CN201459497U - Bearing type support device of strander - Google Patents
Bearing type support device of strander Download PDFInfo
- Publication number
- CN201459497U CN201459497U CN2009201254245U CN200920125424U CN201459497U CN 201459497 U CN201459497 U CN 201459497U CN 2009201254245 U CN2009201254245 U CN 2009201254245U CN 200920125424 U CN200920125424 U CN 200920125424U CN 201459497 U CN201459497 U CN 201459497U
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- CN
- China
- Prior art keywords
- bearing
- cylindrical shell
- strander
- cylinder body
- connector
- 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
The utility model relates to a bearing type support device of a strander, comprising a support seat and a cylinder body, wherein the cylinder body comprises a cylinder body a, a cylinder body b and a cylinder body c. The bearing type support device also comprises bearings and a bearing support seat, one end of the cylinder body a is connected with the support seat, the other end of the cylinder body c is connected with a tooth wheel by a connecting piece, the cylinder body a, the cylinder body b and the cylinder body c are connected by connecting pieces simultaneously, the bearings are connected with the connecting pieces, the inner circles of the bearings are fixed with the connecting pieces, and outer rings of the bearings are fixed with the bearing support seat. The bearing type support device of the strander adopts aircraft bearings, and the strander can reduce noise and frictional resistance, increase limit speed, run smoothly and improve production efficiency when being used.
Description
Technical field
The utility model relates to a kind of strander, particularly relates to a kind of strander bearing-type bracing or strutting arrangement.
Background technology
Being connected between the strander cylindrical shell that is used for making steel wire rope at present and the cylindrical shell all is to adopt plain bearing to connect, when rope is closed in the cylindrical shell rotation, the shaft strength that is used for bearing turning effort is very big, but because the plain bearing quality of fit is not very high, process middle (center) bearing in rotation is easy to and will generates heat, even damage, when rotary speed is too fast, whole Bunching machine also can acutely be shaken, send very big noise, because the connection request between cylindrical shell and the cylindrical shell has certain concentricity, the bearing replacing that weares and teares is also needed the expensive time simultaneously, greatly reduce the production efficiency of steel wire rope.
The utility model content
Technical problem to be solved in the utility model is: improve strander production efficiency, reduce noise, increase bearing service time, thereby a kind of strander bearing-type bracing or strutting arrangement is provided.
For solving the problems of the technologies described above following technical proposals that the utility model adopts:
Strander bearing-type bracing or strutting arrangement mainly comprises bearing, cylindrical shell.Its middle cylinder body is combined by cylindrical shell a, cylindrical shell b and cylindrical shell c; This device also comprises bearing and bearing support block, the end of cylindrical shell a is connected with bearing, the other end of cylindrical shell c is connected with the flute profile wheel by connector, also connect between cylindrical shell a, b, the c simultaneously by connector, and on each connector, all be connected with bearing, bearing cone and connector are fixed, and the outer shroud and the bearing support block of bearing are fixed.
The bearing that is adopted is the standard aircraft bearing.
Adopt the beneficial effect of technique scheme to be:
The utility model changes the standard aircraft bearing that acts on space flight and aviation by having cylindrical shell now with the plain bearing that is connected between the cylindrical shell, the employing aviation grease is lubricated, and plate washer is installed at the aircraft bearing two ends, because of the standard aircraft bearing has the precision height, advantage such as wear-resistant, not only can improve the rotating speed of Bunching machine cylindrical shell greatly, make rotating speed can reach 1800rpm, and frictional resistance is little, operate steadily, greatly reduce the noise of working environment, aviation grease that adopts and cover plate can play the effect of preventing dust and increasing service life, have improved the efficient of Wire Rope Production greatly.Therefore the utlity model has the excellent popularization value and use value.
Description of drawings
Fig. 1 is a strander bearing-type support device structure schematic diagram of the present utility model.
Fig. 2 is the structural representation of strander bearing-type bracing or strutting arrangement middle (center) bearing of the present utility model and bearing support block.
Among the figure: 1-bearing, 2-cylindrical shell, 2-1-cylindrical shell a, 2-2-cylindrical shell b, 2-n-cylindrical shell c, 3-bearing, 4-bearing support block, 5-connector, 6-flute profile wheel, 7-bearing cap, 8-steel wire rope cable-through hole.
The specific embodiment
As shown in Figure 1, strander bearing-type bracing or strutting arrangement comprises bearing 1 cylindrical shell 2, bearing 3 and bearing support block 4, bearing 3 adopts the standard aircraft bearing, and it is blue that basket is housed in the cylindrical shell 2, places the I-beam wheel that is wound with steel wire in basket is blue, the length of cylindrical shell 2 is decided according to the steel wire rope number of share of stock of being pooled capital, long more because of cylindrical shell 2 making, difficulty of processing is just big more, and processing charges is just high more, therefore the cylindrical shell of existing Bunching machine is spliced by more piece cylindrical shell 2, and 2 of cylindrical shells are made up of cylindrical shell a2-1, cylindrical shell b2-2 and cylindrical shell c2-n; The end of cylindrical shell a2-1 is connected with bearing 1, cylindrical shell a2-1, adopt connector 5 to connect between cylindrical shell b2-2 and the cylindrical shell c2-n, on connector 5, be connected with bearing 3, the other end of cylindrical shell c2-n is connected with flute profile wheel 6 by connector 5 simultaneously, gear shaft 6 links to each other with motor by the flute profile band, on the connector 5 that connects cylindrical shell c2-n and flute profile wheel 6, also be connected with bearing 3, and the interior ring of bearing 3 and connector 5 are fixing, the outer shroud of bearing 3 and bearing support block 4 are fixing, simultaneously for preventing that dust from entering in the bearing 3, on bearing 3 both sides bearing cap 7 is installed, bearing cap 7 links to each other with bearing support block 4. and can be adjacent to cylindrical shell 2 rotations for making the blue steel wire that passes of basket from the cylindrical shell 2, on connector 5, offer steel wire rope cable-through hole 8.
As shown in Figure 2, at bearing 3 two ends bearing cap 7 is installed, bearing cap 7 is connected with bearing support block 4.
Claims (4)
1. strander bearing-type bracing or strutting arrangement comprises bearing (1), cylindrical shell (2), it is characterized in that: cylindrical shell (2) is combined by cylindrical shell a (2-1), cylindrical shell b (2-2) and cylindrical shell c (2-n); This device also comprises bearing (3) and bearing support block (4); The end of cylindrical shell a (2-1) is connected with bearing (1), the other end of cylindrical shell c (2-n) is connected with flute profile wheel (6) by connector (5), also connect between cylindrical shell a (2-1), cylindrical shell b (2-2) and the cylindrical shell c (2-n) simultaneously by connector (5), and on each connector (5), all be connected with bearing (3), and bearing (3) inner ring and connector (5) are fixing, and the outer shroud of bearing (3) and bearing support block (4) are fixing.
2. strander bearing-type bracing or strutting arrangement according to claim 1 is characterized in that: described bearing (3) is the standard aircraft bearing.
3. strander bearing-type bracing or strutting arrangement according to claim 1 and 2; It is characterized in that: at bearing (3) two ends bearing cap (7) is installed, bearing cap (7) is connected with bearing support block (4).
4. strander bearing-type bracing or strutting arrangement according to claim 1; It is characterized in that: on described connector (5), offer steel wire rope cable-through hole (8).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009201254245U CN201459497U (en) | 2009-05-27 | 2009-05-27 | Bearing type support device of strander |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009201254245U CN201459497U (en) | 2009-05-27 | 2009-05-27 | Bearing type support device of strander |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201459497U true CN201459497U (en) | 2010-05-12 |
Family
ID=42386851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2009201254245U Expired - Fee Related CN201459497U (en) | 2009-05-27 | 2009-05-27 | Bearing type support device of strander |
Country Status (1)
Country | Link |
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CN (1) | CN201459497U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102297205A (en) * | 2011-07-13 | 2011-12-28 | 宁波凯特机械有限公司 | Bearing pedestal device of wirerope strander for circulatory lubrication of pulsed liquid fat |
-
2009
- 2009-05-27 CN CN2009201254245U patent/CN201459497U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102297205A (en) * | 2011-07-13 | 2011-12-28 | 宁波凯特机械有限公司 | Bearing pedestal device of wirerope strander for circulatory lubrication of pulsed liquid fat |
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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: 20100512 Termination date: 20100527 |