare part that steerable a plurality of hooks are good, make the equal submergence of a plurality of aviation spare parts in the plating solution in the electroplating bath, can electroplate processing to a plurality of aviation spare parts, in electroplating process, through starting second motor work, steerable hollow shaft, the disc, a plurality of rings and a plurality of aviation spare parts carry out low-speed horizontal rotation, make a plurality of aviation spare parts slowly take place to move in the plating solution, make a plurality of aviation spare parts can fully contact with the plating solution, can carry out even electroplating treatment to a plurality of aviation spare part surfaces, thereby the electroplating quality to a plurality of aviation spare parts has been improved.

(2) This device is electroplated with coating to fine processing of aviation spare part, reset work through opening the cylinder, can remove a plurality of aviation spare parts of accomplishing of electroplating to the top of electroplating the pond, through starting first motor corotation, can remove a plurality of aviation spare parts of accomplishing of electroplating directly over the clear water pond, restart cylinder work, can drop a plurality of aviation spare parts of accomplishing of electroplating to the clear water in the clear water pond, can wash a plurality of aviation spare parts surfaces of accomplishing of electroplating, through starting second motor work, the slow motion that takes place in steerable a plurality of aviation spare parts of accomplishing of electroplating carried the clear water, make a plurality of surfaces of accomplishing of electroplating can be fully contacted with the clear water, thereby it is good to a plurality of good aviation spare parts's of electroplating cleaning performance, the sanitization.

(3) This device is electroplated with coating to fine processing of aviation spare part, reset work through starting the cylinder, can rise the top of a plurality of aviation spare parts of sanitization to the clean water basin, through opening electric fan heater work, controllable hot-air is discharged from a plurality of ventholes, blow to aviation spare part surface from a plurality of venthole exhaust hot-air, can blow off the remaining water stain on aviation spare part surface, and can heat the stoving to aviation spare part surface, utilize the hollow shaft to drive the disc, a plurality of rings and a plurality of aviation spare part level are slowly rotatory, make a plurality of aviation spare parts can fully contact with hot-air, accelerate the drying on aviation spare part surface.

Drawings

FIG. 1 is a schematic perspective view of the present invention;

FIG. 2 is a schematic sectional view of the front view of the present invention;

fig. 3 is an enlarged schematic view of a portion a in fig. 2.

In the figure: 1. a base; 2. an electroplating pool; 3. a clean water tank; 4. a column; 5. fixing the transverse plate; 6. a chute; 7. a screw rod; 8. a slide base; 9. a first motor; 10. a cylinder; 11. a telescopic column; 12. a connecting plate; 13. a vertical plate; 14. mounting a plate; 15. mounting holes; 16. a hollow shaft; 17. a disc; 18. a hoisting ring; 19. a cavity; 20. an air outlet; 21. a warm air blower; 22. an exhaust pipe; 23. a second motor; 24. a driving spur gear; 25. a driven spur gear.

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.

As shown in fig. 1-3, the utility model provides a technical solution: a coating electroplating device for finish machining of aviation parts comprises a base 1, wherein an electroplating pool 2 and a clean water pool 3 are fixedly installed at the top of the base 1, the top of the electroplating pool 2 and the top of the clean water pool 3 are both of an open structure, four stand columns 4 are fixedly installed at the top of the base 1, the four stand columns 4 are symmetrically arranged in pairs, the top ends of the four stand columns 4 are fixedly provided with a same fixed transverse plate 5, the bottom of the fixed transverse plate 5 is provided with a chute 6, a screw rod 7 is arranged in the chute 6, a slide seat 8 is sleeved on the screw rod 7 in a threaded manner, a groove is formed in the inner wall of one side of the chute 6, a first motor 9 is fixedly installed in the groove, one end of the screw rod 7 extends into the groove and is fixedly connected with an output shaft end of the first motor 9, the bottom of the slide seat 8 extends out of the chute 6 and is fixedly provided with a cylinder 10, and an extension column 11 is fixedly installed at the output shaft end of the cylinder 10, the bottom end of the telescopic column 11 is fixedly provided with a connecting plate 12, the bottom of the connecting plate 12 is fixedly provided with two vertical plates 13, the bottom of the two vertical plates 13 is fixedly provided with a same mounting plate 14, the top of the mounting plate 14 is provided with a mounting hole 15, a hollow shaft 16 is rotatably arranged in the mounting hole 15, both ends of the hollow shaft 16 extend out of the mounting hole 15, the bottom end of the hollow shaft 16 is fixedly provided with a disc 17, the bottom of the disc 17 is fixedly provided with a plurality of hanging rings 18, the plurality of hanging rings 18 are arranged in an array manner, the top of the mounting plate 14 is provided with a transmission assembly, the electroplating pool 2 is arranged to facilitate the storage of electroplating liquid, the clear water pool 3 is arranged to facilitate the storage of clear water, the cylinder 10 is arranged to facilitate the control of the lifting of the connecting plate 12, the two vertical plates 13, the mounting plate 14, the hollow shaft 16, the disc 17 and the plurality of hanging rings 18, and the plurality of aviation parts to be plated are conveniently hooked on the corresponding hanging rings 18, electroplating treatment is conveniently carried out on a plurality of aviation parts simultaneously, and the hollow shaft 16, the disc 17 and the rings 18 can be controlled to rotate horizontally by arranging the transmission assembly.

In this embodiment, the transmission assembly includes second motor 23, driving spur gear 24 and driven spur gear 25, second motor 23 is installed and is fixed at the top of mounting panel 14, driving spur gear 24 is installed and is fixed at the output shaft end of second motor 23, driven spur gear 25 is fixed the cover and is established on hollow shaft 16, driven spur gear 25 is located the top of mounting panel 14, driven spur gear 25 meshes with driving spur gear 24 mutually, through the meshing transmission that utilizes driving spur gear 24 and driven spur gear 25, steerable hollow shaft 16 rotates, make hollow shaft 16 can drive disc 17 and a plurality of rings 18 and carry out the horizontal rotation.

In this embodiment, cavity 19 has been seted up in rings 18, hollow shaft 16 is linked together with cavity 19, a plurality of ventholes 20 have been seted up to equidistant on the bottom inner wall of cavity 19, the top fixed mounting of mounting panel 14 has electric fan heater 21, the suction end fixed mounting of electric fan heater 21 has the breathing pipe, the exhaust end fixed mounting of electric fan heater 21 has exhaust pipe 22, the one end that electric fan heater 21 was kept away from to exhaust pipe 22 extends to in the hollow shaft 16, through opening electric fan heater 21, can discharge hot-air into cavity 19, make hot-air can discharge from a plurality of ventholes 20, can realize carrying out heating drying process to the plated item after the washing.

In this embodiment, a sealing ring is fixedly installed on the inner wall of the hollow shaft 16, the exhaust pipe 22 is in rotary sealing fit with the hollow shaft 16 through the sealing ring, and by arranging the sealing ring, the gap between the exhaust pipe 22 and the hollow shaft 16 is sealed, so that the hot air is prevented from being discharged from the gap between the exhaust pipe 22 and the hollow shaft 16.

In this embodiment, fixed mounting has the guide bar in the spout 6, slide 8 slip cap is established on the guide bar, fixed mounting has the bearing frame on the one side inner wall that first motor 9 was kept away from to spout 6, the one end that first motor 9 was kept away from to lead screw 7 is rotated and is installed on the bearing frame, through setting up the guide bar, play and carry out the effect of leading to the slip direction of slide 8, make slide 8 can carry out horizontal slip in spout 6, through setting up the bearing frame, play and support and the effect of location the mounted position of lead screw 7, make lead screw 7 can carry out steady smooth and easy rotation in spout 6.

In this embodiment, the hollow shaft 16 is fixedly sleeved with a bearing, the outer ring of the bearing is fixedly connected with the inner wall of the mounting hole, and the bearing is arranged to effectively support and position the mounting position of the hollow shaft 16, so that the hollow shaft 16 can smoothly rotate in the mounting hole

In this embodiment, the first motor 9 is a motor capable of rotating forward and backward, the second motor 23 is a low-speed motor, the fixed transverse plate 5 is provided with the control switch and the external power line, the first motor 9, the cylinder 10, the second motor 23, the control switch and the external power line sequentially pass through the wire electrical connection to form a loop, the control switch can control the start and stop and the forward and backward rotation of the first motor 9, the start and stop and the reset of the cylinder 10, and the start and stop of the second motor 23 can be controlled.

When the electroplating device works, a plurality of aviation parts to be plated are respectively hooked on the corresponding lifting rings 18, then the cylinder 10 is started to work, the telescopic column 11 is enabled to push the connecting plate 12, the two vertical plates 13, the mounting plate 14, the hollow shaft 16, the disc 17, the plurality of lifting rings 18 and the plurality of hooked aviation parts to vertically move downwards, when the plurality of aviation parts are all immersed in electroplating solution in the electroplating pool 2, the cylinder 10 is stopped to work, electroplating processing can be carried out on the plurality of aviation parts, in the electroplating process, the second motor 23 is started to work, the second motor 23 drives the driving straight gear 24 to rotate at a low speed, the driving straight gear 24 drives the driven straight gear 25 and the hollow shaft 16, the disc 17, the plurality of lifting rings 18 and the plurality of aviation parts to rotate horizontally at a low speed, the plurality of aviation parts slowly move in the electroplating solution, and the plurality of aviation parts can be fully contacted with the electroplating solution, the electroplating device can evenly electroplate the surfaces of a plurality of aviation parts, thereby improving the electroplating quality of the aviation parts, after the aviation parts are electroplated, the second motor 23 stops working, the cylinder 10 is started to reset, the telescopic column 11 drives the connecting plate 12, the two vertical plates 13, the mounting plate 14, the hollow shaft 16, the disc 17, the rings 18 and the aviation parts which are hooked to move vertically upwards, when the aviation parts which are electroplated all move to the upper part of the electroplating pool 2, the cylinder 10 stops working, the first motor 9 is started to rotate forwards, the first motor 9 drives the screw rod 7 to rotate, as the screw rod 7 is in threaded connection and matching with the sliding seat 8, the sliding seat 8 drives the cylinder 10, the connecting plate 12, the two vertical plates 13, the mounting plate 14, the hollow shaft 16, the disc 17, the rings 18 and the aviation parts which are electroplated to move horizontally to the right under the guiding action of the guide rod, when a plurality of electroplated aviation parts are moved to be right above a clean water tank 3, the first motor 9 is stopped, then the cylinder 10 is started to work again, the electroplated aviation parts are lowered into clean water in the clean water tank 3, the surfaces of the electroplated aviation parts can be cleaned, the second motor 23 is started to work, the electroplated aviation parts can be controlled to slowly move in the clean water carried by the electroplated aviation parts under the meshing transmission of the driving straight gear 24 and the driven straight gear 25, the surfaces of the electroplated aviation parts can be fully contacted with the clean water, the cleaning effect on the electroplated aviation parts is good, the aviation parts are cleaned, after the cleaning is finished, the cylinder 10 is started to reset, the aviation parts are lifted to be above the clean water tank 3, then the fan heater 21 is started to work, and hot air sequentially passes through the exhaust pipe 22, The hollow shaft 16 enters the cavity 19, hot air entering the cavity 19 is discharged from the air outlets 20, the hot air discharged from the air outlets 20 is blown to the surface of the aviation part, water stains remained on the surface of the aviation part can be blown off, the surface of the aviation part can be heated and dried, the hollow shaft 16 is used for driving the disc 17, the hanging rings 18 and the aviation parts to horizontally and slowly rotate, the aviation parts can be fully contacted with the hot air, the drying of the surface of the aviation part is accelerated, after the drying of the aviation parts is completed, the second motor 23 and the heater 21 are stopped, the electroplating and drying completed aviation parts can be sequentially taken down, the first motor 9 is started to reversely rotate, the first motor 9 drives the screw rod 7 to reversely rotate, so that the cylinder 8 drives the cylinder 10, the connecting plate 12, the two vertical plates 13 and the mounting plate 14, The hollow shaft 16, the disc 17 and the plurality of hanging rings 18 horizontally move leftwards, when the plurality of hanging rings 18 are moved to be right above the electroplating pool, the first motor 9 is stopped to work, and then electroplating, cleaning and heating drying treatment can be carried out on the next batch of aviation parts according to the operation steps, and the content which is not described in detail in the specification belongs to the prior art which is well known by a person skilled in the art.

To sum up, can obtain, this aviation spare part finish machining is with coating electroplating device can carry out electroplating process to a plurality of aviation spare parts simultaneously, can carry out even electroplating treatment to a plurality of aviation spare part surfaces, has improved the electroplating quality to aviation spare part to be convenient for carry out quick effectual washing and heat drying treatment to electroplating good aviation spare part surface, the simple operation has reduced staff's the amount of labour, has improved work efficiency.

Claims

1. The utility model provides an aviation spare part finish machining is with coating electroplating device, includes base (1), its characterized in that: the top of the base (1) is fixedly provided with an electroplating pool (2) and a clean water pool (3), the top of the electroplating pool (2) and the top of the clean water pool (3) are both of an open structure, the top of the base (1) is fixedly provided with four stand columns (4), the four stand columns (4) are arranged in a pairwise symmetry manner, the top ends of the four stand columns (4) are fixedly provided with a same fixed transverse plate (5), the bottom of the fixed transverse plate (5) is provided with a sliding groove (6), a screw rod (7) is arranged in the sliding groove (6), a sliding seat (8) is sleeved on the screw rod (7) in a threaded manner, a groove is formed in the inner wall of one side of the sliding groove (6), a first motor (9) is fixedly arranged in the groove, one end of the screw rod (7) extends into the groove and is fixedly connected with an output shaft end of the first motor (9), the bottom of the sliding seat (8) extends out of the sliding groove (6) and is fixedly provided with an air cylinder (10), an output shaft end of the cylinder (10) is fixedly provided with a telescopic column (11), the bottom end of the telescopic column (11) is fixedly provided with a connecting plate (12), two vertical plates (13) are fixedly arranged at the bottom of the connecting plate (12), the same mounting plate (14) is fixedly arranged at the bottoms of the two vertical plates (13), the top of the mounting plate (14) is provided with a mounting hole (15), a hollow shaft (16) is rotatably mounted in the mounting hole (15), both ends of the hollow shaft (16) extend out of the mounting hole (15), the bottom fixed mounting of hollow shaft (16) has disc (17), the bottom fixed mounting of disc (17) has a plurality of rings (18), and is a plurality of rings (18) are the array and arrange, the top of mounting panel (14) is provided with drive assembly.

2. The coating electroplating device for finishing the aviation parts as claimed in claim 1, wherein: the transmission assembly comprises a second motor (23), a driving straight gear (24) and a driven straight gear (25), the second motor (23) is installed and fixed at the top of the mounting plate (14), the driving straight gear (24) is installed and fixed at the output shaft end of the second motor (23), the driven straight gear (25) is fixedly sleeved on the hollow shaft (16), the driven straight gear (25) is located above the mounting plate (14), and the driven straight gear (25) is meshed with the driving straight gear (24).

3. The coating electroplating device for finishing the aviation parts as claimed in claim 1, wherein: seted up cavity (19) in rings (18), hollow shaft (16) with cavity (19) are linked together, a plurality of ventholes (20) have been seted up to the equidistant bottom inner wall of cavity (19), the top fixed mounting of mounting panel (14) has electric fan heater (21), the suction end fixed mounting of electric fan heater (21) has the breathing pipe, the discharge end fixed mounting of electric fan heater (21) has blast pipe (22), the one end that electric fan heater (21) were kept away from in blast pipe (22) extends to in hollow shaft (16).

4. A coating electroplating device for finishing an aviation part according to claim 3, wherein: the inner wall of the hollow shaft (16) is fixedly provided with a sealing ring, and the exhaust pipe (22) is in rotary sealing fit with the hollow shaft (16) through the sealing ring.

5. The coating electroplating device for finishing the aviation parts as claimed in claim 1, wherein: fixed mounting has the guide bar in spout (6), slide (8) slip cover is established on the guide bar, spout (6) are kept away from fixed mounting has the bearing frame on one side inner wall of first motor (9), the one end that first motor (9) were kept away from in lead screw (7) is rotated and is installed on the bearing frame.

6. The coating electroplating device for finishing the aviation parts as claimed in claim 1, wherein: the hollow shaft (16) is fixedly sleeved with a bearing, and the outer ring of the bearing is fixedly connected with the inner wall of the mounting hole.