CN204308196U - A kind of pulverulent product forming machine airframe structure - Google Patents
A kind of pulverulent product forming machine airframe structure Download PDFInfo
- Publication number
- CN204308196U CN204308196U CN201420687717.3U CN201420687717U CN204308196U CN 204308196 U CN204308196 U CN 204308196U CN 201420687717 U CN201420687717 U CN 201420687717U CN 204308196 U CN204308196 U CN 204308196U
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- China
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- entablature
- guide pillar
- workbench
- locking nut
- forming machine
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Abstract
The utility model relates to a kind of pulverulent product forming machine airframe structure, comprise from upper and entablature that is that once arrange successively, slide block, workbench, the bottom of this workbench is by bearing support, described entablature is connected and fixed by the guide pillar of corner and workbench, corner and the guide pillar of top shoe are slidably matched, described top shoe drives it along the vertically movement of guide pillar axis direction by the master cylinder be arranged on entablature, the two ends up and down of described guide pillar are fixed on entablature upper surface and workbench lower surface respectively by locking nut, some bolts along its axial distribution are circumferentially distributed with at locking nut, the lower surface of this bolt is plane, and be just against on the upper surface of entablature or the lower surface of workbench.The utility model has the advantage of: main body mechanism of the present utility model is by the circumferentially bolt of locking nut, pretension is carried out to guide pillar, after ensureing Long-Time Service, locking nut does not loosen, and strengthens the fixed structure of locking nut to guide pillar, the balance of the fuselage of raising and stability.
Description
Technical field
The utility model relates to a kind of pulverulent product forming machine airframe structure pulverulent product forming machine, particularly a kind of pulverulent product forming machine airframe structure.
Background technology
Powder metallurgy be produce metal or with metal dust (or mixture of metal dust and non-metal powder) as raw material, again by sintering after having pressure or shaping without pressure, manufacture the technology of metal material, compound and all kinds goods.
Because PM technique has unique chemical composition and machinery, physical property, and these performances cannot obtain with traditional casting method.It has become the key solving new material problem, plays a part very important in the development of new material.
PM technique possess significantly energy-conservation, economize the high and series of advantages such as good stability of material, excellent performance, Product Precision, be very suitable for producing in enormous quantities.At present, PM technique has been widely used in the fields such as traffic, machinery, electronics, Aero-Space, weapons, biology, new forms of energy, information and nuclear industry, becomes one of branch of most development vitality in new material science.
The structure of pulverulent product forming machine for comprising master cylinder, entablature, top shoe, negative template, central cylinder, take blame for others, workbench and bearing, described entablature, top shoe, negative template, workbench and bearing set gradually from top to bottom, entablature is connected and fixed by the guide pillar of corner and workbench, corner and the guide pillar of top shoe and negative template are slidably matched, and the bottom of workbench is by bearing support.
The two ends of the guide pillar on current pulverulent product forming machine fuselage are all locked respectively on the upper surface of entablature and the lower surface of workbench by locking nut, and this kind of locking mechanism is weak, and after Long-Time Service, locking nut easily unclamps, and affects the work of equipment.
Summary of the invention
The technical problems to be solved in the utility model is to provide a kind of strengthens fuselage fixed structure, and the pulverulent product forming machine airframe structure of press power when can support compacted products.
For solving the problems of the technologies described above, the technical solution of the utility model is: a kind of pulverulent product forming machine airframe structure, comprise from upper and entablature that is that once arrange successively, slide block, workbench, the bottom of this workbench is by bearing support, described entablature is connected and fixed by the guide pillar of corner and workbench, corner and the guide pillar of top shoe are slidably matched, described top shoe drives it along the vertically movement of guide pillar axis direction by the master cylinder be arranged on entablature, its innovative point is: the two ends up and down of described guide pillar are fixed on entablature upper surface and workbench lower surface respectively by locking nut, some bolts along its axial distribution are circumferentially distributed with at locking nut, the lower surface of this bolt is plane, and be just against on the upper surface of entablature or the lower surface of workbench.
Further, described some bolts are evenly distributed on the periphery of locking nut ringwise.
Further, the two ends up and down of described guide pillar have a circular interior step, between the lower surface of described locking nut step in this circle and the upper surface of entablature, described locking nut bolt circumferentially extends to the upper surface of entablature by the upper surface of circular interior step.
The utility model has the advantage of: pulverulent product forming machine body structure of the present utility model, by circumferentially arranging some bolts along its axial distribution at locking nut, pretension is carried out to guide pillar, after ensureing Long-Time Service, locking nut does not loosen, strengthen the fixed structure of locking nut to guide pillar, utilize again the lower surface of bolt to support press power during compacted products simultaneously, strengthen the structure of fuselage, the balance of the fuselage of raising and stability; In addition at the two ends up and down of guide pillar, there is step in a circle, ensure that the precision of fuselage.
Accompanying drawing explanation
Fig. 1 is the front view of a kind of pulverulent product forming machine of the utility model airframe structure.
Fig. 2 is the top view of a kind of pulverulent product forming machine of the utility model airframe structure.
Detailed description of the invention
As depicted in figs. 1 and 2, the utility model discloses a kind of pulverulent product forming machine airframe structure, comprise from upper and entablature 1 that is that once arrange successively, slide block 2, workbench 3, the bottom of this workbench 3 is supported by bearing 4, entablature 1 is connected and fixed with workbench 3 by the guide pillar 5 of corner, corner and the guide pillar 5 of top shoe 2 are slidably matched, top shoe 2 drives it along the vertically movement of guide pillar 5 axis direction by the master cylinder 6 be arranged on entablature 1, the two ends up and down of its guide pillar 5 are fixed on entablature 1 upper surface and workbench 3 lower surface respectively by locking nut 7, some bolts 8 along its axial distribution are circumferentially distributed with at locking nut 7, the lower surface of this bolt 8 is plane, and be just against on the upper surface of entablature 1 or the lower surface of workbench 3.
In the present embodiment, in order to ensure the stability of guide pillar 5 fixed structure, some bolts 8 are evenly distributed on the periphery of locking nut 7 ringwise; Simultaneously in order to ensure the precision of fuselage, the two ends up and down of guide pillar 5 have a circular interior step 9, between the lower surface of locking nut 7 step 9 in this circle and the upper surface of entablature 1, locking nut 7 bolt 8 circumferentially extends to the upper surface of entablature 1 by the upper surface of circular interior step 9.
Operation principle, guide pillar 5 is by circumferentially arranging some bolts 8 along its axial distribution at locking nut 7, strengthen the fixed structure of locking nut 7 pairs of guide pillars 5, utilize again the lower surface of bolt 8 to support press power during compacted products simultaneously, strengthen the structure of fuselage, the balance of the fuselage of raising and stability.
More than show and describe general principle of the present utility model and principal character and advantage of the present utility model.The technical staff of the industry should understand; the utility model is not restricted to the described embodiments; what describe in above-described embodiment and description just illustrates principle of the present utility model; under the prerequisite not departing from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and equivalent thereof.
Claims (3)
1. a pulverulent product forming machine airframe structure, comprise from upper and entablature that is that once arrange successively, slide block, workbench, the bottom of this workbench is by bearing support, described entablature is connected and fixed by the guide pillar of corner and workbench, corner and the guide pillar of top shoe are slidably matched, described top shoe drives it along the vertically movement of guide pillar axis direction by the master cylinder be arranged on entablature, it is characterized in that: the two ends up and down of described guide pillar are fixed on entablature upper surface and workbench lower surface respectively by locking nut, some bolts along its axial distribution are circumferentially distributed with at locking nut, the lower surface of this bolt is plane, and be just against on the upper surface of entablature or the lower surface of workbench.
2. pulverulent product forming machine airframe structure according to claim 1, is characterized in that: described some bolts are evenly distributed on the periphery of locking nut ringwise.
3. pulverulent product forming machine airframe structure according to claim 1, it is characterized in that: the two ends up and down of described guide pillar have a circular interior step, between the lower surface of described locking nut step in this circle and the upper surface of entablature, described locking nut bolt circumferentially extends to the upper surface of entablature by the upper surface of circular interior step.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420687717.3U CN204308196U (en) | 2014-11-18 | 2014-11-18 | A kind of pulverulent product forming machine airframe structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420687717.3U CN204308196U (en) | 2014-11-18 | 2014-11-18 | A kind of pulverulent product forming machine airframe structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204308196U true CN204308196U (en) | 2015-05-06 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420687717.3U Expired - Fee Related CN204308196U (en) | 2014-11-18 | 2014-11-18 | A kind of pulverulent product forming machine airframe structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204308196U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108436078A (en) * | 2017-12-29 | 2018-08-24 | 南通国谊锻压机床有限公司 | A kind of multiple layer powder product device for automatically molding |
-
2014
- 2014-11-18 CN CN201420687717.3U patent/CN204308196U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108436078A (en) * | 2017-12-29 | 2018-08-24 | 南通国谊锻压机床有限公司 | A kind of multiple layer powder product device for automatically molding |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150506 Termination date: 20161118 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |