CN213997288U - Aircraft thin wall panel beating parts machining frock - Google Patents
Aircraft thin wall panel beating parts machining frock Download PDFInfo
- Publication number
- CN213997288U CN213997288U CN202022535537.1U CN202022535537U CN213997288U CN 213997288 U CN213997288 U CN 213997288U CN 202022535537 U CN202022535537 U CN 202022535537U CN 213997288 U CN213997288 U CN 213997288U
- Authority
- CN
- China
- Prior art keywords
- clamping plate
- side clamping
- sheet metal
- machining tool
- block
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Bending Of Plates, Rods, And Pipes (AREA)
Abstract
The utility model discloses an aircraft thin-wall sheet metal part machining tool, which relates to the technical field of part machining tools and comprises a base, an operation table, a left side abutting block, a right side abutting block, an outer side clamping plate, an inner side clamping plate, a step table, a clamping strip, a cylindrical block, a mould and a connecting piece; the cylinder piece, mould all adopt the arc contact surface, have avoided the material too sharp-pointed to cause the damage to the article, adopt a plurality of outside splint, inboard splint to carry out the crisscross butt of dog tooth, have strengthened the stability of whole equipment, when down moving to the angle that needs bend, the mould begins to stop moving down, begins to up move, takes out the work piece that processing was accomplished, has reached the effect of bending.
Description
Technical Field
The utility model relates to a parts machining frock technical field specifically is an aircraft thin wall panel beating parts machining frock.
Background
The machine manufacturing industry is a post industry which the country depends on to live, and can often show the level of industrialization of one country and one region from one side. With the increasing international competition in the fields of aerospace and the like, higher requirements are put forward on the performance of products, and in order to reduce the weight of the products, improve the structural strength of the products and further improve the performance of the products, a large number of thin-wall structural parts, such as sheet metal parts in aircraft structural members and the like, are used in the fields.
The utility model discloses a current authorized utility model patent, patent application number is 201920757108.3, and the patent name is an aircraft thin wall panel beating parts machining frock, including bottom plate, clamp plate, rings, pull ring, core, bottom plate upper end surface is provided with four group's mounting holes, fixedly connected with shank of bolt in the mounting hole, shank of bolt upper end fixedly connected with nut, nut top fixedly connected with rings, the bottom plate upper end is provided with the panel beating part, the panel beating part upper end is passed through the clamp plate is fixed, clamp plate upper end fixed surface is connected with two sets of connecting plates, be provided with the pull ring on the connecting plate, the clamp plate surface still is provided with the multiunit core. The utility model discloses it is even and positioning accuracy is high to have messenger's panel beating part atress, possess convenient operation, the high beneficial effect of just product percent of pass height of machining efficiency, its mainly used thin wall panel beating class parts machining.
However, the above scheme has some problems, firstly, the metal plate cannot be bent, the molding type is greatly reduced, and secondly, the offset is easy to occur in the machining process, so that the precision is not high.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an aircraft thin-wall sheet metal part machining tool, which is used for solving the technical problems existing in the prior art; firstly, the operation of bending can not be carried out to the panel beating, very big reduction moulding type, secondly, the skew takes place easily in the course of working, leads to the precision not high.
The utility model aims to overcome the not enough of prior art, provide an aircraft thin wall panel beating parts machining frock: comprises a base, an operation table, a left side abutting block, a right side abutting block, an outer side clamping plate, an inner side clamping plate, a ladder bed, clamping strips, a cylindrical block, a mold and a connecting piece;
wherein the bottom of the operating platform is fixedly connected with the top end of the base, the top of the operating platform is provided with a through groove, the left side abutting block and the right side abutting block are respectively detachably arranged at two sides of the groove of the operating platform,
one corner of the bottom edge of the outer side splint is provided with a square unfilled corner, the top end of the corner opposite to the unfilled corner of the bottom edge of the outer side splint is fixedly connected with a step table, the outer side splint is arranged and connected at the bottom of the step table in an array manner, one corner of the bottom edge of the inner side splint is provided with a square unfilled corner, the top end of the unfilled corner of the bottom edge of the inner side splint is fixedly connected with the step table, the inner side splint is arranged and connected at the bottom of the step table in an array manner, the outer side splint and the inner side splint are distributed in a staggered manner,
the top end of the ladder platform is fixedly connected with the holding strip, the inner wall of the holding strip can be disassembled to place the cylindrical block, and the top of the die is fixedly connected with a connecting piece.
Furthermore, a hydraulic device is detachably connected to the top end of the connecting piece.
Furthermore, the mould adopts a semicircular structure, a square groove is formed in the circle center, and the end part of the connecting piece is detachably connected in the groove.
Furthermore, a square block is arranged at the top end of the connecting piece, and a through hole is formed in the square block. Furthermore, oil is arranged at the contact part of the left abutting block and the right abutting block.
Further, the mold can move up and down between the two cylindrical blocks. Furthermore, the outer side clamping plate and the inner side clamping plate are in interference fit. Furthermore, the bottom of the base is fixedly connected with a supporting leg.
The utility model has the advantages that: (1) the cylindrical block and the die both adopt arc-shaped contact surfaces, so that damage to objects caused by excessively sharp materials is avoided.
(2) Adopt a plurality of outside splint, inboard splint to carry out the crisscross butt of dog tooth, strengthened the stability of whole equipment.
(3) When the die moves downwards to an angle required to be bent, the die starts to stop moving downwards and starts to move upwards, a machined workpiece is taken out, and the effect of bending is achieved.
Drawings
Fig. 1 is the utility model relates to an aircraft thin wall panel beating parts machining frock schematic diagram.
Fig. 2 is the utility model relates to an aircraft thin wall panel beating parts machining frock mould view.
Fig. 3 is the utility model relates to an aircraft thin wall panel beating parts machining frock outside splint view.
Figure 4 is the utility model relates to an inboard splint view of aircraft thin wall panel beating parts machining frock.
In the figure, 1-a base, 2-an operation table, 3-a left side abutting block, 4-a right side abutting block, 5-an outer side clamping plate, 6-an inner side clamping plate, 7-a step table, 8-a clamping strip, 9-a cylindrical block, 10-a mould and 11-a connecting piece.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to fig. 1-4 of the present invention, and it should be apparent that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
A thin-wall sheet metal part machining tool for an airplane comprises a base 1, an operation table 2, a left side abutting block 3, a right side abutting block 4, an outer side clamping plate 5, an inner side clamping plate 6, a step table 7, clamping strips 8, a cylindrical block 9, a mold 10 and a connecting piece 11;
wherein the bottom of the operation table 2 is fixedly connected to the top end of the base 1, the top of the operation table 2 is provided with a through groove, the left side support block 3 and the right side support block 4 are respectively detachably arranged at two sides of the groove of the operation table 2, one corner of the bottom edge of the outer side clamp plate 5 is provided with a square unfilled corner, the top end of the corner opposite to the unfilled corner of the bottom edge of the outer side clamp plate 5 is fixedly connected with a step table 7, the outer side clamp plates 5 are arranged at the bottom of the step table 7 in an array manner, one corner of the bottom edge of the inner side clamp plate 6 is provided with a square unfilled corner, the top end of the unfilled corner of the bottom edge of the inner side clamp plate 6 is fixedly connected with the step table 7, the inner side clamp plates 6 are arranged at the bottom of the step table 7 in an array manner, the outer side clamp plates 5 and the inner side clamp plates 6 are distributed in a staggered manner, and the top end of the step table 7 is fixedly connected with a clamp strip 8, the inner wall of holding strip 8 can dismantle and place cylinder piece 9, and the top fixedly connected with connecting piece 11 of mould 10.
Referring to fig. 1-4, the present invention provides a technical solution; the bottom of an operation table 2 is connected to the top end of a base 1, the top of the operation table 2 is provided with a through groove, a left side support block 3 and a right side support block 4 are respectively arranged at two sides of the groove of the operation table 2, one corner of the bottom edge of an outer side splint 5 is provided with a square unfilled corner, the top end of the corner opposite to the unfilled corner of the bottom edge of the outer side splint 5 is connected with a step 7, the outer side splint 5 is arranged and connected at the bottom of the step 7 in an array manner, one corner of the bottom edge of an inner side splint 6 is provided with a square unfilled corner, the top end of the unfilled corner of the bottom edge of the inner side splint 6 is connected with the step 7, the inner side splint 6 is arranged and connected at the bottom of the step 7 in an array manner, the outer side splint 5 and the inner side splint 6 are arranged and distributed in an interlaced manner, a clamping strip 8 is connected at the top end of the step 7, and a cylindrical block 9 is arranged on the inner wall of the clamping strip 8, the top of mould 10 is connected with connecting piece 11, when needs use the utility model discloses the time, adjust outside splint 5, the position of inboard splint 6, when adjusting the position that needs, support piece 3 with the left side, the right side supports piece 4 and places respectively in the position that corresponds, whether detect whole machine is fixed, confirm the back that finishes, the article that will bend need be placed in the top of cylinder piece 9, begin to start the machine, connecting piece 11 drives mould 10 and moves down, when the bottom butt article of mould 10, when the top butt article of cylinder piece 9, begin to bend the article, when the angle that needs bend is moved down to, mould 10 begins to stop and moves down, begin to move up, take out the work piece that the processing was accomplished, the effect of bending has been reached.
Furthermore, a hydraulic device is detachably connected to the top end of the connecting piece 11, so that the workpiece can be deformed conveniently.
Further, the die 10 adopts a semicircular structure, a square groove is formed in the circle center, and the end part of the connecting piece 11 is detachably connected in the groove to play a role in connection.
Furthermore, the top end of the connecting piece 11 is provided with a square block, and the square block is provided with a through hole, so that a hydraulic device above the square block can be conveniently connected.
Furthermore, oil is arranged at the contact part of the left abutting block 3 and the right abutting block 4, so that long-term abrasion is avoided. Further, the mold 10 can move up and down between the two cylindrical blocks 9, which is convenient for the user to operate.
Furthermore, the outer side clamping plate 5 and the inner side clamping plate 6 are in interference fit, so that the stability of the equipment is improved. Furthermore, the bottom of the base 1 is fixedly connected with supporting legs, so that the operation of workers is facilitated.
In the description of the present invention, it should be understood that the terms "counterclockwise", "clockwise", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description of the present invention, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Claims (8)
1. The machining tool for the thin-wall sheet metal parts of the airplane is characterized by comprising a base (1), an operating platform (2), a left side abutting block (3), a right side abutting block (4), an outer side clamping plate (5), an inner side clamping plate (6), a step (7), clamping strips (8), a cylindrical block (9), a mold (10) and a connecting piece (11);
wherein the bottom of the operating platform (2) is fixedly connected with the top end of the base (1), the top of the operating platform (2) is provided with a transversely penetrating groove, the left side supporting block (3) and the right side supporting block (4) are respectively detachably arranged at two sides of the groove of the operating platform (2),
one corner of the bottom edge of the outer side clamping plate (5) is provided with a square unfilled corner, the bottom of the ladder platform (7) is fixedly connected with the outer side clamping plate (5), the outer side clamping plate (5) is arranged and connected with the bottom of the ladder platform (7) in an array manner, one corner of the bottom edge of the inner side clamping plate (6) is provided with a square unfilled corner, the bottom of the ladder platform (7) is fixedly connected with the inner side clamping plate (6), the inner side clamping plate (6) is arranged and connected with the bottom of the ladder platform (7) in an array manner, the outer side clamping plate (5) and the inner side clamping plate (6) are distributed in a staggered manner,
the top end of the ladder platform (7) is fixedly connected with a holding strip (8), the inner wall of the holding strip (8) is detachably provided with a cylindrical block (9), and the mold
(10) The top of the connecting piece (11) is fixedly connected with the connecting piece.
2. The aircraft thin-wall sheet metal part machining tool according to claim 1, characterized in that a hydraulic device is detachably connected to the top end of the connecting piece (11).
3. The aircraft thin-wall sheet metal part machining tool according to claim 1, characterized in that the mold (10) is of a semicircular structure, a square groove is formed in the center of the circle, and the end of the connecting piece (11) is detachably connected in the groove.
4. The aircraft thin-wall sheet metal part machining tool according to claim 1, characterized in that a square block is arranged at the top end of the connecting piece (11), and the square block is provided with a through hole.
5. The aircraft thin-wall sheet metal part machining tool according to claim 1, wherein oil is arranged at a contact part of the left abutting block (3) and the right abutting block (4).
6. The aircraft thin-wall sheet metal part machining tool according to claim 1, characterized in that the die (10) can move up and down between the two cylindrical blocks (9).
7. The aircraft thin-wall sheet metal part machining tool according to claim 1, characterized in that the outer side clamping plate (5) and the inner side clamping plate (6) are in interference fit.
8. The aircraft thin-wall sheet metal part machining tool according to claim 1, characterized in that a support leg is fixedly connected to the bottom of the base (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022535537.1U CN213997288U (en) | 2020-11-05 | 2020-11-05 | Aircraft thin wall panel beating parts machining frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022535537.1U CN213997288U (en) | 2020-11-05 | 2020-11-05 | Aircraft thin wall panel beating parts machining frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213997288U true CN213997288U (en) | 2021-08-20 |
Family
ID=77303586
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022535537.1U Active CN213997288U (en) | 2020-11-05 | 2020-11-05 | Aircraft thin wall panel beating parts machining frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213997288U (en) |
-
2020
- 2020-11-05 CN CN202022535537.1U patent/CN213997288U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN217941509U (en) | A ammunition device for hardware punching press for precision finishing | |
| CN213997288U (en) | Aircraft thin wall panel beating parts machining frock | |
| CN202910484U (en) | Flexible tool clamp platform special for welding mechanical arm | |
| CN209902072U (en) | Frame spare arc angle moulded die | |
| CN212216695U (en) | Hydraulic machine for hardware machining | |
| CN211101906U (en) | Semi-automatic unloading sawtooth milling machine frock of going up | |
| CN211681104U (en) | Clamping jig for machine tool machining | |
| CN210305301U (en) | Junction box side surface punching die with high machining quality | |
| CN213166388U (en) | Positioning fixture is used in plastic mould processing | |
| CN215159382U (en) | Position conversion device for cushion block production | |
| CN218946026U (en) | Arc bending device for aluminum profile | |
| CN221537721U (en) | Steel plate bending and compression molding tool | |
| CN214770621U (en) | Positioning fixture for processing metal sheet parts | |
| CN212019152U (en) | Positioning tool for stamping | |
| CN220612751U (en) | Welding fixture | |
| CN221754536U (en) | Workpiece positioning device for punching machine | |
| CN216369639U (en) | Stamping and bending device for crane connecting piece | |
| CN220259314U (en) | Embossing nail pulling die | |
| CN216501913U (en) | High-precision metal piece stamping continuous die | |
| CN217990508U (en) | Bending equipment for machining | |
| CN215589376U (en) | Anti-deviation template of aluminum foil tableware mould | |
| CN217432733U (en) | Prevent punch press of material slippage | |
| CN217141869U (en) | Moulding-die punch press is used in sealing member production | |
| CN221559560U (en) | Stamping die is used in hardware production | |
| CN214382963U (en) | Spark machine convenient to fix a position product |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |