CN209306141U - A kind of flip structure having route protection - Google Patents
A kind of flip structure having route protection Download PDFInfo
- Publication number
- CN209306141U CN209306141U CN201822127769.6U CN201822127769U CN209306141U CN 209306141 U CN209306141 U CN 209306141U CN 201822127769 U CN201822127769 U CN 201822127769U CN 209306141 U CN209306141 U CN 209306141U
- Authority
- CN
- China
- Prior art keywords
- top cover
- fuselage
- mounting rack
- mounting base
- insertion section
- Prior art date
- 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 - Fee Related
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Abstract
Originally practical to disclose a kind of flip structure for having route protection, including fuselage, top cover, it is equipped with mounting rack in the fuselage, top cover is rotationally connected in the shaft mounting base of mounting rack；The longitudinally connected abacus in the mounting rack at least one end, orifice plate are provided with the side opening concentric with shaft mounting base；Top cover inner surface is equipped with and sets wire box, sets wire box lower end at least provided with an insertion section, insertion section is inserted between adjacent orifice plate and shaft mounting base, and insertion section lower end side is provided with the cartridge apertures of positive contralateral exposure.
Description
Technical field
The utility model relates to intelligent garbage bin technical field more particularly to a kind of flip structures for having route protection.
Background technique
Intelligent garbage bin robot field's top cover mounted array microphone structure is used to judge different sound source positions, Mike
Air control making sheet is installed to dustbin robot body, and microphone power and signal wire need to be connected in robot body by top cover,
The rotational structure that route need to be connected by top cover with fuselage；Its rotational structure is as shown in patent CN201320443754.5 Fig. 1.
The route of intelligent garbage barrel top cover will cause different degrees of drawing during uncapping with dustbin and closing lid at present
It pulls, rub, affect the route service life and increase to uncap and close lid resistance；And route is directly exposed to the external world by conventional design, again
It is unfavorable for the protection of route.
To solve the problems, such as current connection, a kind of circuit installation structure is designed, prevents from uncapping in dustbin and closes lid
It causes to pull in the process, is tortuous, while reducing route to the resistance for closing lid of uncapping, improving the service life of route, installation letter
Easily, maintenance cost is reduced.
Utility model content
In view of the deficiencies of the prior art, the utility model provides a kind of flip structure for having route protection, it is intended to solve
Certainly conventional garbage bucket, which is uncapped during pass is covered, causes route to pull, rub, and to the resistance for closing lid of uncapping, service life is low, dimension
Protect problem at high cost.
To achieve the above object, the utility model provides the following technical solutions: a kind of flip structure having route protection,
Including fuselage, top cover, mounting rack is equipped in the fuselage, top cover is rotationally connected in the shaft mounting base of mounting rack；The peace
The longitudinally connected abacus at least one end is shelved, orifice plate is provided with the side opening concentric with shaft mounting base；Top cover inner surface is equipped with and sets line
Box sets wire box lower end at least provided with an insertion section, and insertion section is inserted between adjacent orifice plate and shaft mounting base, and under insertion section
End side surface is provided with the cartridge apertures of positive contralateral exposure.
In order to realize the stability of rotation connection, a pair of of shaft mounting base, mounting rack two are symmetrically arranged on the mounting rack
It holds longitudinally connected abacus and is provided with side opening, set wire box equipped with two insertion sections.
In order to prevent 90 degree of top cover when, top cover lower end and body interference, the mounting rack are fixed in fuselage port, top cover
Lower end is inwardly fixedly connected with axle sleeve lower than top cover lower end and concentric with shaft mounting base, and top cover is installed by axle sleeve and shaft
Seat shaft connection, and insertion section is lower than top cover lower end.
Detachable in order to realize, the wire box of setting is by being fixed on a circle rib of top cover inner surface and covering the box on rib
Lid is constituted, several hole posts and non-movable piston between the top cover inner surface and lid inner surface in rib by being respectively fixedly connected with
Insertion connection.
It is interfered when rotating in order to prevent, the insertion section bottom is arc surface.
It is protected to be set in interlayer to route and control panel, the fuselage inner wall is fixed with sandwich plate, interlayer
Plate is connected to mounting rack and forms interlayer with fuselage inner wall.
It preferably, is cylinder type in the fuselage.
The utility model has the beneficial effects that
1. dustbin upper cover route " Z " font is arranged between top cover and fuselage (Fig. 3), dustbin uncaps, closes the mistake covered
The relative position of Cheng Zhong, top cover cover slot route and fuselage interior route is rotated along shaft always, and rotation angle is rubbish every time
Barrel top cover opens and closes angle, avoids route and pulls, rubs in bascule part, reduces route and uncaps what pass was covered to dustbin
Resistance improves the service life of route；
2. dustbin upper cover route is hidden between top cover and envelope line lid, have in use process to route certain dust-proof
Water-proof function；
3. rubbish barrel top cover and envelope line lid are coupled, seal circular arc at line cover slot lid and designed with fuselage mounting rack, rotation knot
Structure cooperation is harmonious, guarantees have beautiful and line maintenance convenient advantage while line security.
Detailed description of the invention
Fig. 1 is the usage state diagram of the utility model.
Fig. 2 is the structural schematic diagram of the utility model.
Fig. 3 is that the utility model removes the structural schematic diagram after envelope line lid.
Fig. 4 is the partial enlarged view of the utility model Fig. 3.
Wherein: fuselage 1；Top cover 2；Mounting rack 3；Sandwich plate 4；Set wire box 5；Axle sleeve 21；Shaft mounting base 31；Orifice plate 32；
Side opening 33；Insertion section 51；Cartridge apertures 52；Rib 511；Box cover 512；Non-movable piston 513；Route 6；Shaft 7.
Specific embodiment
As shown in Figure 1, 2, 3,1. a kind of flip structure for having route protection, including fuselage 1, top cover 2, the fuselage 1
Interior to be equipped with mounting rack 3, top cover 2 is rotationally connected in the shaft mounting base 31 of mounting rack 3；The mounting rack 3 at least one end is longitudinal
Abacus 32 is connected, orifice plate 32 is provided with the side opening 33 concentric with shaft mounting base 31；2 inner surface of top cover is equipped with and sets wire box 5, sets line
5 lower end of box is at least provided with an insertion section 51, and insertion section 51 is inserted between adjacent orifice plate 32 and shaft mounting base 31, and insertion section
51 lower end sides are provided with the cartridge apertures 52 of positive contralateral exposure 33.
The wire box 5 of setting of the utility model is used for storage protection route 6, route 6 after 2 outer surface mounted array microphone of top cover
Be placed in wire box 5 across top cover 2, at the same its stitch through insertion section 51 from cartridge apertures 52 enter side opening 33 be in " Z " font, then with machine
Control panel connection in body 1；Again since side opening 33, cartridge apertures 52 and shaft mounting base 31 are concentric, when top cover 2 is rotated by axle sleeve 21
When the shaft 7 of axis mounting base 31 rotates, sets the relative position of route and 1 internal wiring of fuselage in wire box 5 and is rotated always along axle center,
And rotation angle is that top cover 2 opens and closes angle every time, avoids route and pulls, rubs in bascule part, reduces route pair
Dustbin, which is uncapped, closes the resistance of lid, improves the service life of route；Further, route 6 can be pasted or other modes limits
In setting in wire box 5.
In order to realize the stability of rotation connection；A pair of of shaft mounting base 31, mounting rack are symmetrically arranged on the mounting rack 3
The longitudinally connected abacus 32 in 3 both ends is simultaneously provided with side opening 33, sets wire box 5 equipped with two insertion sections 51.
In order to prevent 90 degree of top cover when, top cover lower end and body interference, the mounting rack 3 are fixed in 1 port of fuselage, top
2 lower end of lid is inwardly fixedly connected with axle sleeve 21 lower than 2 lower end of top cover and concentric with shaft mounting base 31, and top cover 2 passes through axle sleeve
21 connect with 31 shaft of shaft mounting base, and insertion section 51 is lower than 2 lower end of top cover；
Detachable in order to realize, the wire box 5 of setting is by being fixed on a circle rib 511 of 2 inner surface of top cover and covering in rib
Box cover 512 on 511 is constituted, by being respectively fixedly connected between 512 inner surface of 2 inner surface of top cover and box cover in rib 511
Several hole posts and non-movable piston 513 insertion connect；
It is interfered when rotating in order to prevent, 51 bottom of insertion section is arc surface；
It is protected to be set in interlayer to route and control panel, 1 inner wall of fuselage is fixed with sandwich plate 4, folder
Laminate 4 is connected to mounting rack 3 and forms interlayer with 1 inner wall of fuselage.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Made any modification, equivalent replacement or improvement etc., should be included in the utility model within the spirit and principle of utility model
Protection scope within.
Claims (7)
1. a kind of flip structure for having route protection, including fuselage (1), top cover (2), the fuselage (1) is interior to be equipped with mounting rack
(3), top cover (2) is rotationally connected in the shaft mounting base (31) of mounting rack (3)；It is characterized in that, the mounting rack (3) is at least
The longitudinally connected abacus in one end (32), orifice plate (32) are provided with the side opening (33) concentric with shaft mounting base (31)；Top cover (2) interior table
Face is equipped with and sets wire box (5), sets wire box (5) lower end at least provided with an insertion section (51), insertion section (51) are inserted into adjacent orifice plate
(32) between shaft mounting base (31), and insertion section (51) lower end side is provided with the cartridge apertures (52) of positive contralateral exposure (33).
2. a kind of flip structure for having route protection according to claim 1, which is characterized in that on the mounting rack (3)
It is symmetrically arranged with a pair of of shaft mounting base (31), the longitudinally connected abacus in mounting rack (3) both ends (32) is simultaneously provided with side opening (33), sets line
Box (5) is equipped with two insertion sections (51).
3. a kind of flip structure for having route protection according to claim 1, which is characterized in that the mounting rack (3) is solid
Due in fuselage (1) port, top cover (2) lower end be inwardly fixedly connected with lower than top cover (2) lower end and with shaft mounting base (31)
Concentric axle sleeve (21), top cover (2) are connect by axle sleeve (21) with shaft mounting base (31) shaft, and insertion section (51) are lower than top
Cover (2) lower end.
4. a kind of flip structure for having route protection according to claim 1, which is characterized in that it is described set wire box (5) by
Circle rib (511) for being fixed on top cover (2) inner surface is constituted with the box cover (512) covered on rib (511), rib (511)
Several hole posts and non-movable piston between interior top cover (2) inner surface and box cover (512) inner surface by being respectively fixedly connected with
(513) insertion connection.
5. a kind of flip structure for having route protection according to claim 1, which is characterized in that insertion section (51) bottom
Portion is arc surface.
6. a kind of flip structure for having route protection according to claim 1, which is characterized in that fuselage (1) inner wall
It is fixed with sandwich plate (4), sandwich plate (4) is connected to mounting rack (3) and forms interlayer with fuselage (1) inner wall.
7. a kind of flip structure for having route protection according to claim 1, which is characterized in that be in the fuselage (1)
Cylinder type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822127769.6U CN209306141U (en) | 2018-12-18 | 2018-12-18 | A kind of flip structure having route protection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822127769.6U CN209306141U (en) | 2018-12-18 | 2018-12-18 | A kind of flip structure having route protection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209306141U true CN209306141U (en) | 2019-08-27 |
Family
ID=67677483
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822127769.6U Expired - Fee Related CN209306141U (en) | 2018-12-18 | 2018-12-18 | A kind of flip structure having route protection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209306141U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11753241B2 (en) | 2019-12-31 | 2023-09-12 | Dreame Technology (shanghai) Co., Ltd. | Intelligent garbage can |
-
2018
- 2018-12-18 CN CN201822127769.6U patent/CN209306141U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11753241B2 (en) | 2019-12-31 | 2023-09-12 | Dreame Technology (shanghai) Co., Ltd. | Intelligent garbage can |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190827 Termination date: 20191218 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |