CN104759670A - Machining method for titanium alloy thin wall double-tab part - Google Patents

Machining method for titanium alloy thin wall double-tab part Download PDF

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Publication number
CN104759670A
CN104759670A CN201510155487.5A CN201510155487A CN104759670A CN 104759670 A CN104759670 A CN 104759670A CN 201510155487 A CN201510155487 A CN 201510155487A CN 104759670 A CN104759670 A CN 104759670A
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China
Prior art keywords
auricle
angle
cutter
milling
milling cutter
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Granted
Application number
CN201510155487.5A
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Chinese (zh)
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CN104759670B (en
Inventor
张鹏
纪鹏
李雯佳
徐冰
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AVIC Aircraft Corp Ltd
AVIC Xian Aircraft Industry Group Co Ltd
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AVIC Aircraft Corp Xian Aircraft Branch
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Priority to CN201510155487.5A priority Critical patent/CN104759670B/en
Publication of CN104759670A publication Critical patent/CN104759670A/en
Application granted granted Critical
Publication of CN104759670B publication Critical patent/CN104759670B/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C3/00Milling particular work; Special milling operations; Machines therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C5/00Milling-cutters
    • B23C5/02Milling-cutters characterised by the shape of the cutter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C2222/00Materials of tools or workpieces composed of metals, alloys or metal matrices
    • B23C2222/88Titanium

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Knives (AREA)
  • Milling Processes (AREA)

Abstract

The invention provides a machining method for a titanium alloy thin wall double-tab part. The part contains parallel double tabs and a web arranged at the base parts of the tabs, wherein the tabs and the web are in a non-right-angle relation; a combined milling cutter is arranged and is formed by connecting three disc milling cutters and gaskets among the milling cutters in series by a central shaft; a part is clamped on a horizontal milling machine through a splicing milling tool so that the machining of tab groove cavities and the outer sides of the tabs is finished; and one angle opening milling cutter and one angle closing milling cutter are used for machining residues of opened angles and closed angles of the outer sides of the tabs of the part.

Description

A kind of processing method of titanium alloy thin wall ears sheet part
Technical field
The application relates to the manufacture of airplane parts, specifically a kind of processing method of titanium alloy thin wall ears sheet part.
Background technology
In field of machining, titanium alloy material has the advantages that other metal materials cannot have: specific strength is high, and heat resistance is high, anticorrosive good.Particularly maximum bottleneck processed by titanium alloy thin wall ears sheet class part is that the processing of material difficulty, dimensional accuracy and Geometrical Tolerance Principle are high.Usually on plain-milling machine or numerical control machining center, adopt cylindrical bar milling cutter cutter to process, and in actual production process, for special ears chip architecture, when especially spending with dihedral angle, when auricle spacing, auricle flatness and wall thickness require strict simultaneously, conventional machining method and cutter cannot ensure.Therefore, design a kind of processing method of titanium alloy thin wall ears sheet class part, greatly can facilitate actual machining, better can ensure the designing requirement of part simultaneously.
Summary of the invention
The object of the application is the processing method providing a kind of titanium alloy thin wall ears sheet part, and this part has parallel ears sheet and the web of auricle base portion, and be on-right angle relation between auricle and web, processing method is as follows:
1) cutter block is had, the pad be connected in series between three wire rod quality and milling cutter by central shaft combines, the thickness of the middle milling cutter of this cutter block mates with the vallecular cavity between auricle, the middle spacer thickness of milling cutter both sides and the consistency of thickness of part auricle, the milling cutter of both sides is for processing the outside of two auricles, and the radius of each milling cutter is less than the distance of auricle peak to web;
2) by assembled milling tool by parts fixation on horizontal milling machine, adjustment part clamping angle, the auricle of part is mated with the direction of feed of cutter block, completes the processing outside auricle vallecular cavity and auricle;
3) again by horizontal for the web of part clamping on normal vertical miller, adopt an angle of release milling cutter, the knife edge angular of this angle of release milling cutter mates with the angle of release outside auricle, the remnants of angle of release outside processing parts auricle; Adopt one and close angular cutter, this knife edge angular and auricle angle of closing outside another closing angular cutter is mated, and processing parts auricle closes the remnants at angle outside another.
The beneficial effect of the application is: 1) by cutter block once by machine-shaping outside the vallecular cavity of auricle and auricle, avoid ears sheet and can not dehisce or remain silent in process, ears sheet uniform wall thickness; 2) ears sheet base angle remnants then use angle milling cutter complete on normal vertical miller, improve the machining accuracy of part.
Below in conjunction with embodiment accompanying drawing, the application is described in further detail:
Accompanying drawing explanation
Fig. 1 is the signal of thin-walled ears sheet design of part
The structural representation of Fig. 2 cutter block
Fig. 3 ears sheet processing signal
Processing signal remaining outside Fig. 4 ears sheet
Number description: 1 web, 2 closes angle, 3 auricles, 4 vallecular cavities, 5 angle of releases, 6 central shafts, 7 first milling cutters, 8 second milling cutters, 9 the 3rd milling cutters, 10 pads, 11 milling tools, 12 angle of release milling cutters, 13 close angular cutter
Detailed description of the invention
See accompanying drawing, the part of embodiment is a titanium alloy ears sheet part, and be non-right-angle relationship between the auricle 3 of part and web 1, auricle and web side angle are angle of release 5, and angle of release also claims obtuse angle, and opposite side angle, for closing angle 2, closes angle and also claims acute angle.In order to high-precision processing auricle, the application adopts a cutter block, this cutter block is by the pad 10 between the first milling cutter 7, second milling cutter and the 3rd milling cutter 9 and milling cutter, be cascadedly combined by convenience center axle 6, the second milling cutter 8 i.e. middle thickness of milling cutter mates with the vallecular cavity 4 between auricle, the vallecular cavity of auricle must not be greater than, preferably and the consistency of thickness of vallecular cavity, it is specifically intended that the radius of each milling cutter is less than the distance of auricle peak to web, in order to avoid add the web chewing part man-hour; During processing auricle, preferably there is an auxiliary milling tool 11, this milling tool 11 is wedge structures, its locating surface is an inclined-plane, by milling tool 11 by parts fixation on horizontal milling machine, adjustment part clamping angle, the auricle 3 of part is mated with the direction of feed of cutter block, as shown in Figure 3, the processing outside auricle vallecular cavity and auricle is completed; The remnants of the angle, outside of following processing auricle 3 and web 1, by the horizontal clamping of web 1 of part on normal vertical miller, adopt an angle of release milling cutter 12, the knife edge angular of this angle of release milling cutter 12 mates with the angle of release 5 outside auricle, the remnants of angle of release outside processing parts auricle; Adopt one and close angular cutter 13, this knife edge angular and auricle angle 2 of closing outside another closing angular cutter 13 is mated, and processing parts auricle closes the remnants at angle outside another, as shown in Figure 4.

Claims (1)

1. a processing method for titanium alloy thin wall ears sheet part, this part contains parallel ears sheet and the web of auricle base portion, is on-right angle relation, it is characterized in that between auricle and web:
1) cutter block is had, the pad be connected in series between three wire rod quality and milling cutter by central shaft combines, the thickness of the middle milling cutter of this cutter block mates with the vallecular cavity between auricle, the middle spacer thickness of milling cutter both sides and the consistency of thickness of part auricle, the milling cutter of both sides is for processing the outside of two auricles, and the radius of each milling cutter is less than the distance of auricle peak to web;
2) by assembled milling tool by parts fixation on horizontal milling machine, adjustment part clamping angle, the auricle of part is mated with the direction of feed of cutter block, completes the processing outside auricle vallecular cavity and auricle;
3) again by horizontal for the web of part clamping on normal vertical miller, adopt an angle of release milling cutter, the knife edge angular of this angle of release milling cutter mates with the angle of release outside auricle, the remnants of angle of release outside processing parts auricle; Adopt one and close angular cutter, this knife edge angular and auricle angle of closing outside another closing angular cutter is mated, and processing parts auricle closes the remnants at angle outside another.
CN201510155487.5A 2015-04-02 2015-04-02 Machining method for titanium alloy thin wall double-tab part Active CN104759670B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510155487.5A CN104759670B (en) 2015-04-02 2015-04-02 Machining method for titanium alloy thin wall double-tab part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510155487.5A CN104759670B (en) 2015-04-02 2015-04-02 Machining method for titanium alloy thin wall double-tab part

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CN104759670A true CN104759670A (en) 2015-07-08
CN104759670B CN104759670B (en) 2017-01-11

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105537657A (en) * 2016-03-17 2016-05-04 沈阳飞机工业(集团)有限公司 Method for machining lug-type notch in numerical control mode
CN106077775A (en) * 2016-08-04 2016-11-09 成都航飞航空机械设备制造有限公司 A kind of processing method of three axle machine tooling back-off class workpiece
CN113352052A (en) * 2021-06-25 2021-09-07 成都飞机工业(集团)有限责任公司 Tolerance distribution machining method for double-lug-piece support part

Citations (7)

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Publication number Priority date Publication date Assignee Title
US5208979A (en) * 1991-09-19 1993-05-11 Howard Schmidt Prefracture laser formation of a stress riser groove
CN102225480A (en) * 2011-06-08 2011-10-26 沈阳飞机工业(集团)有限公司 Method for machining joint with deep and narrow groove complicated structure
CN202498411U (en) * 2012-02-18 2012-10-24 沈阳飞机工业(集团)有限公司 Composite material part contour milling profiling
CN103056433A (en) * 2012-12-31 2013-04-24 四川绵竹鑫坤机械制造有限责任公司 Machining method for conical inclined crown of blade
CN203156404U (en) * 2013-03-06 2013-08-28 西安兴航航空制造有限公司 Precision machining clamp for slide rail lugs of aerofoil
CN104439367A (en) * 2014-11-24 2015-03-25 中航飞机股份有限公司西安飞机分公司 Drilling method of airplane double-lug part and drill jig clamp
CN104475822A (en) * 2014-11-14 2015-04-01 中航飞机股份有限公司西安飞机分公司 Support drill jig structure for drilling double lug piece part

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5208979A (en) * 1991-09-19 1993-05-11 Howard Schmidt Prefracture laser formation of a stress riser groove
CN102225480A (en) * 2011-06-08 2011-10-26 沈阳飞机工业(集团)有限公司 Method for machining joint with deep and narrow groove complicated structure
CN202498411U (en) * 2012-02-18 2012-10-24 沈阳飞机工业(集团)有限公司 Composite material part contour milling profiling
CN103056433A (en) * 2012-12-31 2013-04-24 四川绵竹鑫坤机械制造有限责任公司 Machining method for conical inclined crown of blade
CN203156404U (en) * 2013-03-06 2013-08-28 西安兴航航空制造有限公司 Precision machining clamp for slide rail lugs of aerofoil
CN104475822A (en) * 2014-11-14 2015-04-01 中航飞机股份有限公司西安飞机分公司 Support drill jig structure for drilling double lug piece part
CN104439367A (en) * 2014-11-24 2015-03-25 中航飞机股份有限公司西安飞机分公司 Drilling method of airplane double-lug part and drill jig clamp

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* Cited by examiner, † Cited by third party
Title
张伟: "《典型钛合金支臂零件的全数字化加工》", 《工具技术》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105537657A (en) * 2016-03-17 2016-05-04 沈阳飞机工业(集团)有限公司 Method for machining lug-type notch in numerical control mode
CN106077775A (en) * 2016-08-04 2016-11-09 成都航飞航空机械设备制造有限公司 A kind of processing method of three axle machine tooling back-off class workpiece
CN106077775B (en) * 2016-08-04 2018-05-08 成都航飞航空机械设备制造有限公司 A kind of processing method of three axis machine tooling back-off class workpiece
CN113352052A (en) * 2021-06-25 2021-09-07 成都飞机工业(集团)有限责任公司 Tolerance distribution machining method for double-lug-piece support part

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Address after: No. 710089 in Shaanxi province Xi'an city Yanliang District West Avenue

Patentee after: AVIC Xi'an Aircraft Industry Group Co.,Ltd.

Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee before: AVIC AIRCRAFT Corp.

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Effective date of registration: 20210616

Address after: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee after: AVIC AIRCRAFT Corp.

Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee before: XI'AN AIRCRAFT BRANCH OF XI'AN AIRCRAFT INTERNATIONAL Corp.