CN209566440U - A kind of injection molding machine fuselage of the outer trunking of band - Google Patents
A kind of injection molding machine fuselage of the outer trunking of band Download PDFInfo
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- CN209566440U CN209566440U CN201822271804.1U CN201822271804U CN209566440U CN 209566440 U CN209566440 U CN 209566440U CN 201822271804 U CN201822271804 U CN 201822271804U CN 209566440 U CN209566440 U CN 209566440U
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- wire casing
- longeron
- injection molding
- molding machine
- line slot
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Abstract
The utility model provides a kind of injection molding machine fuselage of outer trunking of band, belongs to injection molding machine body techniques field.This injection molding machine fuselage with outer trunking includes symmetrically arranged a pair of of longeron and the distribution box structure that is arranged in below longeron, not operation side line slot structure is detachably installed on the outside of a longeron wherein, fore side wire casing structure is detachably installed on the outside of another longeron, not operation side line slot structure, fore side wire casing structure is respectively positioned on distribution box structure oblique upper position, the distribution box structure and not operation side line slot structure/fore side wire casing structure are dislocatedly distributed in the vertical direction, the not operation side line slot structure, fore side wire casing structure is respectively equipped with the wire casing of open-top.This injection molding machine fuselage with outer trunking is improved with structural strength, is not easy to damage cable epidermis, cabling more easily advantage.
Description
Technical field
The utility model belongs to injection molding machine body techniques field, is related to a kind of injection molding machine fuselage of outer trunking of band.
Background technique
For injection molding machine fuselage using square steel tube as crossbeam, to guarantee appearance looks elegant, clean and tidy, cable is generally all disposed within
Inside square steel tube crossbeam.Big beam sides has several outlet holes, and there is the handle hole of corresponding outlet hole in crossbeam bottom convenient for stretching out one's hand operation.
Injection molding machine fuselage currently on the market has the following problems:
1, outlet hole and stretch hand hole will affect the intensity of longeron；
2, square steel tube crossbeam internal burr and rough surface can damage the epidermis of cable when pull cable；
3, for the cable of belt lacing because connector is greater than line footpath, square steel tube inside cabling amount is limited.
In conclusion the utility model designs a kind of structural strength raising, it is not easy to damage cable epidermis, cabling is more
Easily with the injection molding machine fuselage of outer trunking.
Summary of the invention
The purpose of this utility model is the presence of the above problem in view of the prior art, proposes a kind of structural strength raising,
It is not easy to damage cable epidermis, cabling is more easily with the injection molding machine fuselage of outer trunking.
The purpose of this utility model can be realized by the following technical scheme: a kind of injection molding machine fuselage of the outer trunking of band,
Including symmetrically arranged a pair of of longeron and the distribution box structure being arranged in below longeron, a longeron wherein
Outside is detachably equipped with not operation side line slot structure, and fore side wire casing knot is detachably equipped on the outside of another longeron
Structure, not operation side line slot structure, fore side wire casing structure are respectively positioned on distribution box structure oblique upper position, the distribution box structure and
Not operation side line slot structure/fore side wire casing structure is dislocatedly distributed in the vertical direction, the not operation side line slot structure, operation
Side line slot structure is respectively equipped with the wire casing of open-top.
The not operation side line slot structure, fore side wire casing structure lead to respectively as a further improvement of the utility model,
Carrying bolt is crossed to be detachably connected with corresponding longeron.
The longeron is set as square steel tube structure as a further improvement of the utility model,.
Based on the above-mentioned technical proposal, the utility model embodiment at least can produce following technical effect: this is with external line
The injection molding machine fuselage compact overall structure of slot, rationally, cable from distribution box come out after on the outside of longeron cabling, outside package
Detachable wire casing, wire casing open-top are used for outlet, the part and longeron of wire casing carrying bolt or similar structures
Connection, such structure setting, so that longeron number of aperture is greatly decreased, intensity is improved；It is different from existing inside crossbeam
Cabling, there is no burrs and rough surface to damage to cable epidermis for this external fuselage；Open cabling is more convenient cloth
Set the cable for carrying larger connector.
Detailed description of the invention
Specific embodiment of the present utility model is described in further detail with reference to the accompanying drawing, in which:
Fig. 1 is the structural schematic diagram of one preferred embodiment of the utility model.
Fig. 2 is the structural schematic diagram at another visual angle of one preferred embodiment of the utility model.
In figure, 1, distribution box structure；2, not operation side line slot structure；3, carrying bolt；4, fore side wire casing structure；5, machine
Body crossbeam.
Specific embodiment
It is specific embodiment of the utility model and in conjunction with attached drawing below, the technical solution of the utility model is made further
Description, but the utility model is not limited to these examples.
Below with reference to Fig. 1 to Fig. 2, technical scheme provided by the present invention will be described in more detail.
As shown in Figure 1 to Figure 2, this injection molding machine fuselage with outer trunking includes 5 He of symmetrically arranged a pair of of longeron
Distribution box structure 1 below longeron 5 is set, and 5 outside of longeron is detachably equipped with not operation side wherein
Wire casing structure 2 is detachably equipped with fore side wire casing structure 4 in 5 outside of another longeron, not operation side line slot structure 2,
Fore side wire casing structure 4 is respectively positioned on 1 oblique upper position of distribution box structure, the distribution box structure 1 and not operation side line slot structure
2/ fore side wire casing structure 4 is dislocatedly distributed in the vertical direction, and the not operation side line slot structure 2, fore side wire casing structure 4 divide
Not She You open-top wire casing.
In the present case, preferably longeron 5 is set as square steel tube structure；It is preferred that not operation side line slot structure 2, operation side line
Slot structure 4 is detachably connected by carrying bolt 3 with corresponding longeron 5 respectively.
Preferably, not operation side line slot structure 2, fore side wire casing structure 4 are symmetrical arranged or are oppositely arranged, and layout is more stepped up
It gathers, rationally, and cabling is convenient, reduces interfering between component.
The utility model protects a kind of injection molding machine fuselage of the outer trunking of band, compact overall structure, rationally, and cable is from distribution
Case come out after along 5 outside cabling of longeron, detachable wire casing is wrapped up in outside, and wire casing open-top is used for outlet, wire casing
It is connected with the part and longeron 5 of carrying bolt 3 or similar structures, such structure setting, so that 5 number of aperture of longeron
It is greatly decreased, intensity improves；Be different from the existing cabling inside the crossbeam, this case external fuselage there is no burrs and rough surface will not
Cable epidermis is damaged；The more convenient arrangement of open cabling carries the cable of larger connector.
The specific embodiments described herein are merely examples of the spirit of the present invention.The utility model institute
Belonging to those skilled in the art can make various modifications or additions to the described embodiments or using similar
Mode substitute, but without departing from the spirit of the present application or beyond the scope of the appended claims.
Claims (3)
1. a kind of injection molding machine fuselage of the outer trunking of band, it is characterised in that: including symmetrically arranged a pair of of longeron and setting
Distribution box structure below longeron is detachably equipped with not operation side line slot knot on the outside of a longeron wherein
Structure is detachably equipped with fore side wire casing structure, not operation side line slot structure, fore side wire casing on the outside of another longeron
Structure is respectively positioned on distribution box structure oblique upper position, the distribution box structure and not operation side line slot structure/fore side wire casing knot
Structure is dislocatedly distributed in the vertical direction, and the not operation side line slot structure, fore side wire casing structure are respectively equipped with open-top
Wire casing.
2. a kind of injection molding machine fuselage of the outer trunking of band according to claim 1, it is characterised in that: the not operation side line
Slot structure, fore side wire casing structure pass through carrying bolt respectively and are detachably connected with corresponding longeron.
3. a kind of injection molding machine fuselage of the outer trunking of band according to claim 1 or 2, it is characterised in that: the fuselage is big
Beam is set as square steel tube structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822271804.1U CN209566440U (en) | 2018-12-30 | 2018-12-30 | A kind of injection molding machine fuselage of the outer trunking of band |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822271804.1U CN209566440U (en) | 2018-12-30 | 2018-12-30 | A kind of injection molding machine fuselage of the outer trunking of band |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209566440U true CN209566440U (en) | 2019-11-01 |
Family
ID=68331615
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822271804.1U Active CN209566440U (en) | 2018-12-30 | 2018-12-30 | A kind of injection molding machine fuselage of the outer trunking of band |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209566440U (en) |
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2018
- 2018-12-30 CN CN201822271804.1U patent/CN209566440U/en active Active
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