Turbine sprue cutting tool
By designing the turbine gate cutting tool, using automatic cylinder clamping and laser pen positioning, the problem of position deviation during the cutting process of the turbine gate workpiece is solved, and efficient and accurate cutting effect is achieved.
Patent Information
- Application Number
- CN202422229804.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-12
- Publication Date
- 2025-08-12
- Estimated Expiration
- 2034-09-12
AI Technical Summary
In the prior art, operators have high technical requirements during the cutting process of turbine gate workpieces, and the cutting position is prone to deviations, resulting in product scrapping.
A turbo gate cutting tool is designed, and the workpiece is automatically clamped by a cylinder-driven indexing plate compression seat, and the cutting position is quickly positioned through a laser pointer, combining anti-rotation components and limit sleeves to improve the accuracy of the cutting position.
It improves operating efficiency and accuracy of cutting position, reduces operation difficulty, and improves product yield.
Smart Images
Figure CN223210923U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of turbine manufacturing equipment, in particular to a turbine gate cutting tool. Background Art
[0002] Currently, the workshop mainly uses handheld cutting machines to cut turbine gate workpieces, which places high technical requirements on the operators. In addition, the product is manually pressed during the cutting process, which can easily cause the workpiece to move during the cutting process, resulting in deviations in the cutting position, and ultimately causing the product to be cut and scrapped.
[0003] Therefore, it is urgent to design a turbine gate cutting tool that can improve cutting efficiency. Utility Model Content
[0004] The purpose of the utility model is to provide a turbine gate cutting tool, which drives its output shaft through a cylinder to drive the indexing plate clamping seat to press the turbine gate workpiece into the limit sleeve, automatically clamping the workpiece, improving operating efficiency, and reducing the operating difficulty of the operator; by rotating the indexing plate clamping seat, the operation is convenient, and the purpose of quickly locating the cutting position of the product is achieved, thereby improving operating efficiency; through the design of the laser pen, the infrared rays emitted by the laser pen are used to quickly locate the cutting position of the cutting blade, thereby improving the accuracy of the cutting position on the turbine gate workpiece and the product yield.
[0005] The cam is provided with a plurality of guide wheels, and the guide wheels are provided with a plurality of guide wheels, and the guide wheels are connected with the guide wheels respectively.
[0006] A sliding frame is provided on one side of the base, and the laser pen is mounted on the sliding frame. The end point of the ray of the laser pen corresponds to the cutting position of the cutting blade on the turbine gate workpiece.
[0007] Furthermore, a plurality of locking grooves are provided on the outer surface of the dividing plate pressing seat, and the anti-rotation assembly includes a connecting plate and a locking pin. The connecting plate is fixedly arranged on one side of the cylinder mounting seat, and the locking pin passes through the connecting plate and extends into any one of the locking grooves. The locking pin is connected to the connecting plate by threads.
[0008] Furthermore, the locking pin and the connecting plate are fastened by a locking nut 1, a gasket and a locking nut 2.
[0009] Furthermore, a plurality of the locking grooves are arranged at equal distances along the circumferential direction.
[0010] Furthermore, the connecting shaft and the dividing plate pressing seat are integrally formed, and a through hole communicating with the placement slot and the inner hole of the connecting shaft is opened in the placement slot and the dividing plate pressing seat, and a screw is provided in the through hole, and the screw is used to connect the output shaft of the cylinder and the connecting shaft.
[0011] Furthermore, a sliding groove is provided on the base, and the limiting seat is slidably connected in the sliding groove.
[0012] Furthermore, the sliding frame is provided with a sliding block slidably connected thereto, and the laser pen is mounted on the sliding block.
[0013] Furthermore, a limiting groove is provided in the limiting sleeve, the limiting groove is conical, and one end of the turbine gate workpiece is placed in the limiting groove.
[0014] The beneficial effects of the utility model are:
[0015] 1. The utility model drives the output shaft of the cylinder to drive the indexing plate pressing seat to press the turbine gate workpiece into the limit sleeve, which can automatically clamp the workpiece, improve operating efficiency, solve the problem of current manual clamping that is time-consuming and labor-intensive, and improve operating efficiency; and through the design of the laser pen, the cutting position of the cutting blade can be quickly located through the infrared rays emitted by the laser pen, thereby improving the accuracy of the cutting position on the turbine gate workpiece and the product yield.
[0016] 2. Through the design of the indexing plate, the connecting shaft and the cylinder connecting shaft, the utility model can manually rotate the indexing plate clamping seat to the cutting position on the turbine gate workpiece, thereby achieving the purpose of adjusting the positioning of the product to different cutting positions; and can lock the position of the indexing plate clamping seat by inserting the locking pin in the anti-rotation component into the lock groove, thereby preventing the turbine gate workpiece from moving during the cutting process, thereby improving the accuracy of the product cutting position and the yield rate.
[0017] 3. The utility model provides a limiting groove in the limiting sleeve, and one end of the turbine gate workpiece is placed in the limiting groove. The limiting groove is conical. This design can drive the turbine gate workpiece to rotate in the limiting groove by rotating the dividing plate clamping seat when adjusting the cutting position on the workpiece, thereby reducing friction between each other, avoiding damage to the end of the workpiece, and improving the product yield.
[0018] 4. In the utility model, the laser pen is mounted on a sliding frame, which is provided with a slider slidably connected thereto. The laser pen is mounted on the slider, and the position where the laser pen emits infrared rays can be changed as the slider moves, thereby achieving the purpose of adjusting the infrared rays to locate different cutting positions, thereby further improving the flexibility of the infrared rays in quickly locating different cutting positions of the cutting blade. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] In order to more clearly illustrate the technical solution of the present invention, the following briefly introduces the drawings required for use in the embodiments or descriptions of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.
[0020] Figure 1 This is a schematic structural diagram of the turbine gate cutting tool of the utility model;
[0021] Figure 2 This is a cross-sectional view of the local structure of the turbine gate cutting tool of the utility model;
[0022] Figure 3 This is a structural diagram of the connecting shaft and indexing plate pressing seat of the utility model;
[0023] Figure 4 This is a partial structural diagram of the anti-rotation component of the utility model;
[0024] Figure 5 This is a schematic diagram of the application of the turbine gate cutting tool of the utility model;
[0025] In the figure: 1-base, 11-slide, 2-cylinder mounting seat, 3-limiting seat, 31-limiting sleeve, 311-limiting groove, 4-cylinder clamping assembly, 5-laser pen, 6-mounting plate, 7-anti-rotation assembly, 71-connecting plate, 72-locking pin, 73-locking nut 1, 74-gasket, 75-locking nut 2, 8-sliding frame, 41-cylinder, 411-output shaft, 42-connecting shaft, 43-indexing plate clamping seat, 431-placement groove, 432-locking groove, 433-through hole, 44-screw, 100-turbine gate workpiece, 200-cutting disc. DETAILED DESCRIPTION
[0026] The following will be combined with the drawings of the present invention specification to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.
[0027] In a specific embodiment of the present invention, Figure 1-5 As shown, a turbine gate cutting tool includes a base 1, a cylinder mounting seat 2, a limit seat 3, a cylinder pressing assembly 4 and a laser pen 5. The cylinder mounting seat 2 and the limit seat 3 are respectively arranged at both ends of the base 1. A mounting plate 6 is provided in the cylinder mounting seat 2. The cylinder pressing assembly 4 includes a cylinder 41, a connecting shaft 42 and a dividing plate pressing seat 43. The cylinder 41 is fixedly mounted on the mounting plate 6, and its output shaft 411 passes through the mounting plate 6 and is fixed to one end of the connecting shaft 42. The other end of the connecting shaft 42 is fixed to the connecting shaft 42. One end is connected to the indexing plate pressing seat 43, and a placement groove 431 is provided in the indexing plate pressing seat 43. The placement groove 431 is used to limit one end of the turbine gate workpiece 100. A limiting sleeve 31 is provided on the limiting seat 3. The limiting sleeve 31 is used to limit the other end of the turbine gate workpiece 100. The cylinder 41 drives its output shaft 411 to drive the indexing plate pressing seat 43 to press the turbine gate workpiece 100 into the limiting sleeve 31. The cylinder mounting seat 2 is provided with an anti-rotation component 7 for limiting the indexing plate pressing seat 43;
[0028] Specifically, in this embodiment, a limiting groove 311 is provided in the limiting sleeve 31, and one end of the turbine gate workpiece 100 is placed in the limiting groove 311. In this embodiment, the limiting groove 311 is conical. This design can facilitate the adjustment of the cutting position by rotating the dividing plate clamping seat 43 to drive the turbine gate workpiece 100 to rotate in the limiting groove 311, thereby reducing friction between each other and avoiding damage to the end of the workpiece.
[0029] Specifically, in this embodiment, a sliding frame 8 is provided on one side of the base 1, and the laser pen 5 is installed on the sliding frame 8. Specifically, a slider (not shown in the figure) is provided on the sliding frame 8 and is slidably connected to it. The laser pen 5 is installed on the slider and can change the position of the laser pen as the slider moves, thereby achieving the purpose of adjusting the infrared positioning; here, the laser pen is installed on the slider as a conventional installation method, so the installation method is not specifically described here, and the end point of the ray of the laser pen 5 in this embodiment corresponds to the cutting position of the cutting blade 200 on the turbine gate workpiece 100, and the cutting position of the cutting blade can be quickly located by the infrared ray emitted by the laser pen, thereby improving the accuracy of the cutting position and the yield of the product.
[0030] like Figure 2As shown, the connecting shaft 42 and the dividing plate pressing seat 43 are integrally formed, and a through hole 433 is provided in the dividing plate pressing seat 43, which is connected to the placement groove 431 and the inner hole of the connecting shaft 42. A screw 44 is provided in the through hole 433, and the screw 44 is used to connect the output shaft of the cylinder 41 and the connecting shaft 42. This connection method improves the firmness between the connecting shaft and the cylinder output shaft.
[0031] like Figure 3-4 As shown, a plurality of locking grooves 432 are provided on the outer surface of the indexing plate pressing seat 43, and the plurality of locking grooves 432 are arranged at equal distances along the circumferential direction. The anti-rotation component 7 includes a connecting plate 71 and a locking pin 72. The connecting plate 71 is fixedly set on one side of the cylinder mounting seat 2. The locking pin 72 passes through the connecting plate 71 and extends into any one of the locking grooves 432. The locking pin 72 is connected to the connecting plate 71 by threads.
[0032] Specifically, if Figure 4 As shown, the locking pin 72 and the connecting plate 71 (not shown in the figure) are fastened by a locking nut 1 73, a gasket 74 and a locking nut 2 75. This design can improve the stability of the locking pin when inserted into the lock groove, thereby improving the stability of the cutting blade during the cutting process, ensuring the accuracy of the cutting position, and achieving the purpose of improving the product yield.
[0033] Specifically, in this embodiment, a slide groove 11 is provided on the base 1, and the limit seat 3 is slidably connected in the slide groove 11, which can be suitable for cutting turbine gate workpieces 100 of various models and specifications. Before cutting, the position of the limit seat 3 in the slide groove 11 is adjusted to replace workpieces of different specifications. When sliding to the appropriate position, the limit seat stops moving.
[0034] The working principle of this utility model is:
[0035] First, according to the size of the turbine gate workpiece 100, the limit seat 3 is adjusted to the appropriate position on the base 1. Here, the appropriate position means that one end of the turbine gate workpiece 100 can be placed in the limit groove and the other end can be placed in the placement groove 431. Then, the cylinder control switch is turned on. The cylinder drives its output shaft to drive the indexing plate pressing seat 43 to press the turbine gate workpiece 100 into the limit sleeve 31, thereby achieving the purpose of clamping the workpiece;
[0036] Then rotate the indexing plate pressing seat 43 to the specified cutting position, and then insert the locking pin 72 into the locking groove 432 to lock the position of the indexing plate pressing seat 43 at this time, so as to achieve the purpose of positioning the cutting position of the product; then turn on the laser pen, adjust the infrared ray emitted by the laser pen to the position on the turbine gate workpiece 100 that needs to be cut, and finally use the cutting blade of the cutting machine to cut the required position on the workpiece according to the position of the infrared ray, which greatly reduces the operating difficulty of the operator.
[0037] The above disclosure is only a preferred embodiment of the present invention and certainly cannot be used to limit the scope of rights of the present invention. Therefore, equivalent changes made according to the claims of the present invention are still within the scope covered by the present invention.
Claims
1. A turbine gate cutting tool, characterized in that: The invention comprises a base (1), a cylinder mounting seat (2), a limiting seat (3), a cylinder pressing assembly (4) and a laser pen (5); the cylinder mounting seat (2) and the limiting seat (3) are respectively arranged at two ends of the base (1); a mounting plate (6) is provided in the cylinder mounting seat (2); the cylinder pressing assembly (4) comprises a cylinder (41), a connecting shaft (42) and a dividing plate pressing seat (43); the cylinder (41) is fixedly mounted on the mounting plate (6), and its output shaft (411) passes through the mounting plate (6) and is fixed to one end of the connecting shaft (42); the other end of the connecting shaft (42) is fixed to the dividing plate The indexing plate pressing seat (43) is connected, a placement groove (431) is provided in the indexing plate pressing seat (43), the placement groove (431) is used to limit one end of the turbine gate workpiece (100), a limiting sleeve (31) is provided on the limiting seat (3), the limiting sleeve (31) is used to limit the other end of the turbine gate workpiece (100), the cylinder (41) drives its output shaft (411) to drive the indexing plate pressing seat (43) to press the turbine gate workpiece (100) into the limiting sleeve (31), and the cylinder mounting seat (2) is provided with an anti-rotation component (7) for limiting the indexing plate pressing seat (43); A sliding frame (8) is provided on one side of the base (1), the laser pen (5) is mounted on the sliding frame (8), and the end point of the ray of the laser pen (5) corresponds to the cutting position of the cutting blade (200) on the turbine gate workpiece (100).
2. A turbine gate cutting tool according to claim 1, characterized in that: A plurality of locking grooves (432) are provided on the outer surface of the indexing plate pressing seat (43); the anti-rotation assembly (7) comprises a connecting plate (71) and a locking pin (72); the connecting plate (71) is fixedly arranged on one side of the cylinder mounting seat (2); the locking pin (72) passes through the connecting plate (71) and extends into any one of the locking grooves (432); the locking pin (72) is connected to the connecting plate (71) by a thread.
3. The turbine gate cutting tool according to claim 2, characterized in that: The locking pin (72) and the connecting plate (71) are fastened together by a locking nut (73), a washer (74) and a locking nut (75).
4. The turbine gate cutting tool according to claim 2, characterized in that: The plurality of locking grooves (432) are arranged at equal distances along the circumferential direction.
5. The turbine gate cutting tool according to claim 1, characterized in that: The connecting shaft (42) and the indexing plate pressing seat (43) are integrally formed; a through hole (433) communicating with the placement groove (431) and the inner hole of the connecting shaft (42) is provided in the placement groove (431) and the indexing plate pressing seat (43); a screw (44) is provided in the through hole (433); the screw (44) is used to connect the output shaft of the cylinder (41) and the connecting shaft (42).
6. The turbine gate cutting tool according to claim 1, characterized in that: A sliding groove (11) is provided on the base (1), and the limiting seat (3) is slidably connected in the sliding groove (11).
7. The turbine gate cutting tool according to claim 1, characterized in that: The sliding frame (8) is provided with a sliding block slidably connected thereto, and the laser pen (5) is mounted on the sliding block.
8. The turbine gate cutting tool according to claim 1, characterized in that: A limiting groove (311) is provided in the limiting sleeve (31), the limiting groove (311) is conical, and one end of the turbine gate workpiece (100) is placed in the limiting groove (311).