Aero-engine part machining equipment

By using a motor-driven rotating frame and a lead screw to drive the cleaning tank, the problem of uneven cleaning of aero-engine components was solved, achieving efficient and flexible cleaning results and improving the cleanliness and processing quality of the components.

CN223454717UActive Publication Date: 2025-10-21JIANGSU POWER ALLIANCE IOT TECH
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Patent Information

Application Number
CN202422499872.9
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-10-16
Publication Date
2025-10-21
Estimated Expiration
2034-10-16

AI Technical Summary

Technical Problem

Existing aero-engine component processing equipment suffers from uneven cleaning and low efficiency, affecting the cleanliness and processing quality of the components.

Method used

The rotating frame is driven by motor A and the lead screw is driven by motor B to lift the cleaning tub. The design of the center hole of the rotating frame and the center column of the cleaning tub enables uniform cleaning of the components and flexible position adjustment, avoiding interference and collision.

Benefits of technology

It achieves uniform cleaning of all corners of the component surface, improving cleaning efficiency and cleanliness, and enhancing the flexibility and quality of cleaning.

✦ Generated by Eureka AI based on patent content.

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    Figure CN223454717U_ABST
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Abstract

The utility model discloses aero-engine part machining equipment which comprises a shell, a supporting frame fixedly connected to the upper surface of the shell, a motor A fixedly connected to the upper surface of the supporting frame, a rotating frame fixedly connected to the output end of the motor A through a rotating shaft, and a containing cylinder movably connected to the lower bottom wall of the rotating frame. A sealing cover is in threaded connection with the upper surface of the placing barrel, a motor B is fixedly connected to the lower surface of the shell, a lead screw is fixedly connected to the output end of the motor B, a cleaning barrel is movably connected to the side surface of the lead screw, and a pipeline is fixedly connected to the lower surface of the cleaning barrel.
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Description

TECHNICAL FIELD

[0001] The utility model relates to aviation engine component processing technical field especially relates to an aviation engine component processing equipment. BACKGROUND

[0002] In the processing of aviation engine components, cleaning is an important link for removing dirt, grease, metal chips and other impurities on the surface of the components to ensure the cleanliness of the components and the quality of subsequent processing, but the existing equipment has the problems of uneven cleaning and low cleaning efficiency, which affects the cleanliness of the aviation engine components. SUMMARY

[0003] The utility model discloses a kind of aviation engine component processing equipment, rotating frame is rotated by motor A drive, so that the aviation engine component placed in placing cylinder can be evenly and sufficiently cleaned in cleaning process, improve cleaning efficiency, ensure that each corner on the surface of the component can be effectively cleaned, it is beneficial to improve the processing quality and cleanliness of component, cleaning barrel is lifted by motor B drive screw rod, the relative position between cleaning barrel and rotating frame can be adjusted as required, the flexibility and effect of cleaning are enhanced, while the center hole of rotating frame and the center column of cleaning barrel, avoid mutual interference and collision, it is beneficial to improve cleaning quality.

[0004] The utility model further provides a kind of aviation engine component processing equipment with the above, it include: shell, the upper surface of the shell is fixedly connected with support frame, the upper surface of the support frame is fixedly connected with motor A, the output end of motor A is fixedly connected with rotating frame by rotating shaft, the lower bottom wall of rotating frame is movably connected with placing cylinder, the upper surface of placing cylinder is threadedly connected with sealing cover, the lower surface of shell is fixedly connected with motor B, the output end of motor B is fixedly connected with screw rod, the side surface of screw rod is movably connected with cleaning barrel, the lower surface of cleaning barrel is fixedly connected with pipeline, by above device, it is beneficial to improve cleaning quality.

[0005] According to the aviation engine component processing equipment, the lower bottom wall of the rotating frame is provided with a placing groove, and the bottom of the placing cylinder is located inside the placing groove.

[0006] According to the aviation engine component processing equipment, the upper surface of the rotating frame is provided with a placing opening, and the placing opening is located directly above the placing groove.

[0007] The utility model relates to an aeroengine component machining equipment, the inside of cleaning bucket is provided with the center column, the lead screw is located the inside of center column, through above device, be helpful to the lead screw drive cleaning bucket.

[0008] The utility model relates to an aeroengine component machining equipment, the inside of rotary frame is provided with the center hole, the center column is located the just below of center hole, through above device, be helpful to the center column and center hole mutual cooperation avoid the influence rotary frame's rotation.

[0009] The utility model relates to an aeroengine component machining equipment, the center hole is through the lower surface of rotary frame, and the cleaning bucket is located the just below of rotary frame, through above device, be helpful to improve the cleaning flexibility.

[0010] The utility model relates to an aeroengine component machining equipment, the pipeline is through with cleaning bucket, and the lateral surface of pipeline is provided with the valve, through above device, be helpful to control the flow of cleaning fluid.

[0011] The utility model relates to an aeroengine component machining equipment, the lower surface of shell is provided with the prop, and the lower end of prop is fixedly connected with the antiskid pad, through above device, be helpful to guarantee the stability of device.

[0012] Beneficial effect

[0013] 1, compared with prior art, the aeroengine component machining equipment of this application, through motor A drive rotary frame rotation, makes the aeroengine component placed in the placing cylinder can be evenly and sufficiently cleaned in the cleaning process, improves the cleaning efficiency, ensures that each corner of the part surface can be effectively cleaned, and is helpful to improve the processing quality and cleanliness of the part.

[0014] 2, compared with prior art, the aeroengine component machining equipment of this application, through motor B drive lead screw drive cleaning bucket lifting, can adjust the relative position between cleaning bucket and rotary frame as required, enhances the flexibility and effect of cleaning, and the center hole of rotary frame and the center column of cleaning bucket avoid mutual interference and collision, which is helpful to improve the cleaning quality. DRAWINGS

[0015] The utility model will be further described below in connection with the drawings and examples;

[0016] Figure 1 It is the perspective view of aeroengine component machining equipment of the utility model;

[0017] Figure 2 It is the internal structure diagram of aeroengine component machining equipment of the utility model;

[0018] Figure 3 It is sectional view of the aero-engine component machining equipment of the utility model.

[0019] Figure 4 It is sectional view of the aero-engine component machining equipment of the utility model.

[0020] Legend:

[0021] 1, shell, 2, support frame, 3, motor A, 4, rotating frame, 5, sealing cover, 6, support column, 7, rotating shaft, 8, placing cylinder, 9, cleaning barrel, 10, center hole, 11, center column, 12, screw rod, 13, motor B, 14, pipeline, 15, valve. DETAILED DESCRIPTION

[0022] This part will describe the specific embodiments of the utility model in detail, the preferred embodiment of the utility model is shown in the drawings, the role of the drawings is to supplement the description of the text part with graphics, so that people can intuitively and visually understand each technical feature and overall technical scheme of the utility model, but it cannot be understood as the limitation of the protection scope of the utility model.

[0023] Referring to Figures 1-4 , the utility model embodiment aero-engine component machining equipment, it includes: shell 1 as the main structure of whole equipment, provide support and protection, ensure the safe operation of equipment internal mechanical parts, the upper surface of shell 1 is fixedly connected with support frame 2, for supporting motor A 3, the upper surface of support frame 2 is fixedly connected with motor A 3 for driving rotating frame 4 rotation, the output end of motor A 3 is fixedly connected with rotating frame 4 through rotating shaft 7, for driving placing cylinder 8 rotation, the lower bottom wall of rotating frame 4 is movably connected with placing cylinder 8, for placing the component of production, the upper surface of placing cylinder 8 is threadedly connected with sealing cover 5, for closing placing barrel 8, the lower bottom wall of rotating frame 4 is provided with placing groove, for positioning placing cylinder 8, the bottom of placing cylinder 8 is located in the inside of placing groove, the upper surface of rotating frame 4 is provided with placing mouth, and the placing mouth is located directly above the placing groove, the inside of rotating frame 4 is provided with center hole 10, for cooperating with center column 11, avoid cleaning barrel 9 influence rotating frame 4 rotation, center hole 10 penetrates the lower surface of rotating frame 4.

[0024] The lower surface of the shell 1 is fixedly connected with a motor B13 for driving the screw rod 12 to rotate, the output end of the motor B13 is fixedly connected with the screw rod 12 for driving the cleaning barrel 9 to lift, the side surface of the screw rod 12 is movably connected with the cleaning barrel 9 for cleaning the production parts, the cleaning barrel 9 is located directly below the rotating frame 4, the inside of the cleaning barrel 9 is provided with a center column 11 for cooperating with the screw rod 12, the center column 11 is located directly below the center hole 10, the screw rod 12 is located inside the center column 11, the lower surface of the cleaning barrel 9 is fixedly connected with a pipeline 14 for the flow of cleaning liquid, the pipeline 14 penetrates through the cleaning barrel 9, the side surface of the pipeline 14 is provided with a valve 15 for controlling the flow of cleaning liquid, the lower surface of the shell 1 is provided with a support 6 for ensuring the stability of the device, the lower end of the support 6 is fixedly connected with an anti-skid pad for further enhancing the stability of the device.

[0025] Working principle: start the motor B13 to drive the screw rod 12 to rotate, the rotary motion of the screw rod 12 is converted into the up-down movement of the cleaning barrel 9 (containing cleaning liquid), when the cleaning barrel 9 rises to contact the rotating frame 4, the center column 11 is automatically aligned with the center hole 10, so that the rotating frame 4 is located inside the cleaning barrel 4, then stop the motor B13, then place the workpiece to be cleaned in the placing cylinder 8, and seal the upper surface of the placing cylinder 8 by screwing the sealing cover 5 thereon, start the motor A3 to drive the rotating frame 4 to rotate through the rotating shaft 7, since the placing cylinder 8 is movably connected with the rotating frame 4, the workpiece will be rotated in the cleaning liquid, so that the cleaning liquid can more evenly cover the surface of the workpiece, thereby improving the cleaning effect, after cleaning, the motor A3 is turned off, the motor B13 is started to drive the screw rod 12 to rotate, so that the cleaning barrel 9 is lowered to reset, then the motor A3 drives the rotating frame 4 again, so that the workpiece is rotated for air drying, after air drying, the waste liquid is discharged by opening the valve at the bottom of the cleaning barrel 9 or the corresponding device, then the sealing cover 5 can be removed, and the cleaned workpiece can be taken out for subsequent processing.

[0026] The above describes the embodiments of the utility model in detail in combination with the drawings, but the utility model is not limited to the above-mentioned embodiments, and various changes can be made within the knowledge range possessed by the ordinary skilled in the art without departing from the purpose of the utility model.

Claims

1. An aircraft engine component machining apparatus, characterized by, Include: The shell (1), the upper surface of the shell (1), the upper surface of the support frame (2) is fixedly connected with motor A (3), the output end of the motor A (3) is fixedly connected with rotating frame (4) through rotating shaft (7), the lower bottom wall of the rotating frame (4) is movably connected with the placement cylinder (8), the upper surface of the placement cylinder (8) is threadedly connected with the sealing cover (5), the lower surface of the shell (1) is fixedly connected with motor B (13), the output end of the motor B (13) is fixedly connected with the lead screw (12), the side surface of the lead screw (12) is movably connected with the cleaning barrel (9), the lower surface of the cleaning barrel (9) is fixedly connected with the pipeline (14).

2. An aircraft engine component machining apparatus according to claim 1, wherein, The lower bottom wall of the rotating frame (4) is provided with a placing groove, and the bottom of the placing cylinder (8) is located in the placing groove.

3. An aircraft engine component machining apparatus according to claim 2, wherein, The upper surface of the rotating frame (4) is provided with a placing opening, and the placing opening is located directly above the placing groove.

4. An aircraft engine component machining apparatus according to claim 1, wherein The inside of the cleaning barrel (9) is provided with a center column (11), and the lead screw (12) is located in the center column (11).

5. An aircraft engine component machining apparatus according to claim 4, wherein, The inside of the rotating frame (4) is provided with a center hole (10), and the center column (11) is located directly below the center hole (10).

6. An aircraft engine component machining apparatus according to claim 5, wherein, The center hole (10) penetrates the lower surface of the rotating frame (4), and the cleaning barrel (9) is located directly below the rotating frame (4).

7. An aircraft engine component machining apparatus according to claim 1, wherein The pipeline (14) is in communication with the cleaning barrel (9), and the side surface of the pipeline (14) is provided with a valve (15).

8. An aircraft engine component machining apparatus according to claim 1, wherein, The lower surface of the shell (1) is provided with a support column (6), and the lower end of the support column (6) is fixedly connected with a non-slip pad.