CN104858614A - Manufacturing method for part of aluminum alloy sheet with non-standard lightening hole - Google Patents

Manufacturing method for part of aluminum alloy sheet with non-standard lightening hole Download PDF

Info

Publication number
CN104858614A
CN104858614A CN201310145598.9A CN201310145598A CN104858614A CN 104858614 A CN104858614 A CN 104858614A CN 201310145598 A CN201310145598 A CN 201310145598A CN 104858614 A CN104858614 A CN 104858614A
Authority
CN
China
Prior art keywords
product
manufacturing
hours
aluminum alloy
low temperature
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
CN201310145598.9A
Other languages
Chinese (zh)
Inventor
李海昌
刘丽红
吕知先
张礼斌
侯洋
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.)
Harbin Aircraft Industry Group Co Ltd
Original Assignee
Harbin 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 Harbin Aircraft Industry Group Co Ltd filed Critical Harbin Aircraft Industry Group Co Ltd
Priority to CN201310145598.9A priority Critical patent/CN104858614A/en
Publication of CN104858614A publication Critical patent/CN104858614A/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
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass

Abstract

The invention belongs to the technical field of metal plate formation, and relates to a manufacturing method for a part of an aluminum alloy sheet with a non-standard lightening hole, and the thickness of the aluminum alloy sheet is less than 0.6 mm. The manufacturing method is a novel process for forming a metal plate in a quenching state, and controlling a material state in the part forming operation to reduce such defects as bumps generated in a flat area in the lightening hole formation. In processing, a novel quenching-state unfolded material preserved more than 30 minutes and within 48 hours at a low temperature room is leveled by a multi-roller leveler; a lightening hole is punched; and the shape is corrected (completed within 1.5 hours after the product is discharged from a low temperature room). The manufacturing method is advantaged in that, the formation and the shape correction of the part in the aging period are completed by using the characteristic that hard aluminum still has excellent plasticity in the aging period after being quenched, and a mechanical method is used for replacing a lot of manual operations to improve the production efficiency and the product forming quality.

Description

The manufacture method of the nonstandard lightening core part of a kind of aluminum alloy thin strip
Technical field
The invention belongs to Sheet Metal Forming Technology field, relate to the manufacture method of a kind of thickness at the nonstandard lightening core part of the aluminum alloy thin strip of below 0.6mm.
Background technology
Tradition forming technology is mainly soft state material molds and is shaped, and then quenches, again mould school shape.Be applicable to the shaping of the general thickness aluminum alloy part of more than 0.6mm.
The product that tradition forming technology is shaped, material is all thicker aluminium sheet, and when being applied to thin aluminum sheet, product easily produces defects such as agitating, and after quenching, school shape workload is large, and production efficiency is low, and product percent of pass is low.
Summary of the invention
The object of the invention is the manufacture method of the nonstandard lightening core part of aluminum alloy thin strip proposing a kind of below 0.6mm thickness.Technical solution of the present invention is,
1) technological preparation
Manufacture punch die by product design, die surface is bright and clean,
2) manufacture
blanking, according to product calculated with mathematical model spread material, digital control milling produces spread material;
oil removing, removes material surface dirt, impurity;
sanding section;
quenching, heat-treats product according to HB/Z276 standard;
low temperature chamber is preserved, temperature ,-15 DEG C ~-21 DEG C times, 30 minutes ~ 48 hours;
product is smoothed,
stamping, be installed debugging mould, located by the semi-finished product after smoothing on mould, eats up part of light holes;
correct, after product goes out low temperature chamber, within 1.5 hours, complete smoothing, stamping and correcting process.
The advantage that the present invention has and beneficial effect, the present invention is new as-quenched sheet metal forming technology, very controls materials behavior during part forming operation, reduces flat area when lightening core is shaped and produces defects such as agitating.Add man-hour, the new as-quenched spread material application multiroller flattening machine smoothing within more than 30 minutes, 48 hours preserved by low temperature chamber; Punching press lightening core; School shape (product completes in 1.5 hours after going out low temperature chamber).
The present invention still has this feature of good plasticity after utilizing duralumin to quench within the timeliness phase, completes shaping and the school shape of part, and instead of a large amount of handwork by mechanization means within the timeliness phase, enhances productivity and product shaping quality.
Detailed description of the invention
1) technological preparation
Manufacture punch die by product design, die surface is bright and clean,
2) manufacture
blanking, according to product calculated with mathematical model spread material, digital control milling produces spread material;
oil removing, removes material surface dirt, impurity;
sanding section;
quenching, heat-treats product according to HB/Z276 standard;
low temperature chamber is preserved, temperature ,-15 DEG C ~-21 DEG C times, 30 minutes ~ 48 hours;
product is smoothed,
stamping, be installed debugging mould, located by the semi-finished product after smoothing on mould, eats up part of light holes;
correct, after product goes out low temperature chamber, within 1.5 hours, complete smoothing, stamping and correcting process.
Embodiment
Preparing product is 0.4mm thin thick plate aluminium alloy mouth frame, and its raw material are thin and soft, easily produces deadfold (not eliminable fold), has not allowed again obvious surface scratch and hammer trace.
Making step is as follows
1) technological preparation
Nonstandard lightening core punch die is manufactured, die body any surface finish by product design.
2) manufacture
blanking, according to product calculated with mathematical model spread material, digital control milling produces spread material;
oil removing, removes material surface dirt, impurity etc.;
hair down thorn also sanding section, makes edge of materials smooth, reduces the probability of lightening core cracking, avoids injuring operator, and scratches other products and mould;
quenching, heat-treats product according to HB/Z276 standard, makes material reach new as-quenched;
low temperature chamber is preserved, temperature ,-15 DEG C ~-21 DEG C times, 30 minutes ~ 48 hours;
smoothing, multiroller flattening machine is smoothed
stamping, be installed debugging mould, location, eats up part of light holes;
correct, after product goes out low temperature chamber, within 1.5 hours, complete smoothing, stamping and correcting process;
inspection, checks the degree of accuracy of product, checks the surface quality of product simultaneously by model and drawing;
oil removing, removes the greasy dirt etc. produced in process;
homogeneous is checked, and detects the hardness of product, electrical conductivity;
mark, marked product figure number, date of manufacture etc.

Claims (1)

1. a manufacture method for the nonstandard lightening core part of aluminum alloy thin strip, is characterized in that,
1) technological preparation
Manufacture punch die by product design, die surface is bright and clean,
2) manufacture
blanking, according to product calculated with mathematical model spread material, digital control milling produces spread material;
oil removing, removes material surface dirt, impurity;
sanding section;
quenching, heat-treats product according to HB/Z276 standard;
low temperature chamber is preserved, temperature ,-15 DEG C ~-21 DEG C times, 30 minutes ~ 48 hours;
product is smoothed,
stamping, be installed debugging mould, located by the semi-finished product after smoothing on mould, eats up part of light holes;
correct, after product goes out low temperature chamber, within 1.5 hours, complete smoothing, stamping and correcting process.
CN201310145598.9A 2013-04-24 2013-04-24 Manufacturing method for part of aluminum alloy sheet with non-standard lightening hole Pending CN104858614A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310145598.9A CN104858614A (en) 2013-04-24 2013-04-24 Manufacturing method for part of aluminum alloy sheet with non-standard lightening hole

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310145598.9A CN104858614A (en) 2013-04-24 2013-04-24 Manufacturing method for part of aluminum alloy sheet with non-standard lightening hole

Publications (1)

Publication Number Publication Date
CN104858614A true CN104858614A (en) 2015-08-26

Family

ID=53905010

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310145598.9A Pending CN104858614A (en) 2013-04-24 2013-04-24 Manufacturing method for part of aluminum alloy sheet with non-standard lightening hole

Country Status (1)

Country Link
CN (1) CN104858614A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105414903A (en) * 2015-12-23 2016-03-23 常熟市淼泉压缩机配件有限公司 Improved technology for processing small-sized thin plate type part
CN106312459A (en) * 2016-09-27 2017-01-11 晋西工业集团有限责任公司 Processing technology of aluminum special-shaped long thin plate
CN106670302A (en) * 2015-11-05 2017-05-17 首都航天机械公司 Stretching forming method for spherical long melon petal-shaped parts
CN107263015A (en) * 2016-04-06 2017-10-20 哈尔滨飞机工业集团有限责任公司 A kind of interior wing flap wall part shaping techniques

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH10317123A (en) * 1997-05-16 1998-12-02 Toshiba Tungaloy Co Ltd Crystalline oriented hard coated member
US20040187312A1 (en) * 2003-03-25 2004-09-30 Shu-Yuan Liao Method of manufacturing for aluminum alloy wheel rim
KR100738796B1 (en) * 2005-05-31 2007-07-12 한국공조엔지니어링 주식회사 Manufacture method of the alumiumn cooling plate that coated by UV varnish contain metallic nano particles and a coating apparatus
CN101342556A (en) * 2008-08-22 2009-01-14 成都飞机工业(集团)有限责任公司 Method for controlling aldural stretch forming covering surface quality
CN101614317A (en) * 2009-07-28 2009-12-30 西南铝业(集团)有限责任公司 A kind of preparation method of aluminum alloy plate materials
CN102142054A (en) * 2011-04-01 2011-08-03 上海飞机制造有限公司 Method for dividing stretch forming passes of aluminum alloy skin

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH10317123A (en) * 1997-05-16 1998-12-02 Toshiba Tungaloy Co Ltd Crystalline oriented hard coated member
US20040187312A1 (en) * 2003-03-25 2004-09-30 Shu-Yuan Liao Method of manufacturing for aluminum alloy wheel rim
KR100738796B1 (en) * 2005-05-31 2007-07-12 한국공조엔지니어링 주식회사 Manufacture method of the alumiumn cooling plate that coated by UV varnish contain metallic nano particles and a coating apparatus
CN101342556A (en) * 2008-08-22 2009-01-14 成都飞机工业(集团)有限责任公司 Method for controlling aldural stretch forming covering surface quality
CN101614317A (en) * 2009-07-28 2009-12-30 西南铝业(集团)有限责任公司 A kind of preparation method of aluminum alloy plate materials
CN102142054A (en) * 2011-04-01 2011-08-03 上海飞机制造有限公司 Method for dividing stretch forming passes of aluminum alloy skin

Non-Patent Citations (5)

* Cited by examiner, † Cited by third party
Title
崔平等: "《飞机钣金成形原理与工艺》", 30 November 1995 *
王俊彪等: "基于知识的飞机钣金零件工艺性评估方法", 《计算机集成制造系统》 *
王俊彪等: "面向制造的飞机钣金零件多态模型", 《航空学报》 *
王俊彪等: "飞机钣金零件多态模型几何信息定义方法", 《西北工业大学学报》 *
陈先有等: "飞机钣金零件高能成形工艺分析", 《航空科学技术》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106670302A (en) * 2015-11-05 2017-05-17 首都航天机械公司 Stretching forming method for spherical long melon petal-shaped parts
CN105414903A (en) * 2015-12-23 2016-03-23 常熟市淼泉压缩机配件有限公司 Improved technology for processing small-sized thin plate type part
CN107263015A (en) * 2016-04-06 2017-10-20 哈尔滨飞机工业集团有限责任公司 A kind of interior wing flap wall part shaping techniques
CN106312459A (en) * 2016-09-27 2017-01-11 晋西工业集团有限责任公司 Processing technology of aluminum special-shaped long thin plate
CN106312459B (en) * 2016-09-27 2018-10-12 晋西工业集团有限责任公司 A kind of processing technology of the long thin plate of aluminum abnormity

Similar Documents

Publication Publication Date Title
CN107199287A (en) The manufacture method and particular manufacturing craft of a kind of phone housing
CN105215629A (en) A kind of forging method of complicated stainless steel forging part of thin rib tape interstitial hole
CN104858614A (en) Manufacturing method for part of aluminum alloy sheet with non-standard lightening hole
CN107855448A (en) The manufacture method of Al-alloy casing
CN106180396A (en) Rigid die thin plate method of stretch forming based on multiple spot mould
JP2013066721A (en) Method for producing face plate of golf club head
CN105537454A (en) Metal plate forming process of aircraft stepped thin-walled part
CN104971975A (en) Skin forming technology combining stretching and stamping
CN108326216B (en) A kind of thin pieces forging technology of golf iron head
CN109127847A (en) A kind of flange manufacturing process based on rubber pocket
CN105619032B (en) Method for machining disc spring
CN106544106B (en) Lubricant for stamping die and magnesium alloy stamping forming process
CN106694694A (en) Sheet metal part stamping process
CN203578543U (en) Special die group for heat insulation cover production
CN204052753U (en) Thin forging close trim mould
CN108180043A (en) A kind of assembling structure and method of turbo blade tenon tooth bottom surface cover board
CN103667819A (en) CTP plate base and preparation method thereof
CN109772966B (en) Bending method for pre-plated copper steel strip punch forming arc striking plate
CN108994205B (en) Process for manufacturing steel spade based on continuous cold punching die
CN103934341A (en) Metal plate stamping method
CN203459546U (en) Forming and shaping die structure
CN103706717A (en) Manufacturing method for hot-shaped die
CN105436370A (en) Air hole and sand hole removal technique for pressure casting
CN107199265A (en) A kind of U-shaped class part shaping techniques with radian
CN104624896A (en) Manufacturing process for L15 air inlet channel outer wall panel through die forging

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20150826