CN103433540A - Axial milling method for titanium alloy slot cavity structure - Google Patents

Axial milling method for titanium alloy slot cavity structure Download PDF

Info

Publication number
CN103433540A
CN103433540A CN2013104248976A CN201310424897A CN103433540A CN 103433540 A CN103433540 A CN 103433540A CN 2013104248976 A CN2013104248976 A CN 2013104248976A CN 201310424897 A CN201310424897 A CN 201310424897A CN 103433540 A CN103433540 A CN 103433540A
Authority
CN
China
Prior art keywords
axial
cutter
milling
corner
vallecular cavity
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
CN2013104248976A
Other languages
Chinese (zh)
Inventor
石海
李亚宏
王金海
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.)
Shenyang Aircraft Industry Group Co Ltd
Original Assignee
Shenyang Aircraft Industry Group 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 Shenyang Aircraft Industry Group Co Ltd filed Critical Shenyang Aircraft Industry Group Co Ltd
Priority to CN2013104248976A priority Critical patent/CN103433540A/en
Publication of CN103433540A publication Critical patent/CN103433540A/en
Pending legal-status Critical Current

Links

Images

Abstract

The invention relates to an axial milling method for a titanium alloy slot cavity structure. The axial milling method comprises the following steps: (1) carrying out rough machining on a slotted hole by adopting a large-diameter cutter with the size close to that of a slot cavity to form a notch with the margin of 0.3mm; (2) carrying out axial milling on the corner of the slot cavity by adopting a conventional milling cutter, wherein the radius of the milling cutter is consistent with that of the corner of the slot cavity to be machined; and (3) carrying out finish machining on the inner wall of the slot cavity. According to the axial milling method, the cutter does feeding movement along the direction of a cutter shaft in a machining process, and a cutting edge at the bottom is utilized for drilling and milling combined cutting. The axial milling method is large in axial cutting force and small in radial cutting force, so that a cutter bar can smoothly operate, meanwhile the machining efficiency is improved, and the product quality is ensured.

Description

The axial method for milling of titanium alloy vallecular cavity class formation
Technical field
The present invention relates to a kind of axial method for milling of titanium alloy vallecular cavity class formation, belong to a kind of machining process.
Background technology
So-called Z axis milling method is exactly a kind of method of axially processing, and corner adopts such processing method, and technical advantage is particularly remarkable.At present, general engineers and technicians are when the numerical programming procedure, no matter be steel, titanium class part, or aluminium alloy class part, all recognize the importance that the corner surplus is taken out in advance, on the corner basically all process accordingly, in the time of most again during the numerical programming program, the shirtsleeve operation mode is the mode that adopts the profile layering processing of corner, the cutting depth that reduces the time guarantees machining state on the corner, but, the working (machining) efficiency of this method is low, simultaneously, the cutter cutter R that only weares and teares when actual cut, tool wear is very fast, the cutter loss is very large, the corner reduction of speed is also way commonly used, but this method can not solve cutting width problem on the corner, easily the cutter phenomenon is fallen in the excessive generation of cutting output.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of axial method for milling of titanium alloy vallecular cavity class formation, the method adopts cutter in process to do feed motion along cutter axis orientation, utilize the bottom cutting edge to be bored, mill the combination cutting, the axial cutting force of the method is larger, radial cutting force is less, from to knife bar is operated steadily, improve working (machining) efficiency simultaneously, guarantee product quality.
For overcoming the above problems, concrete technical scheme of the present invention is as follows: a kind of axial method for milling of titanium alloy vallecular cavity class formation comprises the following steps:
1) employing is carried out roughing with the major diameter cutter that vallecular cavity approaches size to slotted eye, forms and leaves the notch that surplus is 0.3mm;
2) adopt conventional milling cutter to carry out axial milling to the corner of vallecular cavity, the milling cutter radius is consistent with vallecular cavity knuckle radius to be processed;
2.1) milling cutter is axial feed, the amount of feeding is no more than the blade width of 1/3 or inserted welding blade of tool diameter;
2.2) after axial feed cutting, then, along the bisector of two corner planes, with one of them notch inner surface, be 45 ° of line withdrawings;
2.3) successively corner is carried out to axial feed processing, until the corner completion of processing;
3) inwall of vallecular cavity carried out to fine finishining.
The axial method for milling of this titanium alloy vallecular cavity class formation adopts above-mentioned steps, not only working (machining) efficiency can improve, reduced the cost of charp tool, cutter is when axially cutting simultaneously, knife bar mainly bears axial force, add the man-hour radial cutting force lower, the ability that knife bar bears axial load will far be better than radially, so corner adopts the phenomenon that axially adopts axial manner generally not there will be cutter to fracture or fall cutter, from the angle of lathe adaptive type, consider, if the power limited of machining tool used, can consider to adopt the method for axial processing, this is because axially the processing power demand is less than helical milling.
The accompanying drawing explanation
The structural representation of the axial method for milling that Fig. 1 is titanium alloy vallecular cavity class formation.
1-withdrawing track wherein; 2-feed track; The 3-feed speed; The 4-rotating speed; The 5-cutting-in; 6-withdrawing distance.
The specific embodiment
As shown in Figure 1, a kind of axial method for milling of titanium alloy vallecular cavity class formation comprises the following steps:
1) employing is carried out roughing with the major diameter cutter that vallecular cavity approaches size to slotted eye, forms and leaves the notch that surplus is 0.3mm;
2) adopt conventional milling cutter to carry out axial milling to the corner of vallecular cavity, the milling cutter radius is consistent with vallecular cavity knuckle radius to be processed;
2.1) milling cutter is axial feed, the amount of feeding is no more than the blade width of 1/3 or inserted welding blade of tool diameter;
2.2) after axial feed cutting, then, along the bisector of two corner planes, with one of them notch inner surface, be 45 ° of line withdrawings;
2.3) successively corner is carried out to axial feed processing, until the corner completion of processing;
3) inwall of vallecular cavity carried out to fine finishining.
The application adopts axial processing mode, is different from the in the past mode of general conventional corner treatment, be axially a kind of by lathe along cutter axially, incision part blank a kind of, be similar to a kind of processing method of drilling.Conventional side edge milling method, main stressed of knife bar part is radial load, increase along with tool length, the bending moment that knife bar partly is subject to is increasing, the requirement of tool setting bar material is also more and more higher, even employing Hardmetal materials, the knife bar of overlength also easily makes screw-on cutter generation chatter, lower owing to axially adding the man-hour radial cutting force, by traditional diamond-making technique radially become cutter axially, the ability that knife bar bears axial load will far be better than radially, and the cutting force in process also obviously reduces, stable cutting.

Claims (1)

1. the axial method for milling of a titanium alloy vallecular cavity class formation is characterized in that comprising the following steps:
1) employing is carried out roughing with the major diameter cutter that vallecular cavity approaches size to slotted eye, forms and leaves the notch that surplus is 0.3mm;
2) adopt conventional milling cutter to carry out axial milling to the corner of vallecular cavity, the milling cutter radius is consistent with vallecular cavity knuckle radius to be processed;
2.1) milling cutter is axial feed, the amount of feeding is no more than the blade width of 1/3 or inserted welding blade of tool diameter;
2.2) after axial feed cutting, then, along the bisector of two corner planes, with one of them notch inner surface, be 45 ° of line withdrawings;
2.3) successively corner is carried out to axial feed processing, until the corner completion of processing;
3) inwall of vallecular cavity carried out to fine finishining.
CN2013104248976A 2013-09-18 2013-09-18 Axial milling method for titanium alloy slot cavity structure Pending CN103433540A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013104248976A CN103433540A (en) 2013-09-18 2013-09-18 Axial milling method for titanium alloy slot cavity structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013104248976A CN103433540A (en) 2013-09-18 2013-09-18 Axial milling method for titanium alloy slot cavity structure

Publications (1)

Publication Number Publication Date
CN103433540A true CN103433540A (en) 2013-12-11

Family

ID=49687304

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2013104248976A Pending CN103433540A (en) 2013-09-18 2013-09-18 Axial milling method for titanium alloy slot cavity structure

Country Status (1)

Country Link
CN (1) CN103433540A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103801900A (en) * 2014-03-04 2014-05-21 广西玉柴机器股份有限公司 Processing method for cylinder body water tank
CN104923839A (en) * 2015-06-25 2015-09-23 合肥圣达电子科技实业公司 Processing method of aluminum-silicon shell
CN105312835A (en) * 2015-11-27 2016-02-10 成都飞机工业(集团)有限责任公司 Deep cavity processing method based on titanium alloy monobloc forging component
CN105522206A (en) * 2015-12-29 2016-04-27 湖南航天环宇通信科技股份有限公司 Machining method for aluminum alloy thin-walled cavity part
CN105642976A (en) * 2014-11-14 2016-06-08 江西昌河航空工业有限公司 Numerical control machining method of T-type groove for aluminum alloy part
CN105642978A (en) * 2014-12-01 2016-06-08 中航贵州飞机有限责任公司 Method for corner removing through plunge milling in numerical control machining
CN108714704A (en) * 2018-08-27 2018-10-30 沈阳富创精密设备有限公司 A kind of processing technology at the depth angles chamber R
CN108941684A (en) * 2018-08-31 2018-12-07 武汉船用机械有限责任公司 A kind of processing method of the kidney-shaped skewed slot of annular thin-wall parts
CN110202192A (en) * 2019-05-28 2019-09-06 闻泰通讯股份有限公司 Improve the milling method of surface roughness
CN110394488A (en) * 2019-07-30 2019-11-01 湖北三江航天险峰电子信息有限公司 A kind of processing method at the clear angle of depth chamber

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007283452A (en) * 2006-04-19 2007-11-01 Mitsubishi Heavy Ind Ltd Cutting method
CN101428356A (en) * 2008-09-17 2009-05-13 西安飞机工业(集团)有限责任公司 Method for high-efficiency allowance-removing numerical control machining for groove-cavity structured part with corner
JP2009220218A (en) * 2008-03-17 2009-10-01 Jtekt Corp Method of cutting pocket by end mill
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
CN102658390A (en) * 2012-04-19 2012-09-12 西安飞机工业(集团)有限责任公司 Numerical control processing method for corner of groove cavity

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007283452A (en) * 2006-04-19 2007-11-01 Mitsubishi Heavy Ind Ltd Cutting method
JP2009220218A (en) * 2008-03-17 2009-10-01 Jtekt Corp Method of cutting pocket by end mill
CN101428356A (en) * 2008-09-17 2009-05-13 西安飞机工业(集团)有限责任公司 Method for high-efficiency allowance-removing numerical control machining for groove-cavity structured part with corner
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
CN102658390A (en) * 2012-04-19 2012-09-12 西安飞机工业(集团)有限责任公司 Numerical control processing method for corner of groove cavity

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
楚王伟等: "钛合金飞机结构件高效铣削技术研究", 《工具技术》 *

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103801900A (en) * 2014-03-04 2014-05-21 广西玉柴机器股份有限公司 Processing method for cylinder body water tank
CN105642976A (en) * 2014-11-14 2016-06-08 江西昌河航空工业有限公司 Numerical control machining method of T-type groove for aluminum alloy part
CN105642978A (en) * 2014-12-01 2016-06-08 中航贵州飞机有限责任公司 Method for corner removing through plunge milling in numerical control machining
CN104923839A (en) * 2015-06-25 2015-09-23 合肥圣达电子科技实业公司 Processing method of aluminum-silicon shell
CN105312835A (en) * 2015-11-27 2016-02-10 成都飞机工业(集团)有限责任公司 Deep cavity processing method based on titanium alloy monobloc forging component
CN105522206A (en) * 2015-12-29 2016-04-27 湖南航天环宇通信科技股份有限公司 Machining method for aluminum alloy thin-walled cavity part
CN105522206B (en) * 2015-12-29 2018-02-06 湖南航天环宇通信科技股份有限公司 The processing method of aluminium alloy thin-walled cavity parts
CN108714704A (en) * 2018-08-27 2018-10-30 沈阳富创精密设备有限公司 A kind of processing technology at the depth angles chamber R
CN108941684A (en) * 2018-08-31 2018-12-07 武汉船用机械有限责任公司 A kind of processing method of the kidney-shaped skewed slot of annular thin-wall parts
CN110202192A (en) * 2019-05-28 2019-09-06 闻泰通讯股份有限公司 Improve the milling method of surface roughness
CN110394488A (en) * 2019-07-30 2019-11-01 湖北三江航天险峰电子信息有限公司 A kind of processing method at the clear angle of depth chamber
CN110394488B (en) * 2019-07-30 2020-11-24 湖北三江航天险峰电子信息有限公司 Deep cavity corner cleaning processing method

Similar Documents

Publication Publication Date Title
CN103433540A (en) Axial milling method for titanium alloy slot cavity structure
CN102331749B (en) Numerical control processing parameter optimizing method
CN105312835A (en) Deep cavity processing method based on titanium alloy monobloc forging component
CN102615362B (en) Internal screw thread processing method
CN205629488U (en) Composite milling cutter
CN105345406A (en) Efficient machining method of precise valve hole
CN102411334B (en) Plunge milling cutter path optimization method
CN105562796A (en) Step-type layered milling method for narrow-deep slot
CN106312152A (en) Method for machining thin-walled components
CN102950314A (en) Alloy drilling reamer
CN203409276U (en) Round rod inner hole reverse chamfer cutter
CN204262495U (en) Dual boot is to deep hole reamer
CN103659276A (en) Method for numerical control machining of titanium alloy part with deep groove structure
CN102814559A (en) Threading tool bit, lathe tool and method for machining threads
CN104841968A (en) Efficient plunge drilling cavity opening machining method and tool for closed deep cavity
CN110076377A (en) A kind of raising titanium alloy material vallecular cavity fillet processing efficiency method
Krebs et al. Improving the cutting conditions in the five-axis micromilling of hardened high-speed steel by applying a suitable tool inclination
CN104014989A (en) Semi-circular hole machining method
CN203918040U (en) Compound tool
CN202070800U (en) Variable lead spiral cutter and screw rod used with same during machining
CN204953988U (en) Brill mills integrative cutter
CN204295021U (en) A kind of composite hard alloy cutter
CN105479099A (en) Improved technology for machining deep groove parts by numerically-controlled lathe
CN102921987B (en) Fine deep hole machining burr preventing method
CN102825439A (en) Machining method for profile countersink drill

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20131211