CN221336088U - Aviation sheet metal mold machining tool - Google Patents
Aviation sheet metal mold machining tool Download PDFInfo
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- CN221336088U CN221336088U CN202322950770.XU CN202322950770U CN221336088U CN 221336088 U CN221336088 U CN 221336088U CN 202322950770 U CN202322950770 U CN 202322950770U CN 221336088 U CN221336088 U CN 221336088U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
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Abstract
本实用新型公开一种航空用钣金模具加工工装，涉及模具工装技术领域，一种航空用钣金模具加工工装，其包括：底座、支撑架、液压缸、成型头、支撑板、支撑柱和固定垫片。所述底座开设有安装槽。所述支撑架固定设置于所述底座上。所述液压缸设置于所述支撑架上。所述成型头设置于所述液压缸的伸缩端。两组所述支撑板转动设置于所述底座上，且两组支撑板对称设置，两组所述支撑板之间形成用于加工缝隙的空间。所述支撑柱的一端可拆卸设置于所述安装槽中，另一端可与所述支撑板的下端面抵接。所述固定垫片卡设于所述安装槽中，用于固定所述支撑柱。本实用新型提供的航空用钣金模具加工工装，用于用于加工航班钣金零件，可进行冲孔、折弯等多种钣金成型操作，提高工作效率，节省设备成本。
The utility model discloses a sheet metal mold processing tool for aviation, which relates to the technical field of mold tooling. The sheet metal mold processing tool for aviation includes: a base, a support frame, a hydraulic cylinder, a forming head, a support plate, a support column and a fixed gasket. The base is provided with a mounting groove. The support frame is fixedly arranged on the base. The hydraulic cylinder is arranged on the support frame. The forming head is arranged at the telescopic end of the hydraulic cylinder. Two groups of support plates are rotatably arranged on the base, and the two groups of support plates are symmetrically arranged, and a space for processing gaps is formed between the two groups of support plates. One end of the support column is detachably arranged in the mounting groove, and the other end can abut against the lower end surface of the support plate. The fixed gasket is clamped in the mounting groove to fix the support column. The sheet metal mold processing tool for aviation provided by the utility model is used for processing aircraft sheet metal parts, and can perform various sheet metal forming operations such as punching and bending, thereby improving work efficiency and saving equipment costs.
Description
Technical Field
The utility model relates to the technical field of mold tools, in particular to a sheet metal mold machining tool for aviation
Background
The metal plate is a processing technology, the metal plate has not been defined completely, a comprehensive cold processing technology comprises the methods of shearing, punching, cutting, compounding, folding, riveting, splicing, forming and the like, and with the development of industrial technology, a large number of aviation metal plate mold processing tools are put into use, and the metal plate processing efficiency and processing precision are improved through the mold tools.
The patent application number is 201920757108.3, and the patent name is an aircraft thin wall sheet metal part processing frock, has the beneficial effects that makes sheet metal part atress even and positioning accuracy high, possess convenient operation, machining efficiency high and the product percent of pass is high, and it is mainly used thin wall sheet metal part processing.
However, the above scheme has the problems that the sheet metal cannot be subjected to bending operation, so that the type of shaping is greatly reduced.
Disclosure of utility model
The embodiment of the utility model provides a sheet metal die machining tool for aviation, which adopts the following technical scheme:
An aviation sheet metal mold tooling tool, comprising: base, support frame, pneumatic cylinder, shaping head, backup pad, support column and fixed gasket. The base is provided with a mounting groove. The support frame is fixedly arranged on the base. The hydraulic cylinder is arranged on the supporting frame. The forming head is arranged at the telescopic end of the hydraulic cylinder. The two groups of supporting plates are rotationally arranged on the base, the two groups of supporting plates are symmetrically arranged, and a space for processing a gap is formed between the two groups of supporting plates. One end of the support column is detachably arranged in the mounting groove, and the other end of the support column can be abutted with the lower end face of the support plate. The fixing gasket is clamped in the mounting groove and used for fixing the support column.
According to the metal plate mold processing tool for aviation, provided by the embodiment of the utility model, the movable supporting plate and the supporting component are arranged, so that the metal plate bending operation can be performed, the included angle of the supporting plate can be adjusted by adjusting the assembly mode of the supporting component, the bending angle of the metal plate is changed, various processing operations are realized, the equipment cost is saved, and the working efficiency is improved.
Further, the aviation sheet metal mold processing tool further comprises: the bottom of the core mold is provided with a fixing protrusion; the core groove is formed in the base, and the fixing protrusion can be clamped in the core groove; the locking assembly is arranged at the joint of the core die and the base and used for locking and fixing the core die.
Further, the locking assembly includes: the base and the fixing protrusions are provided with fixing screw holes corresponding to each other in position, and the locking studs penetrate through the fixing screw holes.
Further, the aviation sheet metal mold processing tool further comprises: the pressing plate is provided with a fixed clamping groove; one end of the fixed stud is rotatably arranged on the supporting plate, and the other end of the fixed stud can be clamped in the fixed clamping groove; and the locking knob is in threaded connection with the fixed stud.
Further, the pressing plate is rotatably provided with a hanging ring.
Further, a plurality of positioning holes are formed in the pressing plate at intervals.
Further, the base is provided with a waste collection tank detachably connected with the base.
Further, the aviation sheet metal mold processing tool further comprises: the scale plate is fixedly arranged on the base and positioned at one end of the supporting plate, and an angle mark is carved on the scale plate and used for measuring the angle of the supporting plate.
Drawings
Fig. 1 is a perspective view of an aviation sheet metal die tooling tool provided in embodiment 1;
fig. 2 is a cross-sectional view of the tooling for processing the metal plate mold for aviation provided in embodiment 1;
FIG. 3 is an enlarged view of area A of FIG. 2;
FIG. 4 is a diagram of a support post mounting structure;
fig. 5 is a perspective view of the tooling for processing the metal plate mold for aviation provided in embodiment 2;
Fig. 6 is a cross-sectional view of the tooling for processing the metal plate mold for aviation provided in embodiment 2;
Fig. 7 is an enlarged view of region B in fig. 6.
Reference numerals: 1-a base; 2-supporting frames; 3-a hydraulic cylinder; 4-forming head; 5-supporting plates; 6-supporting columns; 7-fixing the gasket; 8-core mold; 9-a core slot; 10-locking a stud; 11-pressing plates; 12-fixing a clamping groove; 13-fixing the stud; 14-locking a knob; 15-hanging rings; 16-positioning holes; 17-a waste collection bin; 18-scale plate.
Detailed Description
Embodiments of the present utility model will be described in detail below with reference to the accompanying drawings.
In the description of the present utility model, it should be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, merely to facilitate describing the present utility model and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model.
The terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
In the case of example 1,
Referring to fig. 1-4, the embodiment provides a sheet metal mold processing tool for aviation, which includes: base 1, support frame 2, pneumatic cylinder 3, shaping head 4, backup pad 5, support column 6 and fixed gasket 7. The base 1 is provided with a mounting groove. The support frame 2 is fixedly arranged on the base 1. The hydraulic cylinder 3 is arranged on the supporting frame 2. The forming head 4 is arranged at the telescopic end of the hydraulic cylinder 3. The two groups of support plates 5 are rotatably arranged on the base 1, the two groups of support plates 5 are symmetrically arranged, and a space for processing gaps is formed between the two groups of support plates 5. One end of the support column 6 is detachably arranged in the mounting groove, and the other end of the support column can be abutted with the lower end face of the support plate 5. The fixing gasket 7 is clamped in the mounting groove and used for fixing the support column 6.
In this embodiment, the base 1 is provided with two sets of support plates 5, and the plate material may be placed on the support plates 5 to perform sheet metal forming operations such as punching and bending. Specifically, two groups of support plates 5 are rotatably connected with the base 1, and a space for processing a gap is formed between the two groups of support plates 5. When the supporting plate 5 is horizontally placed on the base 1, the plate can be directly placed on the supporting plate 5, so that punching or drilling and other operations can be conveniently performed. The base 1 is provided with a mounting groove which can be arranged into a T-shaped structure. The mounting groove is used for placing the support column 6 and the fixed gasket 7. When the support column 6 is placed in the mounting groove, the upper end of the support column 6 is abutted against the lower end face of the support plate 5, so that the support plate 5 is in an inclined state. When two groups of support plates 5 are obliquely placed, an included angle is formed between the support plates 5, and bending operation can be performed on the plates. When the support column 6 is installed in the installation groove, the fixing gasket 7 fills the gap between the support column 6 and the installation groove, so that the stability of the support column 6 is ensured. Referring to fig. 3 and 4, the height of the support column 6 extending out of the base 1 can be adjusted by adjusting the number of fixing pads 7 at the lower end of the support column 6, i.e. the inclination angle of the support plate 5 can be adjusted by adjusting the placement mode of the fixing pads 7, so as to form bending structures with different angles. The angle of the supporting plate 5 is adjusted by adopting the mode of the fixed gasket 7 and the supporting column 6, and the stepless adjustment cannot be realized, but the structure is simple, the cost is low, and the maintenance is easy. Meanwhile, the stability of the support structure formed by the fixing piece and the support column 6 is high, the angle adjustment is accurate, and the angle change caused by compression during processing can be avoided. The support column 6 and the fixed gasket 7 are directly clamped and arranged in the mounting groove, fixed connection is not needed, and the support column 6 can be put in and taken out according to the needs during use. The base 1 is provided with a support frame 2 for installing a hydraulic cylinder 3. The telescopic end of the hydraulic cylinder 3 is connected with a forming head 4. The forming heads 4 are detachably connected with the hydraulic cylinder 3 through bolts, buckles and the like, so that different forming heads 4 can be replaced conveniently, and the forming heads are respectively used for carrying out different processing operations such as punching, bending and the like. The aviation sheet metal die machining tool skill provided by the embodiment is used for plane operations such as shearing, punching, splicing and the like, and also can be used for bending operations, so that equipment cost is saved.
Example 2
Referring to fig. 6 and 7, in this embodiment, on the basis of embodiment 1, the tooling for machining a sheet metal mold for aviation further includes: the mold core die comprises a mold core die 8, a mold core groove 9 and a locking assembly, wherein a fixing protrusion is arranged at the bottom of the mold core die 8. The core groove 9 is formed in the base 1, and the fixing protrusion can be clamped in the core groove 9. The locking assembly is arranged at the joint of the core die 8 and the base 1 and is used for locking and fixing the core die 8.
In this embodiment, the core mold 8 may be replaced according to actual processing requirements, so as to produce workpieces with different structures, and further improve the shaping type of the processing tool. Two core grooves 9 are formed in the base 1, and fixing protrusions at the bottom of the core die 8 are clamped in the core grooves 9. The plurality of fixing protrusions are matched and fixed in the core groove 9, so that the core die 8 is prevented from rotating during processing. The base 1 is provided with a locking assembly, and the core die 8 is locked through the locking assembly, so that the core die 8 is prevented from being displaced and separated.
Further, in some implementations of this embodiment, the locking assembly includes: the locking stud 10, the base 1 and the fixing protrusion are provided with fixing screw holes corresponding to each other, and the locking stud 10 is inserted into the fixing screw holes.
Example 3
Referring to fig. 5, in this embodiment, on the basis of the above embodiments, the tooling for machining a sheet metal mold for aviation further includes: a pressing plate 11, a fixing stud 13 and a locking knob 14. The pressing plate 11 is provided with a fixing clamping groove 12. One end of the fixing stud 13 is rotatably disposed on the supporting plate 5, and the other end thereof may be clamped in the fixing slot 12. The locking knob 14 is in threaded connection with the fixing stud 13.
In this embodiment, the pressing plate 11 is used to fix the processed plate placed on the supporting plate 5, so as to avoid the influence of the movement of the plate during processing. The pressing plate 11 clamps and fixes the plate to be processed on the supporting plate 5, the fixing stud 13 is arranged on the supporting plate 5, the fixing stud 13 is clamped in the fixing clamping groove 12 in a rotating mode, and then the fixing can be completed through tightening of the locking knob 14, so that the operation is convenient.
Optionally, in some implementations of this embodiment, a hanging ring 15 is rotatably disposed on the pressing plate 11, so as to facilitate taking and carrying the pressing plate 11.
Further, in some implementations of the present embodiment, the pressing plate 11 is provided with a plurality of positioning holes 16 at intervals. The pressing plate 11 serves as a fixing device for fixing the plate to be processed, and the pressing plate 11 serves as a processing template. Different locating holes 16 are formed in the machining plate according to actual machining requirements, machining positions of the plate are conveniently and accurately located, and machining efficiency can be improved when certain products are repeatedly machined.
Alternatively, in other embodiments, the base 1 is provided with a waste collection tank 17, the waste collection tank 17 being detachably connected to the base 1. The scraps and leftovers generated during processing fall into the waste collection box 17 at the lower end through the gaps between the support plates 5, so that the recovery and the treatment are facilitated.
Optionally, in some other embodiments, the tooling for machining a sheet metal mold for aviation further includes: the scale plate 18 is fixedly arranged on the base 1 and positioned at one end of the supporting plate 5, and an angle mark is carved on the scale plate 18 and used for measuring the angle of the supporting plate 5.
One side of the supporting plate 5 is provided with a scale plate 18, and angle measuring lines are engraved on the scale plate 18 and used for measuring the included angle between the two supporting plates 5. Because the contained angle between backup pad 5 is adjusted mainly through the structure of placing of adjustment fixed washer 7 and support column 6, need not to adjust against scale plate 18, consequently, the calibrated scale mainly plays the auxiliary role, is convenient for observe current contained angle.
In summary, the utility model provides an aviation sheet metal mold processing tool, which comprises: base 1, support frame 2, pneumatic cylinder 3, shaping head 4, backup pad 5, support column 6 and fixed gasket 7. The base 1 is provided with a mounting groove. The support frame 2 is fixedly arranged on the base 1. The hydraulic cylinder 3 is arranged on the supporting frame 2. The forming head 4 is arranged at the telescopic end of the hydraulic cylinder 3. The two groups of support plates 5 are rotatably arranged on the base 1, the two groups of support plates 5 are symmetrically arranged, and a space for processing gaps is formed between the two groups of support plates 5. One end of the support column 6 is detachably arranged in the mounting groove, and the other end of the support column can be abutted with the lower end face of the support plate 5. The fixing gasket 7 is clamped in the mounting groove and used for fixing the support column 6. Because set up mobilizable backup pad 5 and supporting component, can be used to carry out panel beating bending operation, adjust the contained angle that supporting component's assembled mode can adjust backup pad 5 to change the angle of buckling of panel beating, can realize multiple processing operation, save equipment cost, improve work efficiency.
In the description of the present specification, a particular feature, structure, material, or characteristic may be combined in any suitable manner in one or more embodiments or examples.
The foregoing is merely illustrative of the present utility model, and the present utility model is not limited thereto, and any person skilled in the art will readily recognize that variations or substitutions are within the scope of the present utility model. Therefore, the protection scope of the present utility model shall be subject to the protection scope of the claims.
Claims (8)
1. Aviation sheet metal mold processing frock, its characterized in that includes:
a base (1) provided with a mounting groove;
The support frame (2) is fixedly arranged on the base (1);
the hydraulic cylinder (3) is arranged on the supporting frame (2);
the forming head (4) is arranged at the telescopic end of the hydraulic cylinder (3);
The two groups of support plates (5) are rotationally arranged on the base (1), the two groups of support plates (5) are symmetrically arranged, and a space for processing a gap is formed between the two groups of support plates (5);
One end of the support column (6) is detachably arranged in the mounting groove, and the other end of the support column can be abutted with the lower end surfaces of the two groups of support plates (5);
And the fixing gasket (7) is clamped in the mounting groove and is used for fixing the support column (6).
2. The tooling for machining a sheet metal mold for aviation of claim 1, further comprising:
the bottom of the core mold (8) is provided with a fixing protrusion;
The core groove (9) is formed in the base (1), and the fixing protrusion can be clamped in the core groove (9);
The locking assembly is arranged at the joint of the core die (8) and the base (1) and is used for locking and fixing the core die (8).
3. The tooling for machining a sheet metal mold for aviation of claim 2, wherein the locking assembly comprises:
The locking stud (10), the base (1) with set up the fixed screw that the position corresponds on the fixed arch, locking stud (10) wears to locate in the fixed screw.
4. The tooling for machining a sheet metal mold for aviation of claim 1, further comprising:
the pressing plate (11), the said pressing plate (11) has fixed slot (12);
A fixed stud (13), one end of which is rotatably arranged on the supporting plate (5), and the other end of which can be clamped in the fixed clamping groove (12);
and the locking knob (14) is in threaded connection with the fixed stud (13).
5. The tooling for machining the metal plate mould for aviation according to claim 4, wherein the pressing plate (11) is rotatably provided with a hanging ring (15).
6. The tooling for machining the metal plate mould for aviation according to claim 5, wherein a plurality of positioning holes (16) are formed in the pressing plate (11) at intervals.
7. The tooling for machining sheet metal dies for aviation according to claim 6, characterized in that the base (1) is provided with a waste collection tank (17), the waste collection tank (17) being detachably connected with the base (1).
8. The tooling for machining a sheet metal mold for aviation of claim 1, further comprising:
The scale plate (18) is fixedly arranged on the base (1) and positioned at one end of the supporting plate (5), and an angle mark is carved on the scale plate (18) and used for measuring the angle of the supporting plate (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322950770.XU CN221336088U (en) | 2023-11-01 | 2023-11-01 | Aviation sheet metal mold machining tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322950770.XU CN221336088U (en) | 2023-11-01 | 2023-11-01 | Aviation sheet metal mold machining tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221336088U true CN221336088U (en) | 2024-07-16 |
Family
ID=91837956
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322950770.XU Active CN221336088U (en) | 2023-11-01 | 2023-11-01 | Aviation sheet metal mold machining tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221336088U (en) |
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2023
- 2023-11-01 CN CN202322950770.XU patent/CN221336088U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A sheet metal mold processing fixture for aviation Granted publication date: 20240716 Pledgee: China Co. truction Bank Corp Deyang branch Pledgor: Sichuan Tenghua Aviation Materials Technology Co.,Ltd. Registration number: Y2025980067381 |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right |