CN204367471U - The energy-conservation closed type single point press of high accuracy - Google Patents
The energy-conservation closed type single point press of high accuracy Download PDFInfo
- Publication number
- CN204367471U CN204367471U CN201420854456.XU CN201420854456U CN204367471U CN 204367471 U CN204367471 U CN 204367471U CN 201420854456 U CN201420854456 U CN 201420854456U CN 204367471 U CN204367471 U CN 204367471U
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- Prior art keywords
- fuselage
- brake
- slide block
- energy
- high accuracy
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- Expired - Fee Related
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Abstract
The energy-conservation closed type single point press of high accuracy, air accumulator (12) is installed at fuselage (1) top, both sides, fuselage (1) middle part are erect respectively and are installed column (8), slide block (2) is installed between two heel posts (8), combined type clutch-brake (3) and crankshaft arrangement (9) are installed outside fuselage (1) two respectively, guide rail (13) is installed discharging device (10), at fuselage (1) upper installation electric cam sender mechanism (11), balance cylinder (14) is installed between same heel post (8), adopt the system improvement opportunity measure comprising stable state fuselage design and clutch and brake associated working pattern, support high frequency is processed, reduce operation complexity and energy resource consumption, eliminate safe hidden trouble, save artificial and labour intensity, improve die life and production efficiency, compact conformation, excellent performance, working stability, be particularly useful for machine parts'precise processing in enormous quantities.
Description
Technical field
The utility model relates to press equipment device, especially the energy-conservation closed type single point press of high accuracy.
Background 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.
Utility model content
The purpose of this utility model is to provide the energy-conservation closed type single point press of a kind of high accuracy, takes into account the advantage performance of single-point and two-point press, effectively promotes machining accuracy, and be enhanced to large scale workpiece working ability and efficiency.
The purpose of this utility model will be realized by following technical measures: comprise fuselage, slide block, combined type clutch-brake, workbench, motor, operating desk, electrical control cubicles, column, crankshaft arrangement, discharging device, electric cam sender mechanism, air accumulator, guide rail and balance cylinder, fuselage roof installs air accumulator, waist both sides erect installation column respectively, between two heel posts, slide block is installed, erector's station below slide block, motor is installed in fuselage bottom side, outside fuselage two, combined type clutch-brake or crankshaft arrangement are installed respectively, combined type clutch-brake and motor are arranged on the same side, slide block top is connected with crankshaft arrangement by linkage, operating desk is arranged on front side of workbench, simultaneously, fuselage is connected with electrical control cubicles respectively with operating desk, mounting guide rail is erect respectively in slide block both sides, guide rail is fixed on column, discharging device installed by guide rail, fuselage is installed electric cam sender mechanism, electric cam sender mechanism is connected with electrical control cubicles, between same heel post, balance cylinder is installed, the hydraulic system be connected with combined type clutch-brake installs hydraulic pressure Overloading protection apparatus, the equipment lubrication system be connected with crankshaft arrangement and slide block installs adjustable dense oily self-lubricate oil pump.
Especially, fuselage adopts gantry type frame structure.
Especially, slide block adopts octahedral guiding.
Especially, combined type clutch-brake is dry type pneumatic friction clutch-brake.
Especially, on workbench or between two heel posts, photoelectric protector is installed.
Especially, back front side wall is installed bent axle axle sleeve and crankshaft bearing, bent axle is arranged on fuselage by bent axle axle sleeve and crankshaft bearing, and, back installed in front bent axle front shroud, bent axle inner segment is arranged in bent axle front shroud, and the outer section of bent axle is closed in the crankshaft arrangement part-structure that is arranged on outside back.
Especially, before and after guide rail, side installs material returned fore-stock and the material returned after-poppet of discharging device respectively, and often group material returned fore-stock and the equal symmetry of material returned after-poppet are arranged on the sustained height of column.
Advantage of the present utility model and effect: adopt the system improvement opportunity measure comprising stable state fuselage design and clutch and brake associated working pattern, support high frequency is processed, reduce operation complexity and energy resource consumption, eliminate safe hidden trouble, save artificial and labour intensity, improve die life and production efficiency, compact conformation, excellent performance, working stability, be particularly useful for machine parts'precise processing in enormous quantities.
Accompanying drawing explanation
Fig. 1 is the main TV structure schematic diagram of the utility model embodiment 1.
Fig. 2 is that the utility model embodiment 1 partial cutaway shows structural representation.
Fig. 3 is the right TV structure schematic diagram of the utility model embodiment 1.
Fig. 4 is the left TV structure schematic diagram of the utility model embodiment 1.
Reference numeral comprises: fuselage 1, slide block 2, combined type clutch-brake 3, workbench 4, motor 5, operating desk 6, electrical control cubicles 7, column 8, crankshaft arrangement 9, discharging device 10, electric cam sender mechanism 11, air accumulator 12, guide rail 13, balance cylinder 14; And, the added 3-1 of base tail margin 1-1, brake, brake undercarriage 3-2, work backing plate 4-1, bent axle front shroud 9-1, bent axle axle sleeve 9-2, crankshaft bearing 9-3, material returned fore-stock 10-1, material returned after-poppet 10-2, rail brackets 13-1.
Detailed description of the invention
The utility model comprises: fuselage 1, slide block 2, combined type clutch-brake 3, workbench 4, motor 5, operating desk 6, electrical control cubicles 7, column 8, crankshaft arrangement 9, discharging device 10, electric cam sender mechanism 11, air accumulator 12, guide rail 13 and balance cylinder 14.
Below in conjunction with drawings and Examples, the utility model is described in further detail.
Embodiment 1: as accompanying drawing 1, 2, shown in 3 and 4, air accumulator 12 is installed at fuselage 1 top, in the middle part of fuselage 1, both sides are erect respectively and are installed column 8, between two heel posts 8, slide block 2 is installed, erector's station 4 below slide block 2, bottom fuselage 1, motor 5 is installed in side, fuselage 1 liang of outside installs combined type clutch-brake 3 or crankshaft arrangement 9 respectively, combined type clutch-brake 3 and motor 5 are arranged on the same side, slide block 2 top is connected with crankshaft arrangement 9 by linkage, operating desk 6 is arranged on front side of workbench 4, simultaneously, fuselage 1 is connected with electrical control cubicles 7 respectively with operating desk 6, mounting guide rail 13 is erect respectively in slide block 2 both sides, guide rail 13 is fixed on column 8, guide rail 13 is installed discharging device 10, electric cam sender mechanism 11 is installed on the fuselage 1, electric cam sender mechanism 11 is connected with electrical control cubicles 7, balance cylinder 14 is installed between same heel post, the hydraulic system be connected with combined type clutch-brake 3 installs hydraulic pressure Overloading protection apparatus, the equipment lubrication system be connected with crankshaft arrangement 9 and slide block 2 installs adjustable dense oily self-lubricate oil pump.
In aforementioned, fuselage 1 adopts gantry type frame structure.Be fixed on basis by base tail margin 1-1 bottom fuselage 1.
In aforementioned, slide block 2 adopts octahedral to lead.
In aforementioned, combined type clutch-brake 3 is dry type or wet type Pneumatic friction clutch-brake.Combined type clutch-brake 3 is installed on the fuselage 1 by the added 3-1 of brake of top and the bottom outside fuselage 1 and brake undercarriage 3-2.
In aforementioned, workbench 4 bottom installment work backing plate 4-1, workbench is opened fixing hole and is arranged on above work backing plate 4-1.
In aforementioned, regulation and control photoelectric protector is installed on workbench 4 or between two heel posts 8.When working region because staff's limbs or abnormal foreign material enter, regulation and control photoelectric protector senses fast, reports to the police or shut down real-time guard.
In aforementioned, fuselage 1 top front side wall installs bent axle axle sleeve 9-2 and crankshaft bearing 9-3, bent axle is installed on the fuselage 1 by bent axle axle sleeve 9-2 and crankshaft bearing 9-3, and, fuselage 1 top installed in front bent axle front shroud 9-1, bent axle inner segment is arranged in bent axle front shroud 9-1, and the outer section of bent axle is closed and is arranged in crankshaft arrangement 9 part-structure of fuselage 1 upper outside.
In aforementioned, before and after guide rail 13, side installs material returned fore-stock 10-1 and the material returned after-poppet 10-2 of discharging device 10 respectively, and often group material returned fore-stock 10-1 and the equal symmetry of material returned after-poppet 10-2 are arranged on the sustained height of column 8.
In aforementioned, guide rail 13 is fixed on inside column 8 by rail brackets 13-1.
In the utility model, fuselage 1 integral solder, front and back are symmetrical, eliminate forcing press angular deformation phenomenon, improve stamping parts machining accuracy and die life.Combined type clutch-brake 3 adopts dry type or wet type Pneumatic friction clutch-brake, is active in one's movements reliable, and transmission system gear wheel mechanism precise finiss, it is low that equipment runs noise, operates steadily.Slide block 2 adopts six or octahedral guiding, and precision is high; Hydraulic system adopts hydraulic pressure Overloading protection apparatus, can available protecting forcing press and mould; Slide block 2 nominal pressure 800-4000kn, there is position 4-8mm in ability, slide block 2 stroke 120-280mm, number of strokes S.P.M 20-100, maximum shut height 400-730mm, closed height regulated quantity 80-125mm, left and right two heel post 8 spacing 960-1800mm, left and right two side rails 13 spacing 680mm, workbench 4 size, left and right 920-1600mm, front and back 600-1200mm, plate thickness 140-200mm; Slide block 2 baseplane size, left and right 650-1050mm, front and back 460-800mm; Fuselage 1 side mouth size, upper and lower 350-520mm, front and back 420-920mm; Shank hole diameter 70-80mm, degree of depth 90-120mm; Contour size of the unit(s) left and right 1890-2810mm, front and back 1650-3430mm, high 2900-4790mm; Motor 5 is consolidated/Variable power 7.5/11KW-37/45KW, weight 9500-40500kg.
During utility model works, three-phase alternating current is as power ON, actuating motor 5 equipment, by size V belt, combined type clutch-brake 3, a pair gear driven crankshaft arrangement 9, crankshaft arrangement 9 is pumped by linkage band movable slider 2.
The utility model is applicable to the kinds of processes such as punching, blanking, bending, flanging, shallow stretching, cold extrusion, hot die forming, is 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.
The utility model is based on the structural design optimized, and the certain advantages possessed also comprises:
1. fuselage 1 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;
2. combined type clutch-brake 3 substitutes positive clutch with friction drive, coordinates support high accuracy operation under high frequency with associated mechanisms;
3. in the middle part of fuselage 1, the in-built balance cylinder 14 of putting of the column 8 of both sides alleviates the impact of mode transfer operating physical force as air-cylinder type slide block gravity balancer;
4. equipment lubrication system adopts adjustable dense oily self-lubricate oil pump, plays self-lubricate effect, protects each lubrication face;
5. the regulation and control photoelectric protector of electrical control cubicles 7 connection, guarantees operator safety.
6. combined type clutch-brake 3 performs both clutch-brake and interlocks, first disengage brake before combining at clutch, first cut-off clutch before braking, user provides compressed air for oneself through the process of band table bigeminy part source of the gas, namely, enter the air accumulator 12 at machine top after pressure regulation, then carry out solenoidoperated cluthes in conjunction with separating action through electrical equipment instruction manipulation electromagnetism dual valve; When after dual valve power-off, in brake under Compress Spring effect, discharged by silencer through dual valve fast at balance cylinder 14 compressed air, realize braking action, slide block 2 stops at the position of needs immediately, user in normal conditions of use, if there is following situation to occur, timely shutdown: the reaction of combined type clutch-brake 3 clutch-brake is comparatively slow, or braking retardation; Abnormal noise is had to occur when clutch or braking; Or, have gas leakage sound in balance cylinder 14, when compressed air consumption is excessive.
Above-described embodiment is to explanation of the present utility model, is not to restriction of the present utility model, anyly all belongs to protection domain of the present utility model to the scheme after the utility model simple transformation.
Claims (7)
1. the energy-conservation closed type single point press of high accuracy, comprises fuselage, slide block, combined type clutch-brake, workbench, motor, operating desk, electrical control cubicles, column, crankshaft arrangement, discharging device, electric cam sender mechanism, air accumulator, guide rail and balance cylinder, it is characterized in that, fuselage roof installs air accumulator, waist both sides erect installation column respectively, between two heel posts, slide block is installed, erector's station below slide block, motor is installed in fuselage bottom side, outside fuselage two, combined type clutch-brake and crankshaft arrangement are installed respectively, combined type clutch-brake and motor are arranged on the same side, slide block top is connected with crankshaft arrangement by linkage, operating desk is arranged on front side of workbench, simultaneously, fuselage is connected with electrical control cubicles respectively with operating desk, mounting guide rail is erect respectively in slide block both sides, guide rail is fixed on column, discharging device installed by guide rail, fuselage is installed electric cam sender mechanism, electric cam sender mechanism is connected with electrical control cubicles, between same heel post, balance cylinder is installed, the hydraulic system be connected with combined type clutch-brake installs hydraulic pressure Overloading protection apparatus, the equipment lubrication system be connected with crankshaft arrangement and slide block installs adjustable dense oily self-lubricate oil pump.
2. the energy-conservation closed type single point press of high accuracy as claimed in claim 1, is characterized in that, fuselage adopts gantry type frame structure.
3. the energy-conservation closed type single point press of high accuracy as claimed in claim 1, is characterized in that, slide block adopts octahedral guiding.
4. the energy-conservation closed type single point press of high accuracy as claimed in claim 1, it is characterized in that, combined type clutch-brake is dry type pneumatic friction clutch-brake.
5. the energy-conservation closed type single point press of high accuracy as claimed in claim 1, is characterized in that, install photoelectric protector on workbench or between two heel posts.
6. the energy-conservation closed type single point press of high accuracy as claimed in claim 1, it is characterized in that, back front side wall is installed bent axle axle sleeve and crankshaft bearing, bent axle is arranged on fuselage by bent axle axle sleeve and crankshaft bearing, and, back installed in front bent axle front shroud, bent axle inner segment is arranged in bent axle front shroud, and the outer section of bent axle is closed in the crankshaft arrangement part-structure that is arranged on outside back.
7. the energy-conservation closed type single point press of high accuracy as claimed in claim 1, it is characterized in that, before and after guide rail, side installs material returned fore-stock and the material returned after-poppet of discharging device respectively, and often group material returned fore-stock and the equal symmetry of material returned after-poppet are arranged on the sustained height of column.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201420854456.XU CN204367471U (en) | 2014-12-25 | 2014-12-25 | The energy-conservation closed type single point press of high accuracy |
Applications Claiming Priority (1)
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CN201420854456.XU CN204367471U (en) | 2014-12-25 | 2014-12-25 | The energy-conservation closed type single point press of high accuracy |
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CN204367471U true CN204367471U (en) | 2015-06-03 |
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CN201420854456.XU Expired - Fee Related CN204367471U (en) | 2014-12-25 | 2014-12-25 | The energy-conservation closed type single point press of high accuracy |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105711132A (en) * | 2016-04-20 | 2016-06-29 | 台州市路桥振兴机械有限公司 | Closed type single point press |
CN105922622A (en) * | 2016-05-16 | 2016-09-07 | 广东宏兴机械有限公司 | Closed type single-point high-performance press |
CN108544792A (en) * | 2018-06-22 | 2018-09-18 | 浙江高精锻压股份有限公司 | A kind of half-closed forcing press |
CN109550824A (en) * | 2019-01-25 | 2019-04-02 | 安徽远都机床股份有限公司 | A kind of closed type single point press of the operation is stable |
CN109591359A (en) * | 2019-01-25 | 2019-04-09 | 安徽远都机床股份有限公司 | A kind of straight side double crank press |
CN109591358A (en) * | 2019-01-25 | 2019-04-09 | 安徽远都机床股份有限公司 | A kind of closed type single point press that punching precision is high |
CN110549668A (en) * | 2019-08-02 | 2019-12-10 | 江苏长沐智能装备有限公司 | Desktop-level high-speed high-precision miniature press machine for automatic production |
-
2014
- 2014-12-25 CN CN201420854456.XU patent/CN204367471U/en not_active Expired - Fee Related
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105711132A (en) * | 2016-04-20 | 2016-06-29 | 台州市路桥振兴机械有限公司 | Closed type single point press |
CN105711132B (en) * | 2016-04-20 | 2017-08-15 | 台州市路桥振兴机械有限公司 | A kind of closed type single point press |
CN105922622A (en) * | 2016-05-16 | 2016-09-07 | 广东宏兴机械有限公司 | Closed type single-point high-performance press |
CN108544792A (en) * | 2018-06-22 | 2018-09-18 | 浙江高精锻压股份有限公司 | A kind of half-closed forcing press |
CN109550824A (en) * | 2019-01-25 | 2019-04-02 | 安徽远都机床股份有限公司 | A kind of closed type single point press of the operation is stable |
CN109591359A (en) * | 2019-01-25 | 2019-04-09 | 安徽远都机床股份有限公司 | A kind of straight side double crank press |
CN109591358A (en) * | 2019-01-25 | 2019-04-09 | 安徽远都机床股份有限公司 | A kind of closed type single point press that punching precision is high |
CN109591358B (en) * | 2019-01-25 | 2021-03-16 | 安徽远都机床股份有限公司 | Closed single-point press that stamping accuracy is high |
CN110549668A (en) * | 2019-08-02 | 2019-12-10 | 江苏长沐智能装备有限公司 | Desktop-level high-speed high-precision miniature press machine for automatic production |
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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 | ||
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. |
|
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150603 Termination date: 20211225 |