A clamping and fixing device for aero-engine blade machining

CN224896943UActive Publication Date: 2026-10-27CHINA HANGFA GUIZHOU LIYANG AVIATION POWER CO LTD
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Patent Information

Application Number
CN202522354775.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-11-06
Publication Date
2026-10-27
Estimated Expiration
2035-11-06

AI Technical Summary

Technical Problem

[0003]但是现有技术中的航空发动机叶片加工用夹持固定装置在使用时不能适应不同规格和现状的叶片进行固定坚持,且在夹持固定后不能进行有效的位置调整,进而使得其不能适应不同位置上的加工,降低了其加工效率和使用效率,同时不能对其方向进行有效的调整,使得其不能适应不同方向上的加工操作,进而使得其不能进行有效的移动,使得其不能适应加工设备的位移使用,降低了其适配性和工作效率,因此我们提出了一种航空发动机叶片加工用夹持固定装置

Benefits of technology

[0013]1、本技术方案使得其能适应不同规格和现状的叶片进行固定坚持,且在夹持固定后能进行有效的位置调整,进而使得其能适应不同位置上的加工,提高了其加工效率和使用效率;

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Abstract

The utility model relates to a kind of clamping and fixing devices for aero-engine blade processing, including L type platform, the top of L type platform is movably connected with fixed disc, and the bottom of L type platform is connected with support plate, the top of fixed disc is connected with several even distribution's stand, the top of several stand is connected with same table block, the top of table block is movably connected with three even distribution's swing plate by rotating shaft and bearing, the top of rotating wheel is provided with three arc grooves, the inner sleeve of arc groove is equipped with clamping column, and the bottom end of clamping column is connected on the top of swing plate. The technical scheme makes it can adapt to different specifications and present situation blade to be fixed and persisted, and can be effectively adjusted after clamping and fixing position, and then make it can adapt to different position processing, improve its processing efficiency and use efficiency.
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Description

Technical Field

[0001] This utility model relates to the field of aero-engine blade processing technology, specifically to a clamping and fixing device for aero-engine blade processing. Background Technology

[0002] Aero-engine blades are the core components of aero-engines, hailed as the "jewels" in the "crown jewels of industry." Their primary responsibility is to convert the energy generated by fuel combustion into propulsion for the aircraft, drawing high-temperature, high-pressure gases into the combustion chamber through high-speed rotation to maintain normal engine operation. Clamping and fixing devices for aero-engine blade processing are specialized tooling equipment used for precise positioning and reliable fixation of blades during manufacturing, repair, and inspection. Their core function is to ensure the blades maintain a stable position during processing, inspection, or assembly, preventing positional deviations caused by vibration or external forces, thereby guaranteeing processing accuracy and product quality.

[0003] However, existing clamping and fixing devices for aero-engine blade processing cannot adapt to the use of blades of different specifications and conditions for fixing, and cannot be effectively adjusted in position after clamping and fixing. This makes them unsuitable for processing in different positions, reducing their processing efficiency and utilization efficiency. At the same time, they cannot be effectively adjusted in direction, making them unsuitable for processing operations in different directions. Consequently, they cannot be effectively moved, making them unsuitable for the displacement of processing equipment, reducing their adaptability and working efficiency. Therefore, we propose a clamping and fixing device for aero-engine blade processing. Utility Model Content

[0004] To address the shortcomings of existing technologies, this application proposes a clamping and fixing device for aero-engine blade processing, which can be adapted to fix blades of different specifications and conditions, and can be effectively adjusted in position after clamping and fixing, thereby enabling it to adapt to processing in different positions and improving its processing efficiency and utilization efficiency.

[0005] This utility model provides the following technical solution: a clamping and fixing device for processing aero-engine blades, comprising an L-shaped platform, a fixed plate movably connected to the top of the L-shaped platform, and a support plate connected to the bottom of the L-shaped platform. Several evenly distributed columns are connected to the top of the fixed plate, and the tops of the columns are connected to the same platform block. Three evenly distributed swing plates are movably connected to the top of the platform block via a rotating shaft and bearings. A rotating wheel is provided above the platform block, and three arc-shaped grooves are formed on the top of the rotating wheel. Clamping columns are fitted inside the arc-shaped grooves, and the bottom ends of the clamping columns are connected to the top of the swing plates.

[0006] As a preferred embodiment of this utility model, the top of the fixed plate is movably connected to an electric push rod via a rotating shaft and a bearing, and the top of the platform is connected to a tube via a bearing. A rotating column is sleeved at the bottom of the tube, and the top and bottom of the rotating column are respectively connected to the top of the rotating wheel and the top of the electric push rod.

[0007] As a preferred embodiment of this utility model, the side wall of the rotating column is connected with a number of evenly distributed plug-in plates, and the inner wall of the tube is provided with plug-in grooves that match the plug-in plates.

[0008] As a preferred embodiment of this utility model, the bottom of the fixed plate is connected to a drive motor by bolts, and the bottom end of the electric push rod is connected to the output shaft of the drive motor.

[0009] As a preferred embodiment of this utility model, the top of the L-shaped platform is movably connected to a housing via a rotating shaft and bearings, and the bottom of the L-shaped platform is connected to a rotary motor, with the bottom end of the rotating shaft on the housing connected to the output shaft of the rotary motor.

[0010] As a preferred embodiment of this utility model, a translation block is slidably connected inside the housing, and a mating plate is connected between the top of the translation block and the top of the fixed plate. A threaded hole is opened on the translation block, and a lead screw is inserted into the threaded hole. The two ends of the lead screw are respectively connected to the inner wall of the housing, and a servo motor is connected to the rear side of the housing. The rear end of the lead screw is connected to the output shaft of the servo motor.

[0011] As a preferred embodiment of this utility model, the top of the platform is connected to a pad and an L-shaped platform body. The top of the L-shaped platform body is connected to an electric telescopic rod. A positioning plate is connected to the electric telescopic rod. A round tube is connected to the side wall of the positioning plate. A round rod is sleeved inside the round tube. The round rod is connected to the L-shaped platform body. A buffer spring is sleeved on the round rod. The two ends of the buffer spring are connected to the positioning plate and the L-shaped platform body.

[0012] The beneficial effects of this utility model are:

[0013] 1. This technical solution enables it to fix blades of different specifications and conditions, and allows for effective position adjustment after clamping and fixing, thereby enabling it to adapt to processing in different positions and improving its processing efficiency and utilization efficiency.

[0014] 2. This technical solution can effectively adjust its direction, enabling it to adapt to processing operations in different directions, thereby enabling it to move effectively and adapt to the displacement of processing equipment, thus improving its adaptability and work efficiency. Attached Figure Description

[0015] Figure 1This is a schematic diagram of the overall structure of this utility model;

[0016] Figure 2 for Figure 1 Partial 3D view of components such as the central platform block;

[0017] Figure 3 for Figure 1 Partial bottom-view 3D view of components such as the L-shaped platform;

[0018] Figure 4 for Figure 1 Partial 3D view of components such as the center positioning plate;

[0019] Figure 5 for Figure 1 Partial 3D view of components such as the middle shell;

[0020] Figure 6 for Figure 1 Partial bottom-view perspective of components such as the central fixing plate.

[0021] In the diagram: 1. L-shaped platform; 2. Servo motor; 3. Support plate; 4. Lead screw; 5. Column; 6. Housing; 7. Electric push rod; 8. Connecting plate; 9. Translation block; 10. Fixed plate; 11. Pad; 12. Positioning plate; 13. Electric telescopic rod; 14. L-shaped platform; 15. Buffer spring; 16. Round rod; 17. Round tube; 18. Arc groove; 19. Clamping column; 20. Rotating wheel; 21. Swing plate; 22. Platform; 23. Rotating column; 24. Tube; 25. Insertion plate; 26. Insertion slot; 27. Rotary motor; 28. Drive motor. Detailed Implementation

[0022] To make the technical problems solved by this utility model, the technical solutions adopted, and the technical effects achieved clearer, the technical solutions of the embodiments of this utility model will be further described in detail below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.

[0023] Example 1

[0024] like Figures 1 to 6As shown, a clamping and fixing device for processing aero-engine blades includes: an L-shaped platform 1, a fixed plate 10 movably connected to the top of the L-shaped platform 1, and a support plate 3 connected to the bottom of the L-shaped platform 1. Several evenly distributed columns 5 are connected to the top of the fixed plate 10, and the same platform block 22 is connected to the top of the several columns 5. Three evenly distributed swing plates 21 are movably connected to the top of the platform block 22 through a rotating shaft and bearings. A rotating wheel 20 is provided above the platform block 22. Three arc-shaped grooves 18 are opened on the top of the rotating wheel 20. Clamping columns 19 are sleeved inside the arc-shaped grooves 18, and the bottom end of the clamping column 19 is connected to the top of the swing plate 21.

[0025] In this embodiment, the top of the fixed disk 10 is movably connected to the electric push rod 7 via a rotating shaft and bearing, and the top of the platform 22 is connected to the tube body 24 via a bearing. The bottom of the tube body 24 is fitted with a rotating column 23. The top and bottom of the rotating column 23 are respectively connected to the top of the rotating wheel 20 and the top of the electric push rod 7. Several evenly distributed plug plates 25 are connected to the side wall of the rotating column 23. The inner wall of the tube body 24 is provided with plug slots 26 that match the plug plates 25. The bottom of the fixed disk 10 is connected to the drive motor 28 via bolts. The bottom of the electric push rod 7 is connected to the output shaft of the drive motor 28, so that it can adapt to the fixed blades of different specifications and conditions, and can be effectively adjusted after clamping and fixing, thereby adapting to the processing in different positions and improving its processing efficiency and usage efficiency.

[0026] Example 2

[0027] like Figures 1 to 6 As shown, the top of the L-shaped platform 1 is movably connected to the housing 6 via a rotating shaft and bearings, and the bottom of the L-shaped platform 1 is connected to a rotary motor 27. The bottom end of the rotating shaft on the housing 6 is connected to the output shaft of the rotary motor 27. A translation block 9 is slidably connected inside the housing 6. A mating plate 8 is connected between the top of the translation block 9 and the top of the fixed plate 10. A threaded hole is opened on the translation block 9, and a lead screw 4 passes through the threaded hole. The two ends of the lead screw 4 are respectively connected to the inner wall of the housing 6, and a servo motor 2 is connected to the rear side of the housing 6. The rear end of the lead screw 4 is connected to the output shaft of the servo motor 2.

[0028] Implementation plan: The top of the platform 22 is connected to the pad 11 and the L-shaped platform 14. The top of the L-shaped platform 14 is connected to the electric telescopic rod 13. The electric telescopic rod 13 is connected to the positioning plate 12. The side wall of the positioning plate 12 is connected to the round tube 17. The round tube 17 is fitted with a round rod 16. The round rod 16 is connected to the L-shaped platform 14. The round rod 16 is fitted with a buffer spring 15. The two ends of the buffer spring 15 are connected to the positioning plate 12 and the L-shaped platform 14, which can effectively adjust its direction, so that it can adapt to processing operations in different directions, and thus enable it to move effectively, so that it can adapt to the displacement of the processing equipment, improving its adaptability and work efficiency.

[0029] Working Principle: In this technical solution, the blade is first placed between three clamping columns 19. The drive motor 28, through the electric push rod 7 and the rotating column 23, drives the rotating wheel 20 to rotate forward or backward, causing the swing plate 21 to move the clamping columns 19 together or apart, thus clamping or releasing the blade. The extension and retraction of the electric push rod 7 can move the rotating wheel 20 up or down via the rotating column 23, allowing it to adapt to blades of different specifications and conditions for fixing. After clamping and fixing, effective position adjustment is possible, enabling it to adapt to processing in different positions, improving processing and utilization efficiency. Subsequently, two electric... The extension rod 13 extends and drives the two positioning plates 12 to close together and clamp and fix the blade. The servo motor 2 drives the lead screw 4 to rotate forward or backward, so that the translation block 9 drives the fixed plate 10 to move back and forth through the docking plate 8. The fixed plate 10 drives the blade to move back and forth through the column 5 and platform 22. The rotary motor 27 drives the housing 6 to rotate. The housing 6 drives the blade to rotate through the translation block 9, translation block 8, column 5 and platform 22, which can effectively adjust its direction, so that it can adapt to processing operations in different directions, and thus enable it to move effectively, so that it can adapt to the displacement of the processing equipment, improving its adaptability and working efficiency.

[0030] Although preferred embodiments of the present invention have been described, those skilled in the art, upon learning the basic inventive concept, can make other changes and modifications to these embodiments. Therefore, the appended claims are intended to be interpreted as including the preferred embodiments as well as all changes and modifications falling within the scope of the present invention.

[0031] Obviously, those skilled in the art can make various modifications and variations to this utility model without departing from its spirit and scope. Therefore, if these modifications and variations fall within the scope of the claims of this utility model and their equivalents, this utility model also intends to include these modifications and variations.

Claims

1. A clamping and fixing device for machining aero-engine blades, characterized in that, The device includes an L-shaped platform (1), with a fixed plate (10) movably connected to the top of the L-shaped platform (1) and a support plate (3) connected to the bottom of the L-shaped platform (1). Several evenly distributed columns (5) are connected to the top of the fixed plate (10), and the same platform block (22) is connected to the top of the several columns (5). Three evenly distributed swing plates (21) are movably connected to the top of the platform block (22) through a rotating shaft and bearing. A rotating wheel (20) is provided above the platform block (22). Three arc-shaped grooves (18) are opened on the top of the rotating wheel (20). A clamping column (19) is sleeved inside the arc-shaped groove (18), and the bottom end of the clamping column (19) is connected to the top of the swing plate (21).

2. The clamping and fixing device for processing aero-engine blades according to claim 1, characterized in that, The top of the fixed plate (10) is movably connected to an electric push rod (7) via a rotating shaft and bearing, and the top of the platform (22) is connected to a tube (24) via a bearing. The bottom of the tube (24) is fitted with a rotating column (23), and the top and bottom of the rotating column (23) are respectively connected to the top of the rotating wheel (20) and the top of the electric push rod (7).

3. The clamping and fixing device for processing aero-engine blades according to claim 1, characterized in that, The side wall of the rotating column (23) is connected to several evenly distributed plug plates (25), and the inner wall of the tube (24) is provided with plug grooves (26) that match the plug plates (25).

4. The clamping and fixing device for processing aero-engine blades according to claim 1, characterized in that, The bottom of the fixed plate (10) is connected to the drive motor (28) by bolts, and the bottom end of the electric push rod (7) is connected to the output shaft of the drive motor (28).

5. The clamping and fixing device for machining aero-engine blades according to claim 1, characterized in that, The top of the L-shaped platform (1) is movably connected to the housing (6) via a rotating shaft and bearing, and the bottom of the L-shaped platform (1) is connected to a rotary motor (27). The bottom end of the rotating shaft on the housing (6) is connected to the output shaft of the rotary motor (27).

6. The clamping and fixing device for machining aero-engine blades according to claim 5, characterized in that, A translation block (9) is slidably connected inside the housing (6). A mating plate (8) is connected between the top of the translation block (9) and the top of the fixed plate (10). A threaded hole is provided on the translation block (9), and a lead screw (4) is inserted through the threaded hole. The two ends of the lead screw (4) are respectively connected to the inner wall of the housing (6), and a servo motor (2) is connected to the rear side of the housing (6). The rear end of the lead screw (4) is connected to the output shaft of the servo motor (2).

7. The clamping and fixing device for processing aero-engine blades according to claim 1, characterized in that, The top of the platform (22) is connected to a pad (11) and an L-shaped platform (14). The top of the L-shaped platform (14) is connected to an electric telescopic rod (13). The electric telescopic rod (13) is connected to a positioning plate (12). The side wall of the positioning plate (12) is connected to a round tube (17). A round rod (16) is sleeved inside the round tube (17). The round rod (16) is connected to the L-shaped platform (14). A buffer spring (15) is sleeved on the round rod (16). The two ends of the buffer spring (15) are connected to the positioning plate (12) and the L-shaped platform (14).