CN205019855U - Fuselage fixed structure of clarifier - Google Patents
Fuselage fixed structure of clarifier Download PDFInfo
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- CN205019855U CN205019855U CN201520773197.2U CN201520773197U CN205019855U CN 205019855 U CN205019855 U CN 205019855U CN 201520773197 U CN201520773197 U CN 201520773197U CN 205019855 U CN205019855 U CN 205019855U
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- fuselage
- filter case
- machine body
- body base
- case assembly
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Abstract
The utility model provides a fuselage fixed structure of clarifier, includes aircraft nose and fuselage, its characterized in that the fuselage includes a plurality of box subassembly and fuselage bases strained, and a plurality of box subassembly superpose formulas of straining are assembled on the fuselage base, set up two at least bracing pieces on the fuselage base, and the bracing piece is inserted in proper order and is located a plurality of straining in box subassembly. A plurality of strain in box subassembly about correspond and all be provided with the assembly groove, the bracing piece is inserted in proper order and is located a plurality of assembly inslots of straining box subassembly. Bracing piece and fuselage base rigid connection, and perpendicular to fuselage base surface. The utility model discloses a set up the bracing piece on the fuselage base, then with a plurality of box subassembly layering suits of straining on the bracing piece, make the bracing piece hide the fuselage base with strain a box subassembly the inside, protected the whole outward appearance integrated design of product. It has the characteristics that simple structure is reasonable, the assembly is firm reliably, the appearance is pleasing to the eye, the wholeness is strong.
Description
Technical field
The utility model relates to a kind of air purifier, particularly the fuselage fixed structure of clarifier.
Background technology
The fuselage fixed form of the tower purifier of the most split in current air purifier field adopts the mode of external support bar, destroys the integraty of product appearance to a certain extent.Therefore, be necessary to make further improvements.
Summary of the invention
The purpose of this utility model aim to provide a kind of simple and reasonable, assemble the fuselage fixed structure that solid and reliable, good looking appearance, globality are strong, facilitate the clarifier of screen replacing, to overcome weak point of the prior art.
The fuselage fixed structure of a kind of clarifier designed by this object, comprise head and fuselage, it is characterized in that described fuselage comprises some filter case assemblies and machine body base, some filter case assembly stacked-up types are assemblied in machine body base, machine body base is arranged at least two support bars, support bar is inserted in some filter case assemblies successively.The mode of being connected and fixed of this structural fuselage adopts support bar and machine body base rigid attachment, and then the layering of some filter case assemblies is sleeved on support bar, and support bar is hidden in machine body base and filters inside case assembly, protects the overall appearance integrated design of product
For coordinating the assembling of support bar, in the filter case assembly described in several, correspondence is provided with fitting recess up and down, and support bar is inserted in the fitting recess of some filter case assemblies successively.Described support bar and machine body base rigid attachment, and perpendicular to machine body base surface.
Described machine body base and filter case assembly cross section are mutually corresponding is geometry.Described filter case assembly upper opening, bottom is provided with filter screen.Described filter case assembly edge of opening is provided with continuous print projection, and bottom margin is provided with continuous print groove, and the corresponding assembly of projection of lower metafiltration case assembly is in the groove of upper metafiltration case assembly.Different cross sections can be designed to as required, request the restriction in design.
First scheme: described machine body base is corresponding rectangular with filter case assembly cross section, and described support bar arranges two, and is placed in machine body base both sides, fitting recess correspondence is arranged at filter case assembly inwall both sides.
Alternative plan: described machine body base is corresponding rectangular with filter case assembly cross section, and described support bar arranges four, and is placed on machine body base four side, fitting recess correspondence is arranged at filter case assembly inwall four side.
Third program: described machine body base is corresponding rounded with filter case assembly cross section, and described support bar is distributed in machine body base edge, fitting recess correspondence is distributed in filter case assembly inwall.
The beneficial effects of the utility model are:
The layering of some filter case assemblies, by arranging support bar in machine body base, is then sleeved on support bar by the utility model, and filter case assembly successively can be mentioned along support bar and dismantled, and conveniently to change the filter screen bottom filter case assembly, clean or safeguard; In addition, the assembling mode of this structure makes support bar be hidden in machine body base and filter inside case assembly, protects the overall appearance integrated design of product.It has simple and reasonable, assemble the feature that solid and reliable, good looking appearance, globality are strong, facilitate screen replacing.
Accompanying drawing explanation
Fig. 1 is the decomposition texture schematic diagram of the utility model one embodiment.
Fig. 2 is the profile of fuselage in the utility model one embodiment.
Fig. 3 is the profile of single filter case assembly in the utility model one embodiment.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further described.
First embodiment
See Fig. 1, the fuselage fixed structure of this clarifier, comprises head 1 and fuselage, fuselage comprises four filter case assemblies 2 and machine body base 4, four filter case assembly 2 stacked-up types are assemblied in machine body base 4, machine body base 4 are arranged two support bars 3, and support bar 3 is inserted in four filter case assemblies 2 successively.The mode of being connected and fixed of this structural fuselage adopts support bar 3 and machine body base 4 rigid attachment; then the layering of four filter case assemblies 2 is sleeved on support bar 3 successively; make support bar 3 be hidden in machine body base 4 and filter inside case assembly 2, protect the overall appearance integrated design of product
Further, see Fig. 2-Fig. 3, be coordinate the assembling of support bar 3, correspondingly up and down in four filter case assemblies 2 be provided with fitting recess 2.1, support bar 3 is inserted in the fitting recess 2.1 of four filter case assemblies 2 successively.Support bar 3 and machine body base 4 rigid attachment, and perpendicular to machine body base 4 surface, guarantee four filter case assembly about 2 vertical pile.
In the present embodiment, machine body base 4 and filter case assembly 2 cross section are mutually corresponding rectangular.Filter case assembly 2 upper opening, bottom is provided with filter screen.Filter case assembly 2 edge of opening is provided with continuous print projection 2.2, and bottom margin is provided with continuous print groove 2.3, and the corresponding assembly of projection 2.2 of relative lower metafiltration case assembly 2 is in the groove 2.3 of relative upper metafiltration case assembly 2.
Further, two support bars 3 are placed in the relative both sides of machine body base 4 respectively, and fitting recess 2.1 correspondence is arranged at filter case assembly 2 inwall both sides.
Second embodiment
The fuselage fixed structure of the clarifier of the present embodiment, it is different from the first embodiment part and is: machine body base 4 is corresponding rectangular with filter case assembly 2 cross section, support bar 3 arranges four, and is placed on machine body base 4 four side, and fitting recess 2.1 correspondence is arranged at filter case assembly 2 inwall four side.
Other do not state part with the first embodiment, no longer describe in detail here.
3rd embodiment
The fuselage fixed structure of the clarifier of the present embodiment, it is different from the first embodiment part and is: machine body base 4 is corresponding rounded with filter case assembly 2 cross section, and support bar 3 is distributed in machine body base 4 edge, and fitting recess 2.1 correspondence is distributed in filter case assembly 2 inwall.
Other do not state part with the first embodiment, no longer describe in detail here.
Above-mentioned is preferred version of the present utility model, shows and describes general principle of the present utility model, principal character and advantage of the present utility model.Those skilled in the art should understand the utility model and not be 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 (9)
1. the fuselage fixed structure of a clarifier, comprise head (1) and fuselage, it is characterized in that described fuselage comprises some filter case assemblies (2) and machine body base (4), some filter case assembly (2) stacked-up types are assemblied in machine body base (4), machine body base (4) is upper arranges at least two support bars (3), and support bar (3) is inserted in some filter case assemblies (2) successively.
2. the fuselage fixed structure of clarifier according to claim 1, it is characterized in that in the filter case assembly (2) described in several, correspondence is provided with fitting recess (2.1) up and down, support bar (3) is inserted in the fitting recess (2.1) of some filter case assemblies (2) successively.
3. the fuselage fixed structure of clarifier according to claim 1, is characterized in that described support bar (3) and machine body base (4) rigid attachment, and perpendicular to machine body base (4) surface.
4. the fuselage fixed structure of clarifier according to claim 1, it is characterized in that described machine body base (4) and filter case assembly (2) cross section mutually corresponding be geometry.
5. the fuselage fixed structure of clarifier according to claim 4, it is characterized in that described filter case assembly (3) upper opening, bottom is provided with filter screen.
6. the fuselage fixed structure of clarifier according to claim 4, it is characterized in that described filter case assembly (2) edge of opening is provided with continuous print projection (2.2), bottom margin is provided with continuous print groove (2.3), and projection (2.2) the corresponding assembly of lower metafiltration case assembly (2) is in the groove (2.3) of upper metafiltration case assembly (2).
7. the fuselage fixed structure of clarifier according to any one of claim 1-6, it is characterized in that described machine body base (4) is corresponding rectangular with filter case assembly (2) cross section, described support bar (3) arranges two, and being placed in machine body base (4) both sides, fitting recess (2.1) correspondence is arranged at filter case assembly (2) inwall both sides.
8. the fuselage fixed structure of clarifier according to any one of claim 1-6, it is characterized in that described machine body base (4) is corresponding rectangular with filter case assembly (2) cross section, described support bar (3) arranges four, and being placed on machine body base (4) four side, fitting recess (2.1) correspondence is arranged at filter case assembly (2) inwall four side.
9. the fuselage fixed structure of clarifier according to any one of claim 1-6, it is characterized in that described machine body base (4) is corresponding rounded with filter case assembly (2) cross section, described support bar (3) is distributed in machine body base (4) edge, and fitting recess (2.1) correspondence is distributed in filter case assembly (2) inwall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520773197.2U CN205019855U (en) | 2015-10-06 | 2015-10-06 | Fuselage fixed structure of clarifier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520773197.2U CN205019855U (en) | 2015-10-06 | 2015-10-06 | Fuselage fixed structure of clarifier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205019855U true CN205019855U (en) | 2016-02-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520773197.2U Active CN205019855U (en) | 2015-10-06 | 2015-10-06 | Fuselage fixed structure of clarifier |
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| Country | Link |
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| CN (1) | CN205019855U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112909771A (en) * | 2021-01-25 | 2021-06-04 | 中科瑞能电气股份有限公司 | Install convenient basement looped netowrk cabinet |
-
2015
- 2015-10-06 CN CN201520773197.2U patent/CN205019855U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112909771A (en) * | 2021-01-25 | 2021-06-04 | 中科瑞能电气股份有限公司 | Install convenient basement looped netowrk cabinet |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: Room 2616, 129 Liuhe Road, Xihu District, Hangzhou City, Zhejiang Province Patentee after: Hangzhou Shijing Technology Co., Ltd Address before: 100000, No. 14, building 3, building 11, 1708 Ying Road, Beijing, Chaoyang District, 4 Patentee before: BEIJING ERACLEAN TECHNOLOGY Co.,Ltd. |