CN106151277A - A kind of large axle bush - Google Patents
A kind of large axle bush Download PDFInfo
- Publication number
- CN106151277A CN106151277A CN201610690643.2A CN201610690643A CN106151277A CN 106151277 A CN106151277 A CN 106151277A CN 201610690643 A CN201610690643 A CN 201610690643A CN 106151277 A CN106151277 A CN 106151277A
- Authority
- CN
- China
- Prior art keywords
- copper alloy
- alloy face
- steel back
- correct
- steel
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/08—Attachment of brasses, bushes or linings to the bearing housing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/046—Brasses; Bushes; Linings divided or split, e.g. half-bearings or rolled sleeves
Abstract
The invention belongs to mechanical manufacturing field, particularly to a kind of large axle bush for cane milling or mining machinery etc., it is characterized in that: include copper alloy face and the steel back of the body, described copper alloy face and the steel back of the body are to use by centrifugal casting apparatus one piece casting, the composition surface of described copper alloy face and the steel back of the body is provided with the staggered band Z-Correct bump mapping Z-correct structure embedded that cooperates, having good product quality, intensity is high;Durability is high, uses the features such as wide adaptability.
Description
Technical field
The invention belongs to mechanical manufacturing field, particularly to a kind of big profile shaft for cane milling or mining machinery etc.
Watt.
Background technology
Bearing is used to the mechanical organ supporting axial workpiece and making loading end catch cropping relatively slide, also referred to as sliding bearing
(Sliding Bearing), sliding bearing stable working, reliable, noiseless, it as key foundation parts at lathe, electricity
Extensive application on motivation, electromotor and internal combustion engine, especially large-scale at cane milling, rolling machinery and mining machinery etc.
In plant equipment, the parts of employing are the relatively large parts of ratio, under the conditions of hydrodynamic lubrication, and the part that axle is supported by bearing
Being referred to as axle journal, the part matched with axle journal is referred to as bearing shell, so for large-scale bearing shell, the quality of its performance directly affects
The speed of equipment, bearing capacity, functional reliability and service life.The structure of traditional large size bearing is to use stationary metal
Mould or the form of sand casting copper alloy body, later, people, in order to save the copper alloy of costliness, have invented copper alloy and steel backing run
The structure connect, further also invented and is made up of matrix and the antifriction layer be located on matrix, wherein, matrix by steel back layer and
The basal layer composition of the copper alloy being located on steel back layer, and antifriction layer typically uses Amounts of Lead, Tin Copper ternary alloy coating.But slicker solder
Copper ternary alloy coating is poor with basal layer adhesion, and fatigue resistance is low, can only achieve 100~about 140MPa.Make for a long time
With, Amounts of Lead, Tin Copper ternary alloy coating element is easily diffused into basal layer, causes this Amounts of Lead, Tin Copper ternary alloy coating composition transfer, but its
Low strength, affects bearing shell bearing capacity, and this problem annoyings the development of bearing shell industry for a long time, for this deficiency, at present
The more way is used to be: by certain method, bronze acieral to be compounded in steel substrate formation steel back aluminium bimetallic
Composite plate, to make up acieral intensity and the shortcoming of hardness deficiency, then, is cast into this steel back aluminium ply-metal
Tiles face is also welded into, then the machining carrying out bearing shell shapes.The method can well make up acieral intensity and hardness not
The shortcoming of foot, but, the method exists that follow-up machining is difficult and whole bearing shell manufacturing process complicated, high in cost of production, especially
The large axle bush that to be steel back layer be welded to each other with copper alloy layer.Therefore break through the manufacturing process technology of large axle bush, be one
Individual technical barrier urgently to be resolved hurrily.
Summary of the invention
It is an object of the invention to provide one, to have processing technique simple, rational in infrastructure, the large axle bush that durability is high.
The object of the present invention is achieved like this:
The large axle bush of the present invention, it is characterised in that: include that copper alloy face and the steel back of the body, described copper alloy face and the steel back of the body are overall knots
Configuration formula, the composition surface of described copper alloy face and the steel back of the body is provided with the staggered band Z-Correct bump mapping Z-correct structure embedded that cooperates.
The above overall structure form is to use centrifugal casting apparatus one piece casting or by being carried on the back and copper alloy by steel
Integral solder after the embedding of face.
The above band Z-Correct bump mapping Z-correct structure 3 is that the composition surface carried on the back in copper alloy face and steel is provided with at least two phase interworkings
Close the staggered fin embedded and groove with matching.
The above band Z-Correct bump mapping Z-correct structure is to be provided with at least two rows' projection or shrinkage pools on the inner surface of copper alloy face 1, with
And the steel outer surface that coordinates with copper alloy face of the back of the body is provided with corresponding cooperation and interlocks the shrinkage pool embedded and projection.
The shape of the above fin and groove is rectangle, arc, rhombus, swallow-tail form or other arbitrary shapes.
The large axle bush of the present invention provides the benefit that:
1. good product quality, intensity is high.Owing to the present invention uses the composition surface of copper alloy face and the steel back of the body to be provided with the friendship that cooperates
The wrong fin embedded and groove with matching or the projection of band Z-Correct bump mapping Z-correct structure or shrinkage pool, copper alloy face and steel back of the body phase
Snap tight against mutually, so, owing to using centrifugal casting technique, under centrifugal action, metallographic structure is tight, simultaneously because centrifugal
Power effect, does not haves tissue looseness's defect, substantially increases the adhesion strength of bearing alloy and the steel back of the body, eliminates bearing shell steel
The internal stress of dorsal body setae base, improves the fatigue strength of bearing shell.
2. durability is high, uses wide adaptability.The present invention is to use the steel back of the body to cooperate staggered embedded with copper alloy face
Band Z-Correct bump mapping Z-correct structure, be not only suitable for being cast as integrated artistic, be also suitable for by steel the back of the body and copper alloy face embed after Welder
Skill, copper alloy face is engaged closely with the steel back of the body, substantially increases the service life of bearing shell, also improve the durability of bearing shell, and make
The technique made is simply easy, and this bearing shell not only can be widely applied on lathe, motor, electromotor and internal combustion engine, the suitableeest
Conjunction is applied on the heavy mechanical equipments such as cane milling, rolling machinery and mining machinery.
Accompanying drawing explanation
Fig. 1 is the main TV structure simplified schematic diagram of bearing embodiment 1 of the present invention.
Fig. 2 is the plan structure simplified schematic diagram of Fig. 1.
Fig. 3 is the A-A sectional structure simplified schematic diagram of Fig. 1.
Fig. 4 is the main TV structure simplified schematic diagram in embodiment 1 copper alloy face 1.
Fig. 5 is the plan structure simplified schematic diagram of Fig. 4.
Fig. 6 be Fig. 4 look up structural representation sketch.
Fig. 7 is the B-B sectional structure simplified schematic diagram of Fig. 4.
Fig. 8 is the main TV structure simplified schematic diagram of the steel back of the body 2.
Fig. 9 is the plan structure simplified schematic diagram of Fig. 8.
Figure 10 is the C-C sectional structure simplified schematic diagram of Fig. 8.
Figure 11 is the main TV structure simplified schematic diagram of bearing embodiment 2.
Figure 12 is the plan structure simplified schematic diagram of Figure 11.
Figure 13 is the D-D sectional structure simplified schematic diagram of Figure 11.
Figure 14 is the main TV structure simplified schematic diagram in embodiment 2 copper alloy face 1.
Figure 15 is the plan structure simplified schematic diagram of Figure 14.
Figure 16 be Figure 14 look up structural representation sketch.
Figure 17 is the E-E sectional structure simplified schematic diagram of Figure 14.
Figure 18 is the main TV structure simplified schematic diagram of the steel back of the body 2.
Figure 19 is the plan structure simplified schematic diagram of Figure 18.
Figure 20 is the F-F sectional structure simplified schematic diagram of Figure 18.
Figure 21 is the main TV structure simplified schematic diagram of embodiment 3.
Figure 22 is the main TV structure simplified schematic diagram of embodiment 4.
Component names and sequence number in figure:
Copper alloy face 1, the steel back of the body 2, Z-Correct bump mapping Z-correct structure 3, copper alloy face dovetail tangs 3-1, the steel back of the body dovetail groove 3-2, copper alloy
The protruding 3-5 of face projection 3-3, copper alloy face groove 3-4, the steel back of the body, steel back of the body groove 3-6.
Detailed description of the invention
The structure of the present invention is described below in conjunction with accompanying drawing and embodiment.
The large axle bush of the present invention, carries on the back 2 including copper alloy face 1 and steel, and described copper alloy face 1 and the steel back of the body 2 are overall structures
Form, described overall structure form is that employing centrifugal casting apparatus is cast into overall structure form or employing is welded as overall knot
Configuration formula, the composition surface of described copper alloy face 1 and the steel back of the body 2 is provided with the staggered band Z-Correct bump mapping Z-correct structure 3 embedded that cooperates.
As shown in Fig. 1~Figure 13, described band Z-Correct bump mapping Z-correct structure 3 is that the composition surface in copper alloy face 1 and the steel back of the body 2 is provided with
Article at least two, cooperate the staggered fin embedded and groove with matching, and the shape of described fin and groove is rectangular
Shape, arc, rhombus, swallow-tail form or other arbitrary shapes.
As shown in Figure 17~Figure 20, described band Z-Correct bump mapping Z-correct structure 3 is to be provided with at least two rows on the inner surface of copper alloy face 1
Protruding or shrinkage pool, and the outer surfaces that coordinate with copper alloy face 1 of the steel back of the body 2 be provided with corresponding cooperation interlock embedding shrinkage pool and
Protruding.
Embodiment 1
As shown in Fig. 1~Figure 13, the large axle bush of the present invention, carry on the back 2 including copper alloy face 1 and steel, described copper alloy face 1 and the steel back of the body
2 is to use by centrifugal casting apparatus one piece casting, and the composition surface of described copper alloy face 1 and the steel back of the body 2 is provided with the friendship that cooperates
Wrong band Z-Correct bump mapping Z-correct structure 3(embedded is referring to accompanying drawing 1~Fig. 3), described Z-Correct bump mapping Z-correct structure 3 is the interior table in copper alloy face 1
Face is provided with copper alloy face dovetail tangs 3-1(of three strips such as swallow-tail form referring to accompanying drawing 4~Fig. 7), at the steel back of the body 2 and copper alloy
The staggered steel the embedded back of the body dovetail groove that cooperates of three strips such as swallow-tail form it also is provided with accordingly on the outer surface that face 1 coordinates
3-2(is referring to accompanying drawing 8~Figure 10).
Embodiment 2
As shown in Figure 11~Figure 20, the large axle bush of the present invention, carry on the back 2 including copper alloy face 1 and steel, described copper alloy face 1 and steel
The back of the body 2 is by centrifugal casting apparatus one piece casting, the composition surface of described copper alloy face 1 and the steel back of the body 2 be provided with cooperate staggered
Band Z-Correct bump mapping Z-correct structure 3(embedded is referring to accompanying drawing 11~Figure 13), described Z-Correct bump mapping Z-correct structure 3 is at copper alloy face 1 inner surface
It is provided with copper alloy face projection 3-3 of six row's shape semicircles and copper alloy face shrinkage pool 3-4(referring to accompanying drawing 14~Figure 17);Carry on the back at steel
Shrinkage pool 3-6 and the protruding 3-of the steel back of the body carried on the back by 2 be provided with the cooperate staggered steel that embed corresponding with on the outer surface that copper alloy face 1 coordinates
5(is referring to accompanying drawing 18~Figure 20).That is copper alloy face projection 3-3 cooperates to interlock with steel back of the body shrinkage pool 3-6 and embeds;Copper closes
Gold face shrinkage pool 3-4 3-5 protruding with the steel back of the body cooperates to interlock and embeds.
Embodiment 3
As shown in figure 21, the large axle bush of the present invention, carry on the back 2 including copper alloy face 1 and steel, described copper alloy face 1 and the steel back of the body 2 are to adopt
By the overall structure form being welded as a whole, the composition surface of described copper alloy face 1 and the steel back of the body 2 is provided with staggered embedding that cooperate
Band Z-Correct bump mapping Z-correct structure 3, described Z-Correct bump mapping Z-correct structure 3 is to be provided with five strips such as rectangle on the inner surface in copper alloy face 1
Copper alloy face dovetail tangs 3-1, corresponding also be provided with five strips such as at the steel back of the body 2 on the outer surface of copper alloy face 1 cooperation
The staggered steel the embedded back of the body dovetail groove 3-2 that cooperates of rectangle.
Embodiment 4
As shown in figure 22, the large axle bush of the present invention, carry on the back 2 including copper alloy face 1 and steel, described copper alloy face 1 and the steel back of the body 2 are logical
Crossing centrifugal casting apparatus one piece casting, the composition surface of described copper alloy face 1 and the steel back of the body 2 is provided with the staggered band embedded that cooperates
Z-Correct bump mapping Z-correct structure 3, described Z-Correct bump mapping Z-correct structure 3 is to be provided with the copper alloy of seven row's shape semicircles on the inner surface of copper alloy face 1
Face projection 3-3 and copper alloy face shrinkage pool 3-4;On the outer surface that the steel back of the body 2 coordinates with copper alloy face 1, corresponding being provided with cooperates
The staggered protruding 3-5 of the steel back of the body embedded and steel back of the body shrinkage pool 3-6.The most often row copper alloy face projection 3-3 carries on the back shrinkage pool 3-6 with steel
Cooperate staggered embedding;Respectively each copper alloy face shrinkage pool 3-4 of row 3-5 protruding with the steel back of the body cooperates to interlock and embeds.
Claims (5)
1. a large axle bush, it is characterised in that: include copper alloy face (1) and the steel back of the body (2), described copper alloy face (1) and the steel back of the body
(2) being overall structure form, the composition surface of described copper alloy face (1) and the steel back of the body (2) is provided with the staggered band embedded that cooperates
Z-Correct bump mapping Z-correct structure (3).
Large axle bush the most according to claim 1, it is characterised in that: described overall structure form is to use centrifugal casting apparatus
One piece casting or by by steel the back of the body and copper alloy face embed after integral solder.
Large axle bush the most according to claim 1, it is characterised in that: described band Z-Correct bump mapping Z-correct structure (3) is in copper alloy face
And the composition surface of the steel back of the body (2) is provided with at least two the cooperate staggered fins embedded and grooves with matching (1).
Large axle bush the most according to claim 1, it is characterised in that: described band Z-Correct bump mapping Z-correct structure (3) is in copper alloy face
(1) inner surface is provided with at least two rows' projection or shrinkage pools, and the outer surface that the steel back of the body (2) coordinates with copper alloy face (1) is provided with
Corresponding cooperation interlocks the shrinkage pool embedded with protruding.
Large axle bush the most according to claim 3, it is characterised in that: the shape of described fin and groove be rectangle, arc,
Rhombus, swallow-tail form or other arbitrary shapes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610690643.2A CN106151277A (en) | 2016-08-20 | 2016-08-20 | A kind of large axle bush |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610690643.2A CN106151277A (en) | 2016-08-20 | 2016-08-20 | A kind of large axle bush |
Publications (1)
Publication Number | Publication Date |
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CN106151277A true CN106151277A (en) | 2016-11-23 |
Family
ID=57331296
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201610690643.2A Pending CN106151277A (en) | 2016-08-20 | 2016-08-20 | A kind of large axle bush |
Country Status (1)
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CN (1) | CN106151277A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108730332A (en) * | 2017-04-15 | 2018-11-02 | 广西隆盛双金属铜合金制造有限公司 | A kind of large size bearing and its pressure casting method |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB172719A (en) * | 1920-09-10 | 1921-12-12 | Howard Pneumatic Engineering C | Improvements in or relating to metal castings |
US1480571A (en) * | 1922-10-02 | 1924-01-15 | Buckeye Brass And Mfg Company | Bearing |
DE1800044U (en) * | 1958-08-13 | 1959-11-12 | Herzog & Pistor | PLASTIC BEARINGS FOR REVOLVING SHAFTS OD. DGL. |
AU4412972A (en) * | 1971-07-05 | 1974-01-03 | Pongrass Bros. (Eng) Pty. Ltd | Composite bush |
US5435650A (en) * | 1993-02-04 | 1995-07-25 | Firma Carl Freudenberg | Guide sleeve |
CN102869892A (en) * | 2010-03-30 | 2013-01-09 | 大同金属工业株式会社 | Sliding member and method of manufacturing same |
CN206017445U (en) * | 2016-08-20 | 2017-03-15 | 南宁钛银科技有限公司 | A kind of large axle bush |
-
2016
- 2016-08-20 CN CN201610690643.2A patent/CN106151277A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB172719A (en) * | 1920-09-10 | 1921-12-12 | Howard Pneumatic Engineering C | Improvements in or relating to metal castings |
US1480571A (en) * | 1922-10-02 | 1924-01-15 | Buckeye Brass And Mfg Company | Bearing |
DE1800044U (en) * | 1958-08-13 | 1959-11-12 | Herzog & Pistor | PLASTIC BEARINGS FOR REVOLVING SHAFTS OD. DGL. |
AU4412972A (en) * | 1971-07-05 | 1974-01-03 | Pongrass Bros. (Eng) Pty. Ltd | Composite bush |
US5435650A (en) * | 1993-02-04 | 1995-07-25 | Firma Carl Freudenberg | Guide sleeve |
CN102869892A (en) * | 2010-03-30 | 2013-01-09 | 大同金属工业株式会社 | Sliding member and method of manufacturing same |
CN206017445U (en) * | 2016-08-20 | 2017-03-15 | 南宁钛银科技有限公司 | A kind of large axle bush |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108730332A (en) * | 2017-04-15 | 2018-11-02 | 广西隆盛双金属铜合金制造有限公司 | A kind of large size bearing and its pressure casting method |
CN108730332B (en) * | 2017-04-15 | 2023-09-08 | 广西隆盛双金属铜合金制造有限公司 | Large bearing and die casting method thereof |
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Application publication date: 20161123 |
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