CN204365942U - Novel straight side press stable state fuselage - Google Patents
Novel straight side press stable state fuselage Download PDFInfo
- Publication number
- CN204365942U CN204365942U CN201420854071.3U CN201420854071U CN204365942U CN 204365942 U CN204365942 U CN 204365942U CN 201420854071 U CN201420854071 U CN 201420854071U CN 204365942 U CN204365942 U CN 204365942U
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- CN
- China
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- fuselage
- stable state
- column
- support
- girdle
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Abstract
Novel straight side press stable state fuselage, left and right sides symmetry erects column (1) the upper end level fixing top top gem of a girdle-pendant beam (2) of installing, in downside, top top gem of a girdle-pendant beam (2), crankcase (3) is installed, support of motor (8) is installed above base, and, in left side column (1) external wall of upper portion, clutch and brake support (10) is installed, in right side uprights (1) external wall of upper portion, bent axle cover (11) is installed.Adopt the system improvement opportunity measure comprising stable state fuselage design, support high frequency processing, under long-term heavy load runs, fuselage bulk deformation is little, production cost is low for fuselage.Effective lifting means rigidity and machining accuracy, overcome angular deformation, supports steady in a long-term operation, and be enhanced to large scale workpiece working ability and efficiency.Working stability, eliminates safe hidden trouble, and is particularly useful for machine parts'precise processing in enormous quantities.
Description
Technical field
The utility model relates to press equipment carrying or bracing or strutting arrangement, especially novel straight side press stable state fuselage.
Background technology
The fuselage body of forcing press, is the body bearing structure of forcing press, belongs to important and basic technology.Straight side press is divided into single-point and two point two type according to lathe bed structure, wherein, kinds of point mode forcing press adopts two bent axles, workbench face width, operating pressure is large, tonnage is large, but owing to relating to synchronous coordination between two bent axles, the very complicated punch forming being only applicable to large-scale part of device structure; One point press adopts independent bent axle on the other hand, avoids the synchronous coordination problem between different bent axle, although energy consumption is little during work, is subject to the restriction that tonnage is little and work top is little, only can meets the part punching forming requirements that size is less.
Forcing press is a kind of common apparatus of extensive use in the industrial production such as forging, and press frame can be divided into cast moulding and solder type.Cast moulding fuselage good integral strength, but from great, cost is high.Solder type fuselage, fuselage deadweight is comparatively light, and waste of material is few, cost is light, is widely adopted, but when punching press, due to the effect of reaction force, fuselage body is caused easily to be out of shape, even welding position fracture, have a strong impact on fuselage parts and mold use life-span, increase production cost, goods precision also cannot ensure, the manufacture method of thickened material is generally adopted in order to make up this defect, this makes again fuselage consumptive material strengthen, and complete machine weight strengthens, and production cost improves.
Utility model content
The purpose of this utility model is to provide a kind of novel straight side press stable state fuselage, take into account the respective advantage performance of single-point and two-point press fuselage, preferably absorb the respective advantage of forging and welding fuselage simultaneously, effective lifting means rigidity and machining accuracy, overcome angular deformation, support steady in a long-term operation, and large scale workpiece working ability and efficiency are enhanced.
The purpose of this utility model will be realized by following technical measures: comprise column, top top gem of a girdle-pendant beam, crankcase, front and back mouth, side mouth, a work platform, support of motor, clutch and brake support, bent axle cover and base; Left and right sides symmetry erects the column upper end level fixing top top gem of a girdle-pendant beam installed, on the downside of the top gem of a girdle-pendant beam of top, crankcase is installed, before and after between the column of the left and right sides, side is open front and back mouth respectively, all there are two columns in left or right middle side part front and rear part simultaneously, and opening has horizontal side mouth between these two columns, between the column of the left and right sides, platform is propped up in the horizontal installment work in middle and lower part, column is in bottom mounting seat, above base, support of motor is installed, and, in left side column external wall of upper portion, clutch and brake support is installed, in right side uprights external wall of upper portion, bent axle cover is installed.
Especially, crankcase installed in front protecgulum.
Especially, push up top gem of a girdle-pendant beam outer end and fix hanger.
Especially, left and right two heel post erects mounting guide rail respectively by support, and guide rail is 8 guide rails.
Especially, a work platform is horizontally fixed on inside two columns, and the dull and stereotyped downside of a platform that works when mounted is respectively connected and fixed a little all installs stiffener.
Especially, clutch and brake support comprises upper and lower two parts, and clutch and brake support and the bent axle cover of its middle and upper part are fixed on same level height and dead in line.
Advantage of the present utility model and effect: adopt the system improvement opportunity measure comprising stable state fuselage design, support high frequency processing, and under long-term heavy load runs, fuselage bulk deformation is little, production cost is low for fuselage.Take into account the respective advantage performance of single-point and two-point press fuselage, effective lifting means rigidity and machining accuracy, overcome angular deformation, supports steady in a long-term operation, and be enhanced to large scale workpiece working ability and efficiency.Compact conformation, easy to operate, excellent performance, working stability, eliminate safe hidden trouble, and is particularly useful for machine parts'precise processing in enormous quantities.Not only have lightweight, material is economized, and cost is low, and under long-term heavy load runs, fuselage bulk deformation is little, production cost is low.
Accompanying drawing explanation
Fig. 1 is the utility model embodiment 1 structural representation.
Fig. 2 is the right TV structure schematic diagram of the utility model embodiment 1.
Fig. 3 is the middle and upper part cross section plan structure schematic diagram after installing in the utility model embodiment 1.
Fig. 4 is the middle and lower part work platform position cross section plan structure schematic diagram after installing in the utility model embodiment 1.
Fig. 5 is the utility model embodiment 1 middle and upper part clutch and brake support and bent axle cover position cross-sectional structure schematic diagram.
Reference numeral comprises: column 1, top top gem of a girdle-pendant beam 2, crankcase 3, protecgulum 4, front and back mouth 5, side mouth 6, a work platform 7, support of motor 8, guide rail 9, clutch and brake support 10, bent axle cover 11, base 15, hanger 16, slide block 17.
Detailed description of the invention
The utility model principle is, closed type structure is optimized further, reasonable Arrangement slide block, balance cylinder and clutch, installation position of drive shafting, while the acquisition rigidity of structure significantly promotes, keep comparatively economic equipment size, and be convenient to coordinate to promote processing characteristics further.
The utility model comprises: column 1, top top gem of a girdle-pendant beam 2, crankcase 3, front and back mouth 5, side mouth 6, a work platform 7, support of motor 8, clutch and brake support 10, bent axle cover 11 and base 15.
Below in conjunction with drawings and Examples, the utility model is described in further detail.
Embodiment 1: as accompanying drawing 1, shown in 2, left and right sides symmetry erects the column 1 upper end level fixing top top gem of a girdle-pendant beam 2 installed, on the downside of top top gem of a girdle-pendant beam 2, crankcase 3 is installed, before and after between left and right sides column 1, side is open front and back mouth 5 respectively, all there are two columns 1 in left or right middle side part front and rear part simultaneously, and opening has horizontal side mouth 6 between these two columns 1, between left and right sides column 1, platform 7 is propped up in the horizontal installment work in middle and lower part, column 1 is in bottom mounting seat 15, support of motor 8 is installed above base, and, in left side column 1 external wall of upper portion, clutch and brake support 10 is installed, in right side uprights 1 external wall of upper portion, bent axle cover 11 is installed.
In aforementioned, crankcase 3 installed in front protecgulum 4.
In aforementioned, hanger 16 is fixed in top gem of a girdle-pendant beam 2 outer end, top.Hanger 16 is convenient to equipment moving and installation.
In aforementioned, as shown in Figure 3, left and right two heel post 1 erects mounting guide rail 9 respectively by support, and guide rail 9 is 4 or 6.Slide block 17 is arranged between guide rail 9, and slide block 17 top is connected with bent axle by linkage.
In aforementioned, as shown in Figure 4, a work platform 7 is horizontally fixed on inside each column 1, and on the downside of a platform 7 that works when mounted, individual being connected and fixed a little all installs stiffener, to ensure enough bearing capacitys.
In aforementioned, as shown in Figure 5, clutch and brake support 10 comprises upper and lower two parts, and clutch and brake support 10 and the bent axle of its middle and upper part overlap 11 and be fixed on same level height and dead in line.
In aforementioned, side mouth 6 is of a size of, upper and lower 350-520mm, front and back 420-920mm; Fuselage appearance size left and right pillar 1 outer wall spacing 1890-2810mm, front and back column 1 outer wall spacing 1650-3430mm, fuselage height 2900-4790mm; Weight 9500-40500kg.
The utility model adopts gantry type frame structure, and it coordinates with large scale workbench, balance cylinder, guide rail and bent axle, and ensure the distortion of Sheet Metal Forming Technology non-angular, product size precision is higher.
In the utility model, in the column of waist both sides, symmetrical balance cylinder of installing alleviates the impact of mode transfer operating physical force as air-cylinder type slide block gravity balancer respectively.
The utility model adopts quality steel plate and advanced technologies to be welded, and then through eliminating stress PROCESS FOR TREATMENT, has precision high, stability and good rigidly; Front and back are symmetrical, eliminate angular deformation phenomenon, improve stamping parts machining accuracy.
The utility model for the manufacture of forcing press, be applicable to the kinds of processes such as punching, blanking, bending, flanging, shallow stretching, cold extrusion, hot die forming, be widely used in the Forging Technology that the manufacturings such as automobile fitting, hot-water heating, air-conditioning, standard component, motor and various pressure stroke are permitted.
During utility model works, fuselage bottom is fixed on basis by base tail margin.
Advantage of the present utility model comprises: compare like product fuselage weight lighter, save considerably material, reduce production cost, equipment precision and intensity good, anti-torsion ability is strong, and when long-duration load is moved, frame deflection is little, support made with high precision, effectively extend the service life of mould and related components.
Below be only preferred embodiments of the present utility model, not any pro forma restriction is done to the utility model, every above example is done according to technical spirit of the present utility model any simple modification, equivalent variations and modification, all still belong in the scope of technical solutions of the utility model.
Claims (6)
1. novel straight side press stable state fuselage, comprises column (1), top top gem of a girdle-pendant beam (2), crankcase (3), front and back mouth (5), side mouth (6), work platform (7), support of motor (8), clutch and brake support (10), bent axle cover (11) and base (15), it is characterized in that, left and right sides symmetry erects column (1) the upper end level fixing top top gem of a girdle-pendant beam (2) of installing, in downside, top top gem of a girdle-pendant beam (2), crankcase (3) is installed, before and after between left and right sides column (1), side is open front and back mouth (5) respectively, all there are two columns (1) in left or right middle side part front and rear part simultaneously, and opening has horizontal side mouth (6) between these two columns (1), between left and right sides column (1), platform (7) is propped up in the horizontal installment work in middle and lower part, column (1) is in bottom mounting seat (15), support of motor (8) is installed above base, and, in left side column (1) external wall of upper portion, clutch and brake support (10) is installed, in right side uprights (1) external wall of upper portion, bent axle cover (11) is installed.
2. novel straight side press stable state fuselage as claimed in claim 1, is characterized in that, crankcase (3) installed in front protecgulum (4).
3. novel straight side press stable state fuselage as claimed in claim 1, is characterized in that, hanger (16) is fixed in top gem of a girdle-pendant beam (2) outer end, top.
4. novel straight side press stable state fuselage as claimed in claim 1, is characterized in that, mounting guide rail (9) is erect respectively by support in left and right two heel post (1), and guide rail (9) is 8 guide rails.
5. novel straight side press stable state fuselage as claimed in claim 1, it is characterized in that, a work platform (7) is horizontally fixed on two columns (1) inner side, and the dull and stereotyped downside of a platform (7) that works when mounted is respectively connected and fixed a little all installs stiffener.
6. novel straight side press stable state fuselage as claimed in claim 1, it is characterized in that, clutch and brake support (10) comprises upper and lower two parts, and clutch and brake support (10) and the bent axle cover (11) of its middle and upper part are fixed on same level height and dead in line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420854071.3U CN204365942U (en) | 2014-12-24 | 2014-12-24 | Novel straight side press stable state fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420854071.3U CN204365942U (en) | 2014-12-24 | 2014-12-24 | Novel straight side press stable state fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204365942U true CN204365942U (en) | 2015-06-03 |
Family
ID=53322191
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420854071.3U Expired - Fee Related CN204365942U (en) | 2014-12-24 | 2014-12-24 | Novel straight side press stable state fuselage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204365942U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107297537A (en) * | 2017-06-21 | 2017-10-27 | 中钢集团西安重机有限公司 | A kind of reinforced cold shears frame |
| CN109248984A (en) * | 2018-10-22 | 2019-01-22 | 江苏双赢锻压机床有限公司 | A kind of fine press upper beam structure |
-
2014
- 2014-12-24 CN CN201420854071.3U patent/CN204365942U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107297537A (en) * | 2017-06-21 | 2017-10-27 | 中钢集团西安重机有限公司 | A kind of reinforced cold shears frame |
| CN107297537B (en) * | 2017-06-21 | 2018-11-27 | 中钢集团西安重机有限公司 | A kind of reinforced cold shears rack |
| CN109248984A (en) * | 2018-10-22 | 2019-01-22 | 江苏双赢锻压机床有限公司 | A kind of fine press upper beam structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190107 Address after: 243131 East Side of Dongcheng Road, Bowang Town, Bowang District, Ma'anshan City, Anhui Province Patentee after: ANHUI YUANDU MACHINE TOOL Co.,Ltd. Address before: 201317 No. 5285 Hunan Road, Hangtou Town, Pudong New Area, Shanghai Patentee before: Shanghai Chaoyang Forging Machine Tool Factory Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150603 Termination date: 20211224 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |