Rapid clamping jig special for aeronautical part milling machine machining

By designing a special quick clamping fixture for aviation parts milling machines, the coordination and positioning structure of the fixture body and the circular pressure plate are used to solve the problem of parts clamping deformation in traditional milling machines, and stable clamping and efficient production are achieved.

CN223186085UActive Publication Date: 2025-08-05SUZHOU NAFCO PRECISION LTD
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Patent Information

Application Number
CN202422435871.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-10-10
Publication Date
2025-08-05
Estimated Expiration
2034-10-10

AI Technical Summary

Technical Problem

When existing milling machines process precision parts, the traditional compression method is single, making it difficult to mass produce, and the parts are prone to deform during clamping, resulting in the generation of defective products.

Method used

A special quick clamping fixture for aviation parts milling machines is designed. Through the coordination of the fixture body and the circular pressure plate, the precise positioning and fixing of the workpiece is achieved by using positioning columns and screws. Combined with the connecting structure of the bidirectional threaded rod and the transmission slider, the workpiece is ensured to be firmly fixed to the fixture.

Benefits of technology

The stable clamping of workpieces is achieved, assembly errors are avoided, the work intensity of operators is reduced, and the stability of production quality is improved.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of jigs, and discloses a special rapid clamping jig for aeronautical part milling machine machining, which comprises a workbench and workpiece bodies, a mounting plate is mounted on the workbench, a plurality of jig bodies are arranged on the mounting plate, and the workpiece bodies are assembled on the jig bodies. The mounting plate at the bottom of the jig body is fixed to a machine tool workbench, then a plurality of workpiece bodies are loaded to the jig, workpieces are accurately positioned through the positioning columns, the circular pressing plate is fixed to the jig through the screws at the hollowed-out positions of the workpiece bodies, the workpieces are pressed through the circular pressing plate, and the bottom planes of the workpieces are tightly attached to the plane of the jig. The purpose that a workpiece body is firmly fixed to the jig through the jig and the circular pressing plate is achieved, so that the clamping process is completed, if the workpiece is reverse, the workpiece cannot be installed, assembly errors of operators are avoided, errors caused by human factors are reduced, the working intensity of the workers is relieved, and stable production quality is guaranteed.
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Description

Technical Field

[0001] The utility model relates to the technical field of jigs, in particular to a special quick clamping jig for machining aviation parts on milling machines. Background Art

[0002] A milling machine primarily uses a milling cutter to machine various workpiece surfaces. Jigs are a broad category of tools used in carpentry, ironwork, benchwork, mechanics, electronic control, and other crafts, primarily to assist in controlling position or motion. Jigs can be categorized into three types: process assembly jigs, project testing jigs, and circuit board testing jigs.

[0003] When existing milling machines process precision parts, the traditional clamping method is relatively simple and not easy to mass produce. In addition, the parts are prone to deformation during the clamping process, resulting in defective products. Utility Model Content

[0004] (1) Technical problems solved

[0005] In view of the deficiencies in the prior art, the utility model provides a special quick clamping fixture for machining aviation parts on milling machines to solve the above technical problems.

[0006] (2) Technical solution

[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a special quick clamping jig for milling machines of aviation parts, comprising a workbench and a workpiece body, a mounting plate being installed on the workbench, a plurality of jig bodies being arranged on the mounting plate, the workpiece body being assembled on the jig body, two docking posts being provided on the jig body, a circular pressure plate being connected to the docking posts by screws, the bottom of the circular pressure plate being in contact with the top of the workpiece body, a plurality of positioning posts being arranged on the jig body, the positioning posts being adapted to the through holes on the workpiece body, and handles being connected on both sides of the workbench.

[0008] Preferably, a transmission cavity is provided in the mounting plate, a bidirectional threaded rod is rotatably installed in the transmission cavity, and two mutually symmetrical transmission sliders are threadedly connected to the bidirectional threaded rod.

[0009] Preferably, two mutually symmetrical connecting blocks are provided on the top of the workbench, and a protrusion is provided on each side of the two connecting blocks that are close to each other.

[0010] Preferably, locking holes are provided on the two transmission slide blocks, and the locking holes are adapted to the protrusions on the connecting block.

[0011] Preferably, two mutually symmetrical rectangular sliding holes are provided on the bottom inner wall of the transmission cavity, both rectangular sliding holes are communicated with the outside, and the two transmission sliding blocks slide in the two rectangular sliding holes respectively.

[0012] Preferably, an adjustment block is provided at one end of the bidirectional threaded rod that passes through the transmission cavity and extends to the outside, and an inner hexagonal groove is provided at the end of the adjustment block close to the outside.

[0013] Preferably, the docking column is provided with a threaded hole adapted to fit with a screw.

[0014] Compared with the prior art, the present invention provides a special quick clamping fixture for milling machines of aviation parts, which has the following beneficial effects:

[0015] 1. The utility model cooperates with the jig body and the circular pressure plate and other structures, so that when in use, the mounting plate at the bottom of the jig body can be fixed on the machine tool workbench, and then several workpiece bodies can be loaded onto the jig, the workpieces can be accurately positioned by the positioning column, and the circular pressure plate can be fixed to the jig through the hollow part on the workpiece body by screws, and the workpiece is pressed by the circular pressure plate so that the bottom plane of the workpiece is close to the jig plane, thereby achieving the purpose of firmly fixing the workpiece body on the jig through the jig and the circular pressure plate, thereby completing the clamping process. If the workpiece is reversed, it cannot be loaded, avoiding assembly errors by operators, reducing errors caused by human factors, alleviating the workload of workers, and ensuring stable production quality. BRIEF DESCRIPTION OF THE DRAWINGS

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

[0017] Figure 2 This is a schematic side cross-sectional view of the fixture body and connector structure of the present invention;

[0018] Figure 3 This is a schematic cross-sectional view of the bidirectional threaded rod and transmission slider structure of the present invention;

[0019] Figure 4 For the utility model Figure 2 A magnified schematic diagram of the structure in the middle.

[0020] Among them: 1. Workbench; 2. Mounting plate; 3. Fixture body; 4. Handle; 5. Workpiece body; 6. Round pressure plate; 7. Screw; 8. Through hole; 9. Positioning column; 10. Adjustment block; 11. Transmission cavity; 12. Bidirectional threaded rod; 13. Connecting block; 14. Transmission slider; 15. Locking hole; 16. Rectangular slide hole; 17. Docking column; 18. Threaded hole. DETAILED DESCRIPTION

[0021] The following embodiments of the present invention are described in further detail with reference to the accompanying drawings and examples. The following examples are used to illustrate the present invention, but are not intended to limit the scope of the present invention.

[0022] In the description of this utility model, unless otherwise specified, "plurality" means two or more; the terms "upper," "lower," "left," "right," "inner," "outer," "front end," "rear end," "head," "tail," etc., indicating directions or positional relationships, are based on the directions or positional relationships shown in the accompanying drawings and are intended solely to facilitate the description of this utility model and simplify the description. They do not indicate or imply that the devices or components referred to must have a specific direction, be constructed, or operate in a specific direction, and therefore should not be construed as limiting this utility model. Furthermore, the terms "first," "second," "third," etc., are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0023] In the description of this utility model, it should be noted that, unless otherwise specified or limited, the terms "connected" and "connection" should be understood in a broad sense. For example, they can refer to fixed connection, detachable connection, or integral connection; mechanical connection, electrical connection; direct connection, or indirect connection through an intermediary. Those skilled in the art will understand the specific meanings of the above terms in this utility model based on the specific circumstances.

[0024] See also Figure 1-4 A quick clamping jig specially used for milling machines for aviation parts includes a workbench 1 and a workpiece body 5. A mounting plate 2 is installed on the workbench 1, and a number of jig bodies 3 are arranged on the mounting plate 2. The workpiece body 5 is assembled on the jig body 3. Two docking columns 17 are provided on the jig body 3. A circular pressure plate 6 is connected to the docking column 17 by a screw 7. The bottom of the circular pressure plate 6 abuts against the top of the workpiece body 5. A number of positioning columns 9 are arranged on the jig body 3. The positioning columns 9 are adapted to the through holes 8 on the workpiece body 5. Handles 4 are connected to both sides of the workbench 1.

[0025] By cooperating with each other in structures such as the jig body 3 and the circular pressure plate 6, the mounting plate 2 at the bottom of the jig body 3 can be fixed on the machine tool workbench 1 during use, and then several workpiece bodies 5 can be loaded onto the jig. The workpiece can be accurately positioned by the positioning column 9, and the circular pressure plate 6 can be fixed to the jig through the hollow part on the workpiece body 5 by screws 7. The workpiece is pressed tightly by the circular pressure plate 6 so that the bottom plane of the workpiece is close to the jig plane, thereby achieving the purpose of firmly fixing the workpiece body 5 on the jig through the jig and the circular pressure plate 6, thereby completing the clamping process. If the workpiece is reversed, it cannot be loaded, avoiding assembly errors by operators, reducing errors caused by human factors, alleviating the workload of workers, and ensuring stable production quality.

[0026] Specifically, in this embodiment, a transmission cavity 11 is provided in the mounting plate 2, and a bidirectional threaded rod 12 is rotatably installed in the transmission cavity 11. Two mutually symmetrical transmission sliders 14 are threadedly connected to the bidirectional threaded rod 12. Two mutually symmetrical connecting blocks 13 are provided on the top of the workbench 1. The two connecting blocks 13 are protruding with protrusions on the sides close to each other. Locking holes 15 are provided on the two transmission sliders 14, and the locking holes 15 are adapted to the protrusions on the connecting blocks 13. Two mutually symmetrical rectangular sliding holes 16 are provided on the bottom inner wall of the transmission cavity 11. The two rectangular sliding holes 16 are both connected to the outside world, and the two transmission sliders 14 slide in the two rectangular sliding holes 16 respectively.

[0027] By cooperating with the provided bidirectional threaded rod 12, the transmission slider 14 and the connecting block 13, when connecting the mounting plate 2 to the workbench 1, the two rectangular sliding holes 16 at the bottom of the mounting plate 2 are aligned with the workbench 1 and inserted to achieve preliminary limiting of the mounting plate 2. At this time, the bidirectional threaded rod 12 is rotated to drive the two transmission sliders 14 to approach each other and clamp the two connecting blocks 13. When the transmission slider 14 contacts the connecting block 13, the locking hole 15 on the transmission slider 14 is sleeved on the protrusion on the connecting block 13, thereby achieving locking and fixing between the transmission slider 14 and the connecting block 13, thereby completing the connection and fixing process between the mounting plate 2 and the workbench 1.

[0028] Specifically, in this embodiment, the bidirectional threaded rod 12 passes through the transmission cavity 11 and extends to the outside where an adjustment block 10 is provided at one end thereof. The adjustment block 10 is provided with an inner hexagonal groove at one end thereof close to the outside.

[0029] By providing the adjustment block 10 and the inner hexagonal groove, an outer hexagonal wrench can be inserted into the inner hexagonal groove in the adjustment block 10 to drive the adjustment block 10 to rotate, thereby facilitating the rotation of the bidirectional threaded rod 12.

[0030] Specifically, in this embodiment, a threaded hole 18 adapted to the screw 7 is formed on the docking post 17 .

[0031] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A special quick clamping fixture for milling aviation parts, comprising a workbench and a workpiece body, characterized in that: A mounting plate is installed on the workbench, and several jig bodies are arranged on the mounting plate. The workpiece body is assembled on the jig body. Two docking columns are provided on the jig body. A circular pressure plate is connected to the docking columns by screws. The bottom of the circular pressure plate abuts against the top of the workpiece body. Several positioning columns are arranged on the jig body, and the positioning columns are adapted to the through holes on the workpiece body. Handles are connected to both sides of the workbench.

2. The quick clamping fixture for milling machines of aviation parts according to claim 1, characterized in that: A transmission cavity is provided in the installation plate, a bidirectional threaded rod is rotatably installed in the transmission cavity, and two mutually symmetrical transmission sliding blocks are threadedly connected to the bidirectional threaded rod.

3. The special quick clamping fixture for milling of aviation parts according to claim 1, characterized in that: Two mutually symmetrical connecting blocks are arranged on the top of the workbench, and a protrusion is provided on each side of the two connecting blocks close to each other.

4. The special quick clamping fixture for milling of aviation parts according to claim 2, characterized in that: The two transmission slide blocks are both provided with locking holes, which are matched with the protrusions on the connecting block.

5. The special quick clamping fixture for milling of aviation parts according to claim 2, characterized in that: Two mutually symmetrical rectangular sliding holes are provided on the bottom inner wall of the transmission cavity. Both rectangular sliding holes are communicated with the outside, and two transmission sliding blocks slide in the two rectangular sliding holes respectively.

6. The special quick clamping fixture for milling of aviation parts according to claim 2, characterized in that: The bidirectional threaded rod passes through the transmission cavity and extends to one end of the outside world, and an adjustment block is provided. The end of the adjustment block close to the outside world is provided with an inner hexagonal groove.

7. The special quick clamping fixture for milling of aviation parts according to claim 1, characterized in that: The docking column is provided with a threaded hole adapted to the screw.