Tool for aviation parts

Abstract

The utility model discloses a tooling for aeronautical parts, which belongs to the technical field of machining, and comprises two workbenches which are tightly attached to each other and are used for mounting aeronautical part machining equipment, the peripheries of the workbenches are sleeved with a limiting frame, the vertical inner wall of the limiting frame is connected with an assembly plate, and the vertical inner wall of the assembly plate is connected with a clamping plate. A vertical linear motor is connected to the side face of the assembling plate through screws, and a moving part of the vertical linear motor is fixedly connected with the workbench. The top end of the limiting frame is connected with a fixing combination, the bottom end of the limiting frame is welded with a bearing plate, a counterweight plate is arranged below the bearing plate, the top end of the counterweight plate is connected with four transverse linear motors, moving parts of the transverse linear motors are fixedly connected with the bearing plate, and the top end of the counterweight plate is detachably connected with a material receiving box. And sealing gaskets are adhered to the top ends of the material receiving box and the transverse supporting plate. According to the tool for the aviation parts, the size of a gap can be conveniently adjusted, and the tool can adapt to fixing of the aviation parts of different sizes.

Description

Technical Field

[0001] The utility model belongs to the technical field of mechanical processing, in particular to a tooling for aviation parts. Background Art

[0002] When aviation parts are being processed, they need to be fixed with tooling to facilitate subsequent processing. Existing tooling for aviation parts will be adjusted due to usage needs to ensure that it can adapt to aviation parts of different sizes. However, for different aviation parts processing, if waste occurs, a discharge channel needs to be opened for unloading. However, for some processing procedures that do not produce waste, it is troublesome to block the discharge channel, which greatly increases the workload of the staff.

[0003] Chinese patent document (authorization announcement number CN213765597U) A fixture for processing automobile parts, which has the advantages of automation and convenient disassembly and assembly. In actual use, the automated operation facilitates the clamping and reinforcement of automobile parts and improves production efficiency. Although the slide plate can be adjusted, it is a manual operation, which greatly increases the workload of the staff. Utility Model Content

[0004] The utility model aims to provide a tooling for aviation parts to solve the problems raised in the background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a tooling for aviation parts, comprising two closely arranged workbenches for installing aviation parts processing equipment, the outer periphery of the workbenches is sleeved with a limit frame, the vertical inner wall of the limit frame is connected with an assembly plate, the side surface of the assembly plate is screwed with a vertical linear motor, and the moving part of the vertical linear motor is connected and fixed to the workbench;

[0006] The top end of the limit frame is connected to a fixed combination, the bottom end of the limit frame is welded with a bearing plate, a counterweight plate is arranged below the bearing plate, the top end of the counterweight plate is connected to four transverse linear motors, the moving part of the transverse linear motor is fixedly connected to the bearing plate, and the top end of the counterweight plate is detachably connected to a material receiving box.

[0007] As a preferred embodiment, auxiliary support plates are detachably connected to both sides of the material receiving box, and sealing gaskets are bonded to the top ends of the material receiving box and the transverse support plates.

[0008] As a preferred embodiment, an inclined block is welded to the inner wall of the material receiving box, and the inclined block is detachably connected to a filter frame with a filter screen. A plurality of inclined material receiving slide bars are also welded to the inner wall of the material receiving box.

[0009] As a preferred embodiment, a discharge channel is provided on one side of the receiving box, and the discharge channel is rotatably connected to a discharge door through a hinge.

[0010] As a preferred embodiment, the fixed combination includes a mounting plate connected to the top of the limit frame, an adjustable linear motor installed on the side of the mounting plate, and an electric push rod connected to the side of the moving part of the adjustable linear motor. A diagonal support rod for improving stability is connected between the mounting plate and the assembly plate.

[0011] As a preferred embodiment, a motor seat is connected to the side of the moving part of the electric push rod, and a servo motor is installed on the side of the motor seat.

[0012] As a preferred embodiment, the output shaft of the servo motor is connected to a rotating rod, and the side of the rotating rod is connected to a clamping plate for fixing aviation parts.

[0013] Compared with the prior art, the technical effects and advantages of the utility model are as follows:

[0014] The tooling for aviation parts benefits from the design of the limit frame, vertical linear motor and workbench. The sliding design of the limit frame and the workbench improves the convenience of operation. The vertical linear motor can change the distance between the two workbenches, and the exposed gap is convenient for unloading waste materials, which saves time and effort. In addition, the size of the gap is adjustable, which can adapt to the processing of aviation parts of different sizes.

[0015] Thanks to the design of the fixed combination and the transverse linear motor, the linear motor, electric push rod and servo motor can be adjusted to adjust the position of aviation parts to meet different usage needs. The adjustment of the transverse linear motor can change the position of the limit frame, increasing the adaptability of the fixed combination.

[0016] Thanks to the design of the receiving box, the receiving box can receive waste materials and aviation parts. The slide bar facilitates the sliding of aviation parts, and the filter net can filter the waste materials.

[0017] The tooling for aviation parts is not only convenient for adjusting the size of the gap, but also can adapt to the fixation of aviation parts of different sizes. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] In order to more clearly illustrate the specific implementation methods of the utility model or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0019] Figure 1 It is a structural schematic diagram of the utility model;

[0020] Figure 2 It is a right side view of the material receiving box of the utility model;

[0021] Figure 3 It is a top view of the material receiving box of the utility model;

[0022] Figure 4 It is a structural schematic diagram of the fixed combination of the utility model.

[0023] Description of reference numerals:

[0024] In the figure: 1. workbench; 2. limit frame; 3. assembly plate; 4. vertical linear motor; 5. fixed assembly; 6. load-bearing plate; 7. counterweight plate; 8. horizontal linear motor; 9. receiving box; 10. auxiliary support plate; 12. filter frame; 13. receiving slide bar; 14. discharge door;

[0025] 50. Mounting plate; 51. Adjustment linear motor; 52. Electric push rod; 53. Motor seat; 54. Servo motor; 55. Clamping plate; 56. Diagonal support rod. DETAILED DESCRIPTION

[0026] In the following description, a large number of specific details are given to provide a more thorough understanding of the utility model. However, it is obvious to those skilled in the art that the utility model can be implemented without one or more of these details. In other examples, in order to avoid confusion with the utility model, some technical features known in the art are not described.

[0027] Unless otherwise defined, the directions of up, down, left, right, front, back, inside and outside involved in this document are based on the directions of up, down, left, right, front, back, inside and outside in the figures shown in the present utility model, and are explained here together.

[0028] The connection method can be bonding, welding, bolt connection, etc., depending on actual needs.

[0029] In order to adjust the gap between the two workbenches 1 to adapt to processing of different sizes and different needs, such as Figures 1 to 4A tooling for aviation parts shown in the figure comprises two closely arranged workbenches 1 for installing aviation parts processing equipment, the outer periphery of the workbench 1 is sleeved with a limit frame 2, the vertical inner wall of the limit frame 2 is connected with an assembly plate 3, the side screws of the assembly plate 3 are connected with a vertical linear motor 4, the moving part of the vertical linear motor 4 is connected and fixed to the workbench 1, if it is necessary to expose a gap, the vertical linear motor 4 is controlled to drive the workbench 1 to move, exposing a gap of a specified size, and the waste generated by the processing and the processed aviation parts can also fall into the receiving box 9 by gravity.

[0030] In order to be able to adjust the distance between the two limit frames 2, a bearing plate 6 is welded to the bottom end of the limit frame 2, and a counterweight plate 7 is arranged below the bearing plate 6. The counterweight plate 7 is connected and fixed to the ground by multiple fixing bolts. Four transverse linear motors 8 are connected to the top of the counterweight plate 7. The cooperation between the transverse linear motor 8 and the electric push rod 52 enables the clamping plate 50 to fix aviation parts of different sizes. The moving part of the transverse linear motor 8 is connected and fixed to the bearing plate 6, and the top of the counterweight plate 7 is detachably connected to a receiving box 9.

[0031] In order to ensure the sealing performance, auxiliary support plates 10 are detachably connected to both sides of the material receiving box 9, and sealing pads are bonded to the top ends of the material receiving box 9 and the transverse support plates.

[0032] In order to receive waste materials and processed aviation parts, an inclined block is welded to the inner wall of the receiving box 9, and the inclined block is detachably connected to a filter frame 12 with a filter screen. A plurality of inclined receiving slide bars 13 are also welded to the inner wall of the receiving box 9, and the receiving slide bars 13 are arranged above the filter frame 12 to separate the waste materials from the aviation parts. A discharge channel is provided on one side of the receiving box 9, and the discharge channel is connected to a discharge door 14 through a hinge rotation. One side of the receiving box 9 can be connected to an exhaust gas treatment device, similar to a welding smoke processor.

[0033] In order to adjust and fix, a fixing assembly 5 is connected to the top of the limit frame 2, and the fixing assembly 5 includes a mounting plate 50 connected to the top of the limit frame 2, an adjusting linear motor 51 installed on the side of the mounting plate 50, and an electric push rod 52 connected to the side of the moving part of the adjusting linear motor 51. A diagonal support rod 56 for improving stability is connected between the mounting plate 50 and the assembly plate 3. A motor seat 53 is connected to the side of the moving part of the electric push rod 52, and a servo motor 54 is installed on the side of the motor seat 53. The output shaft of the servo motor 54 is connected to a rotating rod, and a clamping plate 55 for fixing aviation parts is connected to the side of the rotating rod. The electric push rod 52 is adjusted to change the distance between the two clamping plates 55, so that the clamping plate 55 can process the aviation parts.

[0034] The electric push rod 52, servo motor 54, auxiliary linear motor 51, lateral linear motor 8 and vertical linear motor 4 are all configured according to the prior art. The working principle, size and model are irrelevant to the function of the present application, so no further description will be given. The control method of the present invention is controlled by a controller. The control circuit of the controller can be realized by simple programming by technicians in this field. The provision of power is also common knowledge in this field. The present invention is mainly used to protect mechanical devices, so the present invention will no longer explain the control method and circuit connection in detail.

[0035] How it works

[0036] The tooling for aviation parts pre-adjusts the auxiliary linear motor 51, the horizontal linear motor 8 and the vertical linear motor 4 according to the needs of use, and then adjusts the electric push rod 52 to change the distance between the two clamping plates 55 so that the clamping plates 55 can process the aviation parts. If a gap needs to be exposed, the vertical linear motor 4 is controlled to drive the workbench 1 to move to expose a gap of a specified size. The waste generated by the processing and the processed aviation parts can also fall into the receiving box 9 due to gravity.

[0037] It should be noted that, in this article, relational terms such as one and two are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions. The sentence "includes an element defined by ... does not exclude the existence of other identical elements in the process, method, article or device including the element".

[0038] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A tooling for aviation parts, comprising two closely arranged workbenches (1) for mounting aviation parts processing equipment, characterized in that: The outer periphery of the workbench (1) is sleeved with a limit frame (2), the vertical inner wall of the limit frame (2) is connected to an assembly plate (3), the side surface of the assembly plate (3) is screw-connected to a vertical linear motor (4), and the moving part of the vertical linear motor (4) is connected and fixed to the workbench (1); The top end of the limit frame (2) is connected to a fixed assembly (5), the bottom end of the limit frame (2) is welded to a bearing plate (6), a counterweight plate (7) is arranged below the bearing plate (6), the top end of the counterweight plate (7) is connected to four transverse linear motors (8), the moving part of the transverse linear motor (8) is fixedly connected to the bearing plate (6), and the top end of the counterweight plate (7) is detachably connected to a material receiving box (9).

2. The tooling for aviation parts according to claim 1, characterized in that: Auxiliary support plates (10) are detachably connected to both sides of the material receiving box (9), and sealing pads are bonded to the top ends of the material receiving box (9) and the transverse support plates.

3. A tooling for aviation parts according to claim 2, characterized in that: An inclined block is welded to the inner wall of the material receiving box (9), and a filter frame (12) with a filter screen is detachably connected to the inclined block. A plurality of inclined material receiving slide bars (13) are also welded to the inner wall of the material receiving box (9).

4. A tooling for aviation parts according to claim 3, characterized in that: A discharge channel is provided on one side of the material receiving box (9), and the discharge channel is rotatably connected to a discharge door (14) via a hinge.

5. The tooling for aviation parts according to claim 1, characterized in that: The fixed assembly (5) comprises a mounting plate (50) connected to the top of the limit frame (2), an adjustable linear motor (51) mounted on the side of the mounting plate (50), and an electric push rod (52) connected to the side of the moving part of the adjustable linear motor (51); a diagonal support rod (56) for improving stability is connected between the mounting plate (50) and the assembly plate (3).

6. A tooling for aviation parts according to claim 5, characterized in that: The side surface of the moving part of the electric push rod (52) is connected to a motor seat (53), and the side surface of the motor seat (53) is installed with a servo motor (54).

7. A tooling for aviation parts according to claim 6, characterized in that: The output shaft of the servo motor (54) is connected to a rotating rod, and the side of the rotating rod is connected to a clamping plate (55) for fixing aviation parts.

Images