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 PDFInfo
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- 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
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- product
- manufacturing
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- aluminum alloy
- low temperature
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making 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
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.
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 |
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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 |
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CN (1) | CN104858614A (en) |
Cited By (4)
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)
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JPH10317123A (en) * | 1997-05-16 | 1998-12-02 | Toshiba Tungaloy Co Ltd | Crystalline oriented hard coated member |
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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 |
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2013
- 2013-04-24 CN CN201310145598.9A patent/CN104858614A/en active Pending
Patent Citations (6)
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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 |
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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 |
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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》 * |
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Cited By (5)
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 |
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Application publication date: 20150826 |