A dust removal device for aircraft parts production

By combining vibration, cleaning, and dust removal components, the problem of low dust removal efficiency in existing devices is solved, achieving efficient cleaning of aerospace parts surfaces and improving production efficiency.

CN224423728UActive Publication Date: 2026-06-30CHENGDU TIANQI RUIHE AEROSPACE EQUIP INTELLIGENT MFG CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
CHENGDU TIANQI RUIHE AEROSPACE EQUIP INTELLIGENT MFG CO LTD
Filing Date
2025-07-23
Publication Date
2026-06-30

AI Technical Summary

Technical Problem

Existing dust removal equipment in aerospace parts production has low dust removal efficiency and cannot effectively remove iron filings and dust from the surface of parts, thus affecting production efficiency.

Method used

It adopts a combined structure of vibration component, cleaning component and dust removal component. The motor drives components such as pinion, gear, cam, and connecting rod to drive the vibration plate to vibrate. Combined with high-pressure nozzle cleaning and dust removal brush, it realizes the coordinated operation of multiple dust removal methods.

Benefits of technology

It improves the dust removal efficiency and cleanliness of aerospace parts, thereby increasing production and processing efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

This utility model relates to the field of aerospace parts manufacturing technology, specifically a dust removal device for aircraft parts manufacturing. It includes a dust removal tank, an installation box fixedly mounted on the outside of the dust removal tank, a water tank fixedly connected to the top of the installation box, a cleaning component fixedly mounted on one side of the water tank, a column fixedly connected inside the dust removal tank, a waterproof frame fixedly connected to the top of the column, a vibration component inside the waterproof frame, dust removal components fixedly mounted inside both the dust removal tank and the installation box, a vibrating plate movably mounted inside the dust removal tank, through holes evenly distributed inside the vibrating plate, vibration springs symmetrically fixedly connected to the bottom of the vibrating plate, and multiple vibration springs having their other ends fixedly connected to the waterproof frame, a drain pipe fixedly connected to the bottom of the dust removal tank, and a control panel fixedly mounted on the outside of the installation box. This utility model includes a vibration component to facilitate the vibration of the vibrating plate, thereby shaking off dust from the surface of the aerospace parts, helping to keep the aerospace parts clean and tidy.
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Description

Technical Field

[0001] This utility model relates to the field of aerospace parts manufacturing technology, specifically a dust removal device for aircraft parts manufacturing. Background Technology

[0002] Aircraft engaged in flight activities, also known as aircraft, are divided into two categories: lighter-than-air aircraft and heavier-than-air aircraft. The former rely on static buoyancy to take off, such as balloons or airships, while the latter rely on aerodynamic forces generated by relative motion with the air, such as airplanes or helicopters. They are all composed of different aircraft parts. During the production and processing of aircraft parts, grinding and cutting are required. During these processes, a large amount of iron filings and dust will adhere to the surface of the aircraft parts. Therefore, dust removal equipment is needed to remove dust from the surface of the aircraft parts.

[0003] Most existing dust removal devices used in aircraft parts production have a single dust removal structure and cannot effectively remove dust from aircraft parts. During use, the dust removal efficiency of aircraft parts is low, thereby reducing the efficiency of aircraft parts production and processing. Therefore, we propose a dust removal device for aircraft parts production. Utility Model Content

[0004] The purpose of this utility model is to provide a dust removal device for aircraft parts production, which solves the problem of low dust removal efficiency of existing dust removal devices by using a combination of vibration components, cleaning components and dust removal components.

[0005] To achieve the above objectives, this utility model provides the following technical solution:

[0006] A dust removal device for aircraft parts manufacturing includes a dust removal tank, an installation box fixedly mounted on the outside of the dust removal tank, a water tank fixedly connected to the top of the installation box, a cleaning component fixedly mounted on one side of the water tank, a column fixedly connected inside the dust removal tank, a waterproof frame fixedly connected to the top of the column, a vibration component inside the waterproof frame, dust removal components fixedly mounted inside both the dust removal tank and the installation box, a vibrating plate movably mounted inside the dust removal tank, through holes evenly distributed inside the vibrating plate, vibration springs symmetrically fixedly connected to the bottom of the vibrating plate, the other ends of multiple vibration springs fixedly connected to the waterproof frame, a drain pipe fixedly connected to the bottom of the dust removal tank, and a control panel fixedly mounted on the outside of the installation box.

[0007] Preferably, the cleaning assembly includes a water pump, which is fixedly installed on the top of the mounting box. An input pipe is fixedly connected to the input end of the water pump, and an output pipe is fixedly connected to the output end of the water pump. A connecting pipe is fixedly connected to the other end of the output pipe. A water outlet pipe is fixedly connected to the end of the connecting pipe away from the output pipe through the dust removal tank. High-pressure nozzles are uniformly and symmetrically fixedly connected to the outside of the water outlet pipe, and the water outlet pipe is fixedly connected to the dust removal tank.

[0008] Preferably, the vibration assembly includes a motor, which is fixedly mounted on the inner wall of the mounting box. A small gear is fixedly connected to the output end of the motor, and a large gear is meshed with the outside of the small gear. A rotating rod is fixedly connected inside the large gear. One end of the rotating rod is rotatably connected to the inner wall of the mounting box, and the other end of the rotating rod passes through the dust removal tank and is rotatably connected to the side wall of the dust removal tank.

[0009] Preferably, the rotating rod is symmetrically fixedly connected to the outside of a cam, and a connecting rod is rotatably connected inside each of the two cams. The end of the connecting rod away from the cam is rotatably connected to a slider, and the other end of the slider is slidably connected to a sleeve block.

[0010] Preferably, a vertical rod is fixedly connected inside the sleeve block, a protrusion is fixedly connected to one end of the vertical rod away from the sleeve block, a compression spring is fixedly connected to the top of the protrusion, the other end of the compression spring is fixedly connected to the top of the slider, and the sleeve block is fixedly connected to the vibration plate.

[0011] Preferably, the dust removal assembly includes a drive wheel, which is fixedly connected to the output end of the motor, and a driven wheel is rotatably connected to the side wall of the mounting box. Belts are synchronously provided on the outside of the drive wheel and the driven wheel.

[0012] Preferably, both the driving wheel and the driven wheel are provided with a rotating shaft inside. Both rotating shafts pass through the outside of the dust removal tank and are fixedly connected to a dust removal brush. The other end of both rotating shafts is rotatably connected to the side wall of the dust removal tank.

[0013] Compared with the prior art, the beneficial effects of this utility model are:

[0014] 1. This solution includes a vibration assembly, which works in conjunction with a motor, pinion, gear, cam, connecting rod, slider, sleeve, vertical rod, protrusion, and compression spring to drive the vibration plate to vibrate, thereby shaking off dust from the surface of aerospace parts and keeping them clean and tidy.

[0015] 2. This solution is equipped with a dust removal component and a cleaning component. Driven by a motor, the drive wheel rotates via a belt, which in turn drives the rotating shaft and dust removal brush to rotate, thus removing dust from the aerospace parts. At the same time, the cleaning component cleans the aerospace parts, which can further keep the aerospace parts clean and tidy, improve the dust removal efficiency of the parts, and thus improve the production and processing efficiency of aerospace parts. Attached Figure Description

[0016] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0017] Figure 2 This is a front sectional view of the overall structure of this utility model;

[0018] Figure 3 This is a sectional view of the mounting box of this utility model;

[0019] Figure 4 This is a side sectional view of the entire utility model;

[0020] Figure 5 This is a cross-sectional view of the vibration component structure of this utility model.

[0021] The components represented by each number in the attached diagram are listed below: 1. Dust collection tank; 2. Mounting box; 3. Water tank; 4. Cleaning assembly; 401. Water pump; 402. Inlet pipe; 403. Outlet pipe; 404. Connecting pipe; 405. Water outlet pipe; 406. High-pressure nozzle; 5. Vibration assembly; 501. Motor; 502. Pinion; 503. Gear; 504. Rotating rod; 505. Cam; 506. Connecting rod; 507. Slider; 508. Sleeve block; 509. Vertical rod; 510. Protrusion; 511. Compression spring; 6. Dust collection assembly; 601. Drive wheel; 602. Belt; 603. Driven wheel; 604. Rotating shaft; 605. Dust brush; 7. Column; 8. Waterproof frame; 9. Vibration spring; 10. Vibration plate; 11. Through hole; 12. Drain pipe; 13. Control panel. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments.

[0023] like Figures 1-5As shown in the figure, a dust removal device for aircraft parts manufacturing includes a dust removal tank 1. The dust removal tank 1 has legs at its bottom and is made of stainless steel. Shock-absorbing pads are fixed to the bottom of each of the legs. An installation box 2 is fixedly installed outside the dust removal tank 1. A water tank 3, made of plastic, is fixedly connected to the top of the installation box 2. A cleaning component 4 is fixedly installed on one side of the water tank 3. The cleaning component 4 is used to clean the aircraft parts. Specifically, the cleaning component 4 includes a water pump 401. The specific model of the water pump 401 is selected according to the actual situation. The water pump 401 is a cleaning... The washing assembly 4 provides the power source. A water pump 401 is fixedly installed on the top of the mounting box 2. An input pipe 402 is fixedly connected to the input end of the water pump 401, and an output pipe 403 is fixedly connected to the output end of the water pump 401. A connecting pipe 404 is fixedly connected to the other end of the output pipe 403. A water outlet pipe 405 is fixedly connected to the end of the connecting pipe 404 away from the output pipe 403, passing through the dust collection tank 1. High-pressure nozzles 406 are evenly and symmetrically fixed to the outside of the water outlet pipe 405. The water outlet pipe 405 is fixedly connected to the dust collection tank 1. Water from the water tank 3 is pumped through the water pump 401. The input pipe 402 and output pipe 403 deliver water to the inside of the connecting pipe 404, and then clean the aircraft parts through the water outlet pipe 405 and high-pressure nozzle 406, which helps to improve the cleaning efficiency of aircraft parts. A column 7 is fixedly connected inside the dust removal tank 1, and a waterproof frame 8 is fixedly connected to the top of the column 7. Both the column 7 and the waterproof frame 8 are made of waterproof material. A vibration component 5 is installed inside the waterproof frame 8 to shake off dust from the surface of the aircraft parts, facilitating dust removal. Dust removal components 6 are fixedly installed inside both the dust removal tank 1 and the mounting box 2. The internal movable part of the dust removal tank 1... There is a vibrating plate 10. In order to better clean the aviation parts, a tray can be provided on the surface of the vibrating plate 10. The vibrating plate 10 has through holes 11 evenly opened inside. Vibrating springs 9 are symmetrically fixedly connected to the bottom of the vibrating plate 10. There are two sets of vibrating springs 9, which are symmetrically arranged. The other end of the multiple vibrating springs 9 is fixedly connected to the waterproof frame 8, which can increase the stability of the vibrating plate 10 and facilitate vibration. The bottom of the dust removal tank 1 is fixedly connected to the drain pipe 12. The drain pipe 12 is provided with a drain valve on the outside. The control panel 13 is fixedly installed on the outside of the mounting box 2.

[0024] For further details, please refer to Figure 2 , Figure 3 and Figure 5The vibration assembly 5 includes a motor 501. The specific model of the motor 501 is selected according to the actual situation. The motor 501 provides the power source for the vibration assembly 5. The motor 501 is fixedly installed on the inner wall of the mounting box 2. A small gear 502 is fixedly connected to the output end of the motor 501. A large gear 503 is meshed externally with the small gear 502. A rotating rod 504 is fixedly connected internally to the large gear 503. One end of the rotating rod 504 is rotatably connected to the inner wall of the mounting box 2, and the other end of the rotating rod 504 passes through the dust collection tank 1 and is rotatably connected to the side wall of the dust collection tank 1. Specifically, cams 505 are symmetrically fixedly connected to the outside of the rotating rod 504. A connecting rod 506 is rotatably connected to the inside of each of the two cams 505. The end of the connecting rod 506 away from the cam 505 is rotatably connected to a slider 507. The other end of the slider 507 is slidably connected to a sleeve block 508. A vertical rod 509 is fixedly connected internally to the sleeve block 508. A protrusion 510 is fixedly connected to the end of the vertical rod 509 away from the sleeve block 508. A compression spring 511 is fixedly connected to the top of the protrusion 510. The other end of the compression spring 511 is fixedly connected to the top of the slider 507. The sleeve block 508 is fixedly connected to the vibrating plate 10. The rotation of the motor 501 drives the small gear 502 to rotate, which in turn drives the large gear 503 and the rotating rod 504 to rotate, thereby driving the cam 505 to rotate, which in turn drives the connecting rod 506 to move, thereby driving the slider 507 to slide along the sleeve block 508. At the same time, the slider 507 hits the protrusion 510, and then the compression spring 511 and the vertical rod 509, together with the vibration spring 9, drive the vibrating plate 10 to vibrate, which is convenient for shaking off the dust on the surface of the aviation parts. At the same time, the vibration can be performed on the aviation parts after the cleaning component 4 has finished cleaning, which can shake off the surface water stains, thereby improving the dust removal efficiency and the production and processing efficiency of aviation parts.

[0025] Specifically, please refer to Figure 2 and Figure 3 The dust removal assembly 6 includes a drive wheel 601, which is fixedly connected to the output end of the motor 501. A driven wheel 603 is rotatably connected to the side wall of the mounting box 2. Belts 602 are synchronously provided on the outside of the drive wheel 601 and the driven wheel 603. A rotating shaft 604 is provided inside both the drive wheel 601 and the driven wheel 603. Dust removal brushes 605 are fixedly connected to the outside of the dust removal tank 1 through both rotating shafts 604. The dust removal brushes 605 can be made of nylon bristles, which are durable and have strong cleaning power. Various hardnesses can be selected, and other materials can also be selected according to needs. The other ends of the two rotating shafts 604 are rotatably connected to the side wall of the dust removal tank 1. By providing the dust removal assembly 6, fine dust on the surface of aerospace parts can be cleaned. In conjunction with the vibration assembly 5 and the cleaning assembly 4, multiple dust removal methods can be used, which helps to increase the functionality of the device and improve the dust removal efficiency, thereby improving the production and processing efficiency of aerospace parts.

[0026] In summary, when using this device, the aircraft parts to be dusted are first placed inside the dust removal tank 1. Then, the motor 501 is started via the control panel 13. The rotation of the motor 501 drives the small gear 502 to rotate, which in turn drives the large gear 503 and the rotating rod 504 to rotate, thereby driving the cam 505 to rotate, which in turn drives the connecting rod 506 to move, thereby causing the slider 507 to slide along the sleeve block 508. At the same time, the slider 507 strikes the protrusion 510, which in turn causes the compression spring 511 and the vertical rod 509 to work with the vibration spring 9 to drive the vibration plate 10 to vibrate, thus shaking off the dust from the surface of the parts. Meanwhile, driven by the motor 501, the drive wheel 601 drives the driven wheel 603 to rotate via the belt 602, which in turn drives the rotating shaft 604 and the dust removal brush 605 to rotate, thus removing dust from the parts. At the same time, the water pump 401 is started, and the water pump 401 transports the water in the water tank 3 to the inside of the connecting pipe 404 through the input pipe 402 and the output pipe 403, and then cleans the parts through the water outlet pipe 405 and the high-pressure nozzle 406. The wastewater after cleaning is temporarily stored at the bottom of the dust removal tank 1 through the through hole 11. When the wastewater inside the dust removal tank 1 is full, it can be discharged through the drain pipe 12.

[0027] It is understood that this utility model has been described through some embodiments, and those skilled in the art will recognize that various changes or equivalent substitutions can be made to these features and embodiments without departing from the spirit and scope of this utility model. Furthermore, under the teachings of this utility model, these features and embodiments can be modified to adapt to specific situations and materials without departing from the spirit and scope of this utility model. Therefore, this utility model is not limited to the specific embodiments disclosed herein, and all embodiments falling within the scope of the claims of this application are protected by this utility model.

Claims

1. Dust removal device for the production of aircraft parts, comprising a dust removal basin (1), characterized in that, An installation box (2) is fixedly installed on the outside of the dust removal tank (1). A water tank (3) is fixedly connected to the top of the installation box (2). A cleaning component (4) is fixedly installed on one side of the water tank (3). A column (7) is fixedly connected inside the dust removal tank (1). A waterproof frame (8) is fixedly connected to the top of the column (7). A vibration component (5) is provided inside the waterproof frame (8). Dust removal components (6) are fixedly installed inside both the dust removal tank (1) and the installation box (2). A vibrating plate (10) is movably installed inside the dust removal tank (1). Through holes (11) are evenly opened inside the vibrating plate (10). Vibrating springs (9) are symmetrically fixedly connected to the bottom of the vibrating plate (10). The other end of multiple vibrating springs (9) is fixedly connected to the waterproof frame (8). A drain pipe (12) is fixedly connected to the bottom of the dust removal tank (1). A control panel (13) is fixedly installed on the outside of the installation box (2).

2. A dust extraction apparatus for the production of aircraft parts as claimed in claim 1, wherein: The cleaning assembly (4) includes a water pump (401), which is fixedly installed on the top of the mounting box (2). The input end of the water pump (401) is fixedly connected to an input pipe (402), and the output end of the water pump (401) is fixedly connected to an output pipe (403). The other end of the output pipe (403) is fixedly connected to a connecting pipe (404). The end of the connecting pipe (404) away from the output pipe (403) passes through the dust removal tank (1) and is fixedly connected to a water outlet pipe (405). High-pressure nozzles (406) are evenly and symmetrically fixedly connected to the outside of the water outlet pipe (405). The water outlet pipe (405) is fixedly connected to the dust removal tank (1).

3. A dust extraction apparatus for the production of aircraft parts as claimed in claim 1, wherein: The vibration assembly (5) includes a motor (501), which is fixedly installed on the inner wall of the mounting box (2). A small gear (502) is fixedly connected to the output end of the motor (501). A large gear (503) is meshed with the outside of the small gear (502). A rotating rod (504) is fixedly connected inside the large gear (503). One end of the rotating rod (504) is rotatably connected to the inner wall of the mounting box (2), and the other end of the rotating rod (504) passes through the dust removal tank (1) and is rotatably connected to the side wall of the dust removal tank (1).

4. A dust extraction apparatus for the production of aircraft parts as claimed in claim 3, wherein: The rotating rod (504) is symmetrically fixedly connected to the outside of the cam (505), and the two cams (505) are rotatably connected to the inside of the connecting rod (506). The end of the connecting rod (506) away from the cam (505) is rotatably connected to the slider (507), and the other end of the slider (507) is slidably connected to the sleeve (508).

5. A dust extraction apparatus for the production of aircraft parts as claimed in claim 4, wherein: A vertical rod (509) is fixedly connected inside the sleeve (508). A protrusion (510) is fixedly connected to one end of the vertical rod (509) away from the sleeve (508). A compression spring (511) is fixedly connected to the top of the protrusion (510). The other end of the compression spring (511) is fixedly connected to the top of the slider (507). The sleeve (508) is fixedly connected to the vibrating plate (10).

6. A dust extraction apparatus for the production of aircraft parts as claimed in claim 3, wherein: The dust removal assembly (6) includes a drive wheel (601), which is fixedly connected to the output end of the motor (501). A driven wheel (603) is rotatably connected to the side wall of the mounting box (2). A belt (602) is synchronously provided on the outside of the drive wheel (601) and the driven wheel (603).

7. A dust extraction apparatus for the production of aircraft parts as claimed in claim 6, wherein: Both the driving wheel (601) and the driven wheel (603) are equipped with a rotating shaft (604). Both rotating shafts (604) pass through the outside of the dust removal tank (1) and are fixedly connected to a dust removal brush (605). The other end of both rotating shafts (604) is rotatably connected to the side wall of the dust removal tank (1).