CN105344779A - Forming method for artificial ageing aluminum alloy thin plate - Google Patents

Forming method for artificial ageing aluminum alloy thin plate Download PDF

Info

Publication number
CN105344779A
CN105344779A CN201510659482.6A CN201510659482A CN105344779A CN 105344779 A CN105344779 A CN 105344779A CN 201510659482 A CN201510659482 A CN 201510659482A CN 105344779 A CN105344779 A CN 105344779A
Authority
CN
China
Prior art keywords
aluminum alloy
manufacturing process
artificial aging
aluminium alloy
aging state
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
CN201510659482.6A
Other languages
Chinese (zh)
Inventor
臧金鑫
李国爱
李惠曲
李超
郝敏
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.)
BEIJING INSTITUTE OF AERONAUTICAL MATERIALS CHINA AVIATION INDUSTRY GROUP Corp
Original Assignee
BEIJING INSTITUTE OF AERONAUTICAL MATERIALS CHINA AVIATION INDUSTRY GROUP Corp
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 BEIJING INSTITUTE OF AERONAUTICAL MATERIALS CHINA AVIATION INDUSTRY GROUP Corp filed Critical BEIJING INSTITUTE OF AERONAUTICAL MATERIALS CHINA AVIATION INDUSTRY GROUP Corp
Priority to CN201510659482.6A priority Critical patent/CN105344779A/en
Publication of CN105344779A publication Critical patent/CN105344779A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/02Stamping using rigid devices or tools
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B08CLEANING
    • B08BCLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
    • B08B7/00Cleaning by methods not provided for in a single other subclass or a single group in this subclass
    • B08B7/0007Cleaning by methods not provided for in a single other subclass or a single group in this subclass by explosions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B08CLEANING
    • B08BCLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
    • B08B7/00Cleaning by methods not provided for in a single other subclass or a single group in this subclass
    • B08B7/0064Cleaning by methods not provided for in a single other subclass or a single group in this subclass by temperature changes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/02Stamping using rigid devices or tools
    • B21D22/022Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D37/00Tools as parts of machines covered by this subclass
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23GCLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
    • C23G1/00Cleaning or pickling metallic material with solutions or molten salts
    • C23G1/02Cleaning or pickling metallic material with solutions or molten salts with acid solutions
    • C23G1/04Cleaning or pickling metallic material with solutions or molten salts with acid solutions using inhibitors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Cleaning And De-Greasing Of Metallic Materials By Chemical Methods (AREA)

Abstract

The invention provides a forming method for an artificial ageing aluminum alloy thin plate. A die is cleaned through a cleaner and die cleaning gel to improve the smoothness of the die surface, and the scratch on the surface of a part in the forming process is reduced; the plate is preheated through a method of rapid induction heating, the material forming property is effectively improved. In addition, precipitated phase redissolution and recrystallization of materials can not occur due to short heating time, and thus the material property is not changed in the heating process. Heat of the part can be rapidly taken away in the forming process by conducting cooling treatment on an upper die, and thus the material property is not changed in the forming process. The artificial ageing aluminum alloy thin plate is formed through the forming method, and the process is simple, the cost is low, the large-scale industrial production can be easily achieved.

Description

A kind of manufacturing process of artificial aging state aluminium alloy sheet
Technical field
The present invention relates to a kind of manufacturing process of golden thin plate, specifically relate to a kind of manufacturing process of artificial aging state aluminium alloy sheet.
Background technology
Aluminium alloy, with combination properties such as its higher fracture toughness, good anti-fatigue performance and good corrosion resistances, is widely used as the agent structure of metal plate parts and aircraft.Because 6061-T6 aluminium alloy sheet is through artificial aging, room temperature forming property is 1/3rd of annealed state sheet material, therefore after causing part forming, resilience is serious.So at present the annealed sheet that adopts is shaped more, carry out after shaping quenching, school shape, artificial aging.Although also can realize the manufacture of part through such PROCESS FOR TREATMENT, there is grain coarsening, intensity decline, skid wire, the surface tear such as repeating heat treatment and cause, the drawback such as energy consumption is high, production efficiency is low.Therefore, need to seek a kind of cheap for manufacturing cost, machinability better and can keep the manufacturing process of material property.
Disclosing one in CN103695817 can the synchronous quenching formed technique of heat-treatable aluminum alloy, quench comprising with aqueous medium, but need again to quench and subsequent artefacts's timeliness makes material arrive using state, this forming efficiency is lower, energy consumption is larger, and it has certain limitation, below 1.0mm sheet material is not suitable for the material of repetition heat treatment number of times.
CN102974675A discloses thermo shaping method after a kind of aluminum alloy sheet metal component solid solution shrend, this method needs mold heated, then by heat transfer, Part temperature is improved, forming property is improved, but the material processed in the prior art is at 150 DEG C ~ 400 DEG C temperature range stay longer, and the time is uncertain, this means to produce considerable influence to material property.Disclosed in prior art, (" ML377 aluminum alloy heat stability study ") shows, aluminium alloy stops more than 200 DEG C, and material property will decline to a great extent, and it is comparatively large to mold heated energy consumption, and efficiency is lower.
Summary of the invention
The object of the present invention is to provide a kind of manufacturing process of artificial aging state aluminium alloy sheet, the deficiency such as overcome that efficiency in existing preparation process of aluminium alloy is lower, energy consumption is comparatively large and material property is low, this technique have cheap for manufacturing cost, machinability better and can keep the advantages such as material property.
For achieving the above object, the present invention is by the following technical solutions:
A manufacturing process for artificial aging state aluminium alloy sheet, described method comprises following processing step:
(1) cleaning solution is prepared;
(2) cleaning die is to Ra0.6 ~ 0.8 surface roughness;
(3) clean 6061-T6 aluminum alloy slab;
(4) bed die placed successively flexible heat insulating mattress and aluminum alloy slab and be fixed;
(5) by Dry ice cleaning mold extremely-20 DEG C ~-10 DEG C surface temperatures;
(6) with eddy-current heating, with 50 DEG C/s ~ 180 DEG C/s programming rate, aluminum alloy slab is heated to 510 DEG C ~ 560 DEG C, insulation 2-3min, removes described heat insulating mattress, stamping and pressurize;
(7) part of trimming correction step (6) obtains final part shape.
First preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, in described step (1), by mass, described cleaning solution comprises: hydrochloric acid 40-50g, EDTA0.2-0.3 gram, corrosion inhibiter 65-70g, water 1000-1100 gram.
Second preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, in described step (3), described the clean of aluminum alloy slab surface is comprised: with the clean cotton wiping aluminum alloy slab surface being moistened with ethanol or acetone, to wiping cotton without after greasy dirt, the manual polishing aluminum alloy slab surface of emergy that deionized water and granularity are 20 μm is dipped in fine sand felt, at least clean 5min by deionized water again, with without oily anhydrous compressed air, aluminum alloy slab surface is dried up.
3rd preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, described heat insulating mattress thickness is 1 ~ 3mm.
4th preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, in described step (5), comprise by the step of Dry ice cleaning mold: the bar-shaped dry ice of length 7-10mm and diameter 4 ~ 8mm adds in dry ice cleaner glacial cirque by (1); (2) the rifle mouth of dry ice cleaner is vertically placed in be cleaned of the mold of 20 ~ 25mm, goes out ice amount with 2 ~ 2.5kg/min, the expulsion pressure of 9 ~ 10bar and 0.2 ~ 0.25s/cm 2cleaning speed cleans.
5th preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, making top mold surface temperature reach-20 DEG C ~-10 DEG C times is 30s-60s.
6th preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, in described step (6), insulation 2min.
7th preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, in described step (6), stamping speed is 50mm/s ~ 95mm/s.
8th preferred version of described a kind of artificial aging state aluminium alloy sheet manufacturing process, in described step (6), dwell time 130 ~ 180s.
Compared with immediate prior art, the present invention has following beneficial effect:
1, technical scheme provided by the invention, by using cleaning agent, clear mould glue to mold clean, improving the roughness of die surface, decreasing the scuffing to piece surface in forming process.
2, by adopting the mode of induction Fast Heating to sheet material preheating, the effective material property improved.In addition, because the heat time is short, can not there is precipitated phase back dissolving, recrystallization in material, and therefore, in heating process, material property can not change.In addition, by carrying out cooling processing to mold, can take away rapidly part heat in forming process, therefore, in forming process, material property can not change.
3, formed artificial aging state aluminium alloy sheet by the present invention, technique is simple, cost is lower, is easy to realize large-scale industrial production.
Detailed description of the invention
Below in conjunction with embodiment, be clearly and completely described technical scheme of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.Embodiment 1:
(1) prepare cleaning solution to clean the step of die surface according to cleaning, removal black film, cleaning fluid composition is that % includes by weight: hydrochloric acid 45g, EDTA0.2g, corrosion inhibiter 65g, water 1000g.Then adopt clear mould glue to clean die surface, make mold surface roughness be Ra0.6.
(2) use the clean cotton being moistened with ethanol by clean for 6061-T6 aluminum alloy slab (thickness 1.5mm) surface wipes, nothing oil on visual cotton, manual polishing aluminum alloy slab (thickness 1.5mm) surface of emergy that deionized water and granularity are 20 μm is dipped in fine sand felt, use washed with de-ionized water piece surface to wait to brush position 5min, with without oily anhydrous compressed air, aluminum alloy slab (thickness 1.5mm) surface is dried up.
(3) be positioned over above bed die by flexible heat insulating mattress, heat insulating mattress thickness is 2mm, is positioned over by 6061-T6 aluminum alloy slab (thickness 1.5mm) above flexible heat insulating mattress also fixing.
(4) the pole shape dry ice that length is 7-10mm, diameter is 4 ~ 8mm is chosen, dry ice is joined in the glacial cirque of dry ice cleaner, by perpendicular to mold to be cleaned of the rifle mouth of dry ice cleaner, rifle mouth is apart to be cleaned 20mm, treat cleaning surface injection dry ice to clean, going out ice amount is 2.5kg/min, and expulsion pressure is 10bar, and cleaning speed is 0.25s/cm 2, after 1min, top mold surface temperature reaches-18 DEG C.
(5) after adopting the mode of (and step 4 interval 20s) eddy-current heating, with the firing rate of 50 DEG C/s, 6061-T6 aluminum alloy slab (thickness 1.5mm) is warming up to 530 DEG C immediately, insulation 3min, used time, 3s removed heat insulating mattress fast, then carrying out stamping speed is 60mm/s, pressurize 130s.
(6) to part trimming correction, final part shape is obtained, part springback capacity <0.5%.
(7) single part preparation process needs the used time to be about 8 minutes.Compared with comparative example 1, efficiency significantly increases.
Embodiment 2:
(1) prepare cleaning solution to clean the step of die surface according to cleaning, removal black film, cleaning fluid composition is that % includes by weight: hydrochloric acid 45g, EDTA0.2g, corrosion inhibiter 65g, water 1000g.Then adopt clear mould glue to clean die surface, make mold surface roughness be Ra0.6.
(2) use the clean cotton being moistened with ethanol by clean for 6061-T6 aluminum alloy slab (thickness 1.5mm) surface wipes, nothing oil on visual cotton, manual polishing 6061-T6 aluminum alloy slab (thickness 1.5mm) surface of emergy that deionized water and granularity are 20 μm is dipped in fine sand felt, use washed with de-ionized water piece surface to wait to brush position 10min, with without oily anhydrous compressed air, aluminum alloy slab (thickness 1.5mm) surface is dried up.
(3) be positioned over above counterdie by flexible heat insulating mattress, heat insulating mattress thickness is 1mm, is positioned over by 6061-T6 aluminum alloy slab (thickness 1.5mm) above flexible heat insulating mattress also fixing.
(4) the pole shape dry ice that length is 7-10mm, diameter is 4 ~ 8mm is chosen, dry ice is joined in the glacial cirque of dry ice cleaner, by perpendicular to mold to be cleaned of the rifle mouth of dry ice cleaner, rifle mouth is apart to be cleaned 22mm, treat cleaning surface injection dry ice to clean, going out ice amount is 2.3kg/min, and expulsion pressure is 9bar, and cleaning speed is 0.22 second/cm 2, after 2min, top mold surface temperature reaches-12 DEG C.
(5) after adopting the mode of (and step 4 interval 10s) eddy-current heating, with the firing rate of 180 DEG C/s, 6061-T6 aluminum alloy slab (thickness 1.5mm) is warming up to 560 DEG C immediately, insulation 2min, used time, 2s removed heat insulating mattress fast, then carrying out stamping speed is 70mm/s, pressurize 160s.
(6) to part trimming correction, final part shape is obtained, part springback capacity <0.5%.
(7) single part preparation process needs the used time to be about 8 minutes.Compared with comparative example 1, efficiency significantly increases.
Comparative example:
(1) select thickness to be 1.5mm6061-O thin plate, adopt the mould in embodiment 1 to carry out part manufacture, stamping speed is 60mm/s, pressurize 130s.
(2) part after shaping is carried out solution hardening process, solid solubility temperature is 520 DEG C, and insulation 35min, then quench in aqueous medium, water temperature is 4 DEG C.
(3) part after quenching is positioned in mould corrects shape.
(4) to part trimming correction, final part shape is obtained, part springback capacity <0.5%.
(5) after high-ranking officers' shape, part carries out artificial aging, and artificial aging system is 160 DEG C/18h.
(6) single part preparation process needs the used time to be about 19 hours 35 minutes.
Experimentally standard HB5143-1996, cutting sample on the slab in above-described embodiment and comparative example and part respectively, carry out tensile property test, test result is as shown in table 1.
Table 1 tensile property is tested
Above embodiment is only in order to illustrate that technical scheme of the present invention is not intended to limit; those of ordinary skill in the field are to be understood that; can modify to the specific embodiment of the present invention with reference to above-described embodiment or equivalent to replace, these do not depart from any amendment of spirit and scope of the invention or equivalently to replace within the claims that all awaits the reply in application.

Claims (9)

1. a manufacturing process for artificial aging state aluminium alloy sheet, is characterized in that described method comprises following processing step:
(1) cleaning solution is prepared;
(2) cleaning die is to Ra0.6 ~ 0.8 surface roughness;
(3) clean 6061-T6 aluminum alloy slab;
(4) bed die placed successively flexible heat insulating mattress and 6061-T6 aluminum alloy slab and be fixed;
(5) by Dry ice cleaning mold extremely-20 DEG C ~-10 DEG C surface temperatures;
(6) with eddy-current heating, with 50 DEG C/s ~ 180 DEG C/s programming rate, 6061-T6 aluminum alloy slab is heated to 510 DEG C ~ 560 DEG C, insulation 2-3min, removes described heat insulating mattress, stamping and pressurize;
(7) part of trimming correction step (6) obtains final part shape.
2. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, is characterized in that, in described step (1), by mass, described cleaning solution comprises: hydrochloric acid 40-50g, EDTA0.2-0.3 gram, corrosion inhibiter 65-70g, water 1000-1100 gram.
3. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, it is characterized in that, in described step (3), described the clean of aluminum alloy slab surface is comprised: with the clean cotton wiping aluminum alloy slab surface being moistened with ethanol or acetone, to wiping cotton without after greasy dirt, the manual polishing aluminum alloy slab surface of emergy that deionized water and granularity are 20 μm is dipped in fine sand felt, at least clean 5min by deionized water again, with without oily anhydrous compressed air, aluminum alloy slab surface is dried up.
4. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, described heat insulating mattress thickness is 1 ~ 3mm.
5. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, it is characterized in that, in described step (5), comprise by the step of Dry ice cleaning mold: the bar-shaped dry ice of length 7 ~ 10mm and diameter 4 ~ 8mm adds in dry ice cleaner glacial cirque by (1); (2) the rifle mouth of dry ice cleaner is vertically placed in be cleaned of the mold of 20 ~ 25mm, goes out ice amount with 2 ~ 2.5kg/min, the expulsion pressure of 9 ~ 10bar and 0.2 ~ 0.25s/cm 2cleaning speed cleans.
6. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, it is characterized in that, making top mold surface temperature reach-20 DEG C ~-10 DEG C times is 30s-60s.
7. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, is characterized in that, in described step (6), and insulation 2min.
8. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, it is characterized in that, in described step (6), stamping speed is 50mm/s ~ 95mm/s.
9. a kind of artificial aging state aluminium alloy sheet manufacturing process according to claims 1, is characterized in that, in described step (6), and dwell time 130 ~ 180s.
CN201510659482.6A 2015-10-12 2015-10-12 Forming method for artificial ageing aluminum alloy thin plate Pending CN105344779A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510659482.6A CN105344779A (en) 2015-10-12 2015-10-12 Forming method for artificial ageing aluminum alloy thin plate

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510659482.6A CN105344779A (en) 2015-10-12 2015-10-12 Forming method for artificial ageing aluminum alloy thin plate

Publications (1)

Publication Number Publication Date
CN105344779A true CN105344779A (en) 2016-02-24

Family

ID=55320920

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510659482.6A Pending CN105344779A (en) 2015-10-12 2015-10-12 Forming method for artificial ageing aluminum alloy thin plate

Country Status (1)

Country Link
CN (1) CN105344779A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107626688A (en) * 2016-07-19 2018-01-26 富泰华工业(深圳)有限公司 A kind of electronic installation of automated cleaning screen
CN109487184A (en) * 2018-12-28 2019-03-19 中南大学 A kind of artificial aging state high strength alumin ium alloy recurrence forming synchronous process
CN109623668A (en) * 2018-11-22 2019-04-16 成都飞机工业(集团)有限责任公司 A kind of minimizing technology of composite material component port surface coating

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102216484A (en) * 2008-09-19 2011-10-12 帝国创新有限公司 Process for forming aluminium alloy sheet components
CN102615201A (en) * 2012-04-25 2012-08-01 哈尔滨工业大学 Cold-hot compound die molding method for aluminum alloy sheet metal component
CN102974675A (en) * 2012-11-01 2013-03-20 哈尔滨工业大学 Heat forming method for aluminum alloy sheet metal part after solid solution and water quenching
CN103128267A (en) * 2011-12-01 2013-06-05 福特全球技术公司 Method for forming an F-temper aluminum alloy
CN103447467A (en) * 2013-08-21 2013-12-18 无锡蠡湖叶轮制造有限公司 Method for cleaning metal mould
CN103469221A (en) * 2013-09-05 2013-12-25 天津东义镁制品股份有限公司 Cleaning liquor and treatment method for removing residual magnesium alloys in die
CN103695817A (en) * 2013-12-12 2014-04-02 南京航空航天大学 Heat-treatable aluminum alloy synchronous-quenching thermal-forming process
WO2014068493A1 (en) * 2012-10-31 2014-05-08 Aisin Takaoka Co., Ltd. Die-quenching method and apparatus of an aluminum alloy material
WO2014097631A1 (en) * 2012-12-21 2014-06-26 川崎重工業株式会社 Method for manufacturing aluminum alloy molded component for aircraft, and molded component for aircraft
CN104959437A (en) * 2015-07-10 2015-10-07 中南大学 Forming method for improving forming performance of 6XXX series aluminum alloy plate

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102216484A (en) * 2008-09-19 2011-10-12 帝国创新有限公司 Process for forming aluminium alloy sheet components
CN103128267A (en) * 2011-12-01 2013-06-05 福特全球技术公司 Method for forming an F-temper aluminum alloy
CN102615201A (en) * 2012-04-25 2012-08-01 哈尔滨工业大学 Cold-hot compound die molding method for aluminum alloy sheet metal component
WO2014068493A1 (en) * 2012-10-31 2014-05-08 Aisin Takaoka Co., Ltd. Die-quenching method and apparatus of an aluminum alloy material
CN102974675A (en) * 2012-11-01 2013-03-20 哈尔滨工业大学 Heat forming method for aluminum alloy sheet metal part after solid solution and water quenching
WO2014097631A1 (en) * 2012-12-21 2014-06-26 川崎重工業株式会社 Method for manufacturing aluminum alloy molded component for aircraft, and molded component for aircraft
CN103447467A (en) * 2013-08-21 2013-12-18 无锡蠡湖叶轮制造有限公司 Method for cleaning metal mould
CN103469221A (en) * 2013-09-05 2013-12-25 天津东义镁制品股份有限公司 Cleaning liquor and treatment method for removing residual magnesium alloys in die
CN103695817A (en) * 2013-12-12 2014-04-02 南京航空航天大学 Heat-treatable aluminum alloy synchronous-quenching thermal-forming process
CN104959437A (en) * 2015-07-10 2015-10-07 中南大学 Forming method for improving forming performance of 6XXX series aluminum alloy plate

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107626688A (en) * 2016-07-19 2018-01-26 富泰华工业(深圳)有限公司 A kind of electronic installation of automated cleaning screen
CN109623668A (en) * 2018-11-22 2019-04-16 成都飞机工业(集团)有限责任公司 A kind of minimizing technology of composite material component port surface coating
CN109487184A (en) * 2018-12-28 2019-03-19 中南大学 A kind of artificial aging state high strength alumin ium alloy recurrence forming synchronous process

Similar Documents

Publication Publication Date Title
CN105344779A (en) Forming method for artificial ageing aluminum alloy thin plate
CN103203390A (en) Processing method for beta titanium alloy wires used for glass frames
CN201555422U (en) Device for removing water on surface of material
CN105215124A (en) A kind of manufacturing process of artificial aging state aluminium alloy sheet
CN105215121A (en) A kind of manufacturing process of artificial aging state aluminium alloy sheet
CN105215123A (en) A kind of manufacturing process of natrual ageing state aluminium lithium alloy thin plate
CN105344780A (en) Forming method for artificial aging-state aluminum alloy sheet
CN105215122A (en) A kind of manufacturing process of natrual ageing state aluminium alloy sheet
CN105344786A (en) Forming method for artificial aging-state aluminum alloy sheet
CN105220091A (en) A kind of manufacturing process of artificial aging state Al-Li alloy thin plate
CN102082406B (en) Preparation method of aluminum clad steel pre-stranded wire
CN105215125A (en) A kind of manufacturing process of natrual ageing state aluminium alloy sheet
CN102424908A (en) Spring wire production method
CN102002658B (en) Annealing process of cold rolled titanium roll
CN106694603B (en) A kind of preparation method of beraloy silk material
CN102310357B (en) Liquid-phase plasma polishing liquid and polishing process of aluminum product
CN107052345A (en) Copper alloy injection molding process
CN210647781U (en) Galvanized wire processing device
CN105483502A (en) Production method for spring wire
CN105603339A (en) Electric pulse auxiliary aging treatment method for ZL114A aluminum alloy
CN108311568A (en) A kind of workpiece high efficiency bending technique
CN110205452A (en) Hydrophobic steel plate of a kind of micron of octahedron/nano whiskers structure and preparation method thereof
CN109402538A (en) A kind of natrual ageing state high strength alumin ium alloy recurrence forming synchronous process
CN203728891U (en) Bare wire annealing device
RU2006109798A (en) METHOD FOR PRODUCING PUMP BARS FOR DEPTH PUMPS

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
CB02 Change of applicant information

Address after: 100095 Haidian District hot springs town, Beijing Village

Applicant after: AECC BEIJING INSTITUTE OF AERONAUTICAL MATERIALS

Address before: 100095 Haidian District hot springs town, Beijing Village

Applicant before: AVIC BEIJING INSTITUTE OF AERONAUTICAL MATERIALS

CB02 Change of applicant information
RJ01 Rejection of invention patent application after publication

Application publication date: 20160224

RJ01 Rejection of invention patent application after publication