CN106553027B - Mold assembles position precision holes processing method - Google Patents

Mold assembles position precision holes processing method Download PDF

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Publication number
CN106553027B
CN106553027B CN201611117435.XA CN201611117435A CN106553027B CN 106553027 B CN106553027 B CN 106553027B CN 201611117435 A CN201611117435 A CN 201611117435A CN 106553027 B CN106553027 B CN 106553027B
Authority
CN
China
Prior art keywords
hole
plugging material
hardness
processing method
precision holes
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
CN201611117435.XA
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Chinese (zh)
Other versions
CN106553027A (en
Inventor
刘伟光
王小华
曹云飞
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.)
Shijiazhuang Zhonghang Mechanical And Electrical Equipment Manufacturing Co ltd
Original Assignee
SHIJIAZHUANG AIRCRAFT INDUSTRY 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 SHIJIAZHUANG AIRCRAFT INDUSTRY Co Ltd filed Critical SHIJIAZHUANG AIRCRAFT INDUSTRY Co Ltd
Priority to CN201611117435.XA priority Critical patent/CN106553027B/en
Publication of CN106553027A publication Critical patent/CN106553027A/en
Application granted granted Critical
Publication of CN106553027B publication Critical patent/CN106553027B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Mounting, Exchange, And Manufacturing Of Dies (AREA)

Abstract

The present invention relates to a kind of molds to assemble position precision holes processing method, includes the following steps:Assembling position roughing on die main body slightly first hole, will rough machined thick just hole aperture amplification manufacture, first hole after enlargement ratio is not less than 1.25 times of thick first bore dia;First hole after die main body and enlargement ratio is heat-treated;Plugging material is filled up in first hole, the hardness of the plugging material is less than the hardness of after heat treatment die main body material;It fills up to finish on plugging material after plugging material and makes precision holes.The present invention provides a kind of easy processing and protects precision, and the hole machined time is short, and drilling tool without abrasion, reduces manufacture cost and cost of labor, and fool proof substantially.

Description

Mold assembles position precision holes processing method
Technical field
The present invention relates to the processing methods of precision holes, and in particular to a kind of mold assembles position precision holes processing method.
Background technology
Because of mold manufacturing mesoporous feature:1. polyisocyanate shape, 2. single and mini-batch production in irregular shape 3. required precision height 4. polygamy Make 5. middle or small, deep 6. preferential processing.General hole machined one bores two expansions, three four borings of brill nothing but, is aided with assorted fixture, material hardness is high With regard to using special cutter head.
There is higher hardness requirement in working position in mold manufacturing, considers its preferential processability, the processing of precision holes ordinary priority In place, then carry out heat treatment ensure its hardness, but be heat-treated after precision holes generally have a little deformation, it is difficult to ensure its precision.And When hardness requirement is not high at its pilot hole, original mould process is still processed in a traditional way, and final precision is difficult to ensure that, processing Because of hardness height, cutter is easy to wear, and tipping, which is easy to cause, occurs accident, and some is even basic to process, and increases manufacture cost in hole And cost of labor.
Invention content
To solve the above problems, the present invention, which provides a kind of easy processing, protects precision, the hole machined time is short, drilling tool substantially without Abrasion reduces manufacture cost and cost of labor, and foolproof mold assembling position precision holes processing method.
Technical scheme of the present invention:
A kind of mold assembles position precision holes processing method, includes the following steps:
(1)Assembling position roughing on die main body slightly first hole, rough machined thick just hole aperture amplification is manufactured, is put First hole after big multiplying power is not less than 1.25 times of thick just bore dia;
(2)First hole after die main body and enlargement ratio is heat-treated;
(3)By step(2)Plugging material is filled up at the beginning of treated in hole, the hardness of the plugging material is less than through step (2)The hardness of rear mold material of main part is handled, the intensity of the plugging material meets the intensity requirement of assembling positioning;
(4)The first nose end mouth filled up after plugging material connects flat, finally with benchmark centering, finishes and makes on plugging material Precision holes.Fine machining die subject type face keeps unity.
Further, the plugging material is mild steel Q235 or 20 steel.
Further, the method for filling up plugging material is filled up for pressure.
Further, the first hole after die main body and enlargement ratio be heat-treated to hardness in HRC38 ~ HRC62 Between.
Beneficial effects of the present invention:
Precision hole forming method using the present invention, plugging material hardness is low, and easy processing protects precision.The hole machined time is short, Drilling tool without abrasion, reduces manufacture cost and cost of labor, and fool proof substantially.
The present invention is applied to pin position portion in the molds such as large quantities of molds, bending former, to ensure mold or so Half model face consistency obtains significant effect in terms of saving the process-cycle and saving the cost of charp tool.
Specific embodiment
T8 steel mold bulk workpiece inoperatives part changing firmness requirements are not high, if finally will precision holes Φ 10H7 processed, according to biography System mode first beats thick just hole Φ 10H7, and by roughing, slightly just hole Φ 10H7 apertures amplification, diameter are high-volume not less than 2.5mm, at this time Hardness is relatively low easily to make.It then still provides for being heat-treated to required hardness requirement, after T8 steel quenches HRC58-62, first hole It is lower than T8 steel hardness after quenching that easy processing material Q235, Q235 hardness is filled out in 13 H7 of Φ, finally with benchmark centering, with drill bit essence Precision holes Φ 10H7 holes are made in processing, and finishing drum face keeps unity.
Precision holes Φ 10H7 are directly made after hole Φ 10 at the beginning of conventional method T8 steel roughing slightly, hardness, T8 are protected in reheating processing Steel quenches HRC58-62, and so inevitably bore deformation precision reduces after heat treatment, can not meet requirement.It is first carried out if precision is protected Heat treatment, T8 steel quenching HRC58-62, excessive high hardness after heat treatment, normal drill bit can not be processed at all, need to there is the old skilled worker of experience It is processed with caution with special drill bit, is possible to success, consequently cost of labor and the cost of charp tool are excessively high.And easily crushing knife, It causes danger.
Precision holes Φ 10H7 are beaten with the method for the present invention, precision holes Φ 1,0H7 100 processed scrap 2-3, drill bit.It makes a hole Time 10min used, only more than ten yuan of the cost made a hole.Substantially reduce process time, the cost of charp tool.And safety is without danger Danger, general apprentice can be competent at processing.
The foregoing description of the disclosed embodiments enables professional and technical personnel in the field to realize or use the present invention. A variety of modifications of these embodiments will be apparent for those skilled in the art, it is as defined herein General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, it is of the invention The embodiments shown herein is not intended to be limited to, and is to fit to and the principles and novel features disclosed herein phase one The most wide range caused.

Claims (4)

1. a kind of mold assembles position precision holes processing method, which is characterized in that includes the following steps:
(1)Assembling position roughing on die main body slightly first hole, will rough machined thick just hole aperture amplification manufacture, amplify First hole after multiplying power is not less than 1.25 times of thick just bore dia;
(2)First hole after die main body and enlargement ratio is heat-treated;
(3)By step(2)Plugging material is filled up at the beginning of treated in hole, the hardness of the plugging material is less than through step(2) The hardness of rear mold material of main part is handled, the intensity of the plugging material meets the intensity requirement of assembling positioning;
(4)The first nose end mouth filled up after plugging material connect it is flat, finally with benchmark centering, on plugging material finishing make precision Hole.
2. mold according to claim 1 assembles position precision holes processing method, which is characterized in that the plugging material For mild steel Q235 or 20 steel.
3. mold according to claim 1 assembles position precision holes processing method, which is characterized in that described to fill up closure material The method of material is filled up for pressure.
4. mold according to claim 1 assembles position precision holes processing method, which is characterized in that by die main body and First hole after enlargement ratio be heat-treated to hardness between HRC38 ~ HRC62.
CN201611117435.XA 2016-12-07 2016-12-07 Mold assembles position precision holes processing method Expired - Fee Related CN106553027B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611117435.XA CN106553027B (en) 2016-12-07 2016-12-07 Mold assembles position precision holes processing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611117435.XA CN106553027B (en) 2016-12-07 2016-12-07 Mold assembles position precision holes processing method

Publications (2)

Publication Number Publication Date
CN106553027A CN106553027A (en) 2017-04-05
CN106553027B true CN106553027B (en) 2018-06-22

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611117435.XA Expired - Fee Related CN106553027B (en) 2016-12-07 2016-12-07 Mold assembles position precision holes processing method

Country Status (1)

Country Link
CN (1) CN106553027B (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2734958A1 (en) * 1977-08-03 1979-02-15 Froehlich Air Ag PROCESS FOR MANUFACTURING A PIPE HEAT EXCHANGER AND PIPE HEAT EXCHANGER MANUFACTURED BY THIS PROCESS
CN100462610C (en) * 2007-07-10 2009-02-18 宁波市三浪润滑元件有限公司 Stepwise type distributor
CN101850498B (en) * 2010-06-17 2012-07-18 中信重工机械股份有限公司 Processing method of power senary shunting rotary frame of large-scale vertical mill reducer
CN101942550B (en) * 2010-09-06 2012-05-23 中原特钢股份有限公司 Heat treatment process for hollow drill collar
CN102181836B (en) * 2011-04-14 2012-10-31 北京有色金属研究总院 Method for connecting target with back plate
CN103481040B (en) * 2013-10-16 2015-09-30 青岛肯拉铎机械有限公司 Crank processing technology

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Effective date of registration: 20190401

Address after: 051430 No. 99 Hengjing Road, Luancheng District, Shijiazhuang City, Hebei Province

Patentee after: SHIJIAZHUANG ZHONGHANG MECHANICAL AND ELECTRICAL EQUIPMENT MANUFACTURING Co.,Ltd.

Address before: 051430 No. 99 Hengjing Road, Luancheng District, Shijiazhuang City, Hebei Province

Patentee before: AVIC SHIJIAZHUANG AIRCRAFT INDUSTRY (GROUP) Corp.,Ltd.

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: 20180622