CN204508072U - The anti-lateral deviation base of extendable conveyor - Google Patents
The anti-lateral deviation base of extendable conveyor Download PDFInfo
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- CN204508072U CN204508072U CN201520062345.XU CN201520062345U CN204508072U CN 204508072 U CN204508072 U CN 204508072U CN 201520062345 U CN201520062345 U CN 201520062345U CN 204508072 U CN204508072 U CN 204508072U
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- fuselage
- track adjusting
- lifting guiding
- adjusting wheel
- hydraulic pressure
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- 230000000630 rising effect Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 abstract description 2
- 230000002262 irrigation Effects 0.000 abstract 1
- 238000003973 irrigation Methods 0.000 abstract 1
- 230000001681 protective effect Effects 0.000 description 7
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
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Abstract
The utility model discloses the anti-lateral deviation base of a kind of extendable conveyor, drip irrigation device is: comprise afer bay and be arranged at the hydraulic pressure frame in afer bay front, fuselage and afer bay are rotationally connected, hydraulic pressure frame is hinged with hydraulic actuating cylinder, piston rod and the fuselage of hydraulic actuating cylinder are hinged, hydraulic pressure frame is fixed with lifting guiding frame, lifting guiding frame is two two ends being symmetricly set in fuselage, lifting guiding frame is rotated and is provided with the track adjusting wheel abutted all the time with fuselage outer wall, the utility model is applicable to be provided with the track adjusting wheel that can abut with fuselage side wall all the time by rotating in hydraulic pressure frame, and track adjusting wheel is arranged on the two ends of fuselage, fuselage can be clipped between two lifting guiding frames, and because track adjusting wheel abuts with fuselage side wall all the time, can prevent fuselage from rising or decline process, sidesway occurring by actv., improve service life and the reliability of equipment.
Description
Technical field
The utility model relates to a kind of transmission apparatus field, and more particularly, it relates to the anti-lateral deviation lifting pedestal of a kind of extendable conveyor.
Background technology
Extendable conveyor is a kind of novel, professional loading-unloading vehicle equipment; hydraulic lifting, Moving caster etc. can be equipped with operate; it is a kind of automatic material flow transportation device of the very hommization that operates; be mainly used in the industries such as logistics express delivery; be particularly suitable for shipping occasion on a small scale, also can be applied to the handling goods etc. of factory's platform.
The base of current existing extendable conveyor, mainly comprise support portion and drive division, support portion comprises afer bay, the bottom of fuselage is provided with rotating shaft, afer bay is provided with the bearing coordinated with rotating shaft, the lower rotation of fuselage is arranged on afer bay, drive division comprises hydraulic pressure frame, hydraulic pressure frame bottom-hinged has hydraulic actuating cylinder, piston rod and the fuselage side wall of hydraulic actuating cylinder are hinged, stretching out and regaining by the piston rod of hydraulic actuating cylinder, rising or the decline of fuselage can be realized, but in actual motion, because the length of fuselage is longer, cause the volume of fuselage excessive, when Driven by Hydraulic Cylinder fuselage does and rotates up and down, because body volume is excessive, and base is not arranged again the inhibiting device of restriction fuselage sidesway, fuselage is caused easily along rotating shaft, left and right skew to occur, if things go on like this, the rotating shaft of fuselage is easily caused to be damaged, fuselage is come off from afer bay, reduce service life and the reliability of whole extendable conveyor.
Utility model content
For the deficiency that prior art exists, the purpose of this utility model is to provide a kind of anti-lateral deviation base of retractable vehicle that can prevent expansion box from sidesway occurring when rotating.
For achieving the above object, the utility model adopts following technical scheme, the anti-lateral deviation base of a kind of extendable conveyor, comprise afer bay and be arranged at the hydraulic pressure frame in afer bay front, fuselage and afer bay are rotationally connected, hydraulic pressure frame is hinged with hydraulic actuating cylinder, piston rod and the fuselage of hydraulic actuating cylinder are hinged, described hydraulic pressure frame is fixed with lifting guiding frame, described lifting guiding frame is two and is symmetricly set in the both sides of fuselage, two described lifting guiding frames is all rotated and is provided with the track adjusting wheel abutted all the time with fuselage outer wall.
Preferably, described lifting guiding frame is provided with chute perpendicular to fuselage side wall, in described chute, slippage is connected with guide wheel shaft, and described guide wheel shaft and track adjusting wheel are rotationally connected, and described lifting guiding frame is provided with the compacting part driving track adjusting wheel to abut with fuselage outer wall all the time.
Preferably, described compacting part comprises the bolt abutted with guide wheel shaft, and described screws is arranged in lifting guiding frame.
Preferably, self-lubricating bearing is provided with in described track adjusting wheel.
Preferably, described bolt is provided with operating portion away from one end of guide wheel shaft.
The utility model hinge structure is compared to be had: be provided with the track adjusting wheel that can abut with fuselage side wall all the time by rotating in hydraulic pressure frame, and track adjusting wheel is arranged on the two ends of fuselage, fuselage can be clipped between two lifting guiding frames, and because track adjusting wheel abuts with fuselage side wall all the time, can prevent fuselage from rising or decline process, sidesway occurring by actv., improve service life and the reliability of equipment.
Accompanying drawing explanation
Fig. 1 is the assembled view of the utility model extendable conveyor anti-lateral deviation base embodiment;
Fig. 2 is the driving direct organization schematic diagram of the utility model extendable conveyor anti-lateral deviation base embodiment.
Fig. 3 is A portion enlarged drawing in Fig. 2;
Fig. 4 is the cutaway view Amplified image in A portion in Fig. 2;
Fig. 5 is the track adjusting wheel cutaway view of the utility model extendable conveyor anti-lateral deviation base embodiment.
In figure: 1, afer bay; 2, hydraulic pressure frame; 21, lifting guiding frame; 211, protective cover; 2111, chute; 3, track adjusting wheel; 31, encapsulate; 4, guide wheel shaft; 41, square; 5, bolt; 51, control lever; 6, fuselage; 61, rotating shaft; 7, hydraulic actuating cylinder; 71, piston rod.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model extendable conveyor anti-lateral deviation base embodiment is described further.
The anti-lateral deviation base of a kind of extendable conveyor, comprise afer bay 1 and be arranged at the hydraulic pressure frame 2 in afer bay 1 front, afer bay 1 and hydraulic pressure frame 2 shape of cross section are U-shaped, the bottom surface of afer bay 1 and hydraulic pressure frame 2 is fixedly installed on ground, fuselage 6 and afer bay 1 are rotationally connected, sidewall bottom fuselage 6 is provided with rotating shaft 61, in order to make the rotation of fuselage 6 more flexible, afer bay 1 is provided with the bearing coordinated with the rotating shaft 61 of fuselage 6, hydraulic pressure frame 2 is hinged with hydraulic actuating cylinder 7, the piston rod 71 of hydraulic actuating cylinder 7 is hinged with fuselage 6, the sidewall of fuselage 6 is provided with jointed shaft, piston rod 71 is hinged with jointed shaft, stretching out and regaining by the piston rod 71 of hydraulic actuating cylinder 7, rising or the decline of fuselage 6 can be realized, lateral slip is there is when rising or decline in order to prevent fuselage 6, hydraulic pressure frame 2 is fixed with lifting guiding frame 21, lifting guiding frame 21 is two two ends being symmetricly set in fuselage 6, fuselage 6 is clipped between lifting guiding frame 21, lifting guiding frame 21 is rotated and is provided with the track adjusting wheel 3 abutted all the time with fuselage 6 outer wall, track adjusting wheel 3 in two lifting guiding frames 21, fuselage 6 is clipped in the middle, fuselage 6 can be limited lateral slip occurs.
Lifting guiding frame 21 is integrally formed with protective cover 211, track adjusting wheel 3 is arranged in protective cover 211, protective cover 211 is provided with chute 2111 perpendicular to fuselage 6 sidewall, in chute 2111, slippage is connected with guide wheel shaft 4, guide wheel shaft 4 and track adjusting wheel 3 are rotationally connected, be arranged in track adjusting wheel 3 to make the better rotation of guide wheel shaft 4, self-lubricating bearing is provided with in track adjusting wheel 3, the inner ring of self-lubricating bearing to be set on guide wheel shaft 4 and to coordinate with guide wheel shaft 4, the two ends of guide wheel shaft 4 are provided with square 41, square 41 slippage is arranged in chute 2111, lifting guiding frame 21 is provided with the compacting part driving track adjusting wheel 3 to abut with fuselage 6 outer wall all the time, lifting guiding frame 21 end is provided with compacting part and comprises the bolt 5 abutted with guide wheel shaft 4, bolt 5 rotates and is arranged on protective cover 211, one end of bolt 5 is stretched into protective cover 211 and is abutted with square 41, the other end stretches out protective cover 211, use is rotating bolt 5, projection can be pushed away forward, track adjusting wheel 3 is driven to abut with fuselage 6 sidewall all the time, because in use, track adjusting wheel 3 can be worn and torn, now just need the position with overregulate bolt 5, track adjusting wheel 3 is driven to abut the compression effect ensureing track adjusting wheel 3 all the time with the sidewall of fuselage 6, fuselage 6 is clipped in the middle by track adjusting wheel 3, can prevent fuselage 6 from when rotating, lateral deviation occurring by actv., and then prevent the rotating shaft 61 on fuselage 6 to be damaged, extend service life and the reliability of equipment.
In addition, conveniently rotating bolt 5, be provided with operating portion at bolt 5 away from one end of guide wheel shaft 4, operating portion comprises the control lever 51 perpendicular to bolt 5, during rotation, by control lever 51, rotating bolt 5 that can be convenient.
Finally, in order to reduce the wearing and tearing of track adjusting wheel 3 pairs of fuselage 6 outside faces, track adjusting wheel 3 outside face is coated with one deck encapsulate 31, arranges encapsulate 31, not only can relax impact, and can reduce wearing and tearing, extends service life and the maintenance cycle of equipment.
Below be only preferred implementation of the present utility model; protection domain of the present utility model is also not only confined to above-described embodiment; all technical schemes belonged under the utility model thinking all belong to protection domain of the present utility model; should be understood that; for those skilled in the art; do not departing from the some improvements and modifications under the utility model principle prerequisite, these improvements and modifications also should be considered as protection domain of the present utility model.
Claims (5)
1. the anti-lateral deviation base of extendable conveyor, comprise afer bay and be arranged at the hydraulic pressure frame in afer bay front, described afer bay and hydraulic pressure frame are all fixedly installed on ground, fuselage and afer bay are rotationally connected, hydraulic pressure frame is hinged with hydraulic actuating cylinder, piston rod and the fuselage of hydraulic actuating cylinder are hinged, it is characterized in that: described hydraulic pressure frame is fixed with lifting guiding frame, described lifting guiding frame is two and is symmetricly set in the both sides of fuselage, two described lifting guiding frames is all rotated and is provided with the track adjusting wheel abutted all the time with fuselage outer wall.
2. the anti-lateral deviation base of extendable conveyor according to claim 1, it is characterized in that: described lifting guiding frame is provided with chute perpendicular to fuselage side wall, in described chute, slippage is connected with guide wheel shaft, described guide wheel shaft and track adjusting wheel are rotationally connected, and described lifting guiding frame is provided with the compacting part driving track adjusting wheel to abut with fuselage outer wall all the time.
3. the anti-lateral deviation base of extendable conveyor according to claim 2, is characterized in that: described compacting part comprises the bolt abutted with guide wheel shaft, and described screws is arranged in lifting guiding frame.
4. the anti-lateral deviation base of the extendable conveyor according to Claims 2 or 3, is characterized in that: be provided with self-lubricating bearing in described track adjusting wheel.
5. the anti-lateral deviation base of extendable conveyor according to claim 3, is characterized in that: described bolt is provided with operating portion away from one end of guide wheel shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520062345.XU CN204508072U (en) | 2015-01-29 | 2015-01-29 | The anti-lateral deviation base of extendable conveyor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520062345.XU CN204508072U (en) | 2015-01-29 | 2015-01-29 | The anti-lateral deviation base of extendable conveyor |
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| Publication Number | Publication Date |
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| CN204508072U true CN204508072U (en) | 2015-07-29 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520062345.XU Active CN204508072U (en) | 2015-01-29 | 2015-01-29 | The anti-lateral deviation base of extendable conveyor |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107758377A (en) * | 2016-08-18 | 2018-03-06 | 安得智联科技股份有限公司 | For the flexible truck-loading facilities of the railway carriage or compartment car without railway platform place |
-
2015
- 2015-01-29 CN CN201520062345.XU patent/CN204508072U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107758377A (en) * | 2016-08-18 | 2018-03-06 | 安得智联科技股份有限公司 | For the flexible truck-loading facilities of the railway carriage or compartment car without railway platform place |
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| Date | Code | Title | Description |
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| 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: 215000 No.288, xujiagang Road, Linhu Town, Wuzhong District, Suzhou City, Jiangsu Province Patentee after: Suzhou Shuangqi Automation Equipment Co.,Ltd. Country or region after: China Address before: No. 1189 Ping'an Road, Linhu Town, Wuzhong District, Suzhou City, Jiangsu Province, 215100 Patentee before: SUZHOU SHUANGQI AUTOMATION EQUIPMENT Co.,Ltd. Country or region before: China |