Aviation aluminum alloy part clamp suitable for different specifications

By introducing gears and thread mechanisms into the aerospace aluminum alloy parts clamps, combining soft pads and telescopic springs, the problem of angle fixation and clamping in the prior art is solved, and efficient clamping and angle adjustment of parts of different specifications is achieved. , improves the efficiency and stability of processing operations.

CN119098924AInactive Publication Date: 2024-12-10SHENYANG HUATIAN AVIATION MASCH CO LTD
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Patent Information

Application Number
CN202411513706.8
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-10-28
Publication Date
2024-12-10
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

The existing aerospace aluminum alloy parts clamps that are suitable for different specifications cannot adjust the angle after clamping at limit positions, resulting in a reduction in clamping stability and affecting the efficiency and practicality of subsequent processing operations.

Method used

A clamp including a operating table, motor, gear system and limit block is designed to adjust angle and limit clamp through gears and thread mechanisms, and provide stability and firmness with pads and telescopic springs to ensure surface fit of the parts. .

Benefits of technology

The stable clamping and angle adjustment of parts of different specifications is achieved, which improves working efficiency and clamping stability, and avoids clamping offset and instability.

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Abstract

The embodiment of the invention provides an aviation aluminum alloy part clamp suitable for different specifications, and relates to the technical field of clamps. The aviation aluminum alloy part clamp suitable for the different specifications comprises an operation table, a first motor is fixedly installed at the bottom end of the operation table, a first rotating rod is fixedly installed at the top end of the first motor, the first rotating rod penetrates through the operation table from the center position, and a first gear is fixedly installed at the top end of the first rotating rod. After parts of different specifications are placed on a placing plate, a first motor is driven, a first gear is driven to rotate, a second gear is driven to rotate through meshing of the first gear, the second gear is made to rotate on the surface of a gear belt in a meshing mode with the first gear as the circle center, and then a connecting rod is driven to rotate through the second gear; the connecting rod drives the placing plate to rotate, the angle is adjusted through rotation of the placing plate, limiting clamping is more convenient through the angle, and the follow-up working efficiency is also improved.
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Description

Technical Field

[0001] The embodiments of the present application relate to the field of fixture technology, and in particular to a fixture for aviation aluminum alloy parts that can adapt to different specifications. Background Art

[0002] An alloy based on aluminum with a certain amount of other alloying elements added is one of the light metal materials. In addition to the general characteristics of aluminum, aluminum alloys also have some specific characteristics of alloys due to the different types and quantities of alloying elements added. The density of aluminum alloys is high, the specific strength is close to that of high alloy steel, and the specific stiffness exceeds that of steel. It has good casting properties and plastic processing properties, good electrical and thermal conductivity, good corrosion resistance and weldability, and can be used as a structural material. It is widely used in aerospace, aviation, transportation, construction, electromechanical, light chemicals and daily necessities.

[0003] However, there is a clamp that can adapt to aviation aluminum alloy parts of different specifications. Since it is used to limit clamp parts of different specifications, it needs to fit the surface of the parts more closely to avoid the lack of fit and reduced clamping stability. The angle is fixed after limit clamping, so that the angle of subsequent processing operations is fixed. The inability to adjust the angle will reduce the work efficiency and practicality of the limit clamping. Summary of the invention

[0004] In view of the above problems, an embodiment of the present application provides a clamp that is adaptable to aviation aluminum alloy parts of different specifications to solve the problem that the existing clamp that is adaptable to aviation aluminum alloy parts of different specifications is required to fit the surface of the parts more closely to avoid the inability to fit and reduce the stability of the clamping. The angle is fixed after the limit clamping, so that the angle of subsequent processing operations is fixed, and the inability to adjust the angle will reduce the work efficiency and practicality of the limit clamping.

[0005] The embodiment of the present application provides a fixture for aviation aluminum alloy parts that can adapt to different specifications, including: an operating table, a first motor is fixedly installed at the bottom of the operating table, a first rotating rod is fixedly installed at the top of the first motor, the first rotating rod passes through the operating table from the center, a first gear is fixedly installed at the top of the first rotating rod, a second gear is meshed and connected on the surface of the first gear, the second gear is installed on the outer wall of the connecting rod, and a placement plate is fixedly installed at the top of the connecting rod.

[0006] Through the above scheme, when parts of different specifications are placed on the placement plate, the first motor is driven to drive the first gear to rotate, and the second gear is driven to rotate through the meshing of the first gear, so that the second gear meshes and rotates on the surface of the gear belt with the first gear as the center, and then the connecting rod is driven to rotate through the second gear, so the connecting rod also drives the placement plate to rotate, and the angle is adjusted by the rotation of the placement plate, and the angle makes the limit clamp more useful and also improves the subsequent work efficiency.

[0007] In some embodiments, the second gear surface is meshedly connected with a gear belt, the gear belt is installed on the inner wall of the groove, and the groove is opened at the center of the top of the operating table.

[0008] Through the above solution, when the second gear meshes and rotates on the surface of the gear belt with the first gear as the center, the meshing between the gears is more stable, avoiding deviation during rotation.

[0009] In some embodiments, the bottom end of the connecting rod is movably sleeved inside the annular groove, and the annular groove is opened at the bottom end of the inner wall of the groove.

[0010] Through the above solution, when the second gear meshes and rotates on the surface of the gear belt with the first gear as the center, the connecting rod also moves inside the annular groove, so the annular groove plays a good role in limiting and stabilizing.

[0011] In some embodiments, a second motor is installed at the center position of the inner wall of the placement plate, a second rotating rod is fixedly installed on the top of the second motor, a first bevel gear is fixedly installed on the top of the second rotating rod, a second bevel gear is meshingly connected to the surface of the first bevel gear, a screw is fixedly installed on one side of the second bevel gear, a threaded block is threadedly connected to the surface of the screw, and a limiting block is installed on the top of the threaded block.

[0012] Through the above scheme, parts of different specifications are placed on the placement plate, and the second motor is driven to drive the second rotating rod to rotate, and then the first bevel gear is driven to rotate, and the second bevel gears on the four sides are driven to rotate through the meshing of the first bevel gear, and then the screw is driven to rotate, so that the threaded block is threaded on the surface of the screw, thereby driving the limit block to fit on the top of the placement plate and move, and parts of different specifications are clamped by the limit blocks on the four sides, and the drive makes the clamping more stable.

[0013] In some embodiments, a plurality of limiting grooves are formed on one side of the limiting block, a movable rod is movably sleeved inside the limiting groove, and a soft pad is fixedly installed on one side of the movable rod.

[0014] Through the above scheme, when the limit block clamps parts of different specifications during movement, the force will also push the soft pad to one side, so that the movable rod also slides in the limit groove, and through the telescopic push, the pushing pad can better fit the surface of the part, and the several soft pads on one side of the limit block provide stability and firmness for the limit clamping.

[0015] In some embodiments, a telescopic spring is fixedly mounted on one side of the soft cushion, and the telescopic spring is movably sleeved on the outer wall of the movable rod.

[0016] Through the above scheme, through the elasticity of the telescopic spring, when the limit block clamps parts of different specifications during movement, the soft pad will also fit the surface of the part, and at the same time, the force will push the soft pad to move to one side, so the elasticity will push the soft pad to better fit the surface of the part, providing stability and firmness for the limit clamping.

[0017] In some embodiments, the top of the placement plate is symmetrically provided with slots on four sides, and the threaded block is movably sleeved inside the slots.

[0018] Through the above scheme, the limit block is fitted on the top of the placement plate and moved through the slot. At the same time, the thread block also slides in the slot when it moves on the surface of the screw. The slot also plays the role of limiting the thread block, preventing the thread block from being unable to move and rotate synchronously with the screw.

[0019] The above description is only an overview of the technical solution of the embodiment of the present application. In order to more clearly understand the technical means of the embodiment of the present application, it can be implemented in accordance with the contents of the specification. In order to make the above and other purposes, features and advantages of the embodiment of the present application more obvious and easy to understand, the specific implementation methods of the present application are listed below. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following is a brief introduction to the drawings required for use in the description of the embodiments. Obviously, the drawings described below are some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0021] Figure 1 This is a schematic diagram of a fixture for aviation aluminum alloy parts that can adapt to different specifications in some embodiments of the present application.

[0022] Figure 2 This is a schematic diagram of the cross-sectional structure of the operating table in some embodiments of the present application.

[0023] Figure 3 This is a schematic diagram of the partial cross-sectional structure of the operating table in some embodiments of the present application.

[0024] Figure 4 This is a schematic diagram of the partial structure of the internal structure of the operating console in some embodiments of the present application.

[0025] Figure 5 This is a schematic diagram of the local cross-sectional structure of the placement plate in some embodiments of the present application.

[0026] Figure 6 This is a schematic diagram of the partial cross-sectional structure of the limiting block in some embodiments of the present application.

[0027] Description of reference numerals: 1. Operating table; 2. First motor; 3. First rotating rod; 4. First gear; 5. Second gear; 6. Connecting rod; 7. Annular groove; 8. Gear belt; 9. Groove; 10. Placement plate; 11. Second motor; 12. Second rotating rod; 13. First bevel gear; 14. Second bevel gear; 15. Screw; 16. Threaded block; 17. Limit block; 18. Limit groove; 19. Movable rod; 20. Cushion; 21. Telescopic spring; 22. Slot. DETAILED DESCRIPTION

[0028] In order to make the purpose, technical solution and advantages of the embodiments of the present application clearer, the technical solution in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of this application.

[0029] The terms "including" and "having" and any variations thereof in the specification, claims and drawings of this application are intended to cover but not exclude other contents. The word "a" or "an" does not exclude the existence of a plurality. Unless otherwise specified, the meaning of "plurality" refers to more than two (including two), and similarly, "multiple groups" refers to more than two (including two).

[0030] The directional words appearing in the following description are all directions shown in the drawings, and do not limit the specific structure of the present application. For example, in the description of the present application, the directions or positional relationships indicated by the terms "length", "width", "thickness", "upper", "lower", "front", "back", "left", "right", "inner", "outer", "axial", "radial", "circumferential", etc. are based on the directions or positional relationships shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction, and therefore cannot be understood as a limitation on the present application.

[0031] In addition, the expressions of indicated directions such as the X direction, the Y direction, and the Z direction used to illustrate the operation and construction of the components of the present embodiment are not absolute but relative, and although these indications are appropriate when the components are in the positions shown in the figures, when these positions are changed, these directions should be interpreted differently to correspond to the changes.

[0032] In the description of the present application, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected" and "connected" should be understood in a broad sense. For example, the "connected" or "connected" of a mechanical structure may refer to a physical connection, such as a fixed connection, a detachable connection or an integral connection. In addition to referring to a physical connection, the "connected" or "connected" of a circuit structure may also refer to an electrical connection or a signal connection. For example, it may be a direct connection, that is, a physical connection, or it may be an indirect connection through at least one intermediate element, as long as the circuit is connected. For those of ordinary skill in the art, the specific meanings of the above terms in the present application can be understood according to specific circumstances.

[0033] In order to facilitate the understanding of the technical solutions in the embodiments of the present application, the technical solutions in the embodiments of the present application are clearly and completely described below in conjunction with the drawings in the embodiments of the present application.

[0034] The present application embodiment provides a fixture for aviation aluminum alloy parts of different specifications. Figure 1-Figure 6 As shown, it includes: an operating table 1, a first motor 2 is fixedly installed at the bottom end of the operating table 1, a first rotating rod 3 is fixedly installed on the top of the first motor 2, the first rotating rod 3 passes through the operating table 1 from the center position, a first gear 4 is fixedly installed on the top of the first rotating rod 3, a second gear 5 is meshingly connected to the surface of the first gear 4, the second gear 5 is installed on the outer wall of the connecting rod 6, and a placement plate 10 is fixedly installed on the top of the connecting rod 6.

[0035] When parts of different specifications are placed on the placement plate 10, the first motor 2 is driven to drive the first gear 4 to rotate, and the second gear 5 is driven to rotate through the engagement of the first gear 4, so that the second gear 5 meshes and rotates on the surface of the gear belt 8 with the first gear 4 as the center, and then the connecting rod 6 is driven to rotate through the second gear 5, so the connecting rod 6 also drives the placement plate 10 to rotate, and the angle is adjusted by the rotation of the placement plate 10.

[0036] In the technical solution of the embodiment of the present application, a gear belt 8 is meshedly connected to the surface of the second gear 5 , and the gear belt 8 is installed on the inner wall of a groove 9 , and the groove 9 is opened at the center position of the top of the operating table 1 .

[0037] When the second gear 5 meshes and rotates on the surface of the gear belt 8 with the first gear 4 as the center, the meshing between the gears is more stable, avoiding deviation during rotation.

[0038] In the technical solution of the embodiment of the present application, the bottom end of the connecting rod 6 is movably sleeved inside the annular groove 7 , and the annular groove 7 is provided at the bottom end of the inner wall of the groove 9 .

[0039] When the second gear 5 meshes and rotates on the surface of the gear belt 8 with the first gear 4 as the center, the connecting rod 6 also moves inside the annular groove 7, so the annular groove 7 plays a good role in limiting and stabilizing.

[0040] In the technical solution of the embodiment of the present application, a second motor 11 is installed at the center position of the inner wall of the placing plate 10, a second rotating rod 12 is fixedly installed on the top of the second motor 11, a first bevel gear 13 is fixedly installed on the top of the second rotating rod 12, a second bevel gear 14 is meshingly connected to the surface of the first bevel gear 13, a screw 15 is fixedly installed on one side of the second bevel gear 14, a threaded block 16 is threadedly connected to the surface of the screw 15, and a limiting block 17 is installed on the top of the threaded block 16.

[0041] By placing parts of different specifications on the placement plate 10, driving the second motor 11, driving the second rotating rod 12 to rotate, and then driving the first bevel gear 13 to rotate, and the engagement of the first bevel gear 13 drives the second bevel gears 14 on four sides to rotate, and then drives the screw 15 to rotate, so that the threaded block 16 is threaded on the surface of the screw 15, thereby driving the limit block 17 to fit the top of the placement plate 10 and move, and the parts of different specifications are clamped by the limit blocks 17 on four sides, and the driving makes the clamping more stable.

[0042] In the technical solution of the embodiment of the present application, a plurality of limiting grooves 18 are opened on one side of the limiting block 17, a movable rod 19 is movably sleeved inside the limiting groove 18, and a soft pad 20 is fixedly installed on one side of the movable rod 19.

[0043] When the limit block 17 clamps parts of different specifications during movement, the force will also push the soft pad 20 to one side, so that the movable rod 19 also slides in the limit groove 18. Through the telescopic push, the soft pad 20 can better fit the surface of the part. The several soft pads 20 on one side of the limit block 17 provide stability and firmness for the limit clamping.

[0044] In the technical solution of the embodiment of the present application, a telescopic spring 21 is fixedly installed on one side of the soft cushion 20 , and the telescopic spring 21 is movably sleeved on the outer wall of the movable rod 19 .

[0045] Through the elasticity of the telescopic spring 21, when the limit block 17 clamps parts of different specifications during movement, the soft pad 20 will also fit the surface of the part, and at the same time, the force will push the soft pad 20 to move to one side, so the elasticity will push the soft pad 20 to better fit the surface of the part, providing stability and firmness for the limit clamping.

[0046] In the technical solution of the embodiment of the present application, the top of the placement plate 10 is symmetrically provided with slots 22 on four sides, and the threaded block 16 is movably sleeved inside the slots 22 .

[0047] The slot 22 allows the limit block 17 to fit on the top of the placement plate 10 and move. At the same time, the thread block 16 also slides in the slot 22 when it moves on the surface of the screw rod 15. The slot 22 also serves to limit the thread block 16, preventing the thread block 16 from being unable to move and rotate synchronously with the screw rod 15.

[0048] Those skilled in the art will appreciate that, although some embodiments herein include certain features included in other embodiments but not other features, the combination of features of different embodiments is meant to be within the scope of the present application and form different embodiments. For example, in the claims, any one of the claimed embodiments may be used in any combination.

[0049] As described above, the above embodiments are only used to illustrate the technical solutions of the present application, rather than to limit them. Although the present application has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present application.

Claims

1. A fixture for aviation aluminum alloy parts of different specifications, characterized in that: include: An operating table, wherein a first motor is fixedly installed at the bottom end of the operating table, a first rotating rod is fixedly installed at the top end of the first motor, the first rotating rod passes through the operating table from the center position, a first gear is fixedly installed at the top end of the first rotating rod, a second gear is meshingly connected to the surface of the first gear, the second gear is installed on the outer wall of the connecting rod, and a placement plate is fixedly installed at the top end of the connecting rod.

2. The fixture for aviation aluminum alloy parts of different specifications according to claim 1 is characterized in that: The surface of the second gear is meshed with a gear belt, which is installed on the inner wall of the groove, and the groove is opened at the center of the top of the operating table.

3. The fixture for aviation aluminum alloy parts of different specifications according to claim 2 is characterized in that: The bottom end of the connecting rod is movably sleeved inside the annular groove, and the annular groove is arranged at the bottom end of the inner wall of the groove.

4. The fixture for aviation aluminum alloy parts of different specifications according to claim 1 is characterized in that: A second motor is installed at the center position of the inner wall of the placement plate, a second rotating rod is fixedly installed on the top of the second motor, a first bevel gear is fixedly installed on the top of the second rotating rod, a second bevel gear is meshingly connected to the surface of the first bevel gear, a screw is fixedly installed on one side of the second bevel gear, a threaded block is threadedly connected to the surface of the screw, and a limiting block is installed on the top of the threaded block.

5. The fixture for aviation aluminum alloy parts of different specifications according to claim 4 is characterized in that: A plurality of limiting grooves are provided on one side of the limiting block, a movable rod is movably sleeved inside the limiting groove, and a soft pad is fixedly installed on one side of the movable rod.

6. The fixture for aviation aluminum alloy parts of different specifications according to claim 5 is characterized in that: A telescopic spring is fixedly mounted on one side of the soft cushion, and the telescopic spring is movably sleeved on the outer wall of the movable rod.

7. The fixture for aviation aluminum alloy parts of different specifications according to claim 1 is characterized in that: The top of the placement plate is symmetrically provided with slots on four sides, and the threaded block is movably sleeved inside the slots.