CN204469456U - Clarifier and ornamental strip assembly structure thereof - Google Patents
Clarifier and ornamental strip assembly structure thereof Download PDFInfo
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- CN204469456U CN204469456U CN201420872460.9U CN201420872460U CN204469456U CN 204469456 U CN204469456 U CN 204469456U CN 201420872460 U CN201420872460 U CN 201420872460U CN 204469456 U CN204469456 U CN 204469456U
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Abstract
The utility model belongs to purification technology field, aims to provide a kind of clarifier and ornamental strip assembly structure thereof, and this ornamental strip assembly structure comprises fuselage main body, also comprises ornamental strip.The utility model, by being at least convexly equipped with a fastener in the inner side of ornamental strip along its center line, the sidewall of fuselage main body at least offers a buckle slot, wherein, each fastener is arranged in corresponding buckle slot, with this, decorative strip fastener is connected on the sidewall of fuselage main body, moreover, this ornamental strip is also provided with guidance set and/or limit assembly, with this, not only dismounting is convenient in maintenance process, and ornamental strip can realize contraposition well and between fuselage main body in buckle process, and ornamental strip is not easy to depart from from fuselage main body after assembling, in a word, like this, not only be convenient to dismounting, the perfection also achieved between the fuselage main body of clarifier and each housing is fitted, beautify the overall appearance of clarifier.
Description
Technical field
The utility model belongs to purification technology field, relates to the syndeton of a kind of ornamental strip and clarifier fuselage main body, particularly relates to a kind of assembly structure of ornamental strip of clarifier and has the clarifier of this assembly structure.
Background technology
Clarifier is also known as cleaner or cleaner, and the clarifier of indication refers in particular to air purifier usually here, and along with growth in the living standard, the air quality requirements of people to living environment is more and more higher, and air purifier and relevant device obtain and constantly develop.At present, its kind of purification of air utensil on market, profile are various, mainly contain the forms such as vertical, desk-top, and its total housing profile is usually all more single, mainly fixedly mounted to enclose by screw or screw by a procapsid and a back casing and form, but, this mounting means, mainly there is following defect: 1) in installation and maintenance process, be not easy to dismounting; 2) when the profile of the two side of the front and rear housings of assembling is mutually camber line curved surface, the cooperation between fuselage main body, procapsid and back casing is fitted not.
Utility model content
The purpose of this utility model is to provide a kind of clarifier and ornamental strip assembly structure thereof, not easy to assemble in order to the shell structure solving existing clarifier, and the technical problem of fitting not with fuselage main body.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: provide a kind of ornamental strip assembly structure, comprise fuselage main body, also comprise ornamental strip, and described ornamental strip is connected with the sidewall buckle of described fuselage main body; The inner side of described ornamental strip is at least convexly equipped with a fastener along the center line of described ornamental strip, and the sidewall of described fuselage main body at least offers a buckle slot, and each described fastener is arranged in corresponding described buckle slot; Also comprise guidance set and/or limit assembly.
Further, described guidance set comprises at least one first guide frame and/or at least one the second guide frame, and the securement strength of each described first guide frame is greater than each described second guide frame.
Further, each described first guide frame includes the first guide, each described first guide is all convexly equipped in the inner side of described ornamental strip, and the sidewall of described fuselage main body at least offers first gathering sill, and each described first guide is embedded in corresponding described first gathering sill.
Further, each described first guide frame also comprises the first reinforcement be fixedly connected with the first guide described in it, and each described first reinforcement is located at the inner side of described ornamental strip.
Further, each described first guide is arranged in turn along the center line of described ornamental strip.
Further, each described second guide frame includes the second guide, each described second guide is all convexly equipped in the inner side of described ornamental strip, and the sidewall of described fuselage main body at least offers second gathering sill, and each described second guide is embedded in corresponding described second gathering sill.
Further, each described second guide is arranged in turn along the center line of described ornamental strip.
Further, described limit assembly comprises at least one position limiting structure, and each described position limiting structure is convexly equipped in the inner side of described ornamental strip, and the sidewall of described fuselage main body at least offers a stopper slot, and each described position limiting structure is arranged in corresponding stopper slot.
Further, each described position limiting structure includes the first locating part and gap in the second locating part of described first locating part, each described first locating part is arranged in corresponding stopper slot, and a cell wall of described stopper slot is arranged in the gap of described first locating part and described second locating part.
Compared with prior art, the beneficial effect of the ornamental strip assembly structure that the utility model provides is: by the newly-increased ornamental strip matched with the camber line curved surface of the sidewall of fuselage main body, and on the center line of ornamental strip at least projection fastener, the sidewall of fuselage main body at least offers a buckle slot, wherein, the particular location of each fastener need be determined according to the flexural property of this camber line curved surface, certainly, each fastener is fastened in corresponding buckle slot, decorative strip fastener is made to be connected on the sidewall of fuselage main body with this, in addition, guidance set and/or limit assembly is also provided with between fuselage main body and ornamental strip, so, not only dismounting is convenient in maintenance process, and contraposition can be realized well between ornamental strip and fuselage main body in buckle process, and ornamental strip not easily departs from from fuselage main body after assembling, also be, the perfection that can realize between fuselage main body and each housing is fitted.
The utility model additionally provides a kind of clarifier, this clarifier comprises procapsid and back casing, also comprise above-mentioned ornamental strip assembly structure, described procapsid and described back casing are located at described fuselage main body from the front side of described fuselage main body and rear side respectively, the side of described ornamental strip is located on described procapsid, and opposite side is located on described back casing.
Compared with prior art, the beneficial effect of clarifier that the utility model provides is:
(1) by the newly-increased ornamental strip be connected with the two side buckle of fuselage main body, and the both sides of this ornamental strip are arranged on procapsid and back casing respectively, not only simplify the assembly technology of clarifier, also make the overall structure of whole clarifier compact.
(2) ornamental strip matched with the camber line curved surface of the two side of fuselage main body by newly-increased, by the camber line curved surface sidewall phase buckle of this ornamental strip with fuselage main body, guaranteeing under the prerequisite of assembling intensity, the case side mask of clarifier is not only made to have perfect camber line curved surface, beautify the monnolithic case of this clarifier, meet the individual demand of user to a certain extent.
Accompanying drawing explanation
Fig. 1 is the perspective view of the ornamental strip assembly structure of clarifier in the utility model embodiment;
Fig. 2 is one of perspective view of the fuselage main body of ornamental strip assembly structure in Fig. 1;
Fig. 3 is the perspective view two of the fuselage main body of ornamental strip assembly structure in Fig. 1;
Fig. 4 is the perspective view of the ornamental strip of ornamental strip assembly structure in Fig. 1;
Fig. 5 is the stereochemical structure assembling schematic diagram of the critical piece of clarifier in the utility model embodiment.
Label in accompanying drawing is as follows:
1 fuselage main body, 11 buckle slots, 12 first gathering sills, 13 second gathering sills, 14 stopper slots, 15 first connectors, 151 first installing holes;
2 ornamental strips, 21 fasteners, 22 second connectors, 221 second installing holes;
31 first guide frames, 311 first guides, 312 first reinforcements, 32 second guide frames, 321 second guides, 322 second reinforcements;
41 position limiting structures, 411 first locating parts, 412 second locating parts;
5 procapsids, 6 back casings.
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 Fig. 1 ~ Fig. 5, a kind of clarifier provided for the utility model one preferred embodiment and ornamental strip assembly structure thereof.
As shown in Figure 1 to 4, the ornamental strip assembly structure of this clarifier comprises fuselage main body 1, also comprises ornamental strip 2, and ornamental strip 2 is connected with the sidewall buckle of fuselage main body 1, understandably, this ornamental strip assembly structure to be connected with ornamental strip 2 buckle by fuselage main body 1 and jointly to be formed.It should be noted that, usually, as shown in Figure 1, fuselage main body 1 has two side, correspondingly, on its two side, equal buckle is connected with ornamental strip 2, as shown in Figure 2 or Figure 3, the ornamental strip assembly structure that each sidewall and ornamental strip 2 because of fuselage main body 1 are formed is substantially identical, thus, for ease of introducing, herein only with the connection of the buckle of a sidewall of fuselage main body 1 ornamental strip 2 corresponding with it for relying on the technical scheme introducing this ornamental strip assembly structure.Also it should be noted that, if the sidewall of fuselage main body 1 is camber line curved, accordingly, then ornamental strip 2 also should be camber line curved and match with this fuselage main body 1, be convenient to more fit in this fuselage main body 1 with this, understandably, the present embodiment is more suitable for the situation that the sidewall of fuselage main body 1 is camber line curved surface.
As shown in Figure 1 and Figure 4, be connected with the buckle of the sidewall of fuselage main body 1 for ease of realizing ornamental strip 2, thus be convenient to dismounting, in the present embodiment, the inner side of ornamental strip 2 is at least convexly equipped with a fastener 21, wherein, each fastener 21 is arranged along the center line of ornamental strip 2, and the particular location of distance between adjacent two fasteners 21 each fastener 21 in other words, and the quantity of fastener 21, the flexural property of the camber line curved surface that usually all should be presented by the sidewall of fuselage main body 1 is determined, and like this, is convenient to the stable connection of this assembly structure.As shown in Figure 1 to Figure 3, the sidewall of fuselage main body 1 at least offers a buckle slot 11, each fastener 21 is arranged in corresponding buckle slot 11, what remark additionally is, in fact, " sidewall " mentioned here refers to the sidewall in fuselage main body 1 two side, also be, each sidewall of fuselage main body 1 all at least offers a buckle slot 11, each fastener 21 on each ornamental strip 2 is opened in corresponding buckle slot 11, like this, not only ensure and be convenient to dismounting in maintenance process, and also make to be formed between fuselage main body 1 and ornamental strip 2 and can ideally fit, thus make monnolithic case better appearance, general structure is compact.
In addition, as shown in Figures 1 to 4, this ornamental strip assembly structure also comprises guidance set and/or limit assembly.Wherein, guidance set is formed jointly by ornamental strip 2 and fuselage main body 1, and mainly in order in buckle process, ornamental strip 2 well to being positioned at fuselage main body 1, and then can guarantee the quality of fit of ornamental strip 2 and fuselage main body 1; Limit assembly also has ornamental strip 2 and fuselage main body 1 jointly to be formed, mainly in order to after assembling or this ornamental strip 2 in assembling process not easily from fuselage main body 1, there is double swerve, even depart from fuselage main body 1 from left and right directions and go out.
It should be noted that, guaranteeing that ornamental strip 2 is with on the basis of the stable connection of fuselage main body 1, for ease of dismounting, the flexural property of the camber line curved surface that the setting of the particular location between this three of assembly structure that the buckle slot 11 of the fastener 21 on guidance set, limit assembly and ornamental strip 2 and fuselage main body 1 is formed should present according to the sidewall of fuselage main body 1 and determining.
Also it should be noted that, for ease of strengthening the stable connection of ornamental strip 2 and fuselage main body 1, usually, as shown in Figures 1 to 4, the bottom of fuselage main body 1 is provided with the first connector 15, and the first connector 15 offers the first installing hole 151, accordingly, the bottom of ornamental strip 2 sidewall is provided with the second connector 22, and the second connector 22 offers the second installing hole 221, wherein, first installing hole 151 is just relative with the second installing hole 221, be snapped in after in fuselage main body 1 at ornamental strip 2, namely by a fixture (as screw or screw), ornamental strip 2 is fixedly connected in fuselage main body 1.As shown in Figures 1 to 4, for guaranteeing to balance steadiness, ornamental strip 2 is provided with two the second connectors 22, so that this ornamental strip 2 to be fixedly connected with by front-back from fuselage main body 1 respectively.
Further, in the preferred embodiment that the utility model provides, for ease of completing the accurate contraposition between ornamental strip 2 and fuselage main body 1, guidance set comprises at least one first guide frame 31 and/or at least one the second guide frame 32, usually, because ornamental strip 2 mutually fastens with fuselage main body 1 from top to bottom, this can cause in fastening process, the power that the bottom of ornamental strip 2 is born can be greater than the power of bearing on its top, thus, accordingly, for adapting to this characteristic, the securement strength of each first guide frame 31 is greater than each second guide frame 32.
It should be noted that, usually, first guide frame 31 and the second guide frame 32 all have ornamental strip 2 and fuselage main body 1 jointly to be formed, wherein, first guide frame 31 is generally positioned at the top of the second guide frame 32, also namely, the guiding during the first half buckle of the first conductor structure mainly in order to ornamental strip 2 and fuselage main body 1, the guiding during the latter half buckle of the second guide frame 32 mainly in order to ornamental strip 2 and fuselage main body 1.
Further, as shown in Figure 4, in the preferred embodiment that the utility model provides, each first guide frame 31 includes the first guide 311, and each first guide 311 is all convexly equipped in the inner side of ornamental strip 2, preferably, the guide end of each first guide 311 is pre-small post-large trapezoidal shape structure, certainly, the shape of the guide end of each first guide 311 is not limited to said structure, as long as but can play the planform of guide effect.
Accordingly, as shown in Figure 2 or Figure 3, the sidewall of fuselage main body 1 at least offers first gathering sill 12, wherein, each first guide 311 is embedded in the first corresponding gathering sill 12, understandably, the guide end of the first guide 311 is embedded in the slotted eye of the first corresponding gathering sill 12, and the planform of the guide end of the slotted eye shape of the first gathering sill 12 and the first guide 311 is suitable.
Further, as shown in Figure 4, in the preferred embodiment that the utility model provides, each first guide frame 31 also comprises the first reinforcement 312 be fixedly connected with its first guide 311, and obviously, each first reinforcement 312 is located at the inner side of ornamental strip 2.In addition, moreover, because ornamental strip 2 is interlocked with fuselage main body 1 from top to bottom, thus, for ease of realizing the bracing reinforcement effect to each first guide 311 veritably, each first reinforcement 312 is arranged on the top of the first guide 311.
Further, as shown in Figure 4, in the preferred embodiment that the utility model provides, accurately lead better for enable, each first guide 311 is arranged in turn along the center line of ornamental strip 2, wherein, the particular location of each first guide 311 should be determined by the curved surface characteristic of the camber line curved surface of the sidewall of fuselage main body 1.
Further, in like manner, as shown in Figure 4, in the preferred embodiment that the utility model provides, each second guide frame 32 includes the second guide 321, and each second guide 321 is all convexly equipped in the inner side of ornamental strip 2, preferably, the profile of the guide end of each second guide 321 is pre-small post-large trapezoidal shape or is similar to trapezoidal shape, and certainly, the concrete structure of the guide end of each second guide 321 is not limited thereto.
Accordingly, as shown in Figure 2 or Figure 3, the sidewall of fuselage main body 1 at least offers second gathering sill 13, and wherein, each second guide 321 is embedded in the second corresponding gathering sill 13.Understandably, the guide end of the second guide 321 is embedded in the slotted eye of the second corresponding gathering sill 13, and the planform of the guide end of the slotted eye shape of the second gathering sill 13 and the second guide 321 is suitable.
It should be noted that, as shown in Figure 4, each second guide frame 32 also comprises the second reinforcement 322 be fixedly connected with the second guide 321, obviously, each second reinforcement 322 is located at the inner side of ornamental strip 2, and for ease of realizing the bracing reinforcement effect to each second guide 321, each second reinforcement 322 is arranged on the top of the second guide 321.Preferably, as shown in Figure 4, each second reinforcement 322 is fixedly connected with it from the both sides of each second guide 321 of correspondence.
Further, as shown in Figure 4, in the preferred embodiment that the utility model provides, accurately lead better for enable, each second guide 321 is arranged in turn along the center line of ornamental strip 2, wherein, the particular location of each first guide 311 should be determined by the curved surface characteristic of the camber line curved surface of the sidewall of fuselage main body 1.
Further, as shown in Figure 4, in the preferred embodiment that the utility model provides, limit assembly comprises at least one position limiting structure 41, in order to limit ornamental strip 2 rocking in the lateral direction, wherein, each position limiting structure 41 is convexly equipped in the inner side of ornamental strip 2, the sidewall of fuselage main body 1 at least offers a stopper slot 14, and each position limiting structure 41 is arranged in corresponding stopper slot 14.
Further, as shown in Figure 4, in the preferred embodiment that the utility model provides, each position limiting structure 41 includes the first locating part 411 and gap in the second locating part 412 of the first locating part 411.Wherein, as shown in Figure 1 to Figure 3, each first locating part 411 is arranged in corresponding stopper slot 14, one cell wall (not shown) of stopper slot 14 is arranged in the gap of the first locating part 411 and the second locating part 412, understandably, the gap between the first locating part 411 and the second locating part 412 just can hold this cell wall of stopper slot 14.It should be noted that, as shown in Figure 1, the first locating part 411 is positioned at the side of this cell wall, and the second locating part 412 is positioned at the opposite side of this cell wall, limits ornamental strip 2 movement in the lateral direction with this.
Of the present utility model one embodiment still provides a kind of clarifier, wherein, as shown in Figure 5, this clarifier comprises procapsid 5 and back casing 6, also comprises above-mentioned ornamental strip assembly structure, in fact, this clarifier also comprises fuselage main body 1 and ornamental strip 2, wherein, this fuselage main body 1 is the fuselage main body 1 of ornamental strip assembly structure, and this ornamental strip 2 is the ornamental strip 2 of ornamental strip assembly structure.
For ease of simplifying the assembly technology of clarifier, make the overall structure of whole clarifier compact, procapsid 5 is located at fuselage main body 1 from the front side of fuselage main body 1, back casing 6 is located at fuselage main body 1 from the rear side of fuselage main body 1, moreover, the side of the ornamental strip 2 on the two side of clarifier is located on procapsid 5, opposite side is located on back casing 6, thus, to form the closed shell structure of this clarifier, and like this, guaranteeing under the prerequisite of assembling intensity, the case side mask of clarifier is not only made to have perfect camber line curved surface, beautify the monnolithic case of this clarifier, meet the individual demand of user to a certain extent.
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 ornamental strip assembly structure of clarifier, comprise fuselage main body, it is characterized in that: also comprise ornamental strip, the inner side of described ornamental strip is at least convexly equipped with a fastener along the center line of described ornamental strip, the sidewall of described fuselage main body at least offers a buckle slot, and each described fastener is arranged in corresponding described buckle slot; Also comprise guidance set and/or limit assembly.
2. the ornamental strip assembly structure of clarifier as claimed in claim 1, it is characterized in that: described guidance set comprises at least one first guide frame and/or at least one the second guide frame, the securement strength of each described first guide frame is greater than each described second guide frame.
3. the ornamental strip assembly structure of clarifier as claimed in claim 2, it is characterized in that: each described first guide frame includes the first guide, each described first guide is all convexly equipped in the inner side of described ornamental strip, the sidewall of described fuselage main body at least offers first gathering sill, and each described first guide is embedded in corresponding described first gathering sill.
4. the ornamental strip assembly structure of clarifier as claimed in claim 3, is characterized in that: each described first guide frame also comprises the first reinforcement be fixedly connected with the first guide described in it, and each described first reinforcement is located at the inner side of described ornamental strip.
5. the ornamental strip assembly structure of the clarifier as described in claim 3 or 4, is characterized in that: each described first guide is arranged in turn along the center line of described ornamental strip.
6. the ornamental strip assembly structure of clarifier as claimed in claim 2, it is characterized in that: each described second guide frame includes the second guide, each described second guide is all convexly equipped in the inner side of described ornamental strip, the sidewall of described fuselage main body at least offers second gathering sill, and each described second guide is embedded in corresponding described second gathering sill.
7. the ornamental strip assembly structure of clarifier as claimed in claim 6, is characterized in that: each described second guide is arranged in turn along the center line of described ornamental strip.
8. the ornamental strip assembly structure of clarifier as claimed in claim 1 or 2, it is characterized in that: described limit assembly comprises at least one position limiting structure, each described position limiting structure is convexly equipped in the inner side of described ornamental strip, the sidewall of described fuselage main body at least offers a stopper slot, and each described position limiting structure is arranged in corresponding stopper slot.
9. the ornamental strip assembly structure of clarifier as claimed in claim 8, it is characterized in that: each described position limiting structure includes the first locating part and gap in the second locating part of described first locating part, each described first locating part is arranged in corresponding stopper slot, and a cell wall of described stopper slot is arranged in the gap of described first locating part and described second locating part.
10. clarifier, comprise procapsid and back casing, it is characterized in that: also comprise the ornamental strip assembly structure as described in any one of claim 1 to 9, described procapsid and described back casing are located at described fuselage main body from the front side of described fuselage main body and rear side respectively, the side of described ornamental strip is located on described procapsid, and opposite side is located on described back casing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872460.9U CN204469456U (en) | 2014-12-31 | 2014-12-31 | Clarifier and ornamental strip assembly structure thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872460.9U CN204469456U (en) | 2014-12-31 | 2014-12-31 | Clarifier and ornamental strip assembly structure thereof |
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| CN204469456U true CN204469456U (en) | 2015-07-15 |
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| CN201420872460.9U Active CN204469456U (en) | 2014-12-31 | 2014-12-31 | Clarifier and ornamental strip assembly structure thereof |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106369796A (en) * | 2016-11-10 | 2017-02-01 | 海信（山东）空调有限公司 | Air conditioner panel and air conditioner indoor unit |
| CN109028305A (en) * | 2018-07-17 | 2018-12-18 | 广东美的制冷设备有限公司 | Air processor |
| CN109488620A (en) * | 2018-11-16 | 2019-03-19 | 珠海格力电器股份有限公司 | Decorative ring and household appliance |
| CN110799004A (en) * | 2019-12-10 | 2020-02-14 | 广东荧天生物技术有限公司 | Casing for medical equipment |
-
2014
- 2014-12-31 CN CN201420872460.9U patent/CN204469456U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106369796A (en) * | 2016-11-10 | 2017-02-01 | 海信（山东）空调有限公司 | Air conditioner panel and air conditioner indoor unit |
| CN106369796B (en) * | 2016-11-10 | 2019-07-16 | 海信（山东）空调有限公司 | A kind of air-conditioning panel and air conditioner indoor unit |
| CN109028305A (en) * | 2018-07-17 | 2018-12-18 | 广东美的制冷设备有限公司 | Air processor |
| CN109488620A (en) * | 2018-11-16 | 2019-03-19 | 珠海格力电器股份有限公司 | Decorative ring and household appliance |
| CN110799004A (en) * | 2019-12-10 | 2020-02-14 | 广东荧天生物技术有限公司 | Casing for medical equipment |
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