CN1480279A - Precise forming powder in type of top tightened frame mount - Google Patents
Precise forming powder in type of top tightened frame mount Download PDFInfo
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- CN1480279A CN1480279A CNA031398049A CN03139804A CN1480279A CN 1480279 A CN1480279 A CN 1480279A CN A031398049 A CNA031398049 A CN A031398049A CN 03139804 A CN03139804 A CN 03139804A CN 1480279 A CN1480279 A CN 1480279A
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- oil cylinder
- cylinder
- frame
- nested
- powder press
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Abstract
An accurate powder compacting machine with prestressed frame is composed of enclosed frame-type main body, main cylinder assembly and bottom cylinder assembly. Said main cylinder assembly installed at upper part of main body consists of main cylinder, and nested cylinder fixed to the top of piston rod of main cylinder. Its advantages are less tensional deformation, high rigidity, and high machining accuracy. It is suitable for shaping the workpiece with complex shape and central hole.
Description
Technical field
The present invention relates to a kind of powder compaction equipment, particularly a kind of pretension frame-type precision form powder press.
Background technology
Powder metallurgy is to make metal dust and be raw material with metal dust (comprise and sneak into non-metal powder), the technology of usefulness shaping-sintering process manufactured materials and goods; Powder press is a powder pressing equipment, is used for metal dust (perhaps sneaking into non-metal powder) is pressed into required part product.Present domestic powder press, the three beam four-column type structures that adopt more, the rigidity of this structure is poor, being easy to generate tension in process of production makes equipment produce distortion, particularly equipment will produce bigger distortion when the compacting tonnage is big slightly, its machining accuracy can not be guaranteed, thereby can not satisfy the technological requirement of making high-precision part; The shortcoming that exists for the powder press that overcomes this structure, the powder press that adopts tower structure is also arranged in the prior art, but this powder press only is to convert with universal frame type hydraulic press simply, on framework, respectively establishing down an oil cylinder comes the mould of centre exerted pressure and makes wherein powder forming, the powder press of this repacking is not considered the compacting characteristics of powder part, its compacting pattern is identical with the pattern of common hydraulic press, can only be applicable to the individual layer mould preferably, be used for the better simply powder part of shaping form, and for many table tops powder part of shape more complicated, the as above part of two times three table tops, adopt the mould of individual layer to adorn powder according to the final shaping position of part, can not produce different filling amounts according to the difference of each several part structure and exert pressure according to actual pine dress beguine, the parts density of being suppressed is even inadequately, poor-performing can not satisfy requirements of actual production.
Summary of the invention
The object of the invention is to overcome the shortcoming of prior art, but provide a kind of rational in infrastructure, rigidity is big, stretcher strain is little, the pretension frame-type precision form powder press of many table tops part of the high shaping form complexity of machining accuracy.
Purpose of the present invention is achieved through the following technical solutions: this pretension frame-type precision form powder press comprises closed frame fuselage, master cylinder assembly, end cylinder component, master cylinder assembly is installed in the top of closed frame fuselage, the cylinder component relative bottom that is installed in the closed frame fuselage in the end with master cylinder assembly, it is characterized in that described master cylinder assembly comprises master cylinder, nested oil cylinder, nested oil cylinder is fixedly connected on the piston rod end of master cylinder.
Described master cylinder is fixedly installed on the closed frame fuselage, and described nested oil cylinder is fixedly installed on the slide block that is connected with the closed frame sliding machine body.
Described nested oil cylinder also can comprise the nested oil cylinder of next stage, and the nested oil cylinder of next stage is fixedly connected on the piston rod end of nested oil cylinder.
Cylinder component of the described end comprises end oil cylinder, the nested oil cylinder in bottom, and the nested oil cylinder in bottom is fixedly connected on the piston rod end of end oil cylinder; The nested oil cylinder in bottom is mainly used in the powder part of processing belt centre bore.
Described closed frame fuselage comprises entablature, column, base, and entablature is fixedly connected on the column upper end, and base is fixedly connected on column lower end.
Described closed frame fuselage also includes pull bar, and pull bar passes column, and the two ends attaching nut comes the whole closed frame fuselage of pretension.
Action principle of the present invention is: the master cylinder assembly on this pretension frame-type precision form powder press is provided with multistage compacting oil cylinder, can distinguish drive multilayer template, table top to the differing heights of powder part is suppressed respectively, thereby the present invention can only rely on equipment just to suppress the complex parts with two or more table tops and guarantee that the density of each several part is even, and is functional; Simultaneously, cooperate multilayer mould bases, just can suppress the complicated precision powder part that density goes up many table tops (as above two times three table tops) uniformly for different part otherwise designed; The nested oil cylinder in bottom of this powder press end cylinder setting is mainly used in the centre bore that drives the core bar formation of parts in the mould bases, forms the powder part of centre bore; The closed frame fuselage of this powder press adopts the general frame structure, use the pull bar pretension, its objective is by pull bar general frame imposed load in advance, make it in working order down, the fuselage uprights divides suffered tension corresponding reduction, the rigidity of fuselage is increased, and strain reduces, for the high-precision requirement of compacted part is given security.
The present invention has following advantage and effect with respect to prior art: but this pretension frame-type precision form powder press is rational in infrastructure, rigidity is big, stretcher strain is little, many table tops part of the high shaping form complexity of machining accuracy and the part that reaches the band centre bore, widely applicable; This pretension frame-type precision form powder press can be according to the processing request of the different piece of different parts and compacting respectively, and institute's processed powders part each several part density is even, and is functional.
Description of drawings
Fig. 1 is the structural representation of pretension frame-type precision form powder press of the present invention.
Fig. 2 is the side view of pretension frame-type precision form powder press shown in Figure 1.
The specific embodiment
The present invention is described in further detail below in conjunction with embodiment and accompanying drawing, but embodiments of the present invention are not limited thereto.
Embodiment
Fig. 1 shows a kind of version of the present invention, as seen from Figure 1, this pretension frame-type precision form powder press comprises closed frame fuselage, master cylinder assembly, end cylinder component, master cylinder assembly is installed in the top of closed frame fuselage, the relative bottom that is installed in the closed frame fuselage with master cylinder assembly of end cylinder component; Described closed frame fuselage comprises entablature 1, column 2, base 3, pull bar 4, entablature 1 is fixedly welded on column 2 upper ends, base 3 is fixedly welded on column 2 lower ends, entablature 1, column 2, base 3 threes connect and compose the closed frame structure, go back cross-under on the closed frame fuselage pull bar 4 is arranged, pull bar 4 passes column 2, two ends attaching nut 5, the nut 5 of tightening two ends can be to whole closed frame fuselage preload, make under its duty, the corresponding reduction of tension that column 2 parts are suffered can increase the rigidity of whole closed frame fuselage like this, reduces its strain.Described master cylinder assembly comprises master cylinder 6, nested oil cylinder 7, master cylinder 6 is fixedly connected on entablature 1, its piston rod 6-1 is connected with mould bases 9 by nested oil cylinder 7 and slide block 8, nested oil cylinder 7 is fixedly connected on the piston rod 6-1 end of master cylinder 6, the cylinder body of nested oil cylinder 7 is fixedlyed connected with slide block 8 simultaneously, described slide block 8 is slidingly connected with the guide rail 10 that is fixed on the column 2, and the piston rod 7-1 of nested oil cylinder 7 is connected with mould bases 9.Cylinder component of the described end comprises end oil cylinder 11, the nested oil cylinder 12 in bottom, and the nested oil cylinder 12 in bottom is fixedly connected on the piston rod 11-1 end of end oil cylinder 11; The piston rod 11-1 of end oil cylinder 11 directly is connected with mould bases 9, and the piston rod 12-1 of the nested oil cylinder 12 in bottom is connected with the centre bore of shaping powder part with core bar 13 in the mould bases 9.
As seen from Figure 2, this pretension frame-type precision form powder press also is provided with slide rail 14, mould bases 9 is connected on the slide rail 14, can move along slide rail 14, when processing different parts need be changed different mould bases 9, mould bases 9 is moved to position B by position A, again mould bases 9 is retracted position A by position B after the replacing.This pretension frame-type precision form powder press also is provided with feeding oil cylinder 15, is used for powder is sent into the die cavity of mould bases 9.
Claims (6)
1, a kind of pretension frame-type precision form powder press, comprise closed frame fuselage, master cylinder assembly, end cylinder component, master cylinder assembly is installed in the top of closed frame fuselage, the cylinder component relative bottom that is installed in the closed frame fuselage in the end with master cylinder assembly, it is characterized in that: described master cylinder assembly comprises master cylinder (6), nested oil cylinder (7), and nested oil cylinder (7) is fixedly connected on piston rod (6-1) end of master cylinder (6).
2, pretension frame-type precision form powder press according to claim 1, it is characterized in that: described master cylinder (6) is fixedly installed on the closed frame fuselage, and described nested oil cylinder (7) is fixedly installed on the slide block (8) that is connected with the closed frame sliding machine body.
3, pretension frame-type precision form powder press according to claim 1 and 2, it is characterized in that: described nested oil cylinder (7) comprises the nested oil cylinder of next stage, the nested oil cylinder of next stage is fixedly connected on the piston rod end of nested oil cylinder (7).
4, pretension frame-type precision form powder press according to claim 1, it is characterized in that: cylinder component of the described end comprises end oil cylinder (11), the nested oil cylinder in bottom (12), and the nested oil cylinder in bottom (12) is fixedly connected on piston rod (11-1) end of end oil cylinder (11).
5, pretension frame-type precision form powder press according to claim 1, it is characterized in that: described closed frame fuselage comprises entablature (1), column (2), base (3), entablature (1) is fixedly connected on column (2) upper end, and base (3) is fixedly connected on column (2) lower end.
6, pretension frame-type precision form powder press according to claim 1, it is characterized in that: described closed frame fuselage comprises pull bar (4), pull bar (4) passes column (2), two ends attaching nut (5).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 03139804 CN1218802C (en) | 2003-07-15 | 2003-07-15 | Precise forming powder in type of top tightened frame mount |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 03139804 CN1218802C (en) | 2003-07-15 | 2003-07-15 | Precise forming powder in type of top tightened frame mount |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1480279A true CN1480279A (en) | 2004-03-10 |
CN1218802C CN1218802C (en) | 2005-09-14 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN 03139804 Expired - Fee Related CN1218802C (en) | 2003-07-15 | 2003-07-15 | Precise forming powder in type of top tightened frame mount |
Country Status (1)
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CN (1) | CN1218802C (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104029413A (en) * | 2013-03-04 | 2014-09-10 | 李亚东 | Full-automatic pressing type powder forming machine |
CN106925780A (en) * | 2017-04-18 | 2017-07-07 | 扬州鼎隆机械有限公司 | A kind of multilayer mould bases and press integrated mechanism |
-
2003
- 2003-07-15 CN CN 03139804 patent/CN1218802C/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104029413A (en) * | 2013-03-04 | 2014-09-10 | 李亚东 | Full-automatic pressing type powder forming machine |
CN104029413B (en) * | 2013-03-04 | 2016-02-03 | 东莞市九九机械有限公司 | A kind of full-automatic pressing type powder former |
CN106925780A (en) * | 2017-04-18 | 2017-07-07 | 扬州鼎隆机械有限公司 | A kind of multilayer mould bases and press integrated mechanism |
CN106925780B (en) * | 2017-04-18 | 2020-06-09 | 扬州鼎隆机械有限公司 | Integrated mechanism of multilayer die carrier and press |
Also Published As
Publication number | Publication date |
---|---|
CN1218802C (en) | 2005-09-14 |
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