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CN104841991A - Machining method of H-shaped thin-wall parts - Google Patents

Machining method of H-shaped thin-wall parts
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Publication number
CN104841991A
CN104841991ACN201510223018.2ACN201510223018ACN104841991ACN 104841991 ACN104841991 ACN 104841991ACN 201510223018 ACN201510223018 ACN 201510223018ACN 104841991 ACN104841991 ACN 104841991A
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CN
China
Prior art keywords
vice
cutter
parts
blank
blank assembly
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
CN201510223018.2A
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Chinese (zh)
Inventor
潘承民
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.)
Liuzhou Agriculture-Countryside-Farmer Science And Technology Ltd
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Liuzhou Agriculture-Countryside-Farmer Science And Technology Ltd
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Publication date
Application filed by Liuzhou Agriculture-Countryside-Farmer Science And Technology LtdfiledCriticalLiuzhou Agriculture-Countryside-Farmer Science And Technology Ltd
Priority to CN201510223018.2ApriorityCriticalpatent/CN104841991A/en
Publication of CN104841991ApublicationCriticalpatent/CN104841991A/en
Pendinglegal-statusCriticalCurrent

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Abstract

The invention provides a machining method of H-shaped thin-wall parts. The machining method includes steps of selecting tools in various machining stages and sequentially placing the tools into cutter discs; positioning workpieces to be machined by axial fastening reference; setting linear speed and cutting feed of rotation of a spindle of a numerical-control machine tool, clamping parts, aligning the blank ends of two parts to the end faces to form blank components, arranging a cushion block between two jaws of a vice, arranging the blank components on the cushion block and adjusting height of the cushion block so as to enable the blank components to be higher than the upper ends of the jaws of the vice by one fourth of height of the parts, and rotating and tightening screws to enable the jaws of the vice to clamp the blank component. By the machining method of H-shaped thin-wall parts, deformation of thin-wall parts due to the fact that a soft jaw or vice directly clamps thin-wall bases during milling is eliminated, machining procedures of the parts are simplified and parts are machined in pairs.

Description

The processing method of I shape thin-walled parts
Technical field
The present invention relates to a kind of processing method of I shape thin-walled parts, belong to field of mechanical technique.
Background technology
Along with Machine Design industry requires to improve constantly to properties of product, the total class of thin-walled parts quantity increases a kind of trend becoming machine industry gradually, to the crudy of thin-walled parts and required precision also more and more higher.As I shape thin-walled parts, part base is all thin-walled, the clamping thin-walled bases such as soft pawl conventional during milling or vice, and add man-hour thin-walled parts and be easily out of shape, the part quality of processing is unstable; Next is that part handling are wasted time and energy, and procedure of processing is loaded down with trivial details, and working (machining) efficiency is low; Thirdly that this kind of part requirements of handling has skilled professional skill.This, with regard to needing a kind of good processing method to improve the processing technology of this kind of part, improves its crudy and efficiency.
Summary of the invention
For overcoming the defect of prior art, the invention provides a kind of processing method of I shape thin-walled parts.
Technical scheme of the present invention is: a kind of processing method of I shape thin-walled parts, and described processing method comprises the following steps:
A, selection cutter: the cutter choosing needs of each process segment, put into cutterhead in order by it;
B, location: workpiece to be added is adopted and axially steps up origin reference location;
The linear velocity that c, setting main shaft of numerical control machine tool rotate and cutting feeding, rough machined linear velocity and cutting feeding are respectively 200 ~ 230m/min, 70 ~ 74mm/min, and accurately machined linear velocity and cutting feeding are respectively 305 ~ 370m/min, 100 ~ 115mm/min;
D, parts fixation: the blank end face of two parts is close to composition blank assembly to end face, a cushion block is placed between two jaws of vice, blank assembly is placed on cushion block, the height of adjustment cushion block, it is high that blank assembly exceeds vice jaw upper surface 1/4 part, rotates and tighten the two jaw clamping blank assemblies that screw rod makes vice;
E, there is the vice of blank assembly to be placed on the workbench of Digit Control Machine Tool clamping, adjust the position of heavy-duty cutter and blank assembly, make the blade of heavy-duty cutter aim at the cutting starting point of blank assembly, vice is fixed tightly on the workbench of Digit Control Machine Tool;
F, roughing: start Digit Control Machine Tool, with the rough machined linear velocity 200 ~ 230m/min of setting, cut feeding 65 ~ 74mm/min, roughing layer thickness 2 ~ 3 millimeters and the roughing number of plies 4 ~ 7 layers, heavy-duty cutter is from one end feed of blank assembly until the other end of blank assembly, the milling cutter trend of initiating terminal got back to by backward feed again, roughing is carried out to blank assembly, repetition milling cutter moves towards, successively cut a to the last machined layer, roughing terminates, and bottom land and cell wall leave 0.5 ~ 1 millimeter of allowance for finish respectively;
G, fine finishining: take off heavy-duty cutter, finishing cutter is contained on knife rest, start Digit Control Machine Tool, with the accurately machined linear velocity 300 ~ 370m/min of setting and cutting feeding 100 ~ 115mm/min, finishing cutter from blank assembly one end along rough machined groove feed until the other end of blank assembly, reverse milling cutter trend of getting back to initiating terminal along rough machined groove feed again, carry out cutting fine finishining to rough machined bottom land and cell wall, when meeting the requirements of precision, fine finishining terminates;
Screw rod is tightened in h, rotation, unclamps two jaws of vice, takes off two the I shape thin-walled parts censorship processed, be up to the standards, the process finishing of part.
The processing method of this I shape thin-walled parts that the present invention relates to, adopt cushion block to support, vice clamps paired part, and part is easy to loading and unloading, processing technology is simple; Process with the direct clamping thin-walled base such as soft pawl or vice the thin-walled parts distortion caused when eliminating milling; Simplify the manufacturing procedure of part, paired processing, I shape thin-walled parts symmetry is good, low amount of feeding layered milling and rigidity installation way, reduce the vibration of cutter and part, improve crudy and the working (machining) efficiency of I shape thin-walled parts, reduce loss and the processing charges of cutter, be applicable to large-scale production and processing.
Detailed description of the invention
A processing method for I shape thin-walled parts, described processing method comprises the following steps:
A, selection cutter: the cutter choosing needs of each process segment, put into cutterhead in order by it;
B, location: workpiece to be added is adopted and axially steps up origin reference location;
The linear velocity that c, setting main shaft of numerical control machine tool rotate and cutting feeding, rough machined linear velocity and cutting feeding are respectively 200 ~ 230m/min, 70 ~ 74mm/min, and accurately machined linear velocity and cutting feeding are respectively 305 ~ 370m/min, 100 ~ 115mm/min;
D, parts fixation: the blank end face of two parts is close to composition blank assembly to end face, a cushion block is placed between two jaws of vice, blank assembly is placed on cushion block, the height of adjustment cushion block, it is high that blank assembly exceeds vice jaw upper surface 1/4 part, rotates and tighten the two jaw clamping blank assemblies that screw rod makes vice;
E, there is the vice of blank assembly to be placed on the workbench of Digit Control Machine Tool clamping, adjust the position of heavy-duty cutter and blank assembly, make the blade of heavy-duty cutter aim at the cutting starting point of blank assembly, vice is fixed tightly on the workbench of Digit Control Machine Tool;
F, roughing: start Digit Control Machine Tool, with the rough machined linear velocity 200 ~ 230m/min of setting, cut feeding 65 ~ 74mm/min, roughing layer thickness 2 ~ 3 millimeters and the roughing number of plies 4 ~ 7 layers, heavy-duty cutter is from one end feed of blank assembly until the other end of blank assembly, the milling cutter trend of initiating terminal got back to by backward feed again, roughing is carried out to blank assembly, repetition milling cutter moves towards, successively cut a to the last machined layer, roughing terminates, and bottom land and cell wall leave 0.5 ~ 1 millimeter of allowance for finish respectively;
G, fine finishining: take off heavy-duty cutter, finishing cutter is contained on knife rest, start Digit Control Machine Tool, with the accurately machined linear velocity 300 ~ 370m/min of setting and cutting feeding 100 ~ 115mm/min, finishing cutter from blank assembly one end along rough machined groove feed until the other end of blank assembly, reverse milling cutter trend of getting back to initiating terminal along rough machined groove feed again, carry out cutting fine finishining to rough machined bottom land and cell wall, when meeting the requirements of precision, fine finishining terminates;
Screw rod is tightened in h, rotation, unclamps two jaws of vice, takes off two the I shape thin-walled parts censorship processed, be up to the standards, the process finishing of part.
The processing method of this I shape thin-walled parts that the present invention relates to, adopt cushion block to support, vice clamps paired part, and part is easy to loading and unloading, processing technology is simple; Process with the direct clamping thin-walled base such as soft pawl or vice the thin-walled parts distortion caused when eliminating milling; Simplify the manufacturing procedure of part, paired processing, I shape thin-walled parts symmetry is good, low amount of feeding layered milling and rigidity installation way, reduce the vibration of cutter and part, improve crudy and the working (machining) efficiency of I shape thin-walled parts, reduce loss and the processing charges of cutter, be applicable to large-scale production and processing.

Claims (1)

CN201510223018.2A2015-05-052015-05-05Machining method of H-shaped thin-wall partsPendingCN104841991A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
CN201510223018.2ACN104841991A (en)2015-05-052015-05-05Machining method of H-shaped thin-wall parts

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN201510223018.2ACN104841991A (en)2015-05-052015-05-05Machining method of H-shaped thin-wall parts

Publications (1)

Publication NumberPublication Date
CN104841991Atrue CN104841991A (en)2015-08-19

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN107175359A (en)*2017-06-062017-09-19山东金辰机械股份有限公司X-shaped slide block guide rail processing method
CN108405996A (en)*2018-03-202018-08-17深圳市守正航空工业有限公司The processing technology of Thin-walled Workpiece
CN108890227A (en)*2018-07-062018-11-27江西洪都航空工业集团有限责任公司A kind of H-shaped material numerical-control processing method
CN109333092A (en)*2018-12-122019-02-15中国航发湖南南方宇航工业有限公司 An annular thin-walled part fixture and method for machining the thin-walled outer surface of the part
CN112676619A (en)*2019-10-172021-04-20成都飞机工业(集团)有限责任公司Milling method for thin-wall frame part
CN113695948A (en)*2020-05-212021-11-26洛阳福东机械有限公司Machining method of deformation-preventing machining device for thin-walled parts in aviation industry
CN117139993A (en)*2023-07-202023-12-01武汉船用机械有限责任公司 A processing method for wing parts

Citations (6)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN85202659U (en)*1985-06-261986-08-13姜士俊Locating and grinding device for coping clamping chuck jaw
JP2007296596A (en)*2006-04-282007-11-15Toyota Motor Corp Cutting apparatus and cutting method
CN102179708A (en)*2011-03-092011-09-14浙江大学宁波理工学院Multipoint profiling rigid clamp and method for processing thin-wall workpiece by using same
CN102615520A (en)*2012-03-302012-08-01浙江大学宁波理工学院Composite material thin-walled piece clamp and method for processing composite material by using clamp
CN103567781A (en)*2013-10-112014-02-12中航飞机股份有限公司西安飞机分公司Numerical control machining clamping method of long and thin sectional material part
CN104526030A (en)*2014-12-082015-04-22湖南南方宇航工业有限公司Processing method for T-shaped thin-walled parts

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN85202659U (en)*1985-06-261986-08-13姜士俊Locating and grinding device for coping clamping chuck jaw
JP2007296596A (en)*2006-04-282007-11-15Toyota Motor Corp Cutting apparatus and cutting method
CN102179708A (en)*2011-03-092011-09-14浙江大学宁波理工学院Multipoint profiling rigid clamp and method for processing thin-wall workpiece by using same
CN102615520A (en)*2012-03-302012-08-01浙江大学宁波理工学院Composite material thin-walled piece clamp and method for processing composite material by using clamp
CN103567781A (en)*2013-10-112014-02-12中航飞机股份有限公司西安飞机分公司Numerical control machining clamping method of long and thin sectional material part
CN104526030A (en)*2014-12-082015-04-22湖南南方宇航工业有限公司Processing method for T-shaped thin-walled parts

Cited By (10)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN107175359A (en)*2017-06-062017-09-19山东金辰机械股份有限公司X-shaped slide block guide rail processing method
CN107175359B (en)*2017-06-062018-10-09山东金辰机械股份有限公司X-shaped slide block guide rail processing method
CN108405996A (en)*2018-03-202018-08-17深圳市守正航空工业有限公司The processing technology of Thin-walled Workpiece
CN108405996B (en)*2018-03-202019-03-19深圳市守正航空工业有限公司The processing technology of Thin-walled Workpiece
CN108890227A (en)*2018-07-062018-11-27江西洪都航空工业集团有限责任公司A kind of H-shaped material numerical-control processing method
CN108890227B (en)*2018-07-062019-12-17江西洪都航空工业集团有限责任公司numerical control machining method for I-shaped section
CN109333092A (en)*2018-12-122019-02-15中国航发湖南南方宇航工业有限公司 An annular thin-walled part fixture and method for machining the thin-walled outer surface of the part
CN112676619A (en)*2019-10-172021-04-20成都飞机工业(集团)有限责任公司Milling method for thin-wall frame part
CN113695948A (en)*2020-05-212021-11-26洛阳福东机械有限公司Machining method of deformation-preventing machining device for thin-walled parts in aviation industry
CN117139993A (en)*2023-07-202023-12-01武汉船用机械有限责任公司 A processing method for wing parts

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Application publication date:20150819

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