CN209275428U - A kind of roller conveyor connection fuselage stacking bracket - Google Patents
A kind of roller conveyor connection fuselage stacking bracket Download PDFInfo
- Publication number
- CN209275428U CN209275428U CN201822189466.7U CN201822189466U CN209275428U CN 209275428 U CN209275428 U CN 209275428U CN 201822189466 U CN201822189466 U CN 201822189466U CN 209275428 U CN209275428 U CN 209275428U
- Authority
- CN
- China
- Prior art keywords
- block
- fuselage
- bracket
- wall
- stacking
- 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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- Rollers For Roller Conveyors For Transfer (AREA)
Abstract
The utility model discloses warehouses, a kind of roller conveyor connection fuselage stacking bracket in logistics transportation Sorting Technique field, including fuselage, the left and right sides inner wall of the fuselage is respectively provided with spacing block set, the inner wall clamping setting of the fuselage stacks bracket, the left and right sides outer wall for stacking bracket is respectively provided with limit card block, the inner wall for stacking bracket is uniformly arranged four groups of limit holes, four side inner walls of the limit hole are respectively provided with fastening block, the other end of the fastening block connects elastic clamping block, and the inner cavity of limit hole is flexibly connected fixed bracket by elastic clamping block, interval, which is uniformly arranged stacking bracket, in fuselage can rapidly and uniformly make fuselage decompose dynamics, to reinforce the intensity of fuselage entirety, guarantee the efficiency of article conveying sorting, the fixation bracket of different pore size is mounted in limit hole, for connecting the fuselage of two sides, make It must fix that bracket is convenient for disassembly and assembly, and structure is simple, cost is relatively low, easy to operate.
Description
Technical field
The utility model relates to warehouse, logistics transportation Sorting Technique field, specially a kind of roller conveyor connects fuselage
With stacking bracket.
Background technique
The device that warehouse, logistics transportation sorting are used to convey segregating articles mainly makes roller conveyor, and existing roller is defeated
Sending machine fuselage is typically all that whole fashioned iron fixation is formed, and processing cost is higher, and dynamics is unable to Quick uniform decomposition after whole stress,
So that fuselage is easy to produce local deformation, to influence the conveying sorting of article, while the fixation bracket of two sides fuselage is connected
It is to be fixed by the mode welded, it is all relatively complicated in disassembly and installation in this way.For this purpose, it is proposed that a kind of roller conveyor connects
The body that picks stacks bracket.
Utility model content
The purpose of this utility model is to provide a kind of roller conveyor connection fuselages with bracket is stacked, to solve above-mentioned back
The problem of being proposed in scape technology.
To achieve the above object, the utility model provides the following technical solutions: a kind of roller conveyor connection fuselage heap
Folded bracket, including fuselage, the left and right sides inner wall of the fuselage are respectively provided with spacing block set, the inner wall clamping setting heap of the fuselage
Folded bracket, the left and right sides outer wall for stacking bracket is respectively provided with limit card block, and limit card block is flexibly connected spacing block set, institute
The inner wall for stating stacking bracket is uniformly arranged four groups of limit holes, and four side inner walls of the limit hole are respectively provided with fastening block, the fastening
The other end of block connects elastic clamping block, and the inner cavity of limit hole is flexibly connected fixed bracket, and fixed bracket by elastic clamping block
Outer wall setting with the matched limit counterbore of limit card block.
Further, the elastic clamping block includes the telescopic rod for being fixed at fastening block inner wall, and the inner wall of fastening block
The blind hole of fixed telescopic rod is set, and the movable end of telescopic rod connects fixture block, and fixture block is set as semicircle convex block.
Further, two groups of limit card blocks are respectively set in outer wall at left and right sides of the stacking bracket, and limit card block is circle
Cylindrical block.
Further, the outer wall of two sides up and down of the limit card block is respectively provided with clamping groove, and spacing block set is close to limiting card
One end setting and the matched flexible clamping block of clamping groove of block outer wall.
Further, the stacking bracket is I-shaped steelframe, and the inner wall of two sides up and down of fuselage is respectively provided with and stacks branch
The matched I-shaped slot of frame.
Further, the telescopic rod in the elastic clamping block wraps up hollow tube, and the inner cavity setting activity of hollow tube
Bar, motion bar connect hollow tube by adjustable spring in the movable one end in hollow tube inner cavity.
Compared with prior art, the utility model has the beneficial effects that
1. the utility model grafting in fuselage stacks bracket, stacks bracket and be set as I-shaped steelframe, pass through limiting card
Block is connected in spacing block set, can will easily be stacked bracket and is mounted in fuselage, interval is uniformly arranged stacking in fuselage
Bracket can rapidly and uniformly make fuselage decompose dynamics, to reinforce the intensity of fuselage entirety, guarantee the effect of article conveying sorting
Rate；
2. the utility model in stacking bracket on limit hole elastic clamping block is set, elastic clamping block stretched by adjustable spring
Contracting movement, the fixation bracket of different pore size can be mounted in limit hole, for connecting the fuselage of two sides, so that fixed bracket
Convenient for disassembly and assembly, structure is simple, and cost is relatively low, easy to operate.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is that the utility model stacks supporting structure schematic diagram.
In figure: 1, fuselage；2, spacing block set；3, bracket is stacked；4, limit card block；5, limit hole；6, fastening block；7, elastic
Fixture block.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
The utility model provides a kind of technical solution referring to FIG. 1-2: a kind of roller conveyor connection fuselage stacking branch
Frame, including fuselage 1, the left and right sides inner wall of fuselage 1 are respectively provided with spacing block set 2, and the inner wall clamping setting of fuselage 1 stacks bracket 3,
The left and right sides outer wall for stacking bracket 3 is respectively provided with limit card block 4, and limit card block 4 is flexibly connected spacing block set 2, stacks bracket 3
Inner wall be uniformly arranged four groups of limit holes 5, four side inner walls of limit hole 5 are respectively provided with fastening block 6, the other end connection of fastening block 6
Elastic clamping block 7, and the inner cavity of limit hole 5 is flexibly connected fixed bracket by elastic clamping block 7, and the setting of support bracket fastened outer wall with
The matched limit counterbore of limit card block 4.
As shown in Figure 1, telescopic rod of the elastic clamping block 7 including being fixed at 6 inner wall of fastening block, and the inner wall of fastening block 6
The blind hole of fixed telescopic rod is set, and the movable end of telescopic rod connects fixture block, and fixture block is set as semicircle convex block, and telescopic rod pushes
Fixture block movement, fixes elastic clamping block 7 by the fixation bracket being plugged in limit hole 5；
As shown in Figure 1, stacking 3 left and right sides outer wall of bracket is respectively set two groups of limit card blocks 4, and limit card block 4 is circle
Cylindrical block makes fuselage 1 by two groups of limit card blocks 4 and stacks the connection uniform force between bracket 3, stable connection；
As shown in Figure 1, the outer wall of two sides up and down of limit card block 4 is respectively provided with clamping groove, and spacing block set 2 is close to limit card block
One end setting of 4 outer walls passes through elasticity when limit card block 4 is plugged in spacing block set 2 with clamping groove matched flexible clamping block
Clamping block is connected in clamping groove so that limit card block 4 connect with spacing block set 2 it is more stable；
As shown in Figure 1, stacking bracket 3 is I-shaped steelframe, and the inner wall of two sides up and down of fuselage 1 is respectively provided with and stacks bracket
3 matched I-shaped slots facilitate the connection stacked between bracket 3 and fuselage 1；
As shown in Figure 1, the telescopic rod in elastic clamping block 7 wraps up hollow tube, and motion bar is arranged in the inner cavity of hollow tube,
Motion bar connects hollow tube by adjustable spring in the movable one end in hollow tube inner cavity, so that fixed bracket is plugged on limit
When in hole 5, elastic clamping block 7 can pass through the fixation bracket of the fixed different pore size of telescopic rod.
Embodiment: will stack the I-shaped slot on bracket 3 and fuselage 1 and be cooperatively connected, and will stack bracket 3 and is plugged on fuselage 1
In, it will stack in the spacing block set 2 of 4 grafting of limit card block on bracket 3 on the fuselage 1, to make to stack bracket 3 and fuselage 1
Between connection it is more stable, will fixed bracket when being plugged in limit hole, support bracket fastened one end is plugged on limit hole 5
In, 7 stress of elastic clamping block in limit hole 5 moves upwards, and matches when the limit counterbore on fixed bracket is moved to elastic clamping block 7
The position of conjunction, elastic clamping block 7 are connected in limit counterbore by adjustable spring, thus easily fix fixed bracket, it is convenient
Connect the support bracket fastened installation of two sides fuselage.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of roller conveyor connection fuselage stacking bracket, including fuselage (1), it is characterised in that: a left side for the fuselage (1)
Right two sides inner wall is respectively provided with spacing block set (2), and the inner wall clamping setting of the fuselage (1) stacks bracket (3), the stacking bracket
(3) left and right sides outer wall is respectively provided with limit card block (4), and limit card block (4) is flexibly connected spacing block set (2), the stacking
The inner wall of bracket (3) is uniformly arranged four groups of limit holes (5), and four side inner walls of the limit hole (5) are respectively provided with fastening block (6), institute
Other end connection elastic clamping block (7) of fastening block (6) is stated, and the inner cavity of limit hole (5) is flexibly connected admittedly by elastic clamping block (7)
Fixed rack, and the setting of support bracket fastened outer wall and limit card block (4) matched limit counterbore.
2. a kind of roller conveyor connection fuselage stacking bracket according to claim 1, it is characterised in that: the elasticity
Fixture block (7) includes the telescopic rod for being fixed at fastening block (6) inner wall, and fixed telescopic rod is arranged in the inner wall of fastening block (6)
The movable end of blind hole, telescopic rod connects fixture block, and fixture block is set as semicircle convex block.
3. a kind of roller conveyor connection fuselage stacking bracket according to claim 1, it is characterised in that: the stacking
Two groups of limit card blocks (4) are respectively set in outer wall at left and right sides of bracket (3), and limit card block (4) is cylinder cylindricality block.
4. a kind of roller conveyor connection fuselage stacking bracket according to claim 1, it is characterised in that: the limit
The outer wall of two sides up and down of fixture block (4) is respectively provided with clamping groove, and spacing block set (2) is arranged close to one end of limit card block (4) outer wall
With the matched flexible clamping block of clamping groove.
5. a kind of roller conveyor connection fuselage stacking bracket according to claim 1, it is characterised in that: the stacking
Bracket (3) is I-shaped steelframe, and the inner wall of two sides up and down of fuselage (1) is respectively provided with and stacks bracket (3) matched I-shaped slot.
6. a kind of roller conveyor connection fuselage stacking bracket according to claim 1, it is characterised in that: the elasticity
Telescopic rod in fixture block (7) wraps up hollow tube, and motion bar is arranged in the inner cavity of hollow tube, and motion bar is in hollow tube inner cavity
Movable one end connects hollow tube by adjustable spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822189466.7U CN209275428U (en) | 2018-12-25 | 2018-12-25 | A kind of roller conveyor connection fuselage stacking bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822189466.7U CN209275428U (en) | 2018-12-25 | 2018-12-25 | A kind of roller conveyor connection fuselage stacking bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209275428U true CN209275428U (en) | 2019-08-20 |
Family
ID=67607146
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822189466.7U Expired - Fee Related CN209275428U (en) | 2018-12-25 | 2018-12-25 | A kind of roller conveyor connection fuselage stacking bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209275428U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110510101A (en) * | 2019-10-08 | 2019-11-29 | 漳州鹰航电子科技有限公司 | A kind of aircraft |
-
2018
- 2018-12-25 CN CN201822189466.7U patent/CN209275428U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110510101A (en) * | 2019-10-08 | 2019-11-29 | 漳州鹰航电子科技有限公司 | A kind of aircraft |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190820 Termination date: 20191225 |