CN203862421U - Novel centrifugal separator - Google Patents

Novel centrifugal separator Download PDF

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Publication number
CN203862421U
CN203862421U CN201420268673.0U CN201420268673U CN203862421U CN 203862421 U CN203862421 U CN 203862421U CN 201420268673 U CN201420268673 U CN 201420268673U CN 203862421 U CN203862421 U CN 203862421U
Authority
CN
China
Prior art keywords
rotating shaft
fuselage
bearing
bearing block
novel centrifugal
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
Application number
CN201420268673.0U
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Chinese (zh)
Inventor
陈剑华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fujian Erchuang New Material Science & Technology Co Ltd
Original Assignee
Fujian Erchuang New Material Science & Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Fujian Erchuang New Material Science & Technology Co Ltd filed Critical Fujian Erchuang New Material Science & Technology Co Ltd
Priority to CN201420268673.0U priority Critical patent/CN203862421U/en
Application granted granted Critical
Publication of CN203862421U publication Critical patent/CN203862421U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a novel centrifugal separator which is simple in structure, and capable of effectively avoiding bearing abrasion and reducing maintaining frequency. The novel centrifugal separator comprises a machine body, a rotating shaft arranged on the machine body, a driving device for driving the rotating shaft, and a rotating drum arranged on the rotating shaft and placed in the machine body. The two ends of the rotating shaft are arranged on one or more steps respectively, and the steps are respectively provided with a tapered roller bearing. The machine body is provided with a bearing seat, and both the tapered roller bearings are arranged in the bearing seat.

Description

A kind of novel centrifugal seperator
Technical field
The utility model relates to a kind of novel centrifugal seperator.
Background technology
Centrifugal separator is mainly used in the solid particle in suspension and liquid to separate; Or by two kinds of density differences in emulsion, immiscible liquid separates (for example from milk, isolating cream) again; It also can be used for getting rid of the liquid in wet solid, for example, with washing machine, dry wet clothes; Special hypervelocity channel separator is the admixture of gas of separable different densities also, for example concentrated, separating gaseous hex; The different feature of solid particle sinking speed in liquid of utilizing different densities or granularity, some sedimentation centrifuges also can carry out classification by density or granularity to solid particle.Centrifugal separator is widely used in the departments such as chemical industry, oil, food, pharmacy, ore dressing, coal, water treatment and boats and ships.
China Patent No.: 201110235699.6 disclose a kind of bottom-transmission liquid-liquid centrifugal separator, comprise motor, transmission device, rotary drum, seperator shell and upper cover, rotary drum is arranged in seperator shell, upper cover is placed on seperator shell, motor connects rotary drum by transmission device, in rotary drum, be provided with light phase weir and heavy phase weir, between light phase weir and heavy phase weir, be provided with heavy phase weir baffle plate, between rotor cover and seperator shell, be provided with heavy phase collecting ring and light phase collecting ring, on the seperator shell of heavy phase collecting ring top, be provided with heavy out, on seperator shell between heavy phase collecting ring and light phase collecting ring, be provided with light phase export, bottom at seperator shell is provided with charging aperture, in seperator shell rotary drum below deflector is set.This invention can by the liquid-liquid mixture of different specific weight continuously fast separated, improved disposal ability, and be convenient to more commutation weir and maintenance of equipment.But the wearing and tearing at its transmission position are very serious in actual production application, keep in repair also very frequent.
The wearing and tearing of transmission position are the ubiquitous problems of centrifugal separator, and quantity is larger, damage frequently, and comprising positions such as centrifugal separator bearing position, bearing blocks, how to address this problem is the technology perplexing in industry always.
Utility model content
Therefore, for above-mentioned problem, the utility model proposes a kind of simple in structure, can effectively prevent bearing wear, reduce the novel centrifugal seperator of frequency of maintenance.
For achieving the above object, the utility model has adopted following technical scheme: a kind of novel centrifugal seperator, comprise fuselage, be located at rotating shaft on fuselage, drive shaft drive unit, be located at the rotary drum that is positioned at fuselage in rotating shaft, more than one step is located at respectively at the two ends of described rotating shaft, on described each step, be respectively equipped with and be located at taper roll bearing, described fuselage is provided with a bearing block, and described each taper roll bearing is located in bearing block respectively.
Further, be provided with to the corresponding rotating shaft in the upper and lower two ends of described fuselage shaft seat, on described each shaft seat, be respectively equipped with the first ball recess, the two ends up and down of described rotating shaft are respectively equipped with the second ball recess, and described the first ball recess is connected by a ball with the second ball recess.
Further, in the bearing block of described fuselage below, be provided with machine oil, the oil level face of described machine oil is higher than the first ball recess of fuselage below.
Further, the upper end of described bearing block is an inclined-plane, between described bearing block and rotating shaft, is provided with sealing ring.
By adopting aforementioned techniques scheme, the beneficial effects of the utility model are: compare with existing centrifugal separator, this novel centrifugal seperator is by arranging step in rotating shaft, the mode of taper roll bearing is set on step, radial load by original rotating shaft to bearing, resolve into the addition of axial force and radial load, reduced the effect of radial load, thereby wearing and tearing have been reduced, and utilize the mode of step, make force resolution by two ends to centre gradually layer-transferred decompose, reduced stress, protected better rotating shaft and bearing; Further, by ball, rotating shaft is connected with fuselage, makes the axial force of rotating shaft be passed to fuselage, thereby reduced the load of bearing, and utilize the rotary action of ball, can complete more with flying colors the rotation of rotating shaft, make running more stable; Further, the upper end of described bearing block is an inclined-plane, between described bearing block and rotating shaft, be provided with sealing ring, by such arranging, can prevent that the liquid that the sealing on taper roll bearing top does not closely cause from penetrating in taper roll bearing, causes the reduction in service life downwards.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the enlarged drawing at A place in Fig. 1.
The specific embodiment
Now with the specific embodiment, the utility model is further illustrated by reference to the accompanying drawings.
With reference to figure 1, Fig. 2, the present embodiment provides a kind of novel centrifugal seperator, comprise fuselage 1, be located at rotating shaft 2 on fuselage 1, drive shaft 2 drive unit 3, be located at the rotary drum 4 that is positioned at fuselage 1 in rotating shaft 2, two steps 21 are located at respectively at the two ends of described rotating shaft 2, on described each step 21, be respectively equipped with and be located at taper roll bearing 5, described fuselage 1 is provided with a bearing block 11, and described each taper roll bearing 5 is located at respectively in bearing block 11.
Described fuselage is provided with shaft seat 12 in the corresponding rotating shaft in two ends 2 ground Shang Xia 1, on described each shaft seat 12, be respectively equipped with the first ball recess 13, the two ends up and down of described rotating shaft 2 are respectively equipped with the second ball recess 22, and described the first ball recess 13 is connected by a ball 6 with the second ball recess 22.In the bearing block 11 of described fuselage 1 below, be provided with machine oil 7, the oil level face of described machine oil 7 is higher than the first ball recess 13 of fuselage 1 below.
The upper end of described bearing block 11 is an inclined-plane 111, between described bearing block 11 and rotating shaft 2, is provided with sealing ring 112.
Compare with existing centrifugal separator, this novel centrifugal seperator is by arranging step in rotating shaft, the mode of taper roll bearing is set, the radial load by original rotating shaft to bearing, the addition of resolving into axial force and radial load on step, reduced the effect of radial load, thereby reduced wearing and tearing, and utilized the mode of step, make force resolution by two ends to centre gradually layer-transferred decompose, reduce stress, protected better rotating shaft and bearing; Further, by ball, rotating shaft is connected with fuselage, makes the axial force of rotating shaft be passed to fuselage, thereby reduced the load of bearing, and utilize the rotary action of ball, can complete more with flying colors the rotation of rotating shaft, make running more stable; Further, the upper end of described bearing block is an inclined-plane, between described bearing block and rotating shaft, be provided with sealing ring, by such arranging, can prevent that the liquid that the sealing on taper roll bearing top does not closely cause from penetrating in taper roll bearing, causes the reduction in service life downwards.
Although specifically show and introduced the utility model in conjunction with preferred embodiment; but those skilled in the art should be understood that; within not departing from the spirit and scope of the present utility model that appended claims limits; can make a variety of changes the utility model in the form and details, be protection domain of the present utility model.

Claims (4)

1. a novel centrifugal seperator, comprise fuselage, be located at rotating shaft on fuselage, drive shaft drive unit, be located at the rotary drum that is positioned at fuselage in rotating shaft, it is characterized in that: more than one step is located at respectively at the two ends of described rotating shaft, on described each step, be respectively equipped with and be located at taper roll bearing, described fuselage is provided with a bearing block, and described each taper roll bearing is located in bearing block respectively.
2. a kind of novel centrifugal seperator according to claim 1, it is characterized in that: be provided with to the corresponding rotating shaft in the upper and lower two ends of described fuselage shaft seat, on described each shaft seat, be respectively equipped with the first ball recess, the two ends up and down of described rotating shaft are respectively equipped with the second ball recess, and described the first ball recess is connected by a ball with the second ball recess.
3. a kind of novel centrifugal seperator according to claim 2, is characterized in that: in the bearing block of described fuselage below, be provided with machine oil, the oil level face of described machine oil is higher than the first ball recess of fuselage below.
4. a kind of novel centrifugal seperator according to claim 1, is characterized in that: the upper end of described bearing block is an inclined-plane, between described bearing block and rotating shaft, is provided with sealing ring.
CN201420268673.0U 2014-05-23 2014-05-23 Novel centrifugal separator Expired - Fee Related CN203862421U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420268673.0U CN203862421U (en) 2014-05-23 2014-05-23 Novel centrifugal separator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420268673.0U CN203862421U (en) 2014-05-23 2014-05-23 Novel centrifugal separator

Publications (1)

Publication Number Publication Date
CN203862421U true CN203862421U (en) 2014-10-08

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420268673.0U Expired - Fee Related CN203862421U (en) 2014-05-23 2014-05-23 Novel centrifugal separator

Country Status (1)

Country Link
CN (1) CN203862421U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016101838A1 (en) * 2014-12-22 2016-06-30 海尔亚洲株式会社 Drum washing machine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016101838A1 (en) * 2014-12-22 2016-06-30 海尔亚洲株式会社 Drum washing machine
CN107109755A (en) * 2014-12-22 2017-08-29 海尔亚洲株式会社 Roller washing machine
EP3239383A4 (en) * 2014-12-22 2018-08-22 Haier Asia Co., Ltd Drum washing machine

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141008

Termination date: 20190523