Aircraft part machining and positioning device

Abstract

The aircraft part machining and positioning device comprises a base, a workbench is arranged on the base through a rail assembly, a rotating groove is formed in the side wall, away from the base, of the workbench, a rotating block is rotationally connected into the rotating groove, and one end of the rotating block extends out of the rotating groove. A working motor is arranged on the outer wall of one side of the workbench, a working shaft is arranged at the end, close to the rotating groove, of the working motor, the end, away from the working motor, of the working shaft penetrates through the workbench, and the end, away from the working motor, of the working shaft is fixedly connected to the inner wall of the rotating block; a supporting frame is fixedly connected to the side wall, away from the base, of the rotating block, the two ends, away from the base, of the supporting frame are jointly and fixedly connected with a supporting disc, and a supporting motor is arranged on the side wall, close to the supporting frame, of the supporting disc. The direction and the angle of a part can be conveniently adjusted, and then positioning machining work is completed in a matched mode.

Description

Technical Field

[0001] This invention relates to the technical field of aircraft parts processing, and in particular to a positioning device for aircraft parts processing. Background Technology

[0002] An airplane is a heavier-than-air aircraft with wings and one or more engines that can fly in the atmosphere under its own power. The production and manufacturing process of an airplane requires a large number of parts. Different parts of an airplane require different processing methods for their production and processing. In order to effectively ensure the quality of airplane parts processing, corresponding positioning devices are needed for fixing airplane parts.

[0003] While existing devices can move in the left, right, forward, and backward directions in conjunction with processing equipment, the processing requirements for aircraft parts are numerous, involving various tilt angles and directions. To complete such processing work with existing devices, cumbersome installation and fixing operations are required, which is extremely detrimental to the high-quality and efficient operation of aircraft parts.

[0004] Therefore, we propose an aircraft parts processing positioning device to solve the above problems. Summary of the Invention

[0005] The purpose of this invention is to solve the problems existing in the prior art and to propose an aircraft parts processing positioning device.

[0006] To achieve the above objectives, the present invention adopts the following technical solution: A positioning device for processing aircraft parts includes a base. A worktable is mounted on the base via a track assembly. A rotating groove is provided on the side wall of the worktable away from the base. A rotating block is rotatably connected within the rotating groove, with one end of the rotating block extending out of the groove. A working motor is mounted on the outer side wall of the worktable. A working shaft is located at the end of the working motor near the rotating groove. The end of the working shaft away from the working motor passes through the worktable and is fixedly connected to the inner wall of the rotating block. A support frame is fixedly connected to the side wall of the rotating block away from the base. A support plate is fixedly connected to both ends of the support frame away from the base. A support motor is mounted on the side wall of the support plate near the support frame. A support shaft is located at the end of the support motor near the support plate. The end of the support shaft away from the support motor passes through the support plate and is fixedly connected to a mounting plate. Multiple mounting components are provided at the end of the mounting plate away from the support shaft, and these components are arranged symmetrically at the center.

[0007] Preferably, the track assembly includes a base seat mounted on a base. A base groove is provided on the upper surface of the base seat away from the base. A base block is slidably connected within the base groove. The base block has a base threaded opening, and a base threaded post is threadedly connected within the base threaded opening. A base motor is fixedly connected to one outer wall of the base seat, and the base motor is positioned directly opposite the base groove. A base shaft is provided at the end of the base motor near the base groove. The end of the base shaft away from the base motor passes through the base seat. One end of the base threaded post is fixedly connected to the base shaft, and the end of the base threaded post away from the base shaft is rotatably connected to the interior of the base groove on the side away from the base shaft. The base block is located away from the base. A base track is fixedly connected to one side wall of the base. A track groove is provided on the side wall of the base track away from the base. A track block is slidably connected in the track groove. The track block is provided with a track threaded opening. A track threaded post is threaded into the track threaded opening. A track motor is fixedly connected to one side outer wall of the base track. The track motor is positioned directly opposite the track groove. A track shaft is provided at the end of the track motor near the track groove. The end of the track shaft away from the track motor passes through the base track. One end of the track threaded post is fixedly connected to the track shaft. The end of the track threaded post away from the track shaft is rotatably connected to the inner wall of the track groove away from the track shaft. The track block is fixedly connected to the worktable.

[0008] Preferably, the mounting assembly includes a mounting platform fixedly connected to the mounting plate, the mounting platform being located on one side of the mounting plate, the mounting platform having a threaded hole, a threaded rod being threadedly connected to the threaded hole, a rotating groove being provided on one side wall of the threaded rod, a rotating block being rotatably connected in the rotating groove, the rotating groove and the rotating block being configured in a concave-convex fit, a clamping plate being fixedly connected to the side wall of the rotating block away from the rotating groove, and one side wall of the clamping plate being fitted against the mounting plate.

[0009] Preferably, both the base groove and the track groove are concave, and both the base block and the track block are convex. The shape of the base block matches the shape of the base groove, and the shape of the track block matches the shape of the track groove.

[0010] Preferably, the support plate has an annular groove on the side wall away from the base, and a support ring is rotatably connected in the annular groove. The support ring is fixedly connected to the mounting plate.

[0011] Preferably, the upper surface of the base is provided with a plurality of spherical grooves arranged at equal intervals, and each of the plurality of spherical grooves is provided with a rolling ball, and the plurality of rolling balls are all arranged to fit against the outer wall of the base track.

[0012] Compared with the prior art, the beneficial effects of the present invention are: In this invention, after the operator installs the parts on the mounting plate, the working motor controls the working shaft to drive the rotating block to rotate, and the support motor controls the support shaft to drive the mounting plate to rotate. This allows the rotation direction and tilt angle of the parts to be easily adjusted, enabling the parts to cooperate with the processing equipment to complete accurate positioning processing. This greatly ensures the quality and efficiency of aircraft parts processing. At the same time, with the setting of the track assembly, the position of the parts can be easily adjusted, thus enabling the parts to complete accurate processing work better. Attached Figure Description

[0013] Figure 1 This is a front structural cross-sectional view of an aircraft parts processing positioning device proposed in this invention; Figure 2 for Figure 1 Enlarged view of the A-structure in the middle; Figure 3 This is a partial side cross-sectional view of an aircraft parts processing and positioning device proposed in this invention. Figure 4 for Figure 3 Enlarged view of the B-structure; Figure 5 This is a top sectional view of the support plate portion of an aircraft parts processing and positioning device proposed in this invention. Figure 6 This is a side cross-sectional view of the rotating groove portion of an aircraft parts processing and positioning device proposed in this invention.

[0014] In the diagram: 1. Base, 2. Base seat, 3. Base groove, 4. Base block, 5. Base threaded opening, 6. Base threaded column, 7. Base motor, 8. Base shaft, 9. Base rail, 10. Rail groove, 11. Rail block, 12. Rail threaded opening, 13. Rail threaded column, 14. Rail motor, 15. Rail shaft, 16. Worktable, 17. Rotary groove, 18. Rotary block, 19. Work motor, 20. Work shaft, 21. Support frame, 22. Support plate, 23. Support motor, 24. Support shaft, 25. Mounting plate, 26. Mounting platform, 27. Threaded hole, 28. Threaded rod, 29. Clamping plate, 30. Annular groove, 31. Support ring, 32. Spherical groove, 33. Rolling ball, 34. Rotating groove, 35. Rotating block. Detailed Implementation

[0015] The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present invention. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments.

[0016] Reference Figures 1-6A positioning device for processing aircraft parts includes a base 1. A worktable 16 is mounted on the base 1 via a track assembly. The track assembly includes a base seat 2 mounted on the base 1. A base groove 3 is provided on the upper surface of the base seat 2 away from the base 1. A base block 4 is slidably connected within the base groove 3. A base threaded opening 5 is provided on the base block 4. A base threaded post 6 is threadedly connected to the base threaded opening 5. A base motor 7 is fixedly connected to one outer wall of the base seat 2, directly opposite the base groove 3. A base shaft 8 is provided at one end of the base motor 7 near the base groove 3. The end of the base shaft 8 away from the base motor 7 passes through the base seat 2. One end of the base threaded post 6 is fixedly connected to the base shaft 8. The base 4 is rotatably connected to the inside of the base groove 3 on the side away from the base shaft 8. The base block 4 is fixedly connected to the side wall away from the base 1. The upper surface of the base 2 is provided with multiple spherical grooves 32 arranged at equal intervals. Rolling is provided in each of the multiple spherical grooves 32, which makes the base track 9 slide better. The side wall away from the base 1 of the base track 9 is provided with a track groove 10. The track block 11 is slidably connected in the track groove 10. The base groove 3 and the track groove 10 are both concave. The base block 4 and the track block 11 are both convex. The shape of the base block 4 matches the shape of the base groove 3. The shape of the track block 11 matches the shape of the track groove 10. This makes the sliding operation more stable and prevents the problem of separation. The track block 11 is provided with a track threaded opening 12, and a track threaded post 13 is internally threaded into the track threaded opening 12. A track motor 14 is fixedly connected to the outer wall of one side of the base track 9. The track motor 14 is positioned directly opposite the track groove 10. A track shaft 15 is provided at the end of the track motor 14 near the track groove 10. The end of the track shaft 15 away from the track motor 14 passes through the base track 9. One end of the track threaded post 13 is fixedly connected to the track shaft 15, and the end of the track threaded post 13 away from the track shaft 15 is rotatably connected to the inner wall of the track groove 10 away from the track shaft 15. The track block 11 is fixedly connected to the worktable 16, which allows for smooth forward, backward, left, and right movement. This enables the parts to cooperate with the processing equipment to complete different parts of the processing work. A rotating groove 17 is provided on the side wall of the worktable 16 away from the base 1. A rotating block 18 is rotatably connected within the rotating groove 17, and one end of the rotating block 18 extends out of the rotating groove 17. A working motor 19 is provided on one outer wall of the worktable 16. A working shaft 20 is provided at one end of the working motor 19 near the rotating slot 17. The end of the working shaft 20 away from the working motor 19 passes through the worktable 16. The end of the working shaft 20 away from the working motor 19 is fixedly connected to the inner wall of the rotating block 18. A support frame 21 is fixedly connected to the side wall of the rotating block 18 away from the base 1. A support plate 22 is fixedly connected to both ends of the support frame 21 away from the base 1. A support motor 23 is provided on the side wall of the support plate 22 near the support frame 21. A support shaft 24 is provided at one end of the support motor 23 near the support plate 22. The end of the support shaft 24 away from the support motor 23 passes through the support plate 22. A mounting plate 25 is fixedly connected to the end of the support shaft 24 away from the support motor 23. This allows for effective adjustment of the tilt angle and direction. At the same time, this adjustment is more accurate and stable, greatly facilitating the workers to complete the processing work efficiently and with high quality. An annular groove 30 is provided on the side wall of the support plate 22 away from the base 1. A support ring 31 is rotatably connected in the annular groove 30. The support ring 31 is fixedly connected to the mounting plate 25, which makes the rotation of the mounting plate 25 more stable. Multiple mounting components are provided on the end of the mounting plate 25 away from the support shaft 24. The multiple mounting components are arranged in a centrally symmetrical manner. The mounting components include a mounting platform 26 fixedly connected to the mounting plate 25. The mounting platform 26 is located on one side of the mounting plate 25. The mounting platform 26 is provided with a threaded hole 27. A threaded rod 28 is threadedly connected in the threaded hole 27. A rotating groove 34 is provided on one side wall of the threaded rod 28. A rotating block 35 is rotatably connected in the rotating groove 34. The rotating groove 34 and the rotating block 35 are arranged in a concave-convex fit. A clamping plate 29 is fixedly connected to the side wall of the rotating block 35 away from the rotating groove 34. One side wall of the clamping plate 29 is set to fit against the mounting plate 25. In this way, the clamping and fixing of parts can be completed smoothly, so that the processing work can be completed stably.

[0017] In the process of using this invention, the operator first places the corresponding parts on the mounting plate 25, so that the parts fall between multiple mounting platforms 26. Then, the operator can rotate multiple threaded rods 28. When the multiple threaded rods 28 rotate in the corresponding threaded holes 27, the multiple threaded rods 28 can push multiple clamping plates 29 closer to each other, so that the multiple clamping plates 29 can complete the clamping and fixing of the parts. In this way, the initial installation of the parts is successfully completed. Subsequently, when the device is used in conjunction with the processing equipment for processing, the base motor 7 can control the rotation of the base threaded column 6 through the base shaft 8. Then, when the base threaded column 6 rotates in the base threaded opening 5, it can drive the base block 4 to slide to the appropriate position in the base groove 3. The track motor 14 can control the rotation of the track threaded column 13 through the track shaft 15. When the track threaded column 13 rotates in the track threaded opening 12, it can drive the track block 11 to slide in the track groove 10, and then drive the worktable 16 to move along the base track 9. This coordinated setup allows for smooth movement of components in all directions, enabling them to work in conjunction with processing equipment to complete different processing tasks. Simultaneously, the support motor 23 can drive the mounting plate 25 to rotate via the support shaft 24, which in turn rotates the fixed components to the appropriate direction. Furthermore, the working motor 19 can control the working shaft 20 to drive the rotating block 18 to rotate within the rotating groove 17, which in turn drives the support plate 22 and the fixed components to tilt and rotate via the support frame 21. This allows the components to work in conjunction with the processing equipment to complete processing tasks at different tilt angles, greatly satisfying the processing needs of the workers. It also enables multi-angle, multi-directional processing to be completed more accurately, efficiently, and with higher quality.

[0018] The above description is only a preferred embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any equivalent substitutions or modifications made by those skilled in the art within the scope of the technology disclosed in the present invention, based on the technical solution and inventive concept of the present invention, should be covered within the scope of protection of the present invention.

Claims

1. A positioning device for processing aircraft parts, comprising a base (1), characterized in that, The base (1) is provided with a worktable (16) via a track assembly. A rotating groove (17) is provided on the side wall of the worktable (16) away from the base (1). A rotating block (18) is rotatably connected in the rotating groove (17). One end of the rotating block (18) extends out of the rotating groove (17). A working motor (19) is provided on the outer side wall of the worktable (16). A working shaft (20) is provided at the end of the working motor (19) near the rotating groove (17). The end of the working shaft (20) away from the working motor (19) passes through the worktable (16). The end of the working shaft (20) away from the working motor (19) is fixedly connected to the inner wall of the rotating block (18). 8) A support frame (21) is fixedly connected to the side wall away from the base (1). The two ends of the support frame (21) away from the base (1) are fixedly connected to a support plate (22). A support motor (23) is provided on the side wall of the support plate (22) near the support frame (21). A support shaft (24) is provided at the end of the support motor (23) near the support plate (22). The end of the support shaft (24) away from the support motor (23) passes through the support plate (22). An installation plate (25) is fixedly connected at the end of the support shaft (24) away from the support motor (23). Multiple installation components are provided at the end of the installation plate (25) away from the support shaft (24). The multiple installation components are arranged in a centrally symmetrical manner.

2. The aircraft parts processing positioning device according to claim 1, characterized in that, The track assembly includes a base seat (2) mounted on a base (1). A base groove (3) is provided on the upper surface of the base seat (2) away from the base (1). A base block (4) is slidably connected within the base groove (3). A base threaded opening (5) is provided on the base block (4). A base threaded post (6) is threadedly connected within the base threaded opening (5). A base motor (7) is fixedly connected to one outer wall of the base seat (2). The base motor (7) is positioned opposite the base groove (3). A base shaft (8) is provided at one end of the base motor (7) near the base groove (3). The end of the base shaft (8) away from the base motor (7) passes through the base seat (2). One end of the base threaded post (6) is fixedly connected to the base shaft (8). The end of the base threaded post (6) away from the base shaft (8) is rotatably connected to the interior of the base groove (3) away from the base shaft (8). A base track is fixedly connected to one side wall of the base block (4) away from the base (1). The basic track (9) has a track groove (10) on the side wall away from the base (1). A track block (11) is slidably connected in the track groove (10). A track threaded opening (12) is provided on the track block (11). A track threaded column (13) is threadedly connected in the track threaded opening (12). A track motor (14) is fixedly connected to the outer wall of one side of the basic track (9). The track motor (14) is set opposite to the track groove (10). A track shaft (15) is provided at the end of the track motor (14) near the track groove (10). The end of the track shaft (15) away from the track motor (14) passes through the basic track (9). One end of the track threaded column (13) is fixedly connected to the track shaft (15). The end of the track threaded column (13) away from the track shaft (15) is rotatably connected to the inner wall of the track groove (10) away from the track shaft (15). The track block (11) is fixedly connected to the workbench (16).

3. The aircraft parts processing positioning device according to claim 1, characterized in that, The mounting assembly includes a mounting platform (26) fixedly connected to the mounting plate (25). The mounting platform (26) is located on one side of the mounting plate (25). The mounting platform (26) is provided with a threaded hole (27). A threaded rod (28) is threadedly connected in the threaded hole (27). A rotating groove (34) is provided on one side wall of the threaded rod (28). A rotating block (35) is rotatably connected in the rotating groove (34). The rotating groove (34) and the rotating block (35) are arranged in a concave-convex fit. A clamping plate (29) is fixedly connected on the side wall of the rotating block (35) away from the rotating groove (34). The side wall of the clamping plate (29) is set to fit against the mounting plate (25).

4. The aircraft parts processing positioning device according to claim 2, characterized in that, The base groove (3) and the track groove (10) are both concave, the base block (4) and the track block (11) are both convex, the shape of the base block (4) matches the shape of the base groove (3), and the shape of the track block (11) matches the shape of the track groove (10).

5. The aircraft parts processing positioning device according to claim 1, characterized in that, The support plate (22) has an annular groove (30) on one side wall away from the base (1), and a support ring (31) is rotatably connected in the annular groove (30). The support ring (31) is fixedly connected to the mounting plate (25).

6. The aircraft parts processing positioning device according to claim 2, characterized in that, The upper surface of the base (2) is provided with a plurality of spherical grooves (32) arranged at equal intervals, and each of the plurality of spherical grooves (32) is provided with a rolling ball (33), and the plurality of rolling balls (33) are all arranged to fit against the outer wall of the base track (9).

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