CN1552929A - High specific capacitance alloy foil and production method thereof - Google Patents

High specific capacitance alloy foil and production method thereof Download PDF

Info

Publication number
CN1552929A
CN1552929A CNA031324258A CN03132425A CN1552929A CN 1552929 A CN1552929 A CN 1552929A CN A031324258 A CNA031324258 A CN A031324258A CN 03132425 A CN03132425 A CN 03132425A CN 1552929 A CN1552929 A CN 1552929A
Authority
CN
China
Prior art keywords
percent
specific capacitance
alloy
production method
foil
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.)
Granted
Application number
CNA031324258A
Other languages
Chinese (zh)
Other versions
CN100342046C (en
Inventor
涛 王
王涛
粱岩
马保伟
刘桂云
徐涛
王�琦
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.)
Medium Aluminum Foil Co ltd
Original Assignee
Northeast Light Alloy 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 Northeast Light Alloy Co Ltd filed Critical Northeast Light Alloy Co Ltd
Priority to CNB031324258A priority Critical patent/CN100342046C/en
Priority to CNB2007100066704A priority patent/CN100478475C/en
Publication of CN1552929A publication Critical patent/CN1552929A/en
Application granted granted Critical
Publication of CN100342046C publication Critical patent/CN100342046C/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Metal Rolling (AREA)
  • Conductive Materials (AREA)

Abstract

The invention discloses a high specific capacitance alloy foil and a production method thereof, relating to an aluminum-based alloy and a production method thereof, wherein the alloy comprises the following components in parts by weight: cu0.2 to 0.25 percent of Cu0.04 to 0.06 percent of Mg0.20 percent of Zn0.1 to 0.4 percent of Mn0.8 to 1.0 percent of Fe0.8 to 1.0 percent of Si1.0 percent of Ti0.2 percent of Al100, preparing raw materials, forging, carrying out homogenization treatment at 600 ℃, carrying out hot rolling at 500 ℃ to form a thick coil, carrying out cold rolling and intermediate annealing treatment, controlling the intermediate annealing temperature at 380 ℃ to 420 ℃, and finally rolling to form a foil material with the thickness of 0.04 to 0.05 mm. The product manufactured by the method has ideal corrosion speed, can form a uniform porous corrosion surface under specified conditions, and has specific capacitance up to 370-430 Ufcm.

Description

高比电容合金箔及其生产方法High specific capacitance alloy foil and production method thereof

技术领域:本发明涉及的是一种具有高比电容的合金及其生产方法。Technical field: what the present invention relates to is an alloy with high specific capacitance and its production method.

背景技术:已有的技术中,为了增大比电容,一般是将原料在酸溶液中进行化学腐蚀,使其表面形成多孔型腐蚀层,扩大表面积。现有的比电容板,其组成(重量百分比)为Cu←0.20、Mg←0.05、Zn←0.10、Mn1.0-1.6、Fe←0.7、Si←0.60、Ti←0.15,其它杂质总和←0.10(单个元素←0.05)和余量的Al。这种合金的比电容只能达到80uFcm,而且耐蚀,腐蚀速度低,生产效率低。Background technology: In the existing technology, in order to increase the specific capacitance, the raw materials are generally chemically etched in an acid solution to form a porous corrosion layer on the surface and expand the surface area. Existing specific capacitance plate, its composition (weight percent) is Cu←0.20, Mg←0.05, Zn←0.10, Mn1.0-1.6, Fe←0.7, Si←0.60, Ti←0.15, other impurity summature←0.10( single element ←0.05) and the balance of Al. The specific capacitance of this alloy can only reach 80uFcm, and it is corrosion-resistant, with low corrosion rate and low production efficiency.

发明内容:Invention content:

本发明的目的在于:提供一种可以获得理想的腐蚀表面和高比电容的合金箔材料,并能提供一种获得理想的腐蚀表面和高比电容的合金箔的生产方法。The object of the present invention is to provide an alloy foil material that can obtain an ideal corrosion surface and high specific capacitance, and provide a production method for an alloy foil that can obtain an ideal corrosion surface and high specific capacitance.

本发明的目的是这样实现的:The purpose of the present invention is achieved like this:

一种高比电容合金箔,合金成份重量份数比为:Cu0.2-0.25、Mg0.04-0.06、Zn0.20、Mn0.1-0.4、Fe0.8-1.0、Si1.0、Ti0.2、Al100,制成其厚度为0.04-0.05mm的箔材。A high-capacitance alloy foil, the alloy composition weight ratio is: Cu0.2-0.25, Mg0.04-0.06, Zn0.20, Mn0.1-0.4, Fe0.8-1.0, Si1.0, Ti0. 2. Al100, made of foil with a thickness of 0.04-0.05mm.

上述的高比电容合金箔,合金成分的重量份数比Cu0.2、Mg0.3、Zn0.20、Mn0.3、Fe1.0、Si1.0、Ti0.3,Al100。The above-mentioned high-capacitance alloy foil has an alloy composition of Cu0.2, Mg0.3, Zn0.20, Mn0.3, Fe1.0, Si1.0, Ti0.3, Al100 in parts by weight.

一种高比电容合金箔的生产方法,按合金成份重量份数比为:Cu0.2-0.25、Mg0.04-0.06、Zn0.20、Mn0.1-0.4、Fe0.8-1.0、Si1.0、Ti0.2、Al100或者Cu0.2、Mg0.3、Zn0.20、Mn0.3、Fe1.0、Si1.0、Ti0.3,Al100,配制原料,进行锻造,在600℃进行均化处理,在500℃下进行热轧成厚卷,再冷轧然后进行中间退火处理,中间退火温度控制在380-420℃,最终轧成0.04-0.05mm厚的箔材。A production method of high specific capacitance alloy foil, according to the ratio of alloy components by weight: Cu0.2-0.25, Mg0.04-0.06, Zn0.20, Mn0.1-0.4, Fe0.8-1.0, Si1. 0, Ti0.2, Al100 or Cu0.2, Mg0.3, Zn0.20, Mn0.3, Fe1.0, Si1.0, Ti0.3, Al100, prepare raw materials, forge, and homogenize at 600°C For processing, hot rolling is carried out at 500°C to form thick coils, and then cold rolling is carried out, followed by intermediate annealing treatment. The intermediate annealing temperature is controlled at 380-420°C, and finally rolled into 0.04-0.05mm thick foil.

上述的高比电容合金箔的生产方法,所述的均匀化处理的保温时间为8小时。In the production method of the above-mentioned high specific capacitance alloy foil, the holding time of the homogenization treatment is 8 hours.

本发明的优点在于:The advantages of the present invention are:

1.传统的铝合金中Zn、Mn被视为杂质,需要严格控制其含量,本产品中,将其作为必须的添加元素,以相对高的量加入到合金中,并采用本发明的工艺方法制成的产品,其腐蚀速度较普通铝合金快,腐蚀后形成均匀的多孔腐蚀表面,提高比电容,本发明产品的比电容达380-430uFcm。其生产方法比较容易实现,在有效区间内提高Cu、Mg的含量,将有利于产品质量的提高。1. Zn and Mn are regarded as impurities in traditional aluminum alloys, and their content needs to be strictly controlled. In this product, Zn and Mn are added to the alloy in a relatively high amount as a necessary additive element, and the process method of the present invention is adopted The finished product has a faster corrosion rate than ordinary aluminum alloys, forms a uniform porous corrosion surface after corrosion, and improves specific capacitance. The specific capacitance of the product of the invention reaches 380-430uFcm. Its production method is relatively easy to implement, and increasing the content of Cu and Mg within the effective range will be beneficial to the improvement of product quality.

2.合金箔经常在汽车空调器中被应用,原散热器的结构为多根管材穿插入复合箔后经钎焊而成。使用时对损坏的管材可以更换。随着连续挤压技术生产的多孔扁管在汽车空条中的应用,逐渐对散热用钎焊复合箔提出了新的要求。用多孔扁制成的汽车空调器是由一根多孔管经加工后与复合箔钎接在一起的。这样一旦扁管有一处损坏,则会造成整体报废,而现有的复合箔抗腐蚀性能强于多孔扁管材质的抗腐性能。所以在使用过程中往往是多孔扁管先于复合箔损坏,造成整体的报废。本产品是一种既能满足钎焊要求,又能在工作条件下先于多孔扁管腐蚀的钎焊复箔,降低多孔扁管的损坏率。2. Alloy foil is often used in automobile air conditioners. The structure of the original radiator is that multiple pipes are inserted into the composite foil and then brazed. Damaged pipes can be replaced during use. With the application of porous flat tubes produced by continuous extrusion technology in automotive air strips, new requirements are gradually put forward for brazed composite foils for heat dissipation. The automotive air conditioner made of porous flat is brazed together with a composite foil after processing a porous tube. In this way, once one part of the flat tube is damaged, it will be scrapped as a whole, and the corrosion resistance of the existing composite foil is stronger than that of the material of the porous flat tube. Therefore, in the process of use, the porous flat tube is often damaged before the composite foil, resulting in the overall scrap. This product is a brazing composite foil that can not only meet the brazing requirements, but also corrode before the porous flat tube under working conditions, reducing the damage rate of the porous flat tube.

实施例1.Example 1.

高比电容合金箔,合金成份重量份数比为:Cu0.2或0.22或0.25、Mg0.04或0.05或0.06、Zn0.20、Mn0.1或0.25或0.4、Fe0.8或0.9或1.0、Si1.0、Ti0.2、Al100,制成其厚度为0.04-0.05mm的箔材。High specific capacitance alloy foil, alloy composition weight ratio: Cu0.2 or 0.22 or 0.25, Mg0.04 or 0.05 or 0.06, Zn0.20, Mn0.1 or 0.25 or 0.4, Fe0.8 or 0.9 or 1.0, Si1.0, Ti0.2, Al100, made of foil with a thickness of 0.04-0.05mm.

具体生产方法是:配制原料,进行锻造,在600℃进行均化处理,在500℃下进行热轧成厚卷,再冷轧然后进行中间退火处理,中间退火温度控制在380-420℃,最终轧成0.04-0.05mm厚的箔材。The specific production method is: preparing raw materials, forging, homogenizing treatment at 600°C, hot rolling at 500°C into thick coils, cold rolling and then intermediate annealing treatment, the intermediate annealing temperature is controlled at 380-420°C, and finally Rolled into 0.04-0.05mm thick foil.

实施例2.Example 2.

高比电容合金箔,合金成分的重量份数比Cu0.2、Mg0.3、Zn0.20、Mn0.3、Fe1.0、Si1.0、Ti0.3,Al100。其生产方法是:按配比配制原料,进行锻造,在600℃进行均化处理,在500℃下进行热轧成厚卷,再冷轧然后进行中间退火处理,中间退火温度控制在380-420℃,最终轧成0.04-0.05mm厚的箔材。所述的均匀化处理的保温时间为8-10小时。High specific capacitance alloy foil, the weight ratio of alloy components is Cu0.2, Mg0.3, Zn0.20, Mn0.3, Fe1.0, Si1.0, Ti0.3, Al100. The production method is: prepare raw materials according to the ratio, forge, homogenize at 600°C, hot-roll at 500°C to form a thick coil, then cold-roll and then carry out intermediate annealing treatment, and the intermediate annealing temperature is controlled at 380-420°C , and finally rolled into 0.04-0.05mm thick foil. The heat preservation time of the homogenization treatment is 8-10 hours.

Claims (4)

1.一种高比电容合金箔,其特征在于:合金成份重量份数比为:Cu0.2-0.25、Mg0.04-0.06、Zn0.20、Mn0.1-0.4、Fe0.8-1.0、Si1.0、Ti0.2、Al100,制成其厚度为0.04-0.05mm的箔材。1. A high specific capacitance alloy foil, characterized in that: the ratio of alloy components by weight and number is: Cu0.2-0.25, Mg0.04-0.06, Zn0.20, Mn0.1-0.4, Fe0.8-1.0, Si1.0, Ti0.2, Al100, made of foil with a thickness of 0.04-0.05mm. 2.根据权利要求1所述的高比电容合金箔,其特征在于:合金成分的重量份数比Cu0.2、Mg0.3、Zn0.20、Mn0.3、Fe1.0、Si1.0、Ti0.3,Al100。2. The high specific capacitance alloy foil according to claim 1, characterized in that: the weight ratio of the alloy components is Cu0.2, Mg0.3, Zn0.20, Mn0.3, Fe1.0, Si1.0, Ti0.3, Al100. 3.一种高比电容合金箔的生产方法,其特征是:按合盒成份重量份数比为:Cu0.2-0.25、Mg0.04-0.06、Zn0.20、Mn0.1-0.4、Fe0.8-1.0、Si1.0、Ti0.2、Al100或者Cu0.2、Mg0.3、Zn0.20、Mn0.3、Fe1.0、Si1.0、Ti0.3,Al100,配制原料,进行锻造,在600℃进行均化处理,在500℃下进行热轧成厚卷,再冷轧然后进行中间退火处理,中间退火温度控制在380-420℃,最终轧成0.04-0.05mm厚的箔材。3. A production method of high specific capacitance alloy foil, characterized in that: according to the ratio of parts by weight of the combined box components: Cu0.2-0.25, Mg0.04-0.06, Zn0.20, Mn0.1-0.4, Fe0 .8-1.0, Si1.0, Ti0.2, Al100 or Cu0.2, Mg0.3, Zn0.20, Mn0.3, Fe1.0, Si1.0, Ti0.3, Al100, preparation of raw materials, forging , homogenized at 600°C, hot-rolled at 500°C into thick coils, then cold-rolled and then intermediate annealed, the intermediate annealing temperature is controlled at 380-420°C, and finally rolled into 0.04-0.05mm thick foil . 4.根据权利要求3所述的高比电容合金箔的生产方法,其特征在于:所述的均匀化处理的保温时间为8小时。4. The production method of high specific capacitance alloy foil according to claim 3, characterized in that: the holding time of the homogenization treatment is 8 hours.
CNB031324258A 2003-06-06 2003-06-06 High specific capacitance alloy foil and production method Expired - Lifetime CN100342046C (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CNB031324258A CN100342046C (en) 2003-06-06 2003-06-06 High specific capacitance alloy foil and production method
CNB2007100066704A CN100478475C (en) 2003-06-06 2003-06-06 High specific capacitance alloy foil and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB031324258A CN100342046C (en) 2003-06-06 2003-06-06 High specific capacitance alloy foil and production method

Related Child Applications (1)

Application Number Title Priority Date Filing Date
CNB2007100066704A Division CN100478475C (en) 2003-06-06 2003-06-06 High specific capacitance alloy foil and preparation method thereof

Publications (2)

Publication Number Publication Date
CN1552929A true CN1552929A (en) 2004-12-08
CN100342046C CN100342046C (en) 2007-10-10

Family

ID=34322993

Family Applications (2)

Application Number Title Priority Date Filing Date
CNB031324258A Expired - Lifetime CN100342046C (en) 2003-06-06 2003-06-06 High specific capacitance alloy foil and production method
CNB2007100066704A Expired - Lifetime CN100478475C (en) 2003-06-06 2003-06-06 High specific capacitance alloy foil and preparation method thereof

Family Applications After (1)

Application Number Title Priority Date Filing Date
CNB2007100066704A Expired - Lifetime CN100478475C (en) 2003-06-06 2003-06-06 High specific capacitance alloy foil and preparation method thereof

Country Status (1)

Country Link
CN (2) CN100342046C (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100355527C (en) * 2005-05-20 2007-12-19 东北轻合金有限责任公司 Method for fabricating propeller blade made from aluminium alloy
WO2008058708A1 (en) * 2006-11-14 2008-05-22 Aleris Aluminum Duffel Bvba Creep resistant aluminium alloy for multilayer tubes
CN102245788A (en) * 2009-03-05 2011-11-16 东洋铝株式会社 Aluminum alloy foil for current collector and method for producing the same
CN102259252A (en) * 2011-06-14 2011-11-30 福建紫金铜业有限公司 Preparation method of high-elasticity Sn-P bronze alloy foil
CN102031328B (en) * 2009-09-30 2012-06-13 鞍钢股份有限公司 Converter charging method
CN105908021A (en) * 2016-05-18 2016-08-31 登电集团铝加工有限公司 Pure aluminum cathode foil for capacitors and manufacturing method thereof
CN110120302A (en) * 2019-04-03 2019-08-13 乳源东阳光优艾希杰精箔有限公司 A kind of 1XXX system aluminium foil and its application

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1120597A (en) * 1994-10-08 1996-04-17 东北轻合金加工厂 Negative foil of Al-Mn alloy and its prodn. method

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100355527C (en) * 2005-05-20 2007-12-19 东北轻合金有限责任公司 Method for fabricating propeller blade made from aluminium alloy
WO2008058708A1 (en) * 2006-11-14 2008-05-22 Aleris Aluminum Duffel Bvba Creep resistant aluminium alloy for multilayer tubes
US8241719B2 (en) 2006-11-14 2012-08-14 Aleris Aluminum Duffell BVBA Creep resistant aluminium alloy for multilayer tubes
CN102245788A (en) * 2009-03-05 2011-11-16 东洋铝株式会社 Aluminum alloy foil for current collector and method for producing the same
CN102245788B (en) * 2009-03-05 2013-10-23 东洋铝株式会社 Aluminum alloy foil for current collector and method for producing same
CN102031328B (en) * 2009-09-30 2012-06-13 鞍钢股份有限公司 Converter charging method
CN102259252A (en) * 2011-06-14 2011-11-30 福建紫金铜业有限公司 Preparation method of high-elasticity Sn-P bronze alloy foil
CN102259252B (en) * 2011-06-14 2015-08-05 福建紫金铜业有限公司 A kind of preparation method of high-elasticity Sn-P bronze alloy foil
CN105908021A (en) * 2016-05-18 2016-08-31 登电集团铝加工有限公司 Pure aluminum cathode foil for capacitors and manufacturing method thereof
CN110120302A (en) * 2019-04-03 2019-08-13 乳源东阳光优艾希杰精箔有限公司 A kind of 1XXX system aluminium foil and its application

Also Published As

Publication number Publication date
CN100342046C (en) 2007-10-10
CN100478475C (en) 2009-04-15
CN1990890A (en) 2007-07-04

Similar Documents

Publication Publication Date Title
JP4166613B2 (en) Aluminum alloy fin material for heat exchanger and heat exchanger formed by assembling the fin material
JP2003268512A (en) Manufacturing method of aluminum alloy composite for heat exchanger and aluminum alloy composite
CN102641889B (en) A kind of preparation method of soldering clad aluminum foil
CN112955280B (en) Aluminum alloy brazing sheet and method for producing same
CN110356069B (en) A kind of composite aluminum foil and preparation method thereof
WO2015002315A1 (en) Brazing sheet for heat exchanger, and method for manufacturing said sheet
CN115672986B (en) A preparation method for improving the flanging performance of 6-series aluminum alloy automotive sheet metal
CN114148046B (en) Aluminum alloy composite material and preparation method and application thereof
CN111347735A (en) A kind of composite plate for brazing and its manufacturing method
CN101308001A (en) High-performance aluminum alloy composite foil for heat exchanger and manufacturing method thereof
CN112605147B (en) High-corrosion-resistance and low-potential fin aluminum foil for heat exchanger and manufacturing method thereof
JP3801017B2 (en) Method for producing high-strength aluminum alloy brazing sheet for heat exchangers with excellent brazeability, formability and erosion resistance
JP5952995B2 (en) Aluminum alloy fin material for heat exchanger
CN100342046C (en) High specific capacitance alloy foil and production method
JP3801016B2 (en) Method for producing high-strength aluminum alloy brazing sheet for heat exchangers with excellent brazeability, formability and erosion resistance
EP3030684A1 (en) High strength aluminum alloy fin stock for heat exchanger
JP2002256402A (en) Method of producing fin material for use in heat exchanger
CN112626429B (en) Method for improving aging resistance stability of 6000 series aluminum alloy plate
KR20210035138A (en) High corrosion-resistant heat exchanger tube and method for preparing the same
CN118835183A (en) Aluminum foil fin manufactured by 7072 aluminum alloy processing and air conditioner radiator
JP3735700B2 (en) Aluminum alloy fin material for heat exchanger and method for producing the same
KR101401080B1 (en) A strip-cast aluminum-silicon alloy for brazing and Manufacturing method of the same
JPH03197652A (en) Production of aluminum alloy fin material for brazing
CN104233007A (en) High-thermal-conductivity heat transfer fin and manufacturing method thereof
JP2002256403A (en) Method of producing fin material for use in heat exchanger

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20190220

Address after: 401326 Datang, Xipeng Town, Jiulongpo District, Chongqing

Patentee after: CHONGQING ZHONGLYU HUAXI ALUMINIUM Co.,Ltd.

Address before: 150060 No. 11 Sandao Street, Xinjiang, Pingfang District, Harbin City, Heilongjiang Province

Patentee before: NORTHEAST LIGHT ALLOY Co.,Ltd.

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20210514

Address after: No. 488, west section of Xueyuan Road, Xindu District, Chengdu, Sichuan 610500

Patentee after: Medium aluminum foil Co.,Ltd.

Address before: 401326 Datang, Xipeng Town, Jiulongpo District, Chongqing

Patentee before: CHONGQING ZHONGLYU HUAXI ALUMINIUM Co.,Ltd.

TR01 Transfer of patent right
CX01 Expiry of patent term

Granted publication date: 20071010

CX01 Expiry of patent term