A rotary wing integrated molding device

Abstract

The utility model relates to automatic door rotating wing technical field especially relates to a rotating wing integrated forming device. Including the body, the outer wall fixed connection of body has the fixing frame, the outer wall fixed connection of fixing frame has the first motor, the output fixed setting of first motor has the worm, the tooth end of worm has the worm wheel and engages, the inside fixed connection of worm wheel has the support column, the outer wall fixed connection of support column has the support block, the inside screw thread connection of body has the bolt, the inside fixed connection of support block has the fixed block, the upper surface of fixed block is provided with adjusting assembly. The utility model provides a kind of rotating wing integrated forming device, start first motor drive worm and worm wheel rotation, after the fixed rotating wing body is overturned, without turning over rotating wing body, it can be welded to different face thereof, ensure the accuracy of welding position, reduce the welding defect caused by inaccurate welding position, improve finished product quality.

Description

Technical Field

[0001] This utility model relates to the field of automatic door rotating wing technology, and in particular to a rotating wing integral molding device. Background Technology

[0002] An automatic door is a general term for a door system that uses signal acquisition and external power to control the opening and closing of the door panels, allowing people to pass through. The rotating vane is an important component of a revolving automatic door, referring to the door panel that rotates around a center within a fixed curved wall.

[0003] A rotor molding apparatus is a device used to manufacture rotors. It can fix the various components of the rotor before aligning and welding them. Precise alignment and welding can reduce defects in the assembly process, such as component misalignment and loosening, thereby improving the overall quality of the product. In existing rotor molding technologies, manual alignment of the rotor parts is often used before welding, which is prone to misalignment during the docking process, affecting the accuracy of subsequent welding. Utility Model Content

[0004] Therefore, it is necessary to provide a rotor integral molding device to address the above-mentioned technical problems, in order to solve the technical problem that the existing rotor molding technology often adopts the method of manually aligning the rotor parts and then welding them, which is prone to misalignment during the docking process and affects the subsequent welding accuracy.

[0005] To solve the above-mentioned technical problems, the present invention adopts the following technical solution:

[0006] A rotary wing integrated molding device includes a body, a fixed frame fixedly connected to the outer wall of the body, a first motor fixedly connected to the outer wall of the fixed frame, a worm gear fixedly mounted at the output end of the first motor, the outer wall of the worm gear rotatably connected to both sides of the fixed frame, a worm wheel meshing with the tooth end of the worm gear, a support column fixedly connected inside the worm wheel, the outer wall of the support column rotatably connected to the inside of the body, a support block fixedly connected to the outer wall of the support column, a bolt threadedly connected inside the body, the outer wall of the bolt threadedly connected to the inside of the support column, a fixed block fixedly connected inside the support block, and an adjustment component provided on the upper surface of the fixed block.

[0007] In a preferred embodiment of the rotary wing integral molding device provided by this utility model, the adjustment component includes a fixed frame, the lower surface of which is fixedly connected to the upper surface of a fixed block, the outer wall of which is fixedly connected to the interior of a support block, a second motor fixedly connected to the outer wall of the fixed block, a first bidirectional lead screw fixedly provided at the output end of the second motor, both ends of which are rotatably connected to the interior of the fixed block, a first threaded block threadedly connected to the outer wall of the first bidirectional lead screw, the outer wall of which is slidably connected to the inner wall of the fixed block and the fixed frame, a first placement block fixedly connected to the upper surface of the first threaded block, and a rotary wing body slidably connected to the upper surface of the first placement block.

[0008] In a preferred embodiment of the rotary wing integral molding device provided by this utility model, a support frame is fixedly connected to the upper surface of the fixed frame, a third motor is fixedly connected to the outer wall of the support frame, a second bidirectional lead screw is fixedly provided at the output end of the third motor, the two ends of the second bidirectional lead screw are rotatably connected to the inside of the support frame, a second threaded block is threadedly connected to the outer wall of the second bidirectional lead screw, the outer wall of the second threaded block is slidably connected to the inner wall of the support frame, and a second placement block is fixedly connected to the upper surface of the second threaded block.

[0009] In a preferred embodiment of the rotary wing integral molding device provided by this utility model, the outer wall of the rotary wing body is slidably connected to the upper surface of the second placement block, and the outer walls of both the first placement block and the second placement block are provided with fixing components.

[0010] In a preferred embodiment of the rotary wing integral molding device provided by this utility model, the fixing component includes a connecting plate, the outer wall of the connecting plate is fixedly connected to the outer walls of the first placement block and the second placement block, and a fixing cylinder is fixedly connected to the outer wall of the connecting plate, the fixing cylinder having a sliding groove inside.

[0011] In a preferred embodiment of the rotary wing integral molding device provided by this utility model, a slide rod is slidably connected inside the fixed cylinder, a rotating block is fixedly connected to the top of the slide rod, a fixed shaft is fixedly connected to the outer wall of the slide rod, and the outer wall of the fixed shaft is slidably connected to the inner wall of the slide groove.

[0012] In a preferred embodiment of the rotary wing integral molding device provided by this utility model, a pressure block is fixedly connected to the bottom of the slide rod, and the bottom of the pressure block is slidably connected to the upper surface of the rotary wing body.

[0013] In a preferred embodiment of the rotary wing integral molding device provided by this utility model, a spring is slidably connected to the outer wall of the slide rod, one end of the spring is fixedly connected to the bottom of the fixed cylinder, and the other end of the spring is fixedly connected to the top of the pressure block.

[0014] It is clear without a doubt that the technical solution described above in this application can solve the technical problem that this application aims to address.

[0015] At the same time, through the above technical solutions, this utility model has at least the following beneficial effects:

[0016] This utility model provides a rotary wing integrated molding device. The first motor drives the worm gear and worm wheel to rotate, and flips the fixed rotary wing body. Different surfaces can be welded without flipping the rotary wing body, ensuring the accuracy of the welding position, reducing welding defects caused by inaccurate welding position, and improving the quality of the finished product.

[0017] This invention places the various parts of the rotor body on the first placement block and the second placement block. Rotating the rotating block drives the sliding column to rotate and slide. The rotor body is pressed and fixed by the pressure block. Then, the positions of the first placement block and the second placement block are adjusted to achieve precise docking of the rotor body, reduce assembly errors caused by inaccurate component positions, and facilitate subsequent processing. Attached Figure Description

[0018] To more clearly illustrate the technical solutions of the embodiments of this utility model, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0019] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0020] Figure 2 This is a partial structural diagram of the support block of this utility model;

[0021] Figure 3 This is a partial structural diagram of the support column of this utility model;

[0022] Figure 4 This is a partial structural diagram of the first placement block of this utility model;

[0023] Figure 5 This is a partial structural diagram of the fixing component of this utility model;

[0024] Figure 6 This is a schematic diagram of the internal structure of the fixed cylinder of this utility model.

[0025] In the diagram: 1. Airframe; 2. Fixing frame; 3. First motor; 4. Worm gear; 5. Worm wheel; 6. Support column; 7. Support block; 8. Bolt; 9. Fixing block; 10. Support frame; 11. Adjustment assembly; 1101. Fixing frame; 1102. Second motor; 1103. First double-acting lead screw; 1104. First threaded block; 12. First placement block; 13. Rotary wing body; 14. Third motor; 15. Second double-acting lead screw; 16. Second threaded block; 17. Fixing assembly; 18. Connecting plate; 19. Fixing cylinder; 20. Slide groove; 21. Slide rod; 22. Rotating block; 23. Fixing shaft; 24. Pressure block; 25. Spring; 26. Second placement block. Detailed Implementation

[0026] To make the objectives, technical solutions, and advantages of this utility model clearer, the present utility model will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present utility model and are not intended to limit the present utility model.

[0027] To enable those skilled in the art to better understand the present invention, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings.

[0028] It should be noted that, unless otherwise specified, the embodiments and features and technical solutions in the present invention can be combined with each other.

[0029] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0030] Reference Figures 1-6 A rotary wing integrated molding device includes a body 1, a fixing frame 2 fixedly connected to the outer wall of the body 1, a first motor 3 fixedly connected to the outer wall of the fixing frame 2, the fixing frame 2 fixed to the outer wall of the body 1 to support and fix the first motor 3, a worm gear 4 fixedly installed at the output end of the first motor 3, the outer wall of the worm gear 4 rotatably connected to both sides of the fixing frame 2, a worm wheel 5 meshing with the tooth end of the worm gear 4, a support column 6 fixedly connected inside the worm wheel 5, the outer wall of the support column 6 rotatably connected to the inside of the body 1, the support column 6 rotatably inside the body 1 to support and fix the worm wheel 5, a support block 7 fixedly connected to the outer wall of the support column 6, a bolt 8 threadedly connected to the inside of the body 1, the outer wall of the bolt 8 threadedly connected to the inside of the support column 6, a fixing block 9 fixedly connected to the inside of the support block 7, and an adjustment component 11 provided on the upper surface of the fixing block 9.

[0031] The usage process of the one-piece rotary wing molding device provided by this utility model is as follows:

[0032] After fixing the various parts of the rotor body 13 to the first placement block 12 and the second placement block 26, welding can be performed at the four corner joints of the rotor body 13. When welding is required on the other side of the rotor body 13, there is no need to adjust the rotor body 13 itself. Rotate the bolts 8 on both sides of the body 1 to make them slide out from inside the support column 6, release the limiting fixation of the support column 6, start the first motor 3 to drive the worm 4 to rotate stably inside the fixed frame 2. The tooth end of the worm 4 meshes with the worm wheel 5. When it rotates, it will drive the worm wheel 5 to rotate as well, and the rotation of the worm wheel 5 will drive the internal support column 6. The synchronous rotation of the support column 6 causes the support block 7 on the outer wall to rotate synchronously. This, in turn, causes the fixed rotor body 13 to rotate to an angle suitable for welding through the connection of the components above. The bolt 8 is then rotated in the opposite direction to slide into the support column 6. At this point, the position of the support column 6 inside the body 1 is limited and fixed, preventing it from rotating further and ensuring stability during the welding process. Welding can be performed on different surfaces without flipping the rotor body 13, ensuring the accuracy of the welding position, reducing welding defects caused by inaccurate welding positions, and improving the quality of the finished product.

[0033] Reference Figure 1 and Figure 2 and Figure 4The adjusting assembly 11 includes a fixed frame 1101, the lower surface of which is fixedly connected to the upper surface of a fixed block 9. The outer wall of the fixed frame 1101 is fixedly connected to the interior of a support block 7. A second motor 1102 is fixedly connected to the outer wall of the fixed block 9, which serves to fix the second motor 1102. A first bidirectional lead screw 1103 is fixedly installed at the output end of the second motor 1102. Both ends of the first bidirectional lead screw 1103 are rotatably connected to the interior of the fixed block 9. A first threaded block 1104 is threadedly connected to the outer wall of the first bidirectional lead screw 1103. The outer wall of the first threaded block 1104 is slidably connected to the inner walls of the fixed block 9 and the fixed frame 1101. A second threaded block 1104 is fixedly connected to the upper surface of the first threaded block 1104. A placement block 12 is fixed by a first threaded block 1104. A rotating wing body 13 is slidably connected to the upper surface of the first placement block 12. A support frame 10 is fixedly connected to the upper surface of a fixed frame 1101. A third motor 14 is fixedly connected to the outer wall of the support frame 10. A second bidirectional lead screw 15 is fixedly installed at the output end of the third motor 14. The two ends of the second bidirectional lead screw 15 are rotatably connected to the inside of the support frame 10. The support frame 10 supports the second bidirectional lead screw 15. A second threaded block 16 is threadedly connected to the outer wall of the second bidirectional lead screw 15. The outer wall of the second threaded block 16 is slidably connected to the inner wall of the support frame 10. A second placement block 26 is fixedly connected to the upper surface of the second threaded block 16.

[0034] The usage process of the one-piece rotary wing molding device provided by this utility model is as follows:

[0035] The positions of the first placement block 12 and the second placement block 26 can be adjusted according to the different dimensions of the rotating wing body 13. The second motor 1102 is started to drive the first bidirectional lead screw 1103 to rotate inside the fixed block 9. When the first bidirectional lead screw 1103 rotates, it will drive the first threaded blocks 1104 on both sides to slide against the inner wall of the fixed frame 1101 and the fixed block 9, limiting the movement of the first threaded blocks 1104 and preventing deviation during the sliding process. During the sliding process, the first threaded blocks 1104 on both sides will drive the first placement block 12 and the fixed rotating wing. Simultaneously, the main body 13 slides. Similarly, the third motor 14 is started to drive the second bidirectional lead screw 15 to rotate inside the support frame 10. When the second bidirectional lead screw 15 rotates, it will drive the second threaded block 16 to slide against the inner wall of the support frame 10. Similarly, the sliding of the second threaded block 16 is limited. The sliding of the second threaded blocks 16 on both sides can drive the upper second placement block 26 and the rotating wing body 13 to slide. By adjusting the position of the first placement block 12 and the second placement block 26, the precise docking of the rotating wing body 13 can be achieved, ensuring the accuracy of the subsequent welding process.

[0036] Reference Figures 4-6The outer wall of the rotor body 13 is slidably connected to the upper surface of the second placement block 26. The outer walls of the first placement block 12 and the second placement block 26 are both provided with fixing components 17. The fixing components 17 include a connecting plate 18, the outer wall of the connecting plate 18 is fixedly connected to the outer walls of the first placement block 12 and the second placement block 26, and a fixing cylinder 19 is fixedly connected to the outer wall of the connecting plate 18. The inside of the fixing cylinder 19 is provided with a sliding groove 20. A sliding rod 21 is slidably connected inside the fixing cylinder 19. A rotating block 22 is fixedly connected to the top of the sliding rod 21. A fixing shaft 23 is fixedly connected to the outer wall of the sliding rod 21. The outer wall of the fixing shaft 23 is slidably connected to the inner wall of the sliding groove 20. A pressure block 24 is fixedly connected to the bottom of the sliding rod 21. The bottom of the pressure block 24 is slidably connected to the upper surface of the rotor body 13. A spring 25 is slidably connected to the outer wall of the sliding rod 21. One end of the spring 25 is fixedly connected to the bottom of the fixing cylinder 19, and the other end of the spring 25 is fixedly connected to the top of the pressure block 24.

[0037] The usage process of the one-piece rotary wing molding device provided by this utility model is as follows:

[0038] Both the first placement block 12 and the second placement block 26 are equipped with fixing components 17 for fixing the rotor body 13. When it is necessary to press and fix the rotor body 13, the rotating block 22 is rotated to drive the sliding rod 21 and the fixing shaft 23 on its outer wall to rotate. The fixing cylinder 19 has a sliding groove 20 inside. When the fixing shaft 23 rotates, it will slide along the trajectory of the sliding groove 20 on its inner wall. The sliding rod 21 will rotate and slide inside the fixing cylinder 19, and gradually release the restriction on the spring 25 during this process. During the sliding process, the sliding rod 21 will also drive the pressure block 24 to slide. The spring 25 plays a rebound pushing role. When it is not restricted, it will push the pressure block 24 to slide in the opposite direction through its own rebound. The pressure block 24 can press and fix the rotor body 13. After fixing, the alignment between the parts of the rotor body 13 can be performed to improve the finished product quality of the rotor body 13, ensure the precise position of each part of the rotor body 13, reduce the assembly error caused by inaccurate part position, and facilitate subsequent processing.

[0039] In this embodiment, each structure has its own service life. In actual manufacturing and application, the corresponding structure made of different materials can be replaced according to the needs of use.

[0040] In this embodiment, the first motor 3, the second motor 1102, and the third motor 14 are self-locking motors. When they are powered on, they can drive the connected structure to rotate normally. When the first motor 3, the second motor 1102, and the third motor 14 stop working, they can prevent the connected structure from rotating through their self-locking function.

[0041] The preferred embodiments of this utility model disclosed above are merely illustrative of the present utility model. These preferred embodiments do not exhaustively describe all details, nor do they limit the present utility model to the specific implementations described. Clearly, many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of the present utility model, thereby enabling those skilled in the art to better understand and utilize it. This utility model is limited only by the claims and their full scope and equivalents.

Claims

1. A one-piece molded rotary wing device, comprising a fuselage (1), characterized in that, A fixed frame (2) is fixedly connected to the outer wall of the body (1). A first motor (3) is fixedly connected to the outer wall of the fixed frame (2). A worm (4) is fixedly installed at the output end of the first motor (3). The outer wall of the worm (4) is rotatably connected to both sides of the fixed frame (2). A worm wheel (5) is meshed with the tooth end of the worm (4). A support column (6) is fixedly connected inside the worm wheel (5). The outer wall of the support column (6) is rotatably connected to the inside of the body (1). A support block (7) is fixedly connected to the outer wall of the support column (6). A bolt (8) is threadedly connected inside the body (1). The outer wall of the bolt (8) is threadedly connected to the inside of the support column (6). A fixed block (9) is fixedly connected inside the support block (7). An adjustment component (11) is provided on the upper surface of the fixed block (9).

2. The rotary wing integral molding device according to claim 1, characterized in that, The adjustment component (11) includes a fixed frame (1101), the lower surface of which is fixedly connected to the upper surface of the fixed block (9), the outer wall of which is fixedly connected to the inside of the support block (7), the outer wall of which is fixedly connected to a second motor (1102), the output end of which is fixedly provided with a first bidirectional lead screw (1103), the two ends of which are rotatably connected to the inside of the fixed block (9), the outer wall of which is threadedly connected to a first threaded block (1104), the outer wall of which is slidably connected to the inner wall of the fixed block (9) and the fixed frame (1101), the upper surface of which is fixedly connected to a first placement block (12), and the upper surface of which is slidably connected to a rotating wing body (13).

3. The rotary wing integral molding device according to claim 2, characterized in that, A support frame (10) is fixedly connected to the upper surface of the fixed frame (1101). A third motor (14) is fixedly connected to the outer wall of the support frame (10). A second bidirectional lead screw (15) is fixedly installed at the output end of the third motor (14). The two ends of the second bidirectional lead screw (15) are rotatably connected to the inside of the support frame (10). A second threaded block (16) is threadedly connected to the outer wall of the second bidirectional lead screw (15). The outer wall of the second threaded block (16) is slidably connected to the inner wall of the support frame (10). A second placement block (26) is fixedly connected to the upper surface of the second threaded block (16).

4. The rotary wing integral molding device according to claim 2, characterized in that, The outer wall of the rotating wing body (13) is slidably connected to the upper surface of the second placement block (26), and the outer walls of the first placement block (12) and the second placement block (26) are both provided with fixing components (17).

5. The rotary wing integral molding device according to claim 4, characterized in that, The fixing component (17) includes a connecting plate (18), the outer wall of which is fixedly connected to the outer walls of the first placement block (12) and the second placement block (26), and a fixing cylinder (19) is fixedly connected to the outer wall of the connecting plate (18), and a sliding groove (20) is provided inside the fixing cylinder (19).

6. The rotary wing integral molding device according to claim 5, characterized in that, The fixed cylinder (19) is slidably connected to a slide rod (21), the top of the slide rod (21) is fixedly connected to a rotating block (22), the outer wall of the slide rod (21) is fixedly connected to a fixed shaft (23), and the outer wall of the fixed shaft (23) is slidably connected to the inner wall of the slide groove (20).

7. The rotary wing integral molding device according to claim 6, characterized in that, The bottom of the slide bar (21) is fixedly connected to a pressure block (24), and the bottom of the pressure block (24) is slidably connected to the upper surface of the rotor body (13).

8. The rotary wing integral molding device according to claim 6, characterized in that, A spring (25) is slidably connected to the outer wall of the slide rod (21). One end of the spring (25) is fixedly connected to the bottom of the fixed cylinder (19), and the other end of the spring (25) is fixedly connected to the top of the pressure block (24).

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