Machine tool equipment of aviation power turbine working blade production line

By designing an automated flow-through processing structure, including conveyor belts, conveyor slides and lockers, the problems of low efficiency and inaccurate positioning of existing aerodynamic turbine working blade production lines are solved, and an efficient and automated processing process is achieved.

CN120116089AInactive Publication Date: 2025-06-10RIZHAO LIYANG IND EQUIP CO LTD
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Patent Information

Application Number
CN202510448575.8
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-04-10
Publication Date
2025-06-10
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

The machine tool equipment of the existing aerodynamic turbine working blade production lines has problems such as low efficiency, lack of automated processing structure, and inaccurate positioning.

Method used

A machine tool equipment including a conveyor belt, a conveyor slide and a locker is designed to realize an automated flow-through processing structure. The conveyor belt is used to automatically drive the blades to process in different processes. The conveyor slide provides automatic feeding and positioning functions, and the locker realizes automatic locking and positioning.

Benefits of technology

Improve processing efficiency, realize automated processing, reduce the need for manual positioning, and improve processing accuracy and production efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention provides machine tool equipment for an aviation power turbine working blade production line, and relates to the technical field of turbine machining, the machine tool equipment comprises an assembling base, and side mounting frames extending upwards are integrally arranged on the two sides of the assembling base; a recycling drawer is slidably inserted below the assembly base on one side, and a handle is arranged outside the recycling drawer; two groups of conveying belts are rotationally erected above the assembling base; a maintaining guide frame is fixedly arranged between the two side mounting frames, and the top of the maintaining guide frame is of a guide rail structure; the conveying belt is arranged, the assembly line type machining structure capable of automatically conducting machining is provided, the conveying belt can directly drive the blades to be fed, different working procedures are generated, rough grinding and fine grinding are conducted on workpieces, the roots of the blades are firstly machined into corrugated faces, then fine grinding is further conducted, and compared with an automatic machining mode of a machine tool, the machining efficiency is greatly improved. Machining efficiency can be improved, and the problem that existing equipment is insufficient in machining efficiency is solved.
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Description

Technical Field

[0001] The present invention relates to the technical field of turbine processing, and particularly to the machine tools for the production line of working blades of aviation power turbines. Background Art

[0002] The blades used in aviation power turbines are socketed combined blades. Due to the high cost, the blades are made into blades that can be disassembled and assembled individually, which is convenient for individual disassembly and replacement and can effectively reduce costs. Therefore, both sides of the blade root are made into corrugated guiding structures for installation outside the turbine.

[0003] The currently used machine tools have the following disadvantages: 1. The original machine tool uses the method of manual positioning. The workpiece is placed in the machine tool, and a three-axis grinding machine is used for grinding. It is necessary to first use a planing structure to plane arc grooves on both sides of the blade root, and then switch the grinding parts for fine grinding, or use two processes for processing. The efficiency is insufficient, and there is a lack of a flow-type processing structure that can automatically process. 2. There is a lack of synchronous automatic advancement, and there is no conveying structure that does not affect the automatic feeding of workpieces. 3. There is a lack of a positioning structure that automatically locks the blade during feeding. Summary of the Invention

[0004] In view of this, in order to address the above deficiencies in the prior art, the present invention provides a machine tool for the production line of working blades of aviation power turbines.

[0005] The present invention provides machine tool equipment for an aircraft power turbine working blade production line, specifically including: an assembly base, on both sides of which there are integrally provided side mounting frames extending upward; a recycling drawer is slidably inserted below one side of the assembly base, and a handle is provided outside the recycling drawer; above the assembly base, two groups of conveyor belts are rotatably mounted; between the two groups of side mounting frames, a maintenance guide frame is fixedly provided, and the top of the maintenance guide frame is a guide rail structure; outside the left assembly base, an electric cylinder is fixedly provided, the telescopic end of the electric cylinder is fixedly provided with a connecting rod, on both right ends of the connecting rod, two groups of straight guide rods are fixedly provided, and locking devices are fixedly provided at the right ends of the straight guide rods; on the outside of the two groups of conveyor belts, conveying sliders are equidistantly distributed and installed, and trigger sliders are slidably provided on the outside of the conveying sliders; above the inner wall of the right side mounting frame, a mounting seat is fixedly provided, and four groups of processing seats are slidably provided on the left side of the mounting seat in cooperation with the guide rail; on the adjacent surfaces of the front two groups of processing seats, rough grinding frames are vertically slidably provided in cooperation with the guide rail; on the adjacent surfaces of the rear two groups of processing seats, fine grinding frames are vertically slidably provided in cooperation with the guide rail; in the middle of the fine grinding frame, a fine grinding motor is fixedly provided, a transmission wheel is slidably provided on the outer rotor shaft of the fine grinding motor, and the transmission wheel is fixed on the outer rotor shaft of the fine grinding motor by a setscrew; a trapezoidal shaft post is fixedly provided outside the transmission wheel; a fine grinding module is slidably provided on the outside of the fine grinding frame, a trapezoidal groove is opened in the middle of the side of the fine grinding module close to the fine grinding frame, and the trapezoidal shaft post slides in the trapezoidal groove.

[0006] Optionally, two groups of propulsion rods for maintaining balance are fixedly provided on the left side of the connecting rod, and the propulsion rods are slidably connected to the left side mounting frame.

[0007] Optionally, the locking device is a U-shaped cylindrical structure, on the upper and lower ends of the locking device, two groups of self-locking pistons inclined towards the straight guide rod are fixedly provided, and on the telescopic ends of the self-locking pistons, trapezoidal blocks are fixedly provided; on the right ends of the locking devices, trigger pistons are fixedly provided, and a spring for automatic extension is provided inside the trigger pistons; the trigger pistons are communicated with the two groups of self-locking pistons.

[0008] Optionally, on the bottom of each of the conveying sliders, a guiding slider is integrally provided, and the guiding slider can be fitted with the guide rail structure above the maintenance guide frame; in the middle of the conveying slider, a feed slide rod is fixedly provided, and the feed slide rod is slidably connected to the left side of the trigger slider; a spring is sleeved on the outside of the feed slide rod at a position between the left side of the trigger slider and the right side of the conveying slider; on the right ends of the trigger sliders, two groups of docking posts are fixedly provided; on the top of each of the trigger sliders, a positioning frame is fixedly provided, a self-locking rod is slidably provided inside the positioning frame, on the left side of each of the self-locking rods, two groups of spring rods are fixedly provided, the spring rods are sleeved with springs and pass through the left side of the positioning frame and are fixedly provided with a handle structure capable of limiting, and the handle structure is used to control the spring rods.

[0009] Optionally, a support frame is fixedly arranged between the upper left side of the trigger carriage and the lower left side of the positioning frame. The middle of the support frame is an elliptical hole structure; wedge-shaped block structures are integrally arranged at both the upper and lower ends on the right side of the support frame; when the self-locking piston contracts, the whole locking device can pass through the support frame, and the trapezoidal block at the telescopic end of the self-locking piston can contact the wedge-shaped block structure on the right side of the support frame.

[0010] Optionally, four groups of longitudinal axis lead screws are fixedly arranged on the left side of the mounting seat. The longitudinal axis lead screws are respectively in threaded connection with four groups of machining seats; longitudinal axis motors for driving the longitudinal axis lead screws are fixedly arranged at one end of each longitudinal axis lead screw; four docking holes are formed in the mounting seat.

[0011] Optionally, height control lead screws are rotatably arranged in the middle of each machining seat, and height control motors for driving the height control lead screws are fixedly arranged at the bottom of each machining seat; the four groups of height control lead screws are respectively in threaded connection with two groups of rough grinding frames and two groups of fine grinding frames.

[0012] Optionally, rough grinding rollers are rotatably arranged in the middle of each rough grinding frame, and rough grinding motors for driving the rough grinding rollers are fixedly arranged at the right end of each rough grinding frame.

[0013] Optionally, the main body of the fine grinding module is of a U-shaped structure, and the middle of the side of the fine grinding module close to the fine grinding frame is a groove structure.

[0014] The beneficial effects are as follows: 1. The present invention is provided with a conveyor belt, providing a flow-type processing structure capable of automatically performing processing. The conveyor belt can directly drive the blade for feeding, generating different processes, rough grinding and fine grinding the workpiece. First, a corrugated surface is processed at the root of the blade, and then further fine grinding is carried out. Compared with the method of automatic processing by a machine tool, the processing efficiency can be improved, and the fine grinding module is slidably installed, which is convenient for disassembly and replacement. The trapezoidal shaft pile and the trapezoidal groove adopt a trapezoidal contact method, reducing the friction force and facilitating reciprocating grinding.

[0015] 2. The present invention is provided with a conveying slide seat, providing a conveying structure for automatically feeding the workpiece. The conveying slide seat can provide the function of positioning the blade, can drive the blade to move. After feeding, the electric cylinder is used for synchronous automatic propulsion, moving the blade to the processing position, and then automatic processing can be carried out. And while the electric cylinder contracts after processing, the spring outside the feeding slide rod can automatically reset the position of the blade, ensuring that the blade can continue to move backward and feed along with the conveyor belt.

[0016] 3. The present invention is provided with a lock, which provides an automatic locking function. When the trigger piston contacts the left side of the blade, it pushes the blade to the right, and then pulls the trigger carriage to move to the right, inserts the docking pile into the docking hole for positioning. At the same time, the trigger piston is also automatically contracted under pressure, and the hydraulic oil in the trigger piston is input into the self-locking piston, expanding two groups of self-locking pistons. The trapezoidal blocks at the telescopic ends of the self-locking pistons contact the wedge-shaped block structure on the right side of the support frame for self-locking fixation, replacing manual positioning. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 Shows a schematic diagram of the overall structure according to an embodiment of the present invention; Figure 2 Shows a schematic diagram of the structure of the transmission part according to an embodiment of the present invention; Figure 3 Shows a schematic diagram of the axonometric structure according to an embodiment of the present invention; Figure 4 Shows a three-dimensional structure schematic diagram of the mounting seat according to an embodiment of the present invention; Figure 5 Shows a schematic diagram of the axonometric structure of the mounting seat according to an embodiment of the present invention; Figure 6 Shows a schematic diagram of the assembly structure of the conveying slide seat according to an embodiment of the present invention; Figure 7 Shows an embodiment according to the present invention Figure 6 of the side view structure diagram; Figure 8 Shows a schematic diagram of the assembly structure of the fine grinding frame according to an embodiment of the present invention; Figure 9 Shows an embodiment according to the present invention Figure 8 of another angle structure diagram.

[0018] LIST OF REFERENCE NUMERALS 1. Assembly base; 101. Side mounting frame; 102. Recycling drawer; 103. Conveyor belt; 104. Maintenance guide frame; 2. Electric cylinder; 201. Connecting rod; 202. Straight guide rod; 203. Pushing rod; 3. Lock; 301. Self-locking piston; 302. Trigger piston; 4. Conveying slide seat; 401. Guide slide frame; 402. Feed slide rod; 403. Trigger carriage; 404. Docking pile; 405. Positioning frame; 406. Self-locking rod; 407. Spring rod; 5. Support frame; 6. Mounting seat; 601. Longitudinal axis lead screw; 602. Longitudinal axis motor; 603. Docking hole; 7. Processing seat; 701. Height control lead screw; 702. Height control motor; 8. Coarse grinding frame; 801. Coarse grinding roller; 802. Coarse grinding motor; 9. Fine grinding frame; 901. Fine grinding motor; 902. Transmission wheel; 903. Trapezoidal shaft pile; 10. Precision grinding module; 1001. Trapezoidal groove. Detailed implementation mode

[0019] In order to make the objectives, solutions and advantages of the technical solutions of the present invention clearer, the technical solutions of the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings of the specific embodiments of the present invention.

[0020] Embodiment 1: Please refer to Figures 1 to 9 as shown: The present invention provides a machine tool device for an aeroengine power turbine working blade production line, including: an assembly base 1, with upwardly extending side mounting frames 101 integrally arranged on both sides of the assembly base 1; a recycling drawer 102 is slidably inserted under one side of the assembly base 1, and a handle is arranged outside the recycling drawer 102; two groups of conveyor belts 103 are rotatably mounted above the assembly base 1; a maintenance guide frame 104 is fixedly arranged between the two groups of side mounting frames 101, and the top of the maintenance guide frame 104 is a guide rail structure; an electric cylinder 2 is fixedly arranged outside the left assembly base 1, a connecting rod 201 is fixedly arranged at the telescopic end of the electric cylinder 2, two groups of straight guide rods 202 are fixedly arranged at both right ends of the connecting rod 201, and locking devices 3 are fixedly arranged at the right ends of the straight guide rods 202; conveying sliding seats 4 are equidistantly distributed and installed outside the two groups of conveyor belts 103, and trigger sliding frames 403 are slidably arranged outside the conveying sliding seats 4; a mounting seat 6 is fixedly arranged above the inner wall of the right side mounting frame 101, and four groups of processing seats 7 are slidably arranged on the left side of the mounting seat 6 in cooperation with the guide rail; rough grinding frames 8 are vertically slidably arranged on the adjacent surfaces of the front two groups of processing seats 7 in cooperation with the guide rail; fine grinding frames 9 are vertically slidably arranged on the adjacent surfaces of the rear two groups of processing seats 7 in cooperation with the guide rail; a fine grinding motor 901 is fixedly arranged in the middle of the fine grinding frame 9, a transmission wheel 902 is slidably arranged outside the rotor shaft of the fine grinding motor 901, and the transmission wheel 902 is fixed on the rotor shaft of the fine grinding motor 901 by a set screw; a trapezoidal shaft post 903 is fixedly arranged outside the transmission wheel 902; a fine grinding module 10 is slidably arranged outside the fine grinding frame 9, a trapezoidal groove 1001 is opened in the middle of the side of the fine grinding module 10 close to the fine grinding frame 9, and the trapezoidal shaft post 903 slides in the trapezoidal groove 1001. The trapezoidal contact method can reduce friction and improve the sliding speed.

[0021] Among them, two groups of push rods 203 for maintaining balance are fixedly arranged on the left side of the connecting rod 201, and the push rods 203 are slidably connected to the left side mounting frame 101.

[0022] Among them, the locking device 3 is a U-shaped cylindrical structure, and two groups of self-locking pistons 301 inclined towards the straight guide rod 202 are fixedly arranged at both the upper and lower ends of the locking device 3. Trapezoidal blocks are fixedly arranged at the telescopic ends of the self-locking pistons 301; trigger pistons 302 are fixedly arranged at the right ends of the locking devices 3, and springs for automatic extension are arranged inside the trigger pistons 302; the trigger pistons 302 are communicated with the two groups of self-locking pistons 301.

[0023] Among them, a guiding carriage 401 is integrally provided at the bottom of the conveying slide 4, and the guiding carriage 401 can be fitted with the guide rail structure above the maintaining guide 104; a feeding slide bar 402 is fixedly provided in the middle of the conveying slide 4, and the feeding slide bar 402 is slidably connected to the left side of the triggering carriage 403; a spring is sleeved outside the feeding slide bar 402 at a position between the left side of the triggering carriage 403 and the right side of the conveying slide 4; two sets of docking piles 404 are fixedly provided at the right end of the triggering carriage 403; a positioning frame 405 is fixedly provided at the top of the triggering carriage 403, a self-locking rod 406 is slidably arranged inside the positioning frame 405, two sets of spring rods 407 are fixedly provided on the left side of the self-locking rod 406, and the spring rods 407 are sleeved with springs and pass through the left side of the positioning frame 405 and are fixedly provided with a handle structure capable of limiting, and the handle structure is used to control the spring rods 407.

[0024] Among them, a support frame 5 is fixedly provided between the left top of the triggering carriage 403 and the left bottom of the positioning frame 405, and the middle of the support frame 5 is an elliptical hole structure; wedge-shaped block structures are integrally provided at the upper and lower ends on the right side of the support frame 5; when the self-locking piston 301 contracts, the whole locking device 3 can pass through the support frame 5, and the trapezoidal block at the telescopic end of the self-locking piston 301 can contact the wedge-shaped block structure on the right side of the support frame 5.

[0025] Among them, four groups of longitudinal axis lead screws 601 are fixedly provided on the left side of the mounting seat 6, and the longitudinal axis lead screws 601 are respectively threadedly connected to four groups of processing seats 7; longitudinal axis motors 602 for driving the longitudinal axis lead screws 601 are fixedly provided at one end of each of the longitudinal axis lead screws 601; four groups of docking holes 603 are provided in the mounting seat 6.

[0026] Among them, height control lead screws 701 are rotatably arranged in the middle of each of the processing seats 7, and height control motors 702 for driving the height control lead screws 701 are fixedly provided at the bottom of each of the processing seats 7; the four groups of height control lead screws 701 are respectively threadedly connected to two groups of rough grinding frames 8 and two groups of fine grinding frames 9.

[0027] Among them, rough grinding rollers 801 are rotatably arranged in the middle of each of the rough grinding frames 8, and rough grinding motors 802 for driving the rough grinding rollers 801 are fixedly provided at the right end of each of the rough grinding frames 8.

[0028] Among them, the main body of the fine grinding module 10 is of a U-shaped structure, and the middle on the side of the fine grinding module 10 close to the fine grinding frame 9 is a groove structure for accommodating the transmission wheel 902.

[0029] As Figures 1 - 9 shown, a servo motor is set to control the conveyor belt 103. Each time the conveyor belt 103 moves, the blade advances one station, and a proximity sensor is used for positioning. When the sensor contacts the triggering carriage 403 below, automatic positioning can be achieved. The length of the conveyor belt 103 can be set as required and customized according to different workshop scales; Hydraulic oil is filled inside the trigger piston 302 and the self-locking piston 301 in advance; Start the electric cylinder 2 to drive the connecting rod 201 and the straight guide rod 202 to move. The straight guide rod 202 drives the lock 3 to move to the right. After the lock 3 passes through the support frame 5 and continues to move to the right, when the trigger piston 302 contacts the left side of the blade, it pushes the blade to the right, and then pulls the trigger carriage 403 to move to the right, inserting the docking pile 404 into the docking hole 603 for positioning; At this time, the guiding carriage 401 slides outside the maintaining guide 104 for auxiliary positioning; During this period, the trigger piston 302 is also automatically contracted under pressure, and the hydraulic oil in the trigger piston 302 is input into the self-locking piston 301 to expand the two groups of self-locking pistons 301. The trapezoidal blocks at the telescopic ends of the self-locking pistons 301 contact the wedge-shaped block structure on the right side of the support frame 5 for self-locking and fixing; Then, use the program to control the rough grinding motor 802, the fine grinding motor 901, the vertical axis motor 602, and the height control motor 702 to work respectively, and the automatic grinding effect can be achieved. And the processing can be completed by using the double-axis movement method, and the electric cylinder 2 is used for feeding, replacing the horizontal axis movement.

[0030] Embodiment 2: Based on Embodiment 1, in the present invention, the rough grinding roller 801 is a rough grinding roller, mainly for initially grinding both sides of the root of the cast blade. The model can be adjusted according to different sizes, and a roller-shaped processing component for planing can be used to replace the grinding roller for processing to achieve automated processing.

[0031] Embodiment 3: Based on Embodiment 1, place the blade in the positioning frame 405 above the front side, and take out the blade in the positioning frame 405 at the rear side of the equipment. Only manual picking and placing are required. After taking out the blade, use a gauge to measure. When an error beyond the range occurs, stop the machine and replace the fitting; when the fine grinding module 10 is worn out greatly and an error occurs, directly replace the fine grinding module 10 at this time. Loosen the setscrew in the transmission wheel 902 to slide the transmission wheel 902, and pull out the trapezoidal shaft pile 903 from the trapezoidal groove 1001, then the fine grinding module 10 can be slid out to one side for replacement.

[0032] The specific usage method and function of this embodiment: In the present invention, during operation, place the blade in the positioning frame 405 above the front side, and take out the blade in the positioning frame 405 at the rear side of the equipment. Only manual picking and placing are required. After taking out the blade, use a gauge to measure. When an error beyond the range occurs, stop the machine and replace the fitting; A servo motor is set to control the conveyor belt 103. Each time the conveyor belt 103 moves, the blade advances one station. After feeding, start the electric cylinder 2 to drive the connecting rod 201 and the straight guide rod 202 to move. The straight guide rod 202 drives the lock 3 to move to the right. After the lock 3 passes through the support frame 5, it continues to move to the right, triggering the piston 302 to contact the left side of the blade and then push the blade to the right, thereby pulling the trigger carriage 403 to move to the right, inserting the docking pile 404 into the docking hole 603 for positioning. At the same time, the trigger piston 302 is also automatically contracted under pressure, and the hydraulic oil in the trigger piston 302 is input into the self-locking piston 301, expanding the two groups of self-locking pistons 301. The trapezoidal blocks at the telescopic ends of the self-locking pistons 301 contact the wedge-shaped block structure on the right side of the support frame 5 for self-locking fixation. Start the rough grinding motor 802 to drive the rough grinding roller 801 to rotate, providing the rough grinding function. Start the fine grinding motor 901 to drive the transmission wheel 902 and the trapezoidal shaft pile 903 to rotate. The trapezoidal shaft pile 903 slides in the trapezoidal groove 1001 to drive the fine grinding module 10 to move. By using the high-frequency reciprocating movement of the fine grinding module 10, a grinding effect is generated to provide the fine grinding function. Start the longitudinal axis motor 602 to drive the longitudinal axis lead screw 601 to rotate, and then drive the processing seat 7 to move, enabling longitudinal axis feeding. Start the height control motor 702 to drive the height control lead screw 701 to rotate, and then drive the rough grinding frame 8 or the fine grinding frame 9 to move up and down, enabling adjustment of the height axis. Automatic grinding processing can be completed through double-axis adjustment, and the generated waste chips will naturally fall into the recycling drawer 102. After the processing is completed, reset the electric cylinder 2. The trigger carriage 403 will automatically reset through the spring to ensure continuous feeding. By rough grinding first and then fine grinding, the working mode of switching grinding parts can be replaced.

Claims

1. The machine tool equipment for the production line of aviation power turbine working blades is characterized by: include: An assembly base (1), wherein both sides of the assembly base (1) are integrally provided with side mounting frames (101) extending upward; a recovery drawer (102) is slidably inserted below one side of the assembly base (1); two groups of conveyor belts (103) are rotatably mounted above the assembly base (1); a maintaining guide frame (104) is fixedly arranged between the two groups of side mounting frames (101), and the top of the maintaining guide frame (104) is a guide rail structure; an electric cylinder (2) is fixedly arranged outside the left assembly base (1), a connecting rod (201) is fixedly arranged at the telescopic end of the electric cylinder (2), two groups of straight guide rods (202) are fixedly arranged at both ends of the right side of the connecting rod (201), and the right ends of the straight guide rods (202) are fixedly arranged with lockers (3); conveying slides (4) are equidistantly installed outside the two groups of conveyor belts (103), and trigger slides (403) are slidably arranged outside the conveying slides (4); the right side mounting frame ( A mounting seat (6) is fixedly arranged above the inner wall of the mounting seat (6), and four groups of processing seats (7) are slidably arranged on the left side of the mounting seat (6) in cooperation with the guide rail; a coarse grinding frame (8) is vertically slidably arranged on the adjacent surfaces of the two groups of processing seats (7) on the front side in cooperation with the guide rail; a fine grinding frame (9) is vertically slidably arranged on the adjacent surfaces of the two groups of processing seats (7) on the rear side in cooperation with the guide rail; a fine grinding motor (901) is fixedly arranged in the middle of the fine grinding frame (9), and a transmission wheel (902) is slidably arranged on the outside of the rotor shaft of the fine grinding motor (901), and the transmission wheel (902) is fixedly arranged on the outside of the rotor shaft of the fine grinding motor (901) by means of a top screw; a trapezoidal shaft pile (903) is fixedly arranged on the outside of the transmission wheel (902); a fine grinding module (10) is slidably arranged on the outside of the fine grinding frame (9), and a trapezoidal groove (1001) is provided in the middle of the fine grinding module (10) close to the fine grinding frame (9), and the trapezoidal shaft pile (903) slides in the trapezoidal groove (1001).

2. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 1, characterized in that: Two groups of propulsion rods (203) for maintaining balance are fixedly arranged on the left side of the connecting rod (201), and the propulsion rods (203) are slidably connected to the left side mounting frame (101).

3. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 1, characterized in that: The lock (3) is a U-shaped cylindrical structure. Two groups of self-locking pistons (301) tilted toward one side of the straight guide rod (202) are fixedly arranged at the upper and lower ends of the lock (3), and a trapezoidal block is fixedly arranged at the telescopic end of the self-locking piston (301). A trigger piston (302) is fixedly arranged at the right end of the lock (3), and a spring for automatic extension is arranged inside the trigger piston (302); the trigger piston (302) is connected to the two groups of self-locking pistons (301).

4. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 3, characterized in that: The bottom of the conveying slide (4) is integrally provided with a guide slide (401), and the guide slide (401) can be matched with the guide rail structure above the guide frame (104); a feed slide (402) is fixedly provided in the middle of the conveying slide (4), and the feed slide (402) is slidably connected to the left side of the trigger slide (403); a spring is sleeved on the outside of the feed slide (402) at a position between the left side of the trigger slide (403) and the right side of the conveying slide (4); two groups of docking piles (404) are fixedly provided on the right end of the trigger slide (403); a positioning frame (405) is fixedly provided on the top of the trigger slide (403), a self-locking rod (406) is slidably provided inside the positioning frame (405), and two groups of spring rods (407) are fixedly provided on the left side of the self-locking rod (406), and the spring rods (407) are sleeved with springs and pass through the left side of the positioning frame (405) and are fixedly provided with a handle structure capable of limiting position.

5. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 4, characterized in that: A support frame (5) is fixedly arranged between the top left side of the trigger slide (403) and the left bottom side of the positioning frame (405), and the middle of the support frame (5) is an elliptical hole structure; the upper and lower ends of the right side of the support frame (5) are integrally provided with wedge block structures; when the self-locking piston (301) is retracted, the locking device (3) can pass through the support frame (5) as a whole, and the trapezoidal block at the telescopic end of the self-locking piston (301) can contact the wedge block structure on the right side of the support frame (5).

6. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 1, characterized in that: Four groups of longitudinal lead screws (601) are fixedly arranged on the left side of the mounting seat (6), and the longitudinal lead screws (601) are respectively threadedly connected to the four groups of processing seats (7); a longitudinal motor (602) for driving the longitudinal lead screws (601) is fixedly arranged at one end of each longitudinal lead screw (601); and four groups of docking holes (603) are opened in the mounting seat (6).

7. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 1, characterized in that: A height control lead screw (701) is rotatably arranged in the middle of the processing seat (7), and a height control motor (702) for driving the height control lead screw (701) is fixedly arranged at the bottom of the processing seat (7); the four groups of height control lead screws (701) are respectively threadedly connected to the two groups of coarse grinding frames (8) and the two groups of fine grinding frames (9).

8. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 1, characterized in that: A coarse grinding roller (801) is rotatably arranged in the middle of the coarse grinding frame (8), and a coarse grinding motor (802) for driving the coarse grinding roller (801) is fixedly arranged at the right end of the coarse grinding frame (8).

9. The machine tool equipment for the production line of aviation power turbine working blades as claimed in claim 1, characterized in that: The main body of the fine grinding module (10) is a U-shaped structure, and the middle of one side of the fine grinding module (10) close to the fine grinding frame (9) is a groove structure.