CN106179697A - A kind of fuselage capping plate of fine pulverizer - Google Patents

A kind of fuselage capping plate of fine pulverizer Download PDF

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Publication number
CN106179697A
CN106179697A CN201610713921.1A CN201610713921A CN106179697A CN 106179697 A CN106179697 A CN 106179697A CN 201610713921 A CN201610713921 A CN 201610713921A CN 106179697 A CN106179697 A CN 106179697A
Authority
CN
China
Prior art keywords
circle
metallic plate
disc
hole
circular hole
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
Application number
CN201610713921.1A
Other languages
Chinese (zh)
Inventor
柯根祥
彭秋伟
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.)
PINGHU YONGGUANG MACHINERY PARTS Co Ltd
Original Assignee
PINGHU YONGGUANG MACHINERY PARTS 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 PINGHU YONGGUANG MACHINERY PARTS Co Ltd filed Critical PINGHU YONGGUANG MACHINERY PARTS Co Ltd
Priority to CN201610713921.1A priority Critical patent/CN106179697A/en
Publication of CN106179697A publication Critical patent/CN106179697A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B02CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
    • B02CCRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
    • B02C23/00Auxiliary methods or auxiliary devices or accessories specially adapted for crushing or disintegrating not provided for in preceding groups or not specially adapted to apparatus covered by a single preceding group
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B17/00Recovery of plastics or other constituents of waste material containing plastics
    • B29B17/04Disintegrating plastics, e.g. by milling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02WCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
    • Y02W30/00Technologies for solid waste management
    • Y02W30/50Reuse, recycling or recovery technologies
    • Y02W30/62Plastics recycling; Rubber recycling

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  • Engineering & Computer Science (AREA)
  • Environmental & Geological Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Food Science & Technology (AREA)
  • Disintegrating Or Milling (AREA)

Abstract

The invention discloses the fuselage capping plate of a kind of fine pulverizer, including metallic plate and through hole, metallic plate is circular plate, a diameter of 460, and upper and lower thickness is 20;The upper disc of metallic plate is middle, get out downwards interior circular hole, and a diameter of 130, upper and lower thickness is 20, and interior circular hole is a through hole, and interior circular hole and upper disc are concentric circulars;The circumferential edge of the upper disc of metallic plate, being lathed to the chamfering of 30 ° of a circle, chamfering distance is 10;In the upper disc of metallic plate, being drilled with four screwed holes downwards, diameter is all 16, is all through hole;A diameter of the 375 of the circumference that the line in the center of circle of four screwed holes is formed, it is concentric circular with interior circular hole, four screwed holes are evenly distributed in disc, the center of circle of the most adjacent two screwed holes is all 90 ° with the line in the center of circle of interior circular hole, the angle of formation respectively, be positioned at after the angle of horizontal intermediate line of the line in the center of circle of the center of circle of screwed hole in left side and circular hole and upper disc be 45 °.

Description

A kind of fuselage capping plate of fine pulverizer
Technical field
The present invention relates to the fuselage capping plate of a kind of fine pulverizer, specifically to waste tire of automobile, bicycle The fuselage capping plate of a kind of fine pulverizer that the old rubber such as old tire carries out reclaiming, process.
Background technology
Generally, the pulverizing old rubbers such as waste tire of automobile, bicycle old tire reclaimed, process, utilize Machine and fuselage capping plate thereof, owing to designing incorrect, unreasonable structure, the reasons such as size is wrong, installation is not proper, make the rubber of pulverizing Glue fineness does not reaches requirement, and thickness is uneven, and poor product quality does not improves grade, and value is low, it is therefore desirable to this commonly Pulverizer carry out Fine design, innovation, form a kind of fine pulverizer, crudy is good, and product is superior, utilization rate High;And the fuselage capping plate of fine pulverizer is one of them vitals, designs correct, rational in infrastructure, fine powder can be made Broken machine normal operation at work, is connected firmly, favorable working performance, and sealing effectiveness is good, so that it is guaranteed that fine pulverizer work Stable, pulverizing put in place, machining accuracy is high, recycles;Overcome common grinder and fuselage capping plate is designed with By mistake, unreasonable structure, cause processing not in place, poor product quality, the defects such as recovery utilization rate is low.
Summary of the invention
In order to overcome common grinder and fuselage capping plate design thereof wrong, unreasonable structure, causes processing not in place, produces The defects such as quality is poor, and recovery utilization rate is low, the invention provides the fuselage capping plate of a kind of fine pulverizer, and it is fine powder One vitals of broken machine, designs correct, rational in infrastructure, can make fine pulverizer normal operation at work, be connected firmly, Favorable working performance, sealing effectiveness is good, so that it is guaranteed that fine pulverizer working stability, pulverizing puts in place, and machining accuracy is high, returns Receipts are made good use of.
Technical scheme: the fuselage capping plate of a kind of fine pulverizer, including metallic plate and through hole, it is characterised in that metallic plate It is one block of circular plate, has disc, outer circumference surface, lower disc, interior circular hole and screwed hole;The upper disc of metallic plate and cylindrical The diameter of side face and lower disc is all 460, is all concentric circular;The upper and lower thickness of metallic plate is 20;Upper at metallic plate The middle of disc, getting out an interior circular hole, a diameter of the 130 of interior circular hole downwards, upper and lower thickness is 20, so, interior Circular hole is a through hole, drills through the lower disc of metallic plate from the upper disc of metallic plate always, and interior circular hole and upper disc are concentric circulars;? The circumferential edge of the upper disc of metallic plate, being lathed to the chamfering of 30 ° of a circle, chamfering distance is 10;Upper disc at metallic plate In, be drilled with four screwed holes downwards, the diameter of four screwed holes is all 16, and four screwed holes are all through holes, from metallic plate Upper disc drills through the lower disc of metallic plate the most always;A diameter of the 375 of the circumference that the line in the center of circle of four screwed holes is formed , circumference and interior circular hole that the line in the center of circle of four screwed holes is formed are concentric circulars, and four screwed holes are evenly distributed in In disc, the angle that the center of circle of the most adjacent two screwed holes is formed with the line in the center of circle of interior circular hole, these two lines respectively is all Be 90 °, and, be positioned at after in the middle of the center of circle of screwed hole in left side and the line in the center of circle of circular hole and the horizontal of upper disc The angle of line is 45 °;The fuselage capping plate of this fine pulverizer, available rustless steel or the material system such as common iron or aluminium alloy Make.
The beneficial effects of the present invention is: providing the fuselage capping plate of a kind of fine pulverizer, it is fine pulverizer One vitals, designs correct, rational in infrastructure, can make fine pulverizer normal operation at work, be connected firmly, workability Can be good, sealing effectiveness is good, so that it is guaranteed that fine pulverizer working stability, pulverizing puts in place, and processing precision of products is high, reclaims Make good use of;Overcome common grinder and fuselage capping plate design is wrong, unreasonable structure, cause processing not in place, product Of poor quality, the defects such as recovery utilization rate is low;The production standard of enterprise can be met, expand the social need of product.
Accompanying drawing explanation
The structural representation of the vertical view of the fuselage capping plate of a kind of fine pulverizer of Fig. 1
The cross-sectional view that the master of the fuselage capping plate of a kind of fine pulverizer of Fig. 2 regards
Detailed description of the invention
The invention will be further described below in conjunction with the accompanying drawings:
A kind of fine pulverizer fuselage capping plate, including metallic plate and through hole, it is characterised in that metallic plate 1 be one piece circular Plate, has disc, outer circumference surface, lower disc, interior circular hole 3 and screwed hole 4;The upper disc of metallic plate 1 and outer circumference surface and under The diameter of disc is all 460, is all concentric circular;The upper and lower thickness of metallic plate 1 is 20;Metallic plate 1 upper disc it Middle, getting out an interior circular hole 3, a diameter of the 130 of interior circular hole 3 downwards, upper and lower thickness is 20, so, interior circular hole 3 is a through hole, drills through the lower disc of metallic plate 1 from the upper disc of metallic plate 1 always, and interior circular hole 3 is concentric circular with upper disc;? The circumferential edge of the upper disc of metallic plate 1, being lathed to the chamfering 2 of 30 ° of a circle, chamfering distance is 10;Upper circle at metallic plate 1 In face, being drilled with four screwed holes 4 downwards, the diameter of four screwed holes 4 is all 16, and four screwed holes 4 are all through holes, from metal The upper disc of plate 1 drills through the lower disc of metallic plate 1 the most always;The circumference that the line in the center of circle of four screwed holes 4 is formed is straight Footpath is 375, and the circumference that the line in the center of circle of four screwed holes 4 is formed and interior circular hole 3 are concentric circulars, and four screwed holes 4 are uniform Be distributed in disc, the center of circle of the most adjacent two screwed holes 4 respectively with the line in the center of circle, these two lines of interior circular hole 3 The angle formed is all 90 °, and, be positioned at after the center of circle of screwed hole 4 in left side and circular hole 3 the center of circle line and on The angle of the horizontal intermediate line of disc is 45 °;The fuselage capping plate of this fine pulverizer, makes of stainless steel material.

Claims (1)

1. a fuselage capping plate for fine pulverizer, including metallic plate and through hole, it is characterised in that metallic plate (1) is one piece of circle The plate of shape, has disc, outer circumference surface, lower disc, interior circular hole (3) and screwed hole (4);The upper disc of metallic plate (1) is with outer The diameter of periphery and lower disc is all 460, is all concentric circular;The upper and lower thickness of metallic plate (1) is 20;At metal The middle of the upper disc of plate (1), get out an interior circular hole (3), a diameter of the 130 of interior circular hole (3), upper and lower thickness downwards Degree is 20, and interior circular hole (3) is a through hole, drills through the lower disc of metallic plate (1), inner circle from the upper disc of metallic plate (1) always Hole (3) and upper disc are concentric circulars;Metallic plate (1) upper disc circumferential edge, be lathed to the chamfering (2) of 30 ° of a circle, fall Angular distance is 10;In the upper disc of metallic plate (1), it is drilled with four screwed holes (4), the diameter of four screwed holes (4) downwards Being all 16, four screwed holes (4) are all through holes, drill through the lower circle of metallic plate (1) from the upper disc of metallic plate (1) the most always Face;A diameter of the 375 of the circumference that the line in the center of circle of four screwed holes (4) is formed, the line in the center of circle of four screwed holes (4) The circumference formed and interior circular hole (3) are concentric circulars, and four screwed holes (4) are evenly distributed in disc, the most adjacent two spiral shells The angle that the center of circle of pit (4) is formed with the line in the center of circle of interior circular hole (3), these two lines respectively is all 90 °, be positioned at after The angle of the horizontal intermediate line of the center of circle of the screwed hole (4) in left side and the line in the center of circle of interior circular hole (3) and upper disc is 45 °.
CN201610713921.1A 2016-08-24 2016-08-24 A kind of fuselage capping plate of fine pulverizer Pending CN106179697A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610713921.1A CN106179697A (en) 2016-08-24 2016-08-24 A kind of fuselage capping plate of fine pulverizer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610713921.1A CN106179697A (en) 2016-08-24 2016-08-24 A kind of fuselage capping plate of fine pulverizer

Publications (1)

Publication Number Publication Date
CN106179697A true CN106179697A (en) 2016-12-07

Family

ID=57525068

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610713921.1A Pending CN106179697A (en) 2016-08-24 2016-08-24 A kind of fuselage capping plate of fine pulverizer

Country Status (1)

Country Link
CN (1) CN106179697A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102042359A (en) * 2011-01-19 2011-05-04 北京交通大学 Magnetic liquid damping device
CN102599985A (en) * 2012-04-16 2012-07-25 吉林大学 Miniature testing system for testing stress of teeth in drilling process
CN103527638A (en) * 2013-10-11 2014-01-22 平湖市山特螺纹工具有限公司 Bearing cover of main shaft of screw tap relief-grinding machine
CN103760026A (en) * 2014-02-13 2014-04-30 北京工业大学 Loading device for laser-irradiated cylindrical shell test and experimental method
CN204504050U (en) * 2014-11-29 2015-07-29 中航天水飞机工业有限责任公司 Depressor received by bearing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102042359A (en) * 2011-01-19 2011-05-04 北京交通大学 Magnetic liquid damping device
CN102599985A (en) * 2012-04-16 2012-07-25 吉林大学 Miniature testing system for testing stress of teeth in drilling process
CN103527638A (en) * 2013-10-11 2014-01-22 平湖市山特螺纹工具有限公司 Bearing cover of main shaft of screw tap relief-grinding machine
CN103760026A (en) * 2014-02-13 2014-04-30 北京工业大学 Loading device for laser-irradiated cylindrical shell test and experimental method
CN204504050U (en) * 2014-11-29 2015-07-29 中航天水飞机工业有限责任公司 Depressor received by bearing

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PB01 Publication
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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20161207

WD01 Invention patent application deemed withdrawn after publication