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CN110026739A - A kind of processing method of the aluminium alloy thin-walled discoid part of T4 - Google Patents

A kind of processing method of the aluminium alloy thin-walled discoid part of T4
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Publication number
CN110026739A
CN110026739ACN201910304879.1ACN201910304879ACN110026739ACN 110026739 ACN110026739 ACN 110026739ACN 201910304879 ACN201910304879 ACN 201910304879ACN 110026739 ACN110026739 ACN 110026739A
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CN
China
Prior art keywords
workpiece
walled
aluminium alloy
alloy thin
processing method
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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
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CN201910304879.1A
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Chinese (zh)
Inventor
吴高槐
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Guizhou Aerospace Fenghua Precision Equipment Co Ltd
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Guizhou Aerospace Fenghua Precision Equipment Co Ltd
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Priority to CN201910304879.1ApriorityCriticalpatent/CN110026739A/en
Publication of CN110026739ApublicationCriticalpatent/CN110026739A/en
Pendinglegal-statusCriticalCurrent

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Abstract

The present invention provides a kind of processing method of aluminium alloy thin-walled discoid part of T4, including providing cylindrical blank, machining is carried out to blank using lathe and reserves roughing surplus, Milling Process is carried out to workpiece using milling machine and reserve allowance for finish, ageing treatment is carried out to workpiece, workpiece is corrected, processes each shape feature on two end faces of workpiece using lathe finishing workpiece periphery and two end faces, using milling machine.Using technical solution of the present invention, optimize the processing technology sequence of aluminium alloy thin-walled discoid part, ageing treatment remains in the remaining cutting thermal stress in workpiece during eliminating roughing, make workpiece in subsequent finishing stage, reduce the deformation that workpiece is generated by remaining cutting heat stress influence, it lays a good foundation to improve processing quality and machining accuracy, correcting process has modified workpiece outer contour shape, size, the finished product passing rate of processing that ensure that part, improves machining accuracy and processing quality.

Description

A kind of processing method of the aluminium alloy thin-walled discoid part of T4
Technical field
The present invention relates to the processing of mechanical processing technique technical field more particularly to a kind of aluminium alloy thin-walled discoid part of T4Method.
Background technique
Thin-walled discoid part has a wide range of applications in each industrial department in national economy, however, working as thin-walled diskWhen the material of shape part is aluminium alloy, since aluminum alloy material intensity is weak, poor rigidity, the work when processing this kind of thin-walled discoid partPart easily generates deformation, influences the machining accuracy and processing quality of part.For a long time, the processing of aluminium alloy thin-walled discoid partAs a technical problem urgently to be solved among machine cut machining process.
Summary of the invention
In order to solve the above technical problems, the present invention provides a kind of processing methods of the aluminium alloy thin-walled discoid part of T4.
The present invention is achieved by the following technical programs.
The present invention provides a kind of processing method of aluminium alloy thin-walled discoid part of T4, comprising the following steps:
Step 1: providing cylindrical blank, carries out machining to blank using lathe, cuts off blank surface major part materialMaterial, and appropriate roughing surplus is reserved in blank periphery and both ends of the surface, obtain workpiece;
Step 2: Milling Process is carried out to workpiece described in step 1 using milling machine, cuts off workpiece surface roughing surplusIn some materials, and reserve allowance for finish appropriate;
Step 3: the workpiece after completion Milling Process in step 2 is subjected to ageing treatment;
Step 4: the workpiece after completion ageing treatment in step 3 is corrected;
Step 5: turnery processing is carried out to the workpiece after completing correction in step 4 using lathe, cuts off excircle of workpieceAllowance for finish on face and two end faces;
Step 6: Milling Process is carried out to the workpiece after completing turnery processing in step 5 using milling machine, cuts off workpieceSome materials on two end faces obtain each shape feature on two end faces of workpiece.
Roughing surplus described in step 1 is with a thickness of 1mm.
Carrying out Milling Process described in step 6 further includes obtaining each shape feature on one end face of the workpieceLater, Milling Process will be continued between the workpiece turning, obtains each shape on another end face of the workpieceFeature.
Carrying out machining to blank using lathe described in step 1 is by clamping with three-jaw chuck by blank in latheIt is carried out on main shaft.
Workpiece is passed through into auxiliary mould clamping in vehicle when turnery processing described in step 5, Milling Process described in step 6It is carried out on bed main shaft or milling machine table.
The auxiliary mould includes bottom plate and pressing plate, and bottom plate is fixedly connected with the lathe spindle or milling machine table, pressurePlate and bottom plate are fixed together and the workpiece are jumped the queue between bottom plate and pressing plate.
Shape feature described in step 6 includes boss, step and through-hole.
The beneficial effects of the present invention are: technical solution of the present invention is used, aluminium alloy thin-walled discoid part is optimizedProcessing technology sequence, i.e., carry out ageing treatment between roughing process and finishing step and correcting process, ageing treatment goneIn addition to remaining in the remaining cutting thermal stress in workpiece during roughing, makes workpiece in subsequent finishing stage, reduce workThe deformation that part is generated by remaining cutting heat stress influence lays a good foundation to improve processing quality and machining accuracy, corrects workSequence has modified workpiece outer contour shape, size, ensure that the finished product passing rate of processing of part, in addition, the present invention is also finishingUsing suitable clamping workpiece mode in stage, it is effective against the shear action power acted on workpiece, is further ensuredMachining accuracy and processing quality.
Detailed description of the invention
Fig. 1 is process flow chart of the invention;
Fig. 2 is using processing method of the present invention part main view obtained;
Fig. 3 is using processing method of the present invention part top view obtained;
Fig. 4 is using processing method of the present invention part rearview obtained.
Specific embodiment
Be described further below technical solution of the present invention, but claimed range be not limited to it is described.
The present invention provides a kind of processing method of aluminium alloy thin-walled discoid part of T4, as shown in Figures 1 to 4, including it is followingStep:
Step 1: providing cylindrical blank, carries out machining to blank using lathe, cuts off blank surface major part materialMaterial, and appropriate roughing surplus is reserved in blank periphery and both ends of the surface, obtain workpiece;It is preferred that roughing surplus is with a thickness of 1mm.Carrying out machining to blank using lathe is to carry out blank on lathe spindle by clamping with three-jaw chuck.
Step 2: Milling Process is carried out to workpiece in step 1 using milling machine, is cut off in workpiece surface roughing surplusSome materials, and reserve allowance for finish appropriate;
Step 3: the workpiece after completion Milling Process in step 2 is subjected to ageing treatment;
Step 4: the workpiece after completion ageing treatment in step 3 is corrected;
Step 5: turnery processing is carried out to the workpiece after completing correction in step 4 using lathe, cuts off excircle of workpieceAllowance for finish on face and two end faces;Turnery processing in step 5, workpiece passed through when Milling Process in step 6 it is auxiliaryFrock clamping is helped to carry out on lathe spindle or milling machine table.
Step 6: Milling Process is carried out to the workpiece after completing turnery processing in step 5 using milling machine, cuts off workpieceSome materials on two end faces obtain each shape feature on two end faces of workpiece.Milling in step 6 is carried out to addWork further includes after obtaining each shape feature on one end face of workpiece, adding milling is continued between workpiece turningWork obtains each shape feature on another end face of workpiece.Shape feature includes boss, step and through-hole.Auxiliary mouldIncluding bottom plate and pressing plate, bottom plate is fixedly connected with lathe spindle or milling machine table, and pressing plate and bottom plate are fixed together simultaneouslyWorkpiece is jumped the queue between bottom plate and pressing plate.
Using technical solution of the present invention, the processing technology sequence of aluminium alloy thin-walled discoid part is optimized, i.e., is slightly being addedAgeing treatment and correcting process are carried out between work process and finishing step, ageing treatment remains in during eliminating roughingRemaining cutting thermal stress in workpiece, makes workpiece in subsequent finishing stage, reduces workpiece by remaining cutting heat stress influenceAnd the deformation generated, lay a good foundation to improve processing quality and machining accuracy, correcting process have modified workpiece outer contour shape,Size ensure that the finished product passing rate of processing of part, in addition, the present invention is also in finishing stage using suitable clamping workpieceMode is effective against the shear action power acted on workpiece, further ensures machining accuracy and processing quality.

Claims (7)

CN201910304879.1A2019-04-162019-04-16A kind of processing method of the aluminium alloy thin-walled discoid part of T4PendingCN110026739A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
CN201910304879.1ACN110026739A (en)2019-04-162019-04-16A kind of processing method of the aluminium alloy thin-walled discoid part of T4

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN201910304879.1ACN110026739A (en)2019-04-162019-04-16A kind of processing method of the aluminium alloy thin-walled discoid part of T4

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CN110026739Atrue CN110026739A (en)2019-07-19

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN110653402A (en)*2019-10-122020-01-07中国电子科技集团公司第三十八研究所 A burr-free milling method for thin-walled workpieces
CN111195677A (en)*2020-01-112020-05-26中南大学Creep age forming method for large thin-wall component
CN112276118A (en)*2020-09-302021-01-29贵州安大航空锻造有限责任公司Planetary gear carrier cutting machining method
CN113414554A (en)*2021-07-072021-09-21山东明兴金属科技股份有限公司Machining process and tool for large-diameter thin-wall ring workpiece
CN114161089A (en)*2021-12-032022-03-11重庆跃进机械厂有限公司Machining method of thin-wall aluminum connecting piece
CN114643457A (en)*2022-01-202022-06-21无锡汉纳科技有限公司Material sucker processing method of curved surface photoetching machine
CN115255810A (en)*2022-04-282022-11-01三河建华高科有限责任公司Processing technique method of current collecting disc in CMP equipment
CN115446549A (en)*2022-09-212022-12-09沈阳金昌蓝宇新材料股份有限公司 A kind of processing method of thin wall pressure cylinder
CN115647754A (en)*2022-11-152023-01-31成都航新航空装备科技有限公司Deep-cavity thin-wall part machining method

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CN104148896A (en)*2014-08-042014-11-19贵州航宇科技发展股份有限公司Manufacturing method of GH4169 high-temperature alloy semi-ring
CN105710392A (en)*2014-12-042016-06-29苏州道森阀门有限公司Machining process for annular thin-wall part and tool thereof
CN107627075A (en)*2016-07-192018-01-26成都源云机械有限公司A kind of heavy-duty coal mining machine towing tank body processing technology
CN108655669A (en)*2018-05-182018-10-16陕西测易机电设备有限公司A kind of processing method of space flight and aviation thin-walled parts
CN208231370U (en)*2018-04-282018-12-14河南航天液压气动技术有限公司A kind of Thin-wall cylindrical part clamping tooling
CN109514182A (en)*2018-12-282019-03-26湖北三江航天红阳机电有限公司A kind of processing method of the thin-wall aluminum alloy with petal L-type end frame

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Publication numberPriority datePublication dateAssigneeTitle
JPH07136863A (en)*1993-11-221995-05-30Mitsubishi Motors Corp Method for manufacturing austempered ductile cast iron gears
CN102189388A (en)*2011-03-232011-09-21昆山若宇检具工业有限公司Manufacture method of door module of integral vehicle main model checking fixture
CN102886640A (en)*2012-09-042013-01-23昆山市源丰铝业有限公司Method for machining thin-wall aluminum alloy part
CN102941448A (en)*2012-11-222013-02-27河南航天精工制造有限公司Aluminum alloy highly-locking nut machining process
CN103522011A (en)*2013-10-112014-01-22泉州佰源机械科技股份有限公司Machining technology of circular knitting machine large plate
CN104148896A (en)*2014-08-042014-11-19贵州航宇科技发展股份有限公司Manufacturing method of GH4169 high-temperature alloy semi-ring
CN105710392A (en)*2014-12-042016-06-29苏州道森阀门有限公司Machining process for annular thin-wall part and tool thereof
CN107627075A (en)*2016-07-192018-01-26成都源云机械有限公司A kind of heavy-duty coal mining machine towing tank body processing technology
CN208231370U (en)*2018-04-282018-12-14河南航天液压气动技术有限公司A kind of Thin-wall cylindrical part clamping tooling
CN108655669A (en)*2018-05-182018-10-16陕西测易机电设备有限公司A kind of processing method of space flight and aviation thin-walled parts
CN109514182A (en)*2018-12-282019-03-26湖北三江航天红阳机电有限公司A kind of processing method of the thin-wall aluminum alloy with petal L-type end frame

Cited By (12)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN110653402A (en)*2019-10-122020-01-07中国电子科技集团公司第三十八研究所 A burr-free milling method for thin-walled workpieces
CN111195677A (en)*2020-01-112020-05-26中南大学Creep age forming method for large thin-wall component
CN112276118A (en)*2020-09-302021-01-29贵州安大航空锻造有限责任公司Planetary gear carrier cutting machining method
CN112276118B (en)*2020-09-302023-06-16贵州安大航空锻造有限责任公司Planet gear carrier cutting machining method
CN113414554A (en)*2021-07-072021-09-21山东明兴金属科技股份有限公司Machining process and tool for large-diameter thin-wall ring workpiece
CN114161089A (en)*2021-12-032022-03-11重庆跃进机械厂有限公司Machining method of thin-wall aluminum connecting piece
CN114161089B (en)*2021-12-032024-02-27重庆跃进机械厂有限公司Processing method of thin-wall aluminum connecting piece
CN114643457A (en)*2022-01-202022-06-21无锡汉纳科技有限公司Material sucker processing method of curved surface photoetching machine
CN115255810A (en)*2022-04-282022-11-01三河建华高科有限责任公司Processing technique method of current collecting disc in CMP equipment
CN115255810B (en)*2022-04-282024-05-14三河建华高科有限责任公司Processing technique of current collecting disc in CMP equipment
CN115446549A (en)*2022-09-212022-12-09沈阳金昌蓝宇新材料股份有限公司 A kind of processing method of thin wall pressure cylinder
CN115647754A (en)*2022-11-152023-01-31成都航新航空装备科技有限公司Deep-cavity thin-wall part machining method

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Application publication date:20190719

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