CN107717339A - A kind of metal shell hole machined technique - Google Patents

A kind of metal shell hole machined technique Download PDF

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Publication number
CN107717339A
CN107717339A CN201710811941.7A CN201710811941A CN107717339A CN 107717339 A CN107717339 A CN 107717339A CN 201710811941 A CN201710811941 A CN 201710811941A CN 107717339 A CN107717339 A CN 107717339A
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CN
China
Prior art keywords
hole
thick
essences
tool
cutter
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
CN201710811941.7A
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Chinese (zh)
Inventor
唐群
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.)
Guangdong Janus Intelligent Group Corp Ltd
Original Assignee
Guangdong Janus Intelligent Group Corp 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 Guangdong Janus Intelligent Group Corp Ltd filed Critical Guangdong Janus Intelligent Group Corp Ltd
Priority to CN201710811941.7A priority Critical patent/CN107717339A/en
Publication of CN107717339A publication Critical patent/CN107717339A/en
Pending legal-status Critical Current

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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)
  • Knives (AREA)

Abstract

The invention belongs to part processing technique field, and in particular to a kind of metal shell hole machined technique, it comprises the following steps:1) tool diameter is selected:A) open thick tool diameter standard be D1 it is thick=D X, wherein D be functional hole narrow slot width, X=0.3mm, it is twolip to drive thick cutter;B) tool diameter standard with nothing left is D1 essences=D X1, and wherein D is functional hole narrow slot width, and X1=0.3~0.5mm, cutter with nothing left is left-handed knife, and chip removal direction is bottom chip removal, and R1 essences=D1 essence/2, R1 essences are less than R, functional hole minimum angle R=D/2;Tool blade length with nothing left is more than most short function hole depth+0.5mm;2) machined parameters are selected;3) processing mode is selected:A) during roughing, thick cutter both ends subdrilling milling chip-removal hole is opened, then single line or reciprocating feed;When b) finishing, finishing tool walks two knives, along inverse each knife.Present invention process processing hole efficiency high, breaking is not easy, and qualification rate is high.

Description

A kind of metal shell hole machined technique
Technical field
The invention belongs to part processing technique field, and in particular to a kind of metal shell hole machined technique.
Background technology
" functional hole " of metal shell (such as in industry at present:The narrow slots such as power supply/volume hole/SIM card) processing problem be present It is as follows:
1. hole slot is narrow (normally only 1.30~1.60MM), because process tool is smaller from diameter, rigidity deficiency, easily Viscous knife, breaking, length and width are uncoordinated, and assembling is difficult;
2. hole slot edge is sharp edge, processing easily produces the burr to turn up, and after sharp edge deburring, causes to step on side and does not conform to Lattice.
The content of the invention
It is an object of the invention to provide a kind of metal shell hole machined technique of standardization, and hole is processed using the technique, its High in machining efficiency, good processing stability, it is not easy breaking, is not likely to produce burr, and the hole qualification rate processed is high.
A kind of metal shell hole machined technique, comprises the following steps,
1) tool diameter is selected:A) open thick tool diameter standard be D1 it is thick=D-X, wherein D be functional hole narrow slot width, X =0.25~0.35mm, it is twolip to drive thick cutter;B) tool diameter standard with nothing left is D1 essences=D-X1, and wherein D is that functional hole is narrow Well width, X1=0.3~0.5mm, cutter with nothing left are left-handed knife, and chip removal direction is bottom chip removal, and R1 essences=D1 essence/2, R1 are smart Less than R, functional hole minimum angle R=D/2;Tool blade with nothing left, which is grown, is more than most short function hole depth+X2, and the X2=0.4~ 0.6mm;
2) machined parameters are selected:
3) processing mode is selected:A) during roughing, thick cutter both ends subdrilling milling chip-removal hole is opened, then single line or reciprocal Formula feed;When b) finishing, finishing tool walks two knives, along inverse each knife.
Preferably, the X=0.3mm.
Preferably, the X2=0.5mm.
Beneficial effects of the present invention are:Using the metal shell hole machined technique of the standardization, during its machining function hole, Efficiency high, good processing stability, it is not easy breaking, is not likely to produce burr and qualification rate is high.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to embodiments, to this hair It is bright to be further elaborated.It should be appreciated that specific embodiment described herein and does not have to only to explain the present invention It is of the invention in limiting.
A kind of metal shell hole machined technique, comprises the following steps,
1) tool diameter is selected:A) open thick tool diameter standard be D1 it is thick=D-X, wherein D be functional hole narrow slot width, X =0.3mm (is used for chip removal), and it is twolip to drive thick cutter;B) tool diameter standard with nothing left is D1 essences=D-X1, and wherein D is function Hole narrow slot width, X1=0.3~0.5mm, cutter with nothing left are left-handed knife, and chip removal direction is bottom chip removal, R1 essences=D1 essence/2, R1 essences are less than R, functional hole minimum angle R=D/2;Tool blade length with nothing left, which is more than most short function hole depth+0.5mm, (to be prevented vibrated Greatly);
2) machined parameters are selected:
3) processing mode is selected:A) during roughing, thick cutter both ends subdrilling milling chip-removal hole is opened, then single line or reciprocal Formula feed;When b) finishing, finishing tool walks two knives, along inverse each knife.
The present invention processes work for functional hole (narrow slot such as power supply/volume hole/SIM card) CNC of metallic mobile phone shell class product Skill standard, mainly apply to the standardization of CNC section metal products processing technology.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention Any modification, equivalent substitution or improvement made within refreshing and principle etc., should be included in the scope of the protection.

Claims (3)

  1. A kind of 1. metal shell hole machined technique, it is characterised in that:Comprise the following steps,
    1) tool diameter is selected:A) open thick tool diameter standard be D1 it is thick=D-X, wherein D be functional hole narrow slot width, X= 0.25~0.35mm, it is twolip to drive thick cutter;B) tool diameter standard with nothing left is D1 essences=D-X1, and wherein D is functional hole narrow slot Width, X1=0.3~0.5mm, cutter with nothing left are left-handed knife, and chip removal direction is bottom chip removal, and R1 essences=D1 essence/2, R1 essences are less than R, functional hole minimum angle R=D/2;Tool blade length with nothing left is more than most short function hole depth+X2, the X2=0.4~0.6mm;
    2) machined parameters are selected:
    3) processing mode is selected:A) during roughing, open thick cutter both ends subdrilling milling chip-removal hole, then single line or it is reciprocating walk Knife;When b) finishing, finishing tool walks two knives, along inverse each knife.
  2. A kind of 2. metal shell hole machined technique according to claim 1, it is characterised in that:The X=0.3mm.
  3. A kind of 3. metal shell hole machined technique according to claim 1, it is characterised in that:The X2=0.5mm.
CN201710811941.7A 2017-09-08 2017-09-08 A kind of metal shell hole machined technique Pending CN107717339A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710811941.7A CN107717339A (en) 2017-09-08 2017-09-08 A kind of metal shell hole machined technique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710811941.7A CN107717339A (en) 2017-09-08 2017-09-08 A kind of metal shell hole machined technique

Publications (1)

Publication Number Publication Date
CN107717339A true CN107717339A (en) 2018-02-23

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710811941.7A Pending CN107717339A (en) 2017-09-08 2017-09-08 A kind of metal shell hole machined technique

Country Status (1)

Country Link
CN (1) CN107717339A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111098099A (en) * 2020-01-07 2020-05-05 天津银宝山新科技有限公司 Door plate front and rear die processing technology
CN111112958A (en) * 2020-01-07 2020-05-08 天津银宝山新科技有限公司 Processing technology of bumper large insert

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101780557A (en) * 2010-02-09 2010-07-21 保定惠阳航空螺旋桨制造厂 Numerical control milling process method of thin-walled part die cavity
CN102091811A (en) * 2010-12-24 2011-06-15 沈阳飞机工业(集团)有限公司 Quick cutting method for titanium alloy
CN102601438A (en) * 2012-04-09 2012-07-25 合肥波林新材料有限公司 Two-edge special end milling cutter for through groove
CN103737077A (en) * 2013-12-11 2014-04-23 思柏精密模具注塑(无锡)有限公司 Printer terrace die insert block processing method
CN104690354A (en) * 2014-12-04 2015-06-10 贵州西南工具(集团)有限公司 Key slot drill milling cutter
CN104759672A (en) * 2015-04-01 2015-07-08 衡阳风顺车桥有限公司 Long shaft key slot machining process
CN105689751A (en) * 2016-04-13 2016-06-22 重庆江增船舶重工有限公司 Machining method for hollow discontinuous deep hole with inclined workblank face
CN106424873A (en) * 2016-12-28 2017-02-22 中航沈飞民用飞机有限责任公司 Method for milling and processing carbon fiber sacrifice layer of connecting plane
CN106584030A (en) * 2016-12-19 2017-04-26 中国科学院长春光学精密机械与物理研究所 Machining method for small-diameter positioning pin hole

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101780557A (en) * 2010-02-09 2010-07-21 保定惠阳航空螺旋桨制造厂 Numerical control milling process method of thin-walled part die cavity
CN102091811A (en) * 2010-12-24 2011-06-15 沈阳飞机工业(集团)有限公司 Quick cutting method for titanium alloy
CN102601438A (en) * 2012-04-09 2012-07-25 合肥波林新材料有限公司 Two-edge special end milling cutter for through groove
CN103737077A (en) * 2013-12-11 2014-04-23 思柏精密模具注塑(无锡)有限公司 Printer terrace die insert block processing method
CN104690354A (en) * 2014-12-04 2015-06-10 贵州西南工具(集团)有限公司 Key slot drill milling cutter
CN104759672A (en) * 2015-04-01 2015-07-08 衡阳风顺车桥有限公司 Long shaft key slot machining process
CN105689751A (en) * 2016-04-13 2016-06-22 重庆江增船舶重工有限公司 Machining method for hollow discontinuous deep hole with inclined workblank face
CN106584030A (en) * 2016-12-19 2017-04-26 中国科学院长春光学精密机械与物理研究所 Machining method for small-diameter positioning pin hole
CN106424873A (en) * 2016-12-28 2017-02-22 中航沈飞民用飞机有限责任公司 Method for milling and processing carbon fiber sacrifice layer of connecting plane

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
兵器工业部205研究所曲线套筒研制小组: "精密曲线套筒加工工艺", 《应用光学》 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111098099A (en) * 2020-01-07 2020-05-05 天津银宝山新科技有限公司 Door plate front and rear die processing technology
CN111112958A (en) * 2020-01-07 2020-05-08 天津银宝山新科技有限公司 Processing technology of bumper large insert

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Application publication date: 20180223