CN202284057U - Tail roller of mine belt conveyer - Google Patents
Tail roller of mine belt conveyer Download PDFInfo
- Publication number
- CN202284057U CN202284057U CN2011204093191U CN201120409319U CN202284057U CN 202284057 U CN202284057 U CN 202284057U CN 2011204093191 U CN2011204093191 U CN 2011204093191U CN 201120409319 U CN201120409319 U CN 201120409319U CN 202284057 U CN202284057 U CN 202284057U
- Authority
- CN
- China
- Prior art keywords
- roller
- belt
- conny
- fine
- cylinder
- 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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- Structure Of Belt Conveyors (AREA)
Abstract
The utility model relates to a tail roller of a mine belt conveyer. An original used tail roller is in a cylindrical shape, fine conny can be adhered to a belt because of equipment cooling water during operation of the belt conveyer, a part of the fine conny can be adhered to the roller along with rotation of the roller when the belt passes through the roller, a cylinder is irregular after the fine conny is adhered to the roller, and belt deviation is led when the roller rotates. A plurality of key grooves are arranged on a roller plane of the tail roller, the tail roller of the mine belt conveyer keeps the cylindrical shape of the original roller unchanged, enables the roller plane to be transformed into a shape of key grooves, the middle is high, and two sides are low. When the roller rotates, the fine conny adhered to the belt is thrown out from two ends of the key grooves before the fine conny passes through the roller. The tail roller of the mine belt conveyer is simple in structure and low in cost.
Description
Technical field
The utility model relates to a kind of aircraft tail cylinder of belt conveyor in mine.
Background technology
Original use aircraft tail cylinder be one cylindrical; Belt feeder is in operation because the cause of component cooling water; Can be stained with the duff end on the belt, in that some can be bonded on the cylinder along with the cylinder rotation when the cylinder, it is last to be stained with duff on the cylinder; Cylinder is irregular, can cause belt deviation during rotation.
The utility model content
The technical matters that the utility model solved provides a kind of aircraft tail cylinder of simple in structure, the belt conveyor in mine of placing belt deviation.
For solving above-mentioned technical matters, the technical scheme that the utility model is taked:
A kind of aircraft tail cylinder of belt conveyor in mine, its special character is: on the cylinder plane of described aircraft tail cylinder several keyways are set.
The groove depth of several above-mentioned keyways is extended from the centre to both sides from high to low.
Compared with prior art, the utility model remains unchanged the cylindrical shape of original cylinder, transform the cylinder plane as the keyway shape; From the centre to both sides from high to low, cylinder is when rotating, when being bonded at the last process of the duff cylinder on the belt; Throw away from the keyway two ends, simple in structure, with low cost.
Description of drawings
Fig. 1 is the structural representation of the utility model.
Fig. 2 is that the A-A of Fig. 1 is to cutaway view.
The specific embodiment
Below in conjunction with the accompanying drawing and the specific embodiment the utility model is elaborated.
Referring to Fig. 1,2, the utility model is provided with several keyways 2 on the cylinder plane of aircraft tail cylinder 1.
The groove depth of several above-mentioned keyways 2 is extended from the centre to both sides from high to low.
Cylinder when being bonded at the last process of the duff cylinder on the belt, throws away from the keyway two ends when rotating.
Claims (2)
1. the aircraft tail cylinder of a belt conveyor in mine is characterized in that: several keyways (2) are set on the cylinder plane of described aircraft tail cylinder (1).
2. the aircraft tail cylinder of a kind of belt conveyor in mine according to claim 1, it is characterized in that: the groove depth of described several keyways (2) is extended from the centre to both sides from high to low.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011204093191U CN202284057U (en) | 2011-10-25 | 2011-10-25 | Tail roller of mine belt conveyer |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011204093191U CN202284057U (en) | 2011-10-25 | 2011-10-25 | Tail roller of mine belt conveyer |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202284057U true CN202284057U (en) | 2012-06-27 |
Family
ID=46295586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2011204093191U Expired - Fee Related CN202284057U (en) | 2011-10-25 | 2011-10-25 | Tail roller of mine belt conveyer |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN202284057U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103332449A (en) * | 2013-06-26 | 2013-10-02 | 新疆科立机械设备有限公司 | Cage-type drum |
CN107804674A (en) * | 2017-10-09 | 2018-03-16 | 阳泉煤业(集团)有限责任公司 | A kind of air intake lane belt holder tail wheel roller anti-sticking cash method |
-
2011
- 2011-10-25 CN CN2011204093191U patent/CN202284057U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103332449A (en) * | 2013-06-26 | 2013-10-02 | 新疆科立机械设备有限公司 | Cage-type drum |
CN103332449B (en) * | 2013-06-26 | 2015-10-28 | 新疆科立机械设备有限公司 | Cage drum |
CN107804674A (en) * | 2017-10-09 | 2018-03-16 | 阳泉煤业(集团)有限责任公司 | A kind of air intake lane belt holder tail wheel roller anti-sticking cash method |
CN107804674B (en) * | 2017-10-09 | 2023-09-05 | 阳泉煤业(集团)有限责任公司 | Gangue blocking prevention method for tail wheel roller of air inlet lane belt frame |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120627 Termination date: 20121025 |