CN207618414U - Belt feeder spiral adjustment type aircraft tail cylinder - Google Patents
Belt feeder spiral adjustment type aircraft tail cylinder Download PDFInfo
- Publication number
- CN207618414U CN207618414U CN201721568888.4U CN201721568888U CN207618414U CN 207618414 U CN207618414 U CN 207618414U CN 201721568888 U CN201721568888 U CN 201721568888U CN 207618414 U CN207618414 U CN 207618414U
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- China
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- fixed cell
- rolling stand
- aircraft tail
- tail cylinder
- belt feeder
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- 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.)
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Abstract
The utility model belt feeder spiral adjustment type aircraft tail cylinder, including：Tail holder；Rolling stand, the rolling stand are rotatably connected on by rack pin shaft on the tail holder；Aircraft tail cylinder, the aircraft tail cylinder are arranged in the rolling stand；Regulating mechanism, the regulating mechanism are arranged on the tail holder, and the regulating mechanism is connect with the rolling stand；The wherein described regulating mechanism includes：First fixed cell, first fixed cell are connect with the rolling stand；Second fixed cell, second fixed cell are arranged on the tail holder；The both ends of screw rod, the screw rod are separately connected first fixed cell and second fixed cell.The utility model belt feeder is easy to adjust, of simple structure and low cost with spiral adjustment type aircraft tail cylinder.
Description
Technical field
The utility model is related to a kind of belt feeder spiral adjustment type aircraft tail cylinders.
Background technology
At runtime, the main reason for adhesive tape sideslip frequent occurrence at aircraft tail cylinder, sideslip is in adhesive tape to belt feeder
Heart line and aircraft tail cylinder axis out of plumb.Therefore, the sideslip for correcting adhesive tape is by adjusting aircraft tail cylinder axis and adhesive tape center
Angle between line is realized.Common satisfactory after correcting is mainly at present：Aircraft tail cylinder axle bed bolt adjusting method；Hydraulic cylinder adjusts
Method etc..The former, adjustment is inconvenient, and latter configuration is complicated, and cost is higher.
Utility model content
To make up above-mentioned technological deficiency, the purpose of this utility model is to provide a kind of belts solving above-mentioned technical problem
Machine spiral adjustment type aircraft tail cylinder.
In order to solve the above technical problems, the utility model belt feeder spiral adjustment type aircraft tail cylinder, including：Tail branch
Frame；Rolling stand, the rolling stand are rotatably connected on by rack pin shaft on the tail holder；Aircraft tail cylinder, the machine
Stern barrel is arranged in the rolling stand；Regulating mechanism, the regulating mechanism are arranged on the tail holder, the adjusting
Mechanism is connect with the rolling stand；The wherein described regulating mechanism includes：First fixed cell, first fixed cell and institute
State rolling stand connection；Second fixed cell, second fixed cell are arranged on the tail holder；Screw rod, the spiral shell
The both ends of bar are separately connected first fixed cell and second fixed cell.
First fixed cell includes：First bearing, first bearing are connect with the rolling stand；First pin
Axis, first axis pin are arranged in first bearing, and first axis pin is connect with one end of the screw rod.
Second fixed cell includes：Second bearing, second bearing are arranged by the second axis pin in the tail
On holder；The other end of the screw rod is arranged in second bearing.
It is equipped with handle in the other end of the screw rod.
It is equipped with locknut in the outer sheath of the screw rod, the locknut is located at second bearing and the handle
Between.
The utility model belt feeder is easy to adjust, of simple structure and low cost with spiral adjustment type aircraft tail cylinder.
Description of the drawings
Fig. 1 is the utility model belt feeder spiral adjustment type aircraft tail cylinder structural schematic diagram.
The utility model belt feeder reference sign in spiral adjustment type aircraft tail cylinder attached drawing：
1- tail holder 2- rack pin shaft 3- rolling stands
4- aircraft tail cylinders 5- the first bearing the first axis pins of 6-
7- screw rods 8- the second bearing the second axis pins of 9-
10- locknut 11- handle 12- adhesive tapes
Specific implementation mode
The utility model belt feeder is described in further detail with spiral adjustment type aircraft tail cylinder below in conjunction with the accompanying drawings.
As shown in Figure 1, the utility model belt feeder spiral adjustment type aircraft tail cylinder, including tail holder 1, rack pin shaft
2, rolling stand 3, aircraft tail cylinder 4, the first bearing 5, the first axis pin 6, screw rod 7, the second bearing 8, the second axis pin 9, locknut
10, handle 11, adhesive tape 12 etc..
Tail holder 1 is steel construction piece, and on the basis of being fixedly mounted on, rolling stand 3 is steel construction piece, passes through rack pin shaft
2 are mounted on tail holder 1, and aircraft tail cylinder 4 is the component that can be rotated about the axis thereof, and is fixedly mounted on rolling stand 3, first
Bearing 5 is fixedly mounted on rolling stand 3, and the second bearing 8 is mounted on by the second axis pin 9 on tail holder 1, a left side for screw rod 7
Side one end is mounted on by the first axis pin 6 on the first bearing 5, and the other end and 11 fixed connection of handle, locknut 10 are mounted on
On screw rod 7, adhesive tape 12 is from the top of aircraft tail cylinder 4 around entering, laid out from lower part.
When deviation phenomenon occurs in adhesive tape 12, nut 10 is unclamped, rotational handle 11 simultaneously drives rolling stand 3 by screw rod 7
And its aircraft tail cylinder 4 is rotated around rack pin shaft, the angle in direction and rotation that handle 11 rotates is according to the sideslip direction of adhesive tape 12
Depending on sideslip degree, after adhesive tape 12 is returned to normal position, the handle 11 that stops operating tightens locknut 10.
The preferred embodiment that the utility model is created is illustrated, but the utility model is not limited to embodiment,
Those skilled in the art can also make various equivalent changes under the premise of without prejudice to the utility model creative spirit
Type or replacement, these equivalent modifications or replacement are all contained in scope of the present application.
Claims (5)
1. belt feeder spiral adjustment type aircraft tail cylinder, which is characterized in that including：
Tail holder；
Rolling stand, the rolling stand are rotatably connected on by rack pin shaft on the tail holder；
Aircraft tail cylinder, the aircraft tail cylinder are arranged in the rolling stand；
Regulating mechanism, the regulating mechanism are arranged on the tail holder, and the regulating mechanism is connect with the rolling stand；
Wherein
The regulating mechanism includes：
First fixed cell, first fixed cell are connect with the rolling stand；
Second fixed cell, second fixed cell are arranged on the tail holder；
The both ends of screw rod, the screw rod are separately connected first fixed cell and second fixed cell.
2. belt feeder according to claim 1 spiral adjustment type aircraft tail cylinder, which is characterized in that described first fixes list
Member includes：
First bearing, first bearing are connect with the rolling stand；
First axis pin, first axis pin are arranged in first bearing, and one end of first axis pin and the screw rod connects
It connects.
3. belt feeder according to claim 2 spiral adjustment type aircraft tail cylinder, which is characterized in that described second fixes list
Member includes：
Second bearing, second bearing are arranged by the second axis pin on the tail holder；
The other end of the screw rod is arranged in second bearing.
4. belt feeder according to claim 3 spiral adjustment type aircraft tail cylinder, which is characterized in that in the another of the screw rod
One end is equipped with handle.
5. belt feeder according to claim 4 spiral adjustment type aircraft tail cylinder, which is characterized in that in the outer of the screw rod
Side is arranged with locknut, and the locknut is between second bearing and the handle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721568888.4U CN207618414U (en) | 2017-11-21 | 2017-11-21 | Belt feeder spiral adjustment type aircraft tail cylinder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721568888.4U CN207618414U (en) | 2017-11-21 | 2017-11-21 | Belt feeder spiral adjustment type aircraft tail cylinder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207618414U true CN207618414U (en) | 2018-07-17 |
Family
ID=62829322
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721568888.4U Active CN207618414U (en) | 2017-11-21 | 2017-11-21 | Belt feeder spiral adjustment type aircraft tail cylinder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207618414U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112955389A (en) * | 2018-10-25 | 2021-06-11 | 埃博科瑞典有限责任公司 | Conveyor belt adjusting and tracking method and arrangement thereof |
-
2017
- 2017-11-21 CN CN201721568888.4U patent/CN207618414U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112955389A (en) * | 2018-10-25 | 2021-06-11 | 埃博科瑞典有限责任公司 | Conveyor belt adjusting and tracking method and arrangement thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190423 Address after: 242199 Langxi County Economic Development Zone, Xuancheng, Anhui Patentee after: Langxi Dongao Transport Equipment Technology Co., Ltd. Address before: No. 815 Huaqing Road, Qingpu District, Shanghai, 20107 Patentee before: Shanghai Keda Heavy Industry Group Co., Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200421 Address after: No. 29, Jinniu Middle Road, Langxi Economic Development Zone, Langxi County, Xuancheng City, Anhui Province Patentee after: Keda heavy industry group (Langxi) Co., Ltd Address before: 242199 Langxi Economic Development Zone, Anhui, Xuancheng Patentee before: LANGXI DONGAO TRANSPORTATION EQUIPMENT TECHNOLOGY Co.,Ltd. |