CN223670358U - Linear cutting machine for machining aircraft special-shaped parts - Google Patents

Linear cutting machine for machining aircraft special-shaped parts

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Publication number
CN223670358U
CN223670358U CN202520220547.6U CN202520220547U CN223670358U CN 223670358 U CN223670358 U CN 223670358U CN 202520220547 U CN202520220547 U CN 202520220547U CN 223670358 U CN223670358 U CN 223670358U
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CN
China
Prior art keywords
machining
cutting machine
box
mounting
wire cutting
Prior art date
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Active
Application number
CN202520220547.6U
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Chinese (zh)
Inventor
白玉胜
于光尚
施连峰
宋明辉
高运龙
杨枫
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenyang Yuhong Civil Aviation Equipment Manufacturing Co ltd
Original Assignee
Shenyang Yuhong Civil Aviation Equipment Manufacturing Co ltd
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Application filed by Shenyang Yuhong Civil Aviation Equipment Manufacturing Co ltd filed Critical Shenyang Yuhong Civil Aviation Equipment Manufacturing Co ltd
Priority to CN202520220547.6U priority Critical patent/CN223670358U/en
Application granted granted Critical
Publication of CN223670358U publication Critical patent/CN223670358U/en
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Abstract

The utility model provides a wire cutting machine for machining an aircraft special-shaped part, and belongs to the technical field of wire cutting equipment. The utility model relates to a wire cutting machine for machining an aircraft special-shaped piece, which comprises a machine base and a pushing mechanism, wherein a machining table is arranged at the top of the machine base, a machining box is arranged at the top of the machining table, a cutting machine body is arranged at the rear side of the top of the machine base, a placing table is arranged at the bottom of the inner wall of the machining box, a first connecting block and a second connecting block are respectively arranged at the left side and the right side of the placing table, a placing box is arranged at the right side of the bottom of the inner wall of the machining box, a mounting groove is formed in the right side of the first connecting block, a motor is arranged in an inner cavity of the mounting groove, a screw rod is arranged at the output end of the motor, a screw sleeve is arranged on the surface of the screw rod, and the pushing plate is arranged at the top of the screw sleeve.

Description

Linear cutting machine for machining aircraft special-shaped parts
Technical Field
The utility model relates to the technical field of wire cutting equipment, in particular to a wire cutting machine for machining an aircraft special-shaped piece.
Background
The wire cutting equipment is a mechanical equipment for cutting metal by utilizing the electric spark discharging principle, is mainly used for processing various workpieces with complex shapes and precision and fineness, and the basic working principle is that the continuous moving thin metal wire is utilized for carrying out pulse spark discharging and metal removing on the workpieces so as to realize cutting and forming, the wire cutting machine mainly comprises a machine tool, a numerical control system and a high-frequency power supply, the numerical control system is composed of a singlechip, a keyboard and a variable frequency detection system, has main functions of gap compensation, linear interpolation, circular arc interpolation, automatic broken wire treatment and the like, can cut parts with high strength, high toughness, magnetic materials, precision, fineness and complex shape, and is widely applied to various industries of linear cutting technology and linear cutting machine tools.
However, in the prior art, when the workpiece is fed and discharged, the workpiece is required to be placed and taken down manually, and part of parts have waste heat after being cut, so that the operator's fingers can be scalded, the parts are required to be cooled simply or the glove is worn, more time is wasted, and the processing efficiency of the workpiece is affected.
Disclosure of utility model
In order to overcome the above disadvantages, the present utility model provides a wire cutting machine for processing an aircraft profiled element, which overcomes or at least partially solves the above technical problems.
The utility model is realized in the following way:
The utility model provides a wire cutting machine for machining an aircraft special-shaped part, which comprises a machine base, wherein a machining table is arranged at the top of the machine base, a machining box is arranged at the top of the machining table, a cutting machine body is arranged at the rear side of the top of the machine base, a placing table is arranged at the bottom of the inner wall of the machining box, and a first connecting block and a second connecting block are respectively arranged at the left side and the right side of the placing table;
the pushing mechanism comprises a pushing mechanism body;
the discharging box is arranged on the right side of the bottom of the inner wall of the processing box;
the mounting groove is formed in the right side of the first connecting block;
The motor is arranged in the inner cavity of the mounting groove;
The screw rod is arranged at the output end of the motor, and the surface of the screw rod is provided with a screw sleeve;
The push plate is provided with the top of the screw sleeve.
In a preferred scheme, the connecting plate is installed at the top of swivel nut, the torsional spring is installed on the left side at connecting plate top, and the both ends of torsional spring are connected with connecting plate and push pedal respectively.
In a preferred scheme, the left side of the inner wall of the discharging box is provided with two groups of side plates, and the two groups of side plates are respectively arranged on the front surface and the back surface of the push plate.
In a preferred scheme, a collecting box is arranged on the left side of the bottom of the inner wall of the processing box, and the left side of the first connecting block is obliquely arranged.
In a preferred scheme, the fixing base is all installed to the front side and the rear side of processing incasement wall bottom, the mounting bracket is installed at the top of fixing base, and the mounting bracket is L shape setting.
In a preferred scheme, a mounting shaft is mounted on the left side of the mounting frame, and a blocking plate is rotatably mounted on the surface of the mounting shaft.
In a preferred scheme, the left side of barrier plate installs first mount pad, the inboard of mounting bracket is installed the second mount pad, and the inboard of second mount pad rotates and installs electric putter, electric putter's free end rotates with first mount pad to be connected.
In a preferred scheme, limiting plates are arranged on two sides of the connecting plate, and the limiting plates are in sliding connection with the inner cavity of the discharging box.
The utility model provides a wire cutting machine for processing an aircraft special-shaped piece, which has the beneficial effects that:
1. Through setting up pushing equipment, can be after starting pushing equipment for pushing equipment promotes the work piece to place the bench, and then the cutting organism of being convenient for cuts the work piece, can practice thrift the time of manual work with the work piece material loading.
2. Through setting up connecting plate, torsional spring and curb plate, can install at the bottom of the connecting plate installation back torsional spring for the torsional spring is installed the push pedal, can be rotated left side when the push pedal moves right and is blocked by the work piece, and then is convenient for pass the right side that the work piece moved the work piece, and the curb plate can be spacing to the work piece, can be driven the reset by the torsional spring after making the push pedal pass the work piece.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some examples of the present utility model and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is an overall perspective view provided by an embodiment of the present utility model;
fig. 2 is a schematic perspective view of a processing box according to an embodiment of the present utility model;
Fig. 3 is a schematic view of a three-dimensional cross-sectional structure of a placement table according to an embodiment of the present utility model;
Fig. 4 is a schematic perspective view of a mounting frame according to an embodiment of the present utility model;
The device comprises a machine seat, a machine frame, a 2 processing table, a 3 processing box, a 4 cutting machine body, a 5 placing table, a 6 first connecting block, a 7 second connecting block, an 8 pushing mechanism, an 81 discharging box, an 82 mounting groove, an 83, a motor, an 84, a screw rod, an 85, a screw sleeve, an 86, a push plate, a 9, a connecting plate, a 10, a torsion spring, an 11, a side plate, a 12, a collecting box, a 13, a fixed seat, a 14, an installation frame, a 15, an installation shaft, a 16, a blocking plate, a 17, a first installation seat, an 18, a second installation seat, a 19, an electric push rod, a 20 and a limiting plate.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments. All other embodiments, based on the embodiments of the utility model, which are apparent to those of ordinary skill in the art without inventive faculty, are intended to be within the scope of the utility model.
Referring to fig. 1-4, the utility model provides a technical scheme that the wire cutting machine for machining the special-shaped parts of the airplane comprises a machine base 1 and a pushing mechanism 8, wherein a machining table 2 is arranged at the top of the machine base 1, a machining box 3 is arranged at the top of the machining table 2, a cutting machine body 4 is arranged at the rear side of the top of the machine base 1, a placing table 5 is arranged at the bottom of the inner wall of the machining box 3, a first connecting block 6 and a second connecting block 7 are respectively arranged at the left side and the right side of the placing table 5, and after the pushing mechanism 8 is started, the pushing mechanism 8 can push a workpiece to the placing table 5, so that the workpiece is conveniently cut by using the cutting machine body 4, and the time for manually loading and unloading the workpiece can be saved.
Referring to fig. 1 to 3, in a preferred embodiment, by providing a pushing mechanism 8, the pushing mechanism 8 includes a discharge box 81, a mounting groove 82, a motor 83, a screw rod 84, a screw sleeve 85 and a push plate 86, the discharge box 81 is mounted on the right side of the bottom of the inner wall of the processing box 3, the mounting groove 82 is opened on the right side of the first connecting block 6, the motor 83 is mounted in the inner cavity of the mounting groove 82, the screw rod 84 is mounted at the output end of the motor 83, and the screw sleeve 85 is mounted on the surface of the screw rod 84, the push plate 86 is provided at the top of the screw sleeve 85, a workpiece can be placed after the discharge box 81 is mounted, and the motor 83 can be mounted after the mounting groove 82 is opened, so that the motor 83 drives the screw sleeve 85 to move through the screw rod 84 after being started, and the top of the screw sleeve 85 is mounted with the connecting plate 9, the torsional spring 10 is installed in the left side at connecting plate 9 top, and the both ends of torsional spring 10 are connected with connecting plate 9 and push pedal 86 respectively, can make swivel nut 85 install torsional spring 10 to connecting plate 9 after the connecting plate 9 is installed, and then be convenient for install push pedal 86, and limiting plate 20 is all installed to the both sides of connecting plate 9, and limiting plate 20 and the inner chamber sliding connection of blowing box 81, can make limiting plate 20 and the inner chamber sliding of blowing box 81, and then be convenient for carry out spacing to connecting plate 9, avoid swivel nut 85 to take place to rotate when removing, thereby be convenient for push pedal 86 promote the work piece, can promote the work piece and place on the platform 5 and cut, what deserve to say here is, the right side of push pedal 86 bottom and the right side contact at connecting plate 9 top, make push pedal 86 can not rotate right under vertical state.
Referring to fig. 1-2, in a preferred embodiment, the collecting box 12 is installed on the left side of the bottom of the inner wall of the processing box 3, the left side of the first connecting block 6 is inclined, the workpiece can be pushed to the left side after the workpiece is cut, so that the workpiece slides into the collecting box 12 along the inclined surface of the first connecting block 6, the side plates 11 are installed on the left side of the inner wall of the discharging box 81, two groups of side plates 11 are arranged on the front surface and the back surface of the push plate 86 respectively, the side plates 11 can limit the workpiece, and after the push plate 86 passes through the workpiece and moves into a cavity between the workpiece and the side plates 11, the torsion spring 10 can drive the push plate 86 to rotate for resetting.
Referring to fig. 1-4, in a preferred embodiment, the front side and the rear side of the bottom of the inner wall of the processing box 3 are both provided with the fixing seat 13, the top of the fixing seat 13 is provided with the mounting frame 14, the mounting frame 14 is in an L-shaped arrangement, the left side of the mounting frame 14 is provided with the mounting shaft 15, the surface of the mounting shaft 15 rotates to install the blocking plate 16, the mounting frame 14 is provided with the blocking plate 16 after the mounting shaft 15 is installed, the blocking plate 16 can block a workpiece pushed onto the placing table 5, the left side of the blocking plate 16 is provided with the first mounting seat 17, the inner side of the mounting frame 14 is provided with the second mounting seat 18, the inner side of the second mounting seat 18 rotates to be provided with the electric push rod 19, the free end of the electric push rod 19 is rotationally connected with the first mounting seat 17, the electric push rod 19 can be installed after the first mounting seat 17 and the second mounting seat 18, the electric push rod 19 can be driven to rotate after being started, and the blocking plate 16 can be driven to push the workpiece 12 to collect after the blocking plate 16 is pushed.
In particular, the working process or the working principle of the wire cutting machine for machining the airplane special-shaped piece is that when the wire cutting machine is used, firstly, workpieces to be cut are placed in a discharging box 81 in sequence, then, a motor 83 is used for driving a screw rod 84 to rotate, the screw rod 84 can be driven by the screw sleeve 85 to move through a connecting plate 9, the connecting plate 9 is driven by a torsion spring 10 to drive a push plate 86 to move, the push plate 86 drives the bottommost workpieces to move when moving leftwards, so that the workpieces can be conveniently pushed onto a placing table 5, a blocking plate 16 can block the workpieces, the workpieces can be cut through a cutting machine body 4, after the workpieces are cut into special-shaped parts, an electric push rod 19 is started, the electric push rod 19 drives the blocking plate 16 to rotate through a first mounting seat 17, and the motor 83 is started again, the push plate 86 continues to move the workpieces leftwards, the workpieces enter the collecting box 12, then, the motor 83 is reversed, the electric push rod 19 drives the blocking plate 16 to reset, when the push plate 86 moves leftwards to a position of the workpieces, the workpieces which are not cut, the push plate 86 can be conveniently pushed by the push plate 86 to move leftwards, the torsion spring 86 is further, the push plate 86 can be conveniently pushed by the torsion spring 86 to move leftwards, the push plate 86 to the side of the workpieces to be conveniently, the torsion spring 86 can be pushed by the torsion spring 86 to move the side, the side of the workpieces can be conveniently, the side of the workpieces can be cut, the side of the workpieces can be cut, and the side of the workpieces can be conveniently and the cut, and the side can be conveniently and the cut can be repeatedly pushed by the fact the roll and the opposite to move to the side can be cut to move to the side can be cut.
It should be noted that, the cutting machine body 4, the motor 83 and the electric push rod 19 are devices or apparatuses existing in the prior art, or are devices or apparatuses that can be implemented in the prior art, and the power supply, the specific composition and the principle thereof are clear to those skilled in the art, so that detailed descriptions thereof are omitted.

Claims (8)

1. The linear cutting machine for machining the special-shaped parts of the aircraft comprises a machine base (1) and is characterized in that a machining table (2) is arranged at the top of the machine base (1), a machining box (3) is arranged at the top of the machining table (2), a cutting machine body (4) is arranged at the rear side of the top of the machine base (1), a placing table (5) is arranged at the bottom of the inner wall of the machining box (3), and a first connecting block (6) and a second connecting block (7) are respectively arranged at the left side and the right side of the placing table (5);
a pushing mechanism (8), the pushing mechanism (8) comprising;
The discharging box (81) is arranged on the right side of the bottom of the inner wall of the processing box (3);
the mounting groove (82) is formed in the right side of the first connecting block (6);
a motor (83), the motor (83) being mounted in the interior cavity of the mounting slot (82);
The screw rod (84) is arranged at the output end of the motor (83), and a screw sleeve (85) is arranged on the surface of the screw rod (84);
the push plate (86), the push plate (86) is provided with the top of the swivel nut (85).
2. The wire cutting machine for machining of profiled parts of aircraft according to claim 1, characterized in that the top of the screw sleeve (85) is provided with a connecting plate (9), the left side of the top of the connecting plate (9) is provided with a torsion spring (10), and two ends of the torsion spring (10) are respectively connected with the connecting plate (9) and a push plate (86).
3. The wire cutting machine for machining of irregular parts of aircraft according to claim 1, wherein the left side of the inner wall of the discharging box (81) is provided with two groups of side plates (11), and the two groups of side plates (11) are respectively arranged on the front surface and the back surface of the push plate (86).
4. The wire cutting machine for machining of aircraft special-shaped parts according to claim 1, wherein a collecting box (12) is installed on the left side of the bottom of the inner wall of the machining box (3), and the left side of the first connecting block (6) is obliquely arranged.
5. The wire cutting machine for machining of aircraft special-shaped parts according to claim 1, wherein the front side and the rear side of the bottom of the inner wall of the machining box (3) are provided with fixing seats (13), the top of each fixing seat (13) is provided with a mounting frame (14), and the mounting frames (14) are in L-shaped arrangement.
6. Wire cutting machine for machining profiled parts of aircraft according to claim 5, characterized in that the mounting bracket (14) is provided with a mounting shaft (15) on the left side and that the surface of the mounting shaft (15) is rotatably provided with a blocking plate (16).
7. The wire cutting machine for machining of irregular parts of aircraft according to claim 6, wherein a first mounting seat (17) is mounted on the left side of the blocking plate (16), a second mounting seat (18) is mounted on the inner side of the mounting frame (14), an electric push rod (19) is rotatably mounted on the inner side of the second mounting seat (18), and the free end of the electric push rod (19) is rotatably connected with the first mounting seat (17).
8. Wire cutting machine for machining of aircraft profiles according to claim 2, characterized in that limiting plates (20) are mounted on both sides of the connecting plate (9), and that the limiting plates (20) are slidingly connected with the inner cavity of the discharge box (81).
CN202520220547.6U 2025-02-12 2025-02-12 Linear cutting machine for machining aircraft special-shaped parts Active CN223670358U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202520220547.6U CN223670358U (en) 2025-02-12 2025-02-12 Linear cutting machine for machining aircraft special-shaped parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202520220547.6U CN223670358U (en) 2025-02-12 2025-02-12 Linear cutting machine for machining aircraft special-shaped parts

Publications (1)

Publication Number Publication Date
CN223670358U true CN223670358U (en) 2025-12-16

Family

ID=97974799

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202520220547.6U Active CN223670358U (en) 2025-02-12 2025-02-12 Linear cutting machine for machining aircraft special-shaped parts

Country Status (1)

Country Link
CN (1) CN223670358U (en)

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