Aviation part grinding and polishing device

By designing an aerospace parts grinding and polishing device with adjustable polishing and clamping mechanisms, the problem of insufficient flexibility and versatility caused by different pipe diameters of the existing device is solved, and efficient processing of diversified and personalized parts is achieved. .

CN222345147UActive Publication Date: 2025-01-14SUZHOU SAPUDI PRECISION PARTS CO LTD
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Patent Information

Application Number
CN202323547611.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2023-12-26
Publication Date
2025-01-14
Estimated Expiration
2033-12-26

AI Technical Summary

Technical Problem

Due to the different pipe diameters of existing aviation parts, the polishing and polishing devices are only suitable for parts of specific specifications. They lack flexibility and versatility, making it difficult to meet diversified and personalized processing needs.

Method used

A grinding and polishing device for aviation parts including a clamping mechanism and an adjustable polishing mechanism is designed. The clamping mechanism can flexibly clamp tubular parts of different specifications. The polishing inner diameter of the polishing mechanism is adjustable to adapt to the requirements of different tubular parts. .

Benefits of technology

The device has high flexibility and versatility, can meet diversified and personalized processing needs, reduces production difficulty and cost, and improves the assembly quality of parts.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses an aeronautical part grinding and polishing device, and relates to the technical field of aeronautical part machining. An installation frame is fixedly arranged on one side of the top of the base plate, and a U-shaped plate is fixedly arranged on the other side of the top of the base plate. The fixing block is fixedly arranged between the bottom sides of the U-shaped plates, V-shaped clamping grooves are formed in the top of the fixing block at equal intervals, and the tubular parts are embedded in the V-shaped clamping grooves; and the polishing mechanism is used for grinding and polishing the inner wall of the tubular part. By arranging the clamping mechanism, tubular parts of different specifications can be flexibly clamped and fixed, the inner walls of the tubular parts can be ground and polished, the polishing inner diameter of the polishing mechanism can be adjusted so as to meet the requirements of the different tubular parts, and the device has high flexibility and universality, can meet the diversified and personalized machining requirements and is suitable for popularization and application. And the production difficulty and cost are reduced, and the assembly quality of parts is improved.
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Description

Technical Field

[0001] The utility model relates to the technical field of aviation part processing equipment, and particularly relates to a grinding and polishing device for aviation parts. Background Technique

[0002] In the field of aviation manufacturing, some tubular parts (casing) need to be ground and polished after production to remove burrs on their inner walls, obtain a smooth surface to enhance the mechanical adhesion of the coating, and improve the assembly quality of the parts.

[0003] In the prior art, the diameters of tubular parts (casing) are different, which makes the grinding and polishing device for aviation parts have certain limitations and is only applicable to parts of specific specifications. This not only increases the difficulty and cost in the production of parts, but also lacks flexibility and versatility, and is difficult to meet the diversified and personalized processing requirements. Therefore, we propose a grinding and polishing device for aviation parts to solve the above problems. Content of the Utility Model

[0004] The utility model specifically adopts the following technical solutions to achieve the above purposes:

[0005] A grinding and polishing device for aviation parts, comprising:

[0006] A base plate, on one side of the top of which is fixedly provided with a mounting frame, and on the other side is fixedly provided with a U-shaped plate;

[0007] A fixing block and a tubular part, the fixing block is fixedly arranged between the bottom sides of the U-shaped plate, and V-shaped card slots are equally spaced on the top of the fixing block, and the tubular part is embedded in the V-shaped card slots;

[0008] A polishing mechanism for grinding and polishing the inner wall of the tubular part, and the inner diameter of the polishing mechanism is adjustable;

[0009] A clamping mechanism is arranged on the upper side inside the U-shaped plate for clamping and fixing the tubular part.

[0010] Further, the polishing mechanism includes movable rods rotatably connected to the surface of the mounting frame at equal intervals. One end of the movable rod is connected with a hollow plate. The tubular part is sleeved outside the hollow plate. Sliding plates are arranged on both sides of the hollow plate in a vertically staggered manner. A polishing piece is fixedly arranged on one side of the sliding plate outside the hollow plate. A spring is connected between one side of the sliding plate inside the hollow plate and the inner wall of the hollow plate. A driving part for driving the movable rod to rotate is arranged in the mounting frame.

[0011] Further, the driving member includes a worm gear fixed to the end of the movable rod. An installation rod is rotatably connected between the inner side walls of the installation frame. The surface of the installation rod is equidistantly provided with worm shafts, and the worm shafts are engaged with the worm gear. An electric motor is installed on the outer wall of the installation frame, and the output shaft of the electric motor is connected to the installation rod.

[0012] Further, the clamping mechanism includes a rotating rod rotatably connected between the inner side walls of the C-shaped plate. Threads with opposite spiral directions are formed on both sides of the rotating rod, and mounting blocks are symmetrically threadedly connected thereto. The mounting blocks are slidably connected to the inner top wall of the C-shaped plate. A connecting plate is hinged to the bottom side of the mounting block. A lifting plate is slidably arranged below the rotating rod on the inner top wall of the C-shaped plate. One end of the connecting plate away from the mounting block is hinged to the top of the lifting plate. A clamping block is fixedly provided at the bottom of the lifting plate corresponding to the position of the V-shaped card slot.

[0013] Further, both ends of the rotating rod penetrate through the C-shaped plate and are connected with knobs.

[0014] Further, a V-shaped notch is formed in the middle of the bottom of the clamping block.

[0015] The beneficial effects of the present utility model are as follows:

[0016] By setting the clamping mechanism, the present utility model can flexibly clamp and fix tubular parts of different specifications and polish the inner walls thereof. The polishing inner diameter of the polishing mechanism is adjustable to meet the requirements of different tubular parts. The device has high flexibility and versatility, can meet diversified and personalized processing needs, reduces production difficulty and cost, improves the assembly quality of parts, has high practicability, and is worthy of popular application and promotion. Description of the Drawings

[0017] Figure 1 is a three-dimensional structural schematic diagram of the present utility model;

[0018] Figure 2 is another three-dimensional structural schematic diagram of the present utility model;

[0019] Figure 3 is a front structural schematic diagram of the present utility model;

[0020] Figure 4 is a structural schematic diagram of the polishing mechanism of the present utility model.

[0021] : 1. base plate; 2. mounting frame; 3. V-shaped plate; 4. fixing block; 401. V-shaped slot; 5. tubular component; 6. polishing mechanism; 601. movable rod; 602. hollow plate; 603. slide plate; 604. polishing sheet; 605. spring; 7. clamping mechanism; 701. rotating rod; 702. mounting block; 703. connecting plate; 704. lifting plate; 705. clamping block; 8. driving member; 801. worm gear; 802. mounting rod; 803. worm; 804. motor. DETAILED DESCRIPTION

[0022] In order to make the purpose, technical solution and advantages of the embodiments of the present utility model clearer, the technical solution in the embodiments of the present utility model will be clearly and completely described below in conjunction with the drawings in the embodiments of the present utility model.

[0023] The present application provides an aviation component grinding and polishing device, which is mainly used to solve the problem that the diameters of tubular components (casings) are different in the prior art, which makes the aviation component grinding and polishing device have certain limitations and is only applicable to components of specific specifications, which not only increases the difficulty and cost in component production, but also lacks flexibility and versatility. The following technical solutions are provided. Figure 1-Figure 4 Make a detailed description:

[0024] An aviation parts grinding and polishing device, comprising:

[0025] A base plate 1, a mounting frame 2 is fixedly provided on one side of the top thereof, and a molded plate 3 is fixedly provided on the other side;

[0026] The fixing block 4 and the tubular component 5 are fixed between the bottom sides of the shaped plate 3, and the top of the fixing block 4 is evenly spaced with V-shaped grooves 401, and the tubular component 5 is embedded in the V-shaped grooves 401;

[0027] The polishing mechanism 6 is used to grind and polish the inner wall of the tubular component 5. The polishing inner diameter of the polishing mechanism 6 is adjustable. The polishing mechanism 6 includes a movable rod 601 that is rotatably connected to the surface of the mounting frame 2 at equal intervals. One end of the movable rod 601 is connected to a hollow plate 602. The tubular component 5 is sleeved on the outside of the hollow plate 602. Slide plates 603 are arranged on both sides of the hollow plate 602 to slide up and down alternately. A polishing sheet 604 is fixed on one side of the slide plate 603 located outside the hollow plate 602. A spring 605 is connected between one side of the slide plate 603 located inside the hollow plate 602 and the inner wall of the hollow plate 602. A driving member 8 for driving the movable rod 601 to rotate is arranged in the mounting frame 2;

[0028] The clamping mechanism 7 is arranged on the upper side inside the U-shaped plate 3 and is used for clamping and fixing the tubular component 5. The clamping mechanism 7 includes a rotating rod 701 rotatably connected between the inner side walls of the U-shaped plate 3. Threads with opposite spiral directions are formed on both sides of the rotating rod 701, and mounting blocks 702 are symmetrically connected by threads. The mounting blocks 702 are slidably connected to the inner top wall of the U-shaped plate 3. A connecting plate 703 is hinged to the bottom side of the mounting block 702. A lifting plate 704 is slidably arranged on the inner top wall of the U-shaped plate 3 below the rotating rod 701. One end of the connecting plate 703 away from the mounting block 702 is hinged to the top of the lifting plate 704. A clamping block 705 is fixedly arranged at the bottom of the lifting plate 704 corresponding to the position of the V-shaped card slot 401.

[0029] It should be noted that the inner diameter of the tubular component 5 in this device should be greater than the width of the hollow plate 602 to ensure that the polishing sheet 604 will not be stuck under the action of the spring 605.

[0030] The specific implementation process and principle description of this aircraft component grinding and polishing device:

[0031] First step, place the tubular component 5 to be processed in the V-shaped card slot 401 of the fixed block 4 to ensure its stability.

[0032] Second step, by rotating the rotating rod 701, the position of the mounting block 702 can be adjusted, changing the angle between the connecting plate 703 and the lifting plate 704, thereby controlling the lifting of the lifting plate 704, and then driving the clamping block 705 to move downward, so as to realize the clamping and fixing of the tubular component 5.

[0033] Third step, start the driving part 8 to make the movable rod 601 rotate. When the movable rod 601 rotates, the sliding plate 603 moves outward to the outside of the hollow plate 602 under the action of the spring 605, so that the polishing sheet 604 abuts against the inner wall of the tubular component 5. During the rotation of the hollow plate 602 following the movable rod 601, the polishing sheet 604 can polish the inner wall of the tubular component 5. Through the cooperation of the sliding plate 603 and the spring 605, the polishing sheet 604 can abut against the tubular components 5 with different inner diameters, so as to realize the grinding and polishing of tubular components 5 with different specifications.

[0034] Fourth step, after the grinding and polishing are completed, turn off the driving part 8, loosen the clamping mechanism 7, and take out the processed tubular component 5.

[0035] This aircraft component grinding and polishing device can flexibly clamp and fix tubular components 5 with different specifications by setting the clamping mechanism 7, and polish the inner wall thereof. The polishing inner diameter of the polishing mechanism 6 is adjustable to meet the requirements of different tubular components 5. This device has high flexibility and versatility, can meet diversified and personalized processing needs, reduces the production difficulty and cost, and improves the assembly quality of the parts.

[0036] As Figure 1 shown, in some embodiments, the driving member 8 includes a worm gear 801 fixedly arranged at the end of the movable rod 601. A mounting rod 802 is rotatably connected between the inner side walls of the mounting frame 2. A worm 803 is equidistantly arranged on the surface of the mounting rod 802. The worm 803 meshes with the worm gear 801. An electric motor 804 is mounted on the outer wall of the mounting frame 2. The output shaft of the electric motor 804 is connected to the mounting rod 802. More specifically, by the rotation of the output shaft of the electric motor 804, the mounting rod 802 is driven to rotate. Since the worm 803 meshes with the worm gear 801 and the worm gear 801 is fixed at the end of the movable rod 601, the rotation of the mounting rod 802 will drive the movable rod 601 to rotate. In this way, the polishing mechanism 6 can polish the inner wall of the tubular part 5.

[0037] As Figure 3 shown, in some embodiments, both ends of the rotating rod 701 penetrate through the U-shaped plate 3 and are connected with knobs. More specifically, both ends of the rotating rod 701 penetrate through the U-shaped plate 3 and are connected with knobs. Its main function is to facilitate the operator to adjust the clamping mechanism 7. By rotating the knobs, the rotation of the rotating rod 701 can be controlled, thereby driving the movement of the mounting block 702 and realizing the position control of the lifting plate 704.

[0038] As Figure 3 shown, in some embodiments, a V-shaped notch is formed in the middle of the bottom of the clamping block 705. More specifically, the design of forming a V-shaped notch in the middle of the bottom of the clamping block 705 is mainly used to facilitate the fixation of tubular parts 5 of different specifications. The V-shaped notch can adapt to the size of the tubular part 5, limit it in the correct position, and prevent it from shifting during the polishing process. At the same time, this design also improves the stability and firmness of the clamping mechanism 7, ensuring the safety and effect of the processing process. By reasonably adjusting the clamping mechanism 7, the V-shaped notch of the clamping block 705 can be closely adapted to tubular parts 5 of different specifications, thereby realizing the flexibility and versatility of the aviation part polishing and grinding device.

[0039] The above description of the disclosed embodiments enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be apparent to those skilled in the art. The general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention will not be limited to the embodiments shown herein, but rather to the broadest scope consistent with the principles and novel features disclosed herein.

Claims

1. An aviation parts grinding and polishing device, characterized in that: Including: A substrate (1), on one side of the top of which an installation frame (2) is fixedly provided, and on the other side of which a U-shaped plate (3) is fixedly provided; A fixed block (4) and a tubular component (5), the fixed block (4) is fixedly arranged between the bottom sides of the U-shaped plate (3), a V-shaped card slot (401) is constructed at equal intervals on the top of the fixed block (4), and the tubular component (5) is embedded inside the V-shaped card slot (401); A polishing mechanism (6) for polishing the inner wall of the tubular component (5), and the inner diameter of the polishing mechanism (6) is adjustable for polishing; A clamping mechanism (7) is arranged on the upper side inside the U-shaped plate (3) for clamping and fixing the tubular component (5).

2. The aviation parts grinding and polishing device according to claim 1, characterized in that: The polishing mechanism (6) includes movable rods (601) rotatably connected to the surface of the installation frame (2) at equal intervals. One end of the movable rod (601) is connected with a hollow plate (602). The tubular component (5) is sleeved outside the hollow plate (602). Sliding plates (603) are arranged on both sides of the hollow plate (602) in a staggered up-and-down manner. A polishing sheet (604) is fixedly provided on one side of the sliding plate (603) located outside the hollow plate (602). A spring (605) is connected between one side of the sliding plate (603) located inside the hollow plate (602) and the inner wall of the hollow plate (602). A driving member (8) for driving the movable rod (601) to rotate is arranged inside the installation frame (2).

3. The aviation parts grinding and polishing device according to claim 2, characterized in that: The driving member (8) includes a worm gear (801) fixedly arranged at the end of the movable rod (601). An installation rod (802) is rotatably connected between the inner side walls of the installation frame (2). Worm gears (803) are arranged on the surface of the installation rod (802) at equal intervals. The worm gears (803) are meshed with the worm gear (801). A motor (804) is installed on the outer wall of the installation frame (2). The output shaft of the motor (804) is connected with the installation rod (802).

4. The aviation parts grinding and polishing device according to claim 1, characterized in that: The clamping mechanism (7) includes a rotating rod (701) rotatably connected between the inner side walls of the U-shaped plate (3). Threads with opposite spiral directions are constructed on both sides of the rotating rod (701), and mounting blocks (702) are symmetrically threadedly connected. The mounting blocks (702) are slidably connected with the inner top wall of the U-shaped plate (3). A connecting plate (703) is hinged to the bottom side of the mounting block (702). A lifting plate (704) is slidably arranged on the inner top wall of the U-shaped plate (3) below the rotating rod (701). One end of the connecting plate (703) away from the mounting block (702) is hinged to the top of the lifting plate (704). A clamping block (705) is fixedly provided at the bottom of the lifting plate (704) corresponding to the position of the V-shaped card slot (401).

5. The aviation parts grinding and polishing device according to claim 4, characterized in that: Both ends of the rotating rod (701) penetrate through the U-shaped plate (3) and are connected with knobs.

6. The aviation parts grinding and polishing device according to claim 4, characterized in that: A V-shaped notch is constructed in the middle of the bottom of the clamping block (705).