CN204555210U - Clarifier and Wiring structure thereof - Google Patents
Clarifier and Wiring structure thereof Download PDFInfo
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- CN204555210U CN204555210U CN201420872614.4U CN201420872614U CN204555210U CN 204555210 U CN204555210 U CN 204555210U CN 201420872614 U CN201420872614 U CN 201420872614U CN 204555210 U CN204555210 U CN 204555210U
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- trough
- clarifier
- line piece
- wiring structure
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Abstract
The utility model belongs to purification technology field, aims to provide a kind of clarifier and Wiring structure thereof, and this Wiring structure comprises machine body base and is located at the fuselage main body in described machine body base.The utility model, when power line is at clarifier inner chamber cabling, directly Power cord fastener can be located in fuselage main body and the first trough structure is set, second trough structure, and the 3rd in trough structure, wherein, for different clarifier types, the particular location of these three kinds of trough structures and layout can do accommodation, simultaneously at line outlet place, directly the limited block on power line can be fastened on card wire structure that machine body base is arranged, like this, Power cord fastener is located on trough assembly and card wire structure by direction of routing along power line successively, be convenient to cabling, decrease parts required in assembling process, thus simplify the assembly technology of clarifier, moreover also reduce the scrappage of power line, improve the security of clarifier.
Description
Technical field
The utility model belongs to purification technology field, relates to a kind of Wiring structure, particularly relates to a kind of Wiring structure of clarifier and has the clarifier of this Wiring structure.
Background technology
Clarifier is also known as cleaner or cleaner, and the clarifier of indication refers in particular to air purifier usually here, common air purifier can adsorb, decomposes or transform various as air pollutants such as PM2.5, dust, peculiar smell, formaldehyde, along with the development of modern industrial society, air pollution is more and more serious, for giving the air ambient of indoor live and work Creating Comfort cleaning of people, air purifier at home, the field such as medical, industrial obtains and applies more and more widely.
Usually, air purifier is primarily of motor or motor, fan, airstrainer, and the parts such as control unit composition, wherein, existing air purifier mainly completes conducting in air purifier between each parts by power line external civil power, for example, fan just makes the air of surrounding environment be circulated under the drive of motor or motor, control unit could control air purifier miscellaneous part after needing to be communicated with power supply works in an orderly manner, therefore, power line is the indispensable element of existing air purifier, but, because of the characteristic of power line self, when the inner chamber cabling of air purifier easily and around the miscellaneous part generation friction damage such as fan and there is bad phenomenon such as leaking electricity.In prior art, for guaranteeing security, usually multiple pressing plate is used to control the wiring path of power line, and on each pressing plate, play screw so that power line is fixed on appointment in position, following problem can be brought like this: 1) be not only not easy to assembling, and also need to configure corresponding pressing plate and screw in addition, increase the parts of assembling; 2) easily power line is punched in the process of playing screw, there is potential safety hazard.
Utility model content
The purpose of this utility model is to provide a kind of clarifier and Wiring structure thereof, adopts screw fit pressing plate to fix power line in clarifier and the inconvenience assembling that causes and the low technical problem of security in order to solve.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: the Wiring structure providing a kind of clarifier, comprises fuselage main body and machine body base, and described fuselage main body is located in described machine body base; Described fuselage main body is provided with trough assembly, and described machine body base is provided with card wire structure, and line piece is fastened on described trough assembly and described card wire structure successively along its direction of routing.
Further, described trough assembly comprises the first trough structure, described first trough structure comprises at least two limited posts be convexly equipped in described fuselage main body, each described limited post gap arrangement, and described line piece is arranged in the cable tray that two adjacent described limited posts are formed.
Further, each described limited post arranges in turn along the direction of routing of described line piece and is mutually staggeredly arranged.
Further, described first trough structure comprises three described limited posts.
Further, described first trough structure has multiple, and each described first trough structure arranges in turn along the direction of routing of described line piece.
Further, described trough assembly also comprises the second trough structure, described second trough structure comprises the first fastener and gap in the second fastener of described first fastener, and described line piece is arranged in the cable tray that described first fastener and described second fastener formed.
Further, described second trough structure has multiple, and each described second trough structure arranges in turn along the direction of routing of described line piece.
Further, described trough assembly also comprises at least one the 3rd trough structure, and each described 3rd trough structure comprises the gripper shoe being convexly equipped in described fuselage main body, and described gripper shoe offers trough, and described line piece is arranged in described trough.
Further, described card wire structure comprises clamp and is opened in the spacing draw-in groove of described machine body base, described clamp is gone out by a cell wall projection of described spacing draw-in groove, and be positioned at the notch place of described spacing draw-in groove, another cell wall of described spacing draw-in groove offers wire hole, and described line piece to be arranged in described wire hole and by described wire hole outlet.
Compared with prior art, the beneficial effect of the Wiring structure of clarifier that the utility model provides is:
(1) when fuselage body interior cabling, directly line piece (as power line) is fastened on the trough assembly of fuselage main body self setting, at line outlet place, directly line piece (as power line) is fastened on the card wire structure of machine body base setting, like this, very be convenient to cabling, also simplify assembly technology, decrease parts required in the process of fixing line piece, moreover, also ensure the scrappage of line piece (as power line) in installation or use procedure, improve security.
(2) by arranging the first trough structure, the second trough structure, the 3rd trough structure in fuselage main body, wherein, for different types, the particular location layout of these three kinds of trough structures can do adaptability variation, correspondingly, Wiring structure with a type also has adaptability variation, like this, ensure that the wiring path with its inner line piece (as power line) of a type is consistent, ensure that the standardization of wiring path, so that the dismounting in later stage and maintenance.
The utility model additionally provides a kind of clarifier, and this clarifier comprises above-mentioned Wiring structure.
Compared with prior art, the beneficial effect of the clarifier that the utility model provides is: when fuselage body interior cabling, directly line piece (as power line) is fastened on the trough assembly of fuselage main body self setting, at line outlet place, directly line piece (as power line) is fastened on the card wire structure of machine body base setting, like this, very be convenient to cabling, also simplify the assembly technology of whole clarifier, and be also convenient to the standardization of the wiring path of the line piece (as power line) with a its inside of clarifier, decrease parts required in assembling process, be convenient to dismounting and the maintenance in later stage, moreover, also ensure the scrappage of line piece (as power line) in installation or use procedure, improve the security of clarifier.
Accompanying drawing explanation
Fig. 1 is the perspective view of the Wiring structure of clarifier in the utility model embodiment.
Label in accompanying drawing is as follows:
1 fuselage main body, 10 trough assemblies, 11 first trough structures, 111 limited posts, 12 second trough structures, 121 first fasteners, 122 second fasteners, 13 the 3rd trough structures, 131 gripper shoes, 1311 troughs;
2 machine body base, 20 card wire structures, 21 clamps, 22 spacing draw-in grooves, 221 wire holes.
Detailed description of the invention
In order to make technical problem to be solved of the present utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Below in conjunction with concrete accompanying drawing, realization of the present utility model is described in detail.
It should be noted that, when parts are called as " being fixed on " or " being arranged at " another parts, it can directly on another parts or may there are parts placed in the middle simultaneously.When parts are known as " being connected to " another parts, it can be directly connected to another parts or may there are parts placed in the middle simultaneously.
Also it should be noted that, the corresponding same or analogous parts of same or analogous label in the accompanying drawing of the utility model embodiment, in description of the present utility model, it will be appreciated that, if have term " on ", D score, " left side ", orientation or the position relationship of the instruction such as " right side " are based on orientation shown in the drawings or position relationship, only the utility model and simplified characterization for convenience of description, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore, the term of position relationship is described only for exemplary illustration in accompanying drawing, the restriction to this patent can not be interpreted as, for the ordinary skill in the art, the concrete meaning of above-mentioned term can be understood as the case may be.
As shown in Figure 1, a kind of clarifier provided for the utility model one preferred embodiment and Wiring structure thereof.
The Wiring structure of clarifier, mainly in order to wiring path and the fixed power source line of power line in layout clarifier, certainly, this Wiring structure is also applicable to the layout of the wiring path of line piece (not shown) in other electric equipments and the fixed installation of line piece (not shown), wherein, the line piece of indication is often referred to the power line with plug fastener here.Following the utility model embodiment mainly relies on the specific design scheme introducing Wiring structure with clarifier.
As shown in Figure 1, this Wiring structure comprises fuselage main body 1 and machine body base 2, and wherein, fuselage main body 1 is located in machine body base 2, and specifically in the present embodiment, bottom and the machine body base 2 of fuselage main body 1 connect as one.
As shown in Figure 1, for ease of line piece cabling, prevent line piece from having influence on other parts of surrounding when cabling, make, between line piece and other parts, unnecessary friction occurs and the bad phenomenon such as damaged occur, fuselage main body 1 is provided with trough 1311 assembly 10, it should be noted that, this trough 1311 assembly 10 is made up of a series of trough 1311 structure, can according to the thickness of the line piece of reality, suppleness, the characteristics such as length, and for the concrete layout of internal structure in distinct device or type, the characteristics such as the suppleness of each parts in each trough 1311 structure in trough 1311 assembly 10 can be adjusted adaptively, also adaptability ground adjusts particular location and the layout of each trough 1311 structure, in a word, in trough 1311 assembly 10, the particular location of each trough 1311 structure and layout can be determined according to actual conditions.
As shown in Figure 1, for ease of determining that the outlet position machine body base 2 of line piece is provided with card wire structure 20, it should be noted that, fixing, usually, in one end of the close plug of line piece for ease of line piece self, line piece is provided with plug fastener, like this, this plug fastener is fastened on card wire structure 20, can firm line piece well.
Obviously, line piece is fastened on trough 1311 assembly 10 and card wire structure 20 along the direction of routing of himself successively, also be, line piece is that each trough 1311 structure by being fastened on trough 1311 assembly 10 completes the cabling of line piece and fixing, and is that plug fastener by line piece being carried is fastened on cabling when card wire structure 20 completing its outlet and fixing in outlet.
Further, as shown in Figure 1, for ease of line piece being fixed on the position of specifying, trough 1311 assembly 10 comprises the first trough 1311 structure 11, wherein, this the first trough 1311 structure 11 comprises at least two limited posts 111 be convexly equipped in fuselage main body 1, each limited post 111 gap arrangement, and line piece is arranged in the cable tray that two adjacent limited posts 111 are formed.Understandably, the spacing size between two adjacent limited posts 111 is just adaptive with line piece.
Further, as shown in Figure 1, for ease of guaranteeing that line piece is walking the steadiness in line process, each limited post 111 arranges in turn along the direction of routing of line piece, can guarantee that line piece can extend cabling along its direction of routing with this, moreover, each limited post 111 is mutually staggeredly arranged, to strengthen steadiness during line piece cabling, therefore, understandably, line piece is in the first trough 1311 structure 11 during cabling, and its wiring path is curve.
Further, as shown in Figure 1, in the preferred embodiment that the utility model provides, on the basis of steadiness of guaranteeing line piece cabling, material can also be saved, simplify the structure of whole trough 1311 assembly 10, this the first trough 1311 structure 11 comprises three limited posts 111, wherein, three limited posts 111 arrange into a line in such sequence row, and have a gap to allow line piece cabling between two adjacent limited posts 111, moreover, these three limited posts 111 not on the same line, but interlaced arrangement.Certainly, in actual production process, the limited post 111 of other quantity can be selected according to the actual needs to strengthen steadiness.
Further, as shown in Figure 1, in the preferred embodiment that the utility model provides, for ease of strengthen further line piece whole walk steadiness in line process, the first above-mentioned trough 1311 structure 11 has multiple, and each first trough 1311 structure 11 arranges in turn along the direction of routing of line piece, like this, in actual production process, the location layout situation of each first trough 1311 structure 11 can be determined according to the layout scenarios of this Wiring structure peripheral parts, thus, can the wiring path of layout line piece well.
Further, as shown in Figure 1, for ease of optimizing the wiring path of line piece better, trough 1311 assembly 10 also comprises the second trough 1311 structure 12, second trough 1311 structure 12 comprises the first fastener 121 and gap in the second fastener 122 of the first fastener 121, in the preferred embodiment that the utility model provides, preferably, first fastener 121 can be limited post 111 can be also limiting plate, and the second fastener 122 is fixed in a support member (not shown) of fuselage main body 1.Wherein, line piece is arranged in the cable tray of this first fastener 121 and the formation of this second fastener 122, and understandably, the gap length between the first fastener 121 and the second fastener 122 is just adaptive with cabling line piece.It should be noted that, this second trough 1311 structure 12 also can help the direction of ajusting line piece while firm line piece, makes line piece vertically cabling.
Further, for ease of the wiring path of layout line piece better, as shown in Figure 1, the second trough 1311 structure 12 has multiple, and each second trough 1311 structure 12 arranges in turn along the direction of routing of line piece.In the preferred embodiment that the utility model provides, preferably, first trough 1311 structure 11 and the alternate layout of the second trough 1311 structure 12, also be, after first trough 1311 structure 11 is set, immediately following arranging second trough 1311 structure 12, more afterwards immediately following arranging first trough 1311 structure 11.
Further, in the preferred embodiment that the utility model provides, as shown in Figure 1, for ease of cabling, trough 1311 assembly 10 also comprises at least one the 3rd trough 1311 structure 13, each 3rd trough 1311 structure 13 comprises the gripper shoe 131 being convexly equipped in fuselage main body 1, and gripper shoe 131 offers trough 1311, line piece is arranged in trough 1311.Preferably, usually, the 3rd trough 1311 structure 13 is arranged on the position of the close machine body base 2 of fuselage main body 1.
Specifically be, in the preferred embodiment that the utility model provides, location layout between first trough 1311 structure 11, second trough 1311 structure 12 and the 3rd trough 1311 structure 13 can answer the layout of other parts around in fuselage main body 1 and adaptability changes, usually, layout designs with the Wiring structure of a type can be consistent, the standardization of its wiring path of line piece on same type is guaranteed, so that the dismounting in later stage and maintenance with this.
Further, as shown in Figure 1, for ease of line piece outlet and guarantee the steadiness of outlet position line piece, in the preferred embodiment that the utility model provides, above-mentioned card wire structure 20 comprises clamp 21 and is opened in the spacing draw-in groove 22 of machine body base 2, wherein, clamp 21 by spacing draw-in groove 22 vallecular cavity projection from a cell wall to this spacing draw-in groove 22 and go out, and this clamp 21 is positioned at the notch place of spacing draw-in groove 22, with this, when the plug fastener (not shown) that line piece (not shown) carries is installed with in spacing draw-in groove 22, can gear prevent above this plug fastener plug fastener easily in spacing draw-in groove 22 out.It should be noted that, these plug fastener two ends are all connected to line piece, it is mainly fixed for ease of the installation of line piece and arranges, thus, for ease of the outlet of the line piece of leading-out terminal on plug fastener, as shown in Figure 1, another cell wall of spacing draw-in groove 22 offers wire hole 221, and line piece to be arranged in wire hole 221 and by this wire hole 221 outlet.
The utility model embodiment also provides a kind of clarifier (not shown), this clarifier comprises above-mentioned Wiring structure, like this, be convenient to very much the cabling of line piece in clarifier (as power line), also simplify the assembly technology of whole clarifier, and be also convenient to the standardization of the wiring path of the line piece (as power line) with a its inside of clarifier, decrease parts required in assembling process, be convenient to dismounting and the maintenance in later stage, moreover, also ensure the scrappage of line piece (as power line) in installation or use procedure, improve the security of clarifier.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model.For a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within right of the present utility model.
Claims (10)
1. the Wiring structure of clarifier, comprise fuselage main body and machine body base, described fuselage main body is located in described machine body base, it is characterized in that: described fuselage main body is provided with trough assembly, described machine body base is provided with card wire structure, and line piece is fastened on described trough assembly and described card wire structure successively along its direction of routing.
2. the Wiring structure of clarifier as claimed in claim 1, it is characterized in that: described trough assembly comprises the first trough structure, described first trough structure comprises at least two limited posts be convexly equipped in described fuselage main body, each described limited post gap arrangement, described line piece is arranged in the cable tray that two adjacent described limited posts are formed.
3. the Wiring structure of clarifier as claimed in claim 2, is characterized in that: each described limited post arranges in turn along the direction of routing of described line piece and is mutually staggeredly arranged.
4. the Wiring structure of clarifier as claimed in claim 3, is characterized in that: described first trough structure comprises three described limited posts.
5. the Wiring structure of clarifier as claimed in claim 4, it is characterized in that: described first trough structure has multiple, each described first trough structure arranges in turn along the direction of routing of described line piece.
6. the Wiring structure of clarifier as claimed in claim 5, it is characterized in that: described trough assembly also comprises the second trough structure, described second trough structure comprises the first fastener and gap in the second fastener of described first fastener, and described line piece is arranged in the cable tray that described first fastener and described second fastener formed.
7. the Wiring structure of clarifier as claimed in claim 6, it is characterized in that: described second trough structure has multiple, each described second trough structure arranges in turn along the direction of routing of described line piece.
8. the Wiring structure of clarifier as claimed in claim 5, it is characterized in that: described trough assembly also comprises at least one the 3rd trough structure, each described 3rd trough structure comprises the gripper shoe being convexly equipped in described fuselage main body, described gripper shoe offers trough, and described line piece is arranged in described trough.
9. the Wiring structure of the clarifier as described in any one of claim 1 to 8, it is characterized in that: described card wire structure comprises clamp and is opened in the spacing draw-in groove of described machine body base, described clamp is gone out by a cell wall projection of described spacing draw-in groove, and be positioned at the notch place of described spacing draw-in groove, another cell wall of described spacing draw-in groove offers wire hole, and described line piece to be arranged in described wire hole and by described wire hole outlet.
10. clarifier, is characterized in that: comprise the Wiring structure as described in any one of claim 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872614.4U CN204555210U (en) | 2014-12-31 | 2014-12-31 | Clarifier and Wiring structure thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872614.4U CN204555210U (en) | 2014-12-31 | 2014-12-31 | Clarifier and Wiring structure thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204555210U true CN204555210U (en) | 2015-08-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420872614.4U Active CN204555210U (en) | 2014-12-31 | 2014-12-31 | Clarifier and Wiring structure thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204555210U (en) |
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2014
- 2014-12-31 CN CN201420872614.4U patent/CN204555210U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |