CN110238606A - A kind of processing method of the open vallecular cavity of web part - Google Patents

A kind of processing method of the open vallecular cavity of web part Download PDF

Info

Publication number
CN110238606A
CN110238606A CN201910527446.2A CN201910527446A CN110238606A CN 110238606 A CN110238606 A CN 110238606A CN 201910527446 A CN201910527446 A CN 201910527446A CN 110238606 A CN110238606 A CN 110238606A
Authority
CN
China
Prior art keywords
web
vallecular cavity
face
open
precision
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
CN201910527446.2A
Other languages
Chinese (zh)
Inventor
刘翘楚
王元军
邓乙凡
吴国伟
杨玲
牛印
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.)
Chengdu Aircraft Industrial Group Co Ltd
Original Assignee
Chengdu Aircraft Industrial 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 Chengdu Aircraft Industrial Group Co Ltd filed Critical Chengdu Aircraft Industrial Group Co Ltd
Priority to CN201910527446.2A priority Critical patent/CN110238606A/en
Publication of CN110238606A publication Critical patent/CN110238606A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P13/00Making metal objects by operations essentially involving machining but not covered by a single other subclass
    • B23P13/02Making metal objects by operations essentially involving machining but not covered by a single other subclass in which only the machining operations are important

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Slide Fasteners, Snap Fasteners, And Hook Fasteners (AREA)

Abstract

The invention discloses a kind of processing method of the open vallecular cavity of web part, steps are as follows: thick the first face of precision-machined parts structure is in place;The second face of roughing structure;The second face of precision-machined parts end, top rib;Shape in the second face of precision-machined parts;The second face of precision-machined parts web;When the structure of the second face of roughing, the web surplus of open vallecular cavity is two times for closing vallecular cavity.When finishing the second face opening vallecular cavity web, cutting width is the half for closing vallecular cavity, and from open end feed, reciprocal feed later in place along web periphery machining profile finally completes web finishing.Processing method of the invention, it is possible to prevente effectively from bullet knife problem of the open vallecular cavity web in finishing, and the quantity that compression boss are around set is reduced, promote the processing efficiency and surface quality with open vallecular cavity part.

Description

A kind of processing method of the open vallecular cavity of web part
Technical field
The present invention relates to metal cutting process fields, in particular to aerospace component numerical control processing field.
Background technique
Aerospace component is because assembly demand usually has open vallecular cavity, i.e., rib is endless totally-enclosed around vallecular cavity.It is such For structure because open end lacks support, web rigidity is poor, in web finishing, easily causes and plays knife broaching tool, cause part Quality problems.
This class formation traditional numeric-control method is as shown in Fig. 1, connects web using sheet connection boss, will be convex in processing Platform compresses, and to guarantee rigidity of the part web in processing, is later removed boss by pincers worker, and in place by end polishing. But drawback in this way of both processing presence: first, removal boss can generate more bench work amount, influence the processing of part Efficiency;Second, even now ensure that the rigidity of part in numeric control, but difficulty has been transmitted to pincers worker, beat in pincers worker Web rigidity is still poor when mill, and when polishing easily plays knife, very high to pincers worker level requirement.In actual production, due to pincers worker The case for making mistakes when opening vallecular cavity web and causing part overproof or even scrapping of polishing happens occasionally.
Summary of the invention
The purpose of the present invention aims to solve the problem that the problem of conventional open vallecular cavity processing method, and providing one kind can be in numerical control Open vallecular cavity complete stability is processed in place in process, is neither generated in process and is played knife broaching tool, do not need to clamp again The processing method of work polishing.
The present invention is realized by following scheme:
A kind of processing method of the open vallecular cavity of web part, step are as follows:
Step 1, thick the first face of precision-machined parts structure is in place;
Step 2, the second face of roughing structure, for open vallecular cavity, web surplus is two times for closing vallecular cavity;
Step 3, the second face of precision-machined parts end, top rib;
Step 4, shape in the second face of precision-machined parts;
Step 5, the second face of precision-machined parts web, cutting width is the half for closing vallecular cavity.
In the step 5, when finishing open vallecular cavity web, from open end feed, reciprocal feed later, finally along abdomen Plate periphery machining profile in place, completes web finishing.
The beneficial effects of the present invention are:
1, the processing stability of open vallecular cavity is improved, the bullet knife broaching tool being also easy to produce when the finishing of open vallecular cavity web is eliminated.
2, it can be not provided with false boss, reduce workload and quality risk when pincers worker polishing.
Detailed description of the invention
Fig. 1 conventional open vallecular cavity boss connection type.
Fig. 2 opens vallecular cavity web and finishes knife rail.
Specific embodiment
Embodiment 1
A kind of processing method of the open vallecular cavity of web part of the present invention, step are as follows:
Step 1, thick the first face of precision-machined parts structure is in place;
Step 2, the second face of roughing structure, for open vallecular cavity, web surplus is two times for closing vallecular cavity;
Step 3, the second face of precision-machined parts end, top rib;
Step 4, shape in the second face of precision-machined parts;
Step 5, the second face of precision-machined parts web, cutting width is the half for closing vallecular cavity.
In the step 5, when finishing open vallecular cavity web, from open end feed, reciprocal feed later, finally along abdomen Plate periphery machining profile in place, completes web finishing.
Embodiment 2
By taking one of certain 7050-T7451 aluminum alloy part as shown in Figure 2 open vallecular cavity as an example:
The closing vallecular cavity roughing surplus of the part is web 3mm, rib 3mm.
Finishing uses diameter 12mm, and the solid carbide of bottom tooth radius 3mm is processed.
When closing the finishing of vallecular cavity web, cutting width is 6mm.
Then for open vallecular cavity, in roughing, the surplus of web is 6mm.When finishing web, cutting width is 3mm, tool Body cutting line as shown in Fig. 2, from open end feed, in place along web periphery machining profile finally complete by reciprocal feed later Web finishing.

Claims (2)

1. a kind of processing method of the open vallecular cavity of web part, step are as follows:
Step 1, thick the first face of precision-machined parts structure is in place;
Step 2, the second face of roughing structure, for open vallecular cavity, web surplus is two times for closing vallecular cavity;
Step 3, the second face of precision-machined parts end, top rib;
Step 4, shape in the second face of precision-machined parts;
Step 5, the second face of precision-machined parts web, cutting width is the half for closing vallecular cavity.
2. a kind of according to claim 1, processing method of the open vallecular cavity of web part, which is characterized in that finishing is opened When putting vallecular cavity web, from open end feed, reciprocal feed later in place along web periphery machining profile finally completes web essence Processing.
CN201910527446.2A 2019-06-18 2019-06-18 A kind of processing method of the open vallecular cavity of web part Pending CN110238606A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910527446.2A CN110238606A (en) 2019-06-18 2019-06-18 A kind of processing method of the open vallecular cavity of web part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910527446.2A CN110238606A (en) 2019-06-18 2019-06-18 A kind of processing method of the open vallecular cavity of web part

Publications (1)

Publication Number Publication Date
CN110238606A true CN110238606A (en) 2019-09-17

Family

ID=67887882

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910527446.2A Pending CN110238606A (en) 2019-06-18 2019-06-18 A kind of processing method of the open vallecular cavity of web part

Country Status (1)

Country Link
CN (1) CN110238606A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111151985A (en) * 2020-01-07 2020-05-15 天津银宝山新科技有限公司 Method for treating and preventing flicking knife
CN114799357A (en) * 2022-05-26 2022-07-29 成都飞机工业(集团)有限责任公司 Web plate processing method
CN116551335A (en) * 2023-07-07 2023-08-08 成都飞机工业(集团)有限责任公司 L-shaped part machining method and L-shaped part

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02165837A (en) * 1988-12-20 1990-06-26 Nippon Steel Corp Superplastic forging method
JP2006305606A (en) * 2005-04-28 2006-11-09 Nippon Steel Corp Method for producing asymmetrical hat-shaped cross-section material, rolling mill
CN101745668A (en) * 2009-12-09 2010-06-23 昌河飞机工业(集团)有限责任公司 Method for processing thin-wall web plate on part
CN102581359A (en) * 2012-03-22 2012-07-18 沈阳飞机工业(集团)有限公司 Deformation controlling method for machining double-side multi-rib structural part
CN102601432A (en) * 2012-03-22 2012-07-25 沈阳飞机工业(集团)有限公司 Efficient machining method of titanium alloy sheet parts
CN103481017A (en) * 2013-09-18 2014-01-01 沈阳飞机工业(集团)有限公司 Efficient machining method for long beam thin-walled parts
CN103567705A (en) * 2013-10-11 2014-02-12 中航飞机股份有限公司西安飞机分公司 Numerical control machining method of titanium alloy part with double-sided cavity thin web structure
CN103612076A (en) * 2013-12-04 2014-03-05 中航飞机股份有限公司西安飞机分公司 Method for numerical control machining of large aircraft rib parts
CN104759699A (en) * 2015-03-27 2015-07-08 沈阳飞机工业(集团)有限公司 Machining method of double-face thin-wall web plate part
CN105710612A (en) * 2016-04-01 2016-06-29 中航飞机股份有限公司西安飞机分公司 Numerical-control processing method for aircraft wall plate part with complex structure
CN107442823A (en) * 2017-06-23 2017-12-08 成都飞机工业(集团)有限责任公司 A kind of high-rate wireless LAN method of large span vallecular cavity
CN108098255A (en) * 2017-11-30 2018-06-01 江西洪都航空工业集团有限责任公司 A kind of TA15 titanium alloys frame class parts machining process

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02165837A (en) * 1988-12-20 1990-06-26 Nippon Steel Corp Superplastic forging method
JP2006305606A (en) * 2005-04-28 2006-11-09 Nippon Steel Corp Method for producing asymmetrical hat-shaped cross-section material, rolling mill
CN101745668A (en) * 2009-12-09 2010-06-23 昌河飞机工业(集团)有限责任公司 Method for processing thin-wall web plate on part
CN102581359A (en) * 2012-03-22 2012-07-18 沈阳飞机工业(集团)有限公司 Deformation controlling method for machining double-side multi-rib structural part
CN102601432A (en) * 2012-03-22 2012-07-25 沈阳飞机工业(集团)有限公司 Efficient machining method of titanium alloy sheet parts
CN103481017A (en) * 2013-09-18 2014-01-01 沈阳飞机工业(集团)有限公司 Efficient machining method for long beam thin-walled parts
CN103567705A (en) * 2013-10-11 2014-02-12 中航飞机股份有限公司西安飞机分公司 Numerical control machining method of titanium alloy part with double-sided cavity thin web structure
CN103612076A (en) * 2013-12-04 2014-03-05 中航飞机股份有限公司西安飞机分公司 Method for numerical control machining of large aircraft rib parts
CN104759699A (en) * 2015-03-27 2015-07-08 沈阳飞机工业(集团)有限公司 Machining method of double-face thin-wall web plate part
CN105710612A (en) * 2016-04-01 2016-06-29 中航飞机股份有限公司西安飞机分公司 Numerical-control processing method for aircraft wall plate part with complex structure
CN107442823A (en) * 2017-06-23 2017-12-08 成都飞机工业(集团)有限责任公司 A kind of high-rate wireless LAN method of large span vallecular cavity
CN108098255A (en) * 2017-11-30 2018-06-01 江西洪都航空工业集团有限责任公司 A kind of TA15 titanium alloys frame class parts machining process

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
许大华,孙金海: "《机械制造技术》", 28 February 2015 *
黄玲玲: "基于工艺约束的飞机结构件特征识别方法", 《中国优秀硕士学位论文全文数据库》 *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111151985A (en) * 2020-01-07 2020-05-15 天津银宝山新科技有限公司 Method for treating and preventing flicking knife
CN114799357A (en) * 2022-05-26 2022-07-29 成都飞机工业(集团)有限责任公司 Web plate processing method
CN114799357B (en) * 2022-05-26 2022-11-29 成都飞机工业(集团)有限责任公司 Web plate processing method
WO2023226282A1 (en) * 2022-05-26 2023-11-30 成都飞机工业(集团)有限责任公司 Method for machining web
CN116551335A (en) * 2023-07-07 2023-08-08 成都飞机工业(集团)有限责任公司 L-shaped part machining method and L-shaped part
CN116551335B (en) * 2023-07-07 2023-10-03 成都飞机工业(集团)有限责任公司 L-shaped part machining method and L-shaped part

Similar Documents

Publication Publication Date Title
CN110238606A (en) A kind of processing method of the open vallecular cavity of web part
CN104308481A (en) Stator blade machining method of aeroengine compressor without mounting plate
CN108213868B (en) Process for machining metal thin-wall part by machining center
CN102806446A (en) Machining method for molds
CN114042973A (en) Machining method for sheet boss part
CN104801935A (en) Method for processing aircraft aluminum alloy special-shaped cabin
CN105312645B (en) The processing method of thin web plate titanium alloy edge strip
RU2419520C1 (en) Method of maching gas turbine engine vanes
CN101670512B (en) Method for processing ultrathin-wall parts
CN205650880U (en) Modular face milling cutter dish
CN102581359A (en) Deformation controlling method for machining double-side multi-rib structural part
CN106735316A (en) A kind of method for turning of inner hole deep groove
KR20110093706A (en) Method and apparatus for improving sheared functional edges of precision blanked finish parts
CN201871976U (en) Positioning and clamping device for machining mushroom blade shroud
CN105458066B (en) A kind of section bar shaping mould
US2243608A (en) Process of making plug gauges
CN102922232A (en) Machining process for non-standard clamp components
CN108188457A (en) Control stringer part process linear deformation processing unit (plant) and its technique
CN110480284A (en) A kind of web notch arrangement processing method
CN207448037U (en) A kind of testpieces for testing Machine-settings
CN204711332U (en) A kind of reamer with two PCD sword and many alloys guiding sword
CN109434386A (en) The processing method of edge strip jointing strip plate under a kind of wing
CN208391297U (en) A kind of substrate producing cutter
CN109894558B (en) Forging method for claw fork of transmission shaft
TWI304364B (en) Technology for cutting metal panels

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20190917

WD01 Invention patent application deemed withdrawn after publication