CN202922864U - High-rigidity injection molding machine body - Google Patents
High-rigidity injection molding machine body Download PDFInfo
- Publication number
- CN202922864U CN202922864U CN 201220630406 CN201220630406U CN202922864U CN 202922864 U CN202922864 U CN 202922864U CN 201220630406 CN201220630406 CN 201220630406 CN 201220630406 U CN201220630406 U CN 201220630406U CN 202922864 U CN202922864 U CN 202922864U
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- CN
- China
- Prior art keywords
- machine body
- molding machine
- injection molding
- straight beam
- rigidity
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- Injection Moulding Of Plastics Or The Like (AREA)
Abstract
The utility model provides a high-rigidity injection molding machine body. The high-rigidity injection molding machine body comprises a lower straight beam, an upper straight beam, a vertical post, a lower beam and an upper beam which are directly connected to form a frame structure; the vertical post for supporting is arranged between the part under the upper beam and the lower straight beam; and an injection part and a mould closing part are both arranged on the upper straight beam. According to the high-rigidity injection molding machine body, the structure of being integrally supported by the injection part and the mould closing part is adopted, thereby the problems of the conventional injection molding machine body can be overcome; and the straight beams and the beams are combined, so that the whole machine body is impact and is lighter than the general injection molding machine body.
Description
Technical field
The utility model relates to an important component part of injection moulding machine.
Background technology
In injection machine industry now, fuselage is an important component part of injection machine.Common electric injection machine fuselage adopts independent supporting construction because of injection portion and matched moulds part footing span diverse great majority, its structure as shown in Figure 1, if be used for the part that can come with some shortcomings on all-electric injection moulding machine: injection portion and matched moulds part support separately, and integral rigidity is slightly not enough.Some position of injection portion is not directly supported, and can affect the stability of complete machine under mal-condition.Fuselage is laid particular stress on, and manufacturing cost is higher.
The utility model content
Technical problem to be solved in the utility model is to provide a kind of high rigidity injection machine fuselage for the above-mentioned deficiency that overcomes prior art, makes its good rigidly, fuselage light.
The utility model solves the problems of the technologies described above the technical scheme that adopts: high rigidity injection machine fuselage, comprise bottom straight beam, top straight beam, column, lower beam, upper beam, directly connect into frame structure by bottom straight beam, top straight beam, column, lower beam, upper beam, under the straight beam of top and between the straight beam of bottom, upright supports is arranged, injection portion and matched moulds part all are arranged on the straight beam of top.
Compared with prior art, the utility model has the advantage of: the structure that adopts injection portion and matched moulds part integral type to support, overcome the problem that existing injection machine fuselage exists, and adopt straight beam and crossbeam mode to make up, make whole fuselage compacter, and it is lighter to compare the weight of common injection machine fuselage.
Description of drawings
Fig. 1 is the stereogram of existing injection machine fuselage.
Fig. 2 is the stereogram of the high rigidity injection machine of the utility model embodiment fuselage.
The specific embodiment
Embodiment is described in further detail the utility model below in conjunction with accompanying drawing.
As shown in Figure 2, high rigidity injection machine fuselage comprises bottom straight beam 1, top straight beam 2, column 3, lower beam 4, upper beam 5.
Fuselage directly supports to frame structure by bottom straight beam 1, top straight beam 2, column 3, lower beam 4, upper beam 5, there is column 3 to support under top straight beam 2, injection portion and matched moulds part (not shown in FIG.) all are arranged on same straight beam 2, strengthen processing by column 3, whole like this body facility have good rigidity and stability.
Claims (1)
1. high rigidity injection machine fuselage, it is characterized in that: comprise bottom straight beam, top straight beam, column, lower beam, upper beam, directly connect into frame structure by bottom straight beam, top straight beam, column, lower beam, upper beam, under the straight beam of top and between the straight beam of bottom, upright supports is arranged, injection portion and matched moulds part all are arranged on the straight beam of top.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220630406 CN202922864U (en) | 2012-11-26 | 2012-11-26 | High-rigidity injection molding machine body |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220630406 CN202922864U (en) | 2012-11-26 | 2012-11-26 | High-rigidity injection molding machine body |
Publications (1)
Publication Number | Publication Date |
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CN202922864U true CN202922864U (en) | 2013-05-08 |
Family
ID=48212858
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201220630406 Expired - Lifetime CN202922864U (en) | 2012-11-26 | 2012-11-26 | High-rigidity injection molding machine body |
Country Status (1)
Country | Link |
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CN (1) | CN202922864U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106003544A (en) * | 2015-03-31 | 2016-10-12 | 住友重机械工业株式会社 | Injection molding machine |
-
2012
- 2012-11-26 CN CN 201220630406 patent/CN202922864U/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106003544A (en) * | 2015-03-31 | 2016-10-12 | 住友重机械工业株式会社 | Injection molding machine |
CN106003544B (en) * | 2015-03-31 | 2019-04-09 | 住友重机械工业株式会社 | Injection (mo(u)lding) machine |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20130508 |