CN101798645B - Aluminum alloy for heat exchanger fins and preparation method thereof - Google Patents
Aluminum alloy for heat exchanger fins and preparation method thereof Download PDFInfo
- Publication number
- CN101798645B CN101798645B CN 201010149085 CN201010149085A CN101798645B CN 101798645 B CN101798645 B CN 101798645B CN 201010149085 CN201010149085 CN 201010149085 CN 201010149085 A CN201010149085 A CN 201010149085A CN 101798645 B CN101798645 B CN 101798645B
- Authority
- CN
- China
- Prior art keywords
- alloy
- heat exchanger
- aluminum alloy
- exchanger fins
- preparation
- 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.)
- Active
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 21
- 238000002360 preparation method Methods 0.000 title claims abstract description 10
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 56
- 239000000956 alloy Substances 0.000 claims abstract description 56
- 239000011888 foil Substances 0.000 claims abstract description 22
- 238000000034 method Methods 0.000 claims abstract description 14
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 13
- 238000005266 casting Methods 0.000 claims abstract description 12
- 238000005097 cold rolling Methods 0.000 claims abstract description 11
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 10
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 10
- 229910052802 copper Inorganic materials 0.000 claims abstract description 9
- 238000005098 hot rolling Methods 0.000 claims abstract description 8
- 229910052742 iron Inorganic materials 0.000 claims abstract description 8
- 238000000137 annealing Methods 0.000 claims description 8
- 238000003723 Smelting Methods 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- 238000005096 rolling process Methods 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 2
- 239000011261 inert gas Substances 0.000 claims description 2
- 239000010959 steel Substances 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims 1
- 238000002844 melting Methods 0.000 claims 1
- 230000008018 melting Effects 0.000 claims 1
- 239000011572 manganese Substances 0.000 abstract description 11
- 238000013461 design Methods 0.000 abstract description 6
- 239000000203 mixture Substances 0.000 abstract description 6
- 239000010703 silicon Substances 0.000 abstract description 5
- 238000005275 alloying Methods 0.000 abstract description 3
- 239000000463 material Substances 0.000 abstract description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 abstract description 2
- 239000007769 metal material Substances 0.000 abstract description 2
- 238000005219 brazing Methods 0.000 description 9
- 238000010438 heat treatment Methods 0.000 description 7
- 239000010949 copper Substances 0.000 description 6
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 3
- 238000003801 milling Methods 0.000 description 3
- 239000011701 zinc Substances 0.000 description 3
- 229910052725 zinc Inorganic materials 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Landscapes
- Metal Rolling (AREA)
Abstract
一种金属材料技术领域的热交换器翅片用铝合金及其制备方法,所得合金的成分配比为:Mn:1.0-1.3wt%、Si:1.0-1.3wt%、Fe:0.3-0.6wt%、Cu:0.05-0.2wt%、Zr:0.05-0.2wt%、其余为Al。本发明通过向高硅中锰铝合金中添加锆元素、并且采用无锌设计来实现合金化,采用铸造、热轧、冷轧工艺制备了相应的板带箔材。An aluminum alloy for heat exchanger fins in the technical field of metal materials and a preparation method thereof, the composition ratio of the obtained alloy is: Mn: 1.0-1.3wt%, Si: 1.0-1.3wt%, Fe: 0.3-0.6wt% %, Cu: 0.05-0.2wt%, Zr: 0.05-0.2wt%, and the rest is Al. The invention realizes alloying by adding zirconium element to the high-silicon medium-manganese aluminum alloy, adopts zinc-free design, and adopts casting, hot-rolling and cold-rolling processes to prepare corresponding plate, strip and foil materials.
Description
技术领域 technical field
本发明涉及的是一种金属材料技术领域的合金及其制备方法,具体是一种用于热交换器翅片的钎焊后屈服强度为53MPa左右、延伸率高达14%的铝合金及其制备方法。The invention relates to an alloy in the technical field of metal materials and a preparation method thereof, in particular to an aluminum alloy with a yield strength of about 53 MPa and an elongation as high as 14% for heat exchanger fins after brazing and its preparation method.
背景技术 Background technique
3xxx系列铝合金,由于其高比强度、良好的导热性、易成型性和较好的耐腐蚀性能,被大量用于制造汽车、建筑、消费电子产品等领域。近几年我国汽车行业出现了快速发展,对汽车热交换器的需求量迅速增加。作为一种可以替代纯铜的热传输材料,3003Al合金被大量应用于汽车热交换器(如水箱散热器、冷凝器与蒸发器)以实现降低成本、汽车轻量化和节能的目的。在石油资源日益减少的情况下,出于环保、节能减排的目的,汽车整车设计和零部件设计标准日益提高,这对热交换器翅片合金的力学性能提出了更高的要求,因此需要不断提高3003Al合金的力学性能,尤其是该合金的强度和塑性。3xxx series aluminum alloys are widely used in the manufacture of automobiles, construction, consumer electronics and other fields due to their high specific strength, good thermal conductivity, easy formability and good corrosion resistance. In recent years, my country's automobile industry has developed rapidly, and the demand for automobile heat exchangers has increased rapidly. As a heat transfer material that can replace pure copper, 3003Al alloy is widely used in automotive heat exchangers (such as radiators, condensers, and evaporators) to reduce costs, reduce vehicle weight, and save energy. In the case of dwindling oil resources, for the purpose of environmental protection, energy saving and emission reduction, the design standards of automobiles and parts are increasing, which puts forward higher requirements for the mechanical properties of heat exchanger fin alloys, so It is necessary to continuously improve the mechanical properties of 3003Al alloy, especially the strength and plasticity of the alloy.
热交换器翅片用合金板带箔多采用铸造+轧制(热轧,冷轧)方法制造,影响板带箔最终性能的因素较多,包括合金成分、铸造工艺、热轧和冷轧工艺、热处理工艺等。由于从工艺改善角度来提高3003Al合金性能的空间已经不大,合金成分被认为是控制合金箔加工性能和最终钎焊性能的关键。因此,通过合理的合金化设计可望研发出具有高强度、高塑性特征的新型合金以取代传统的3003Al合金。Alloy plate, strip and foil for heat exchanger fins are mostly manufactured by casting + rolling (hot rolling, cold rolling), and there are many factors that affect the final performance of the plate, strip and foil, including alloy composition, casting process, hot rolling and cold rolling process , heat treatment process, etc. Since there is not much room for improving the performance of 3003Al alloy from the perspective of process improvement, the alloy composition is considered to be the key to control the processing performance of the alloy foil and the final brazing performance. Therefore, it is expected to develop a new type of alloy with high strength and high plasticity to replace the traditional 3003Al alloy through reasonable alloying design.
经过对现有技术的检索发现,瑞典的热传输材料生产商SAPA公司(www.sapagroup.com/pages/399484/Sapa_6815.pdf)提供了一种与3003Al合金成分接近、含锌量很少的高锰(1.4-1.8wt%)低硅(0.65-1.0wt%)铝合金(商业牌号FA6800),采用该合金制造的热交换器翅片用铝合金箔钎焊后抗拉强度为130MPa左右,屈服强度为50MPa左右。而传统的AA3003合金箔钎焊后抗拉强度仅为110MPa,屈服强度为40MPa。由于高性能热交换器的发展需要,上述合金箔钎焊后的力学性能仍然需要不断提高。本专利发明人申请的中国专利“用于热交换器翅片的铝合金及其制备方法”(专利申请号CN200610085354.6)发明了一种添加锌元素的中锰(1.0-1.3wt%)高硅(1.0-1.3wt%)铝合金,该合金的强度特性较好,但是由于含有锌元素,因此该合金的腐蚀电位较负,不能满足某些热交换器翅片的需要。After searching the prior art, it was found that SAPA, a Swedish manufacturer of heat transfer materials (www.sapagroup.com/pages/399484/Sapa_6815.pdf), provided a high-quality alloy with a composition close to that of 3003Al alloy and a small amount of zinc. Manganese (1.4-1.8wt%) low-silicon (0.65-1.0wt%) aluminum alloy (commercial brand FA6800), the heat exchanger fins made of this alloy have a tensile strength of about 130MPa after brazing with aluminum alloy foil, and the yield The strength is about 50MPa. The traditional AA3003 alloy foil has a tensile strength of only 110MPa and a yield strength of 40MPa after brazing. Due to the development of high-performance heat exchangers, the mechanical properties of the above-mentioned alloy foils after brazing still need to be continuously improved. The Chinese patent "Aluminum alloy for heat exchanger fins and its preparation method" (patent application number CN200610085354.6) applied by the inventor of this patent has invented a kind of medium manganese (1.0-1.3wt%) high Silicon (1.0-1.3wt%) aluminum alloy has good strength properties, but because it contains zinc element, the corrosion potential of this alloy is relatively negative, which cannot meet the needs of some heat exchanger fins.
发明内容 Contents of the invention
本发明针对现有技术存在的上述不足,提供一种热交换器翅片用铝合金及其制备方法,通过采用高硅、中锰、无锌合金化设计来实现力学强化和腐蚀性能设计,采用铸造、热轧、冷轧工艺制备了相应的板带箔材。Aiming at the above-mentioned deficiencies in the prior art, the present invention provides an aluminum alloy for heat exchanger fins and a preparation method thereof, which realizes mechanical strengthening and corrosion performance design by adopting high-silicon, medium-manganese, and zinc-free alloying designs. The corresponding strips and foils were prepared by casting, hot rolling and cold rolling processes.
本发明是通过以下技术方案实现的:The present invention is achieved through the following technical solutions:
本发明涉及一种热交换器翅片用铝合金,其组分和重量百分比为:Mn:1.0-1.3wt%、Si:1.0-1.3wt%、Fe:0.3-0.6wt%、Cu:0.05-0.2wt%、Zr:0.05-0.2wt%、其余为Al。The invention relates to an aluminum alloy for heat exchanger fins, the composition and weight percentage of which are: Mn: 1.0-1.3wt%, Si: 1.0-1.3wt%, Fe: 0.3-0.6wt%, Cu: 0.05- 0.2wt%, Zr: 0.05-0.2wt%, the rest is Al.
本发明涉及上述热交换器翅片用铝合金的制备方法,包括以下步骤:The present invention relates to the preparation method of aluminum alloy for above-mentioned heat exchanger fin, comprises the following steps:
第一步、依次选取Al、Mn、Si、Fe、Cu和Zr或含有所述Al、Mn、Si、Fe、Cu和Zr的合金,经熔炼浇注成20-100mm的铸造合金坯后铣面,然后对铣面后的铸造合金坯进行热轧,得到合金板带,其中:Mn元素、Si元素、Fe元素、Cu元素和Zr元素分别占总质量的1.0-1.3wt%、1.0-1.3wt%、0.3-0.6wt%、0.05-0.2wt%和0.05-0.2wt%。The first step, sequentially select Al, Mn, Si, Fe, Cu and Zr or the alloy containing said Al, Mn, Si, Fe, Cu and Zr, melt and pour into a cast alloy billet of 20-100mm, and then mill the surface, Then hot-roll the cast alloy billet after face milling to obtain alloy strips, in which: Mn element, Si element, Fe element, Cu element and Zr element account for 1.0-1.3wt% and 1.0-1.3wt% of the total mass respectively , 0.3-0.6wt%, 0.05-0.2wt% and 0.05-0.2wt%.
所述的熔炼浇注是指:采用惰性气体保护熔炼炉将Al、Mn、Si、Fe、Cu和Zr在700-760℃熔化均匀后浇注入钢制模具内冷却获得铸造合金坯。The smelting and pouring refers to: Al, Mn, Si, Fe, Cu and Zr are uniformly melted at 700-760° C. in a smelting furnace protected by an inert gas, and then poured into a steel mold and cooled to obtain a casting alloy billet.
所述的热轧是指:将铣面的铸造合金坯在500℃-520℃的加热炉中预热后热轧至厚度为2-4mm。The hot rolling refers to: preheating the milled cast alloy billet in a heating furnace at 500° C. to 520° C. and then hot rolling it to a thickness of 2-4 mm.
第二步、将合金板带进行多道次冷轧后经中温退火并继续冷轧,获得用于热交换器翅片的冷轧合金箔。In the second step, the alloy strip is cold-rolled for multiple passes, then annealed at a medium temperature and continued to be cold-rolled to obtain a cold-rolled alloy foil for heat exchanger fins.
所述的多道次冷轧是指:将合金板带轧制成0.15mm的合金箔。The multi-pass cold rolling refers to rolling alloy strips into 0.15mm alloy foil.
所述的中温退火是指:在360℃-420℃的环境下退火;The medium temperature annealing refers to: annealing under the environment of 360°C-420°C;
所述的多道次冷轧是指,将合金板带轧制成厚度为0.15mm的合金箔。The multi-pass cold rolling refers to rolling alloy strips into alloy foils with a thickness of 0.15mm.
所述的继续冷轧是指:将退火后的合金箔轧制至厚度为0.10mm。The continuous cold rolling refers to rolling the annealed alloy foil to a thickness of 0.10mm.
本发明通过以下方式进行性能评价:将冷轧铝合金箔经过模拟钎焊热处理,在600℃的热处理炉内保温5分钟后出炉冷却至室温后在电子拉伸试验机上进行室温拉伸力学性能测试。The present invention conducts performance evaluation by the following method: the cold-rolled aluminum alloy foil is subjected to simulated brazing heat treatment, kept in a heat treatment furnace at 600°C for 5 minutes, then taken out of the furnace and cooled to room temperature, and then tested on the tensile mechanical properties at room temperature on an electronic tensile testing machine .
采用本发明制备所得的铝合金焊后抗拉强度可高达136MPa,屈服强度为53MPa左右,延伸率可高达14%,可适用于热交换器的翅片制造领域。The aluminum alloy prepared by the method can have a post-weld tensile strength of up to 136MPa, a yield strength of about 53MPa, and an elongation of up to 14%, and can be used in the fin manufacturing field of heat exchangers.
具体实施方式 Detailed ways
下面对本发明的实施例作详细说明,本实施例在以本发明技术方案为前提下进行实施,给出了详细的实施方式和具体的操作过程,但本发明的保护范围不限于下述的实施例。The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.
实施例1Example 1
本实施例采用熔炼和铸造方法首先制备Al-1.2Mn-1.1Si-0.5Fe-0.05Cu-0.2Zr合金板材(厚度为30mm),铣面至厚度为25mm后在500℃加热1小时后热轧成4mm,其后冷轧至0.15mm,在380℃退火后冷轧至0.10mm,采用模拟钎焊热处理后用电子拉伸试验机测试合金箔的力学性能,合金箔的抗拉强度为136MPa、屈服强度为53MPa、延伸率为14%。该合金箔的强度特性明显优于商业3003铝合金的焊后抗拉强度和屈服强度,也优于FA6800合金的强度特性。In this example, Al-1.2Mn-1.1Si-0.5Fe-0.05Cu-0.2Zr alloy plate (thickness: 30mm) is prepared by smelting and casting methods, milled to a thickness of 25mm, heated at 500°C for 1 hour, and then hot-rolled 4mm, then cold-rolled to 0.15mm, annealed at 380°C and then cold-rolled to 0.10mm, the mechanical properties of the alloy foil were tested with an electronic tensile testing machine after simulated brazing heat treatment, the tensile strength of the alloy foil was 136MPa, Yield strength was 53 MPa, and elongation was 14%. The strength characteristics of the alloy foil are significantly better than the post-weld tensile strength and yield strength of the commercial 3003 aluminum alloy, and also better than the strength characteristics of the FA6800 alloy.
实施例2Example 2
采用熔炼和铸造方法首先制备Al-1.1Mn-1.2Si-0.4Fe-0.05Cu-0.10Zr合金板材(厚度为35mm),铣面至厚度为28mm后在500℃加热1小时后热轧成2.6mm,其后冷轧至0.15mm,在380℃退火后冷轧至0.10mm,模拟钎焊热处理后测试合金箔的抗拉强度大于130MPa、延伸率大于13%。First prepare Al-1.1Mn-1.2Si-0.4Fe-0.05Cu-0.10Zr alloy plate (thickness 35mm) by smelting and casting method, face milling to thickness 28mm, heat at 500°C for 1 hour and hot roll to 2.6mm , then cold-rolled to 0.15mm, and then cold-rolled to 0.10mm after annealing at 380°C. After simulated brazing heat treatment, the tensile strength of the tested alloy foil was greater than 130MPa, and the elongation was greater than 13%.
实施例3Example 3
采用熔炼和铸造方法首先制备Al-1.3Mn-1.1Si-0.6Fe-0.1Cu-0.08Zr合金板材(厚度为25mm),铣面至厚度为20mm后在500℃加热1小时后热轧和冷轧至0.15mm,在390℃退火后冷轧至0.10mm,模拟钎焊热处理后测试合金箔的抗拉强度大于135MPa,延伸率大于14%。First prepare Al-1.3Mn-1.1Si-0.6Fe-0.1Cu-0.08Zr alloy plate (thickness 25mm) by smelting and casting method, after milling to a thickness of 20mm, heat at 500°C for 1 hour and then hot-roll and cold-roll To 0.15mm, cold rolled to 0.10mm after annealing at 390°C, after simulated brazing heat treatment, the tensile strength of the tested alloy foil is greater than 135MPa, and the elongation is greater than 14%.
显然,与热交换器翅片合金(商业3003铝合金和FA6800合金)相比,本实施例制备的合金具有高强度、高塑性特点,可获得焊后屈服强度为53MP左右、延伸率为13-14%的热交换器翅片用合金箔。上述性能的获得主要是由于采用合理的成分设计,即铝合金中锰含量适中以减少粗大含锰化合物的产生,硅含量较高以提高焊后强度,添加少量锆以产生第二相强化效应,不添加锌以控制腐蚀特性并改变相应力学性能。Obviously, compared with heat exchanger fin alloys (commercial 3003 aluminum alloy and FA6800 alloy), the alloy prepared in this example has the characteristics of high strength and high plasticity, and the yield strength after welding can be about 53MP, and the elongation is 13- 14% alloy foil for heat exchanger fins. The above performance is mainly due to the reasonable composition design, that is, the moderate manganese content in the aluminum alloy to reduce the generation of coarse manganese-containing compounds, the high silicon content to improve the post-weld strength, and the addition of a small amount of zirconium to produce the second phase strengthening effect. Zinc is not added to control the corrosion characteristics and change the corresponding mechanical properties.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201010149085 CN101798645B (en) | 2010-04-17 | 2010-04-17 | Aluminum alloy for heat exchanger fins and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201010149085 CN101798645B (en) | 2010-04-17 | 2010-04-17 | Aluminum alloy for heat exchanger fins and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101798645A CN101798645A (en) | 2010-08-11 |
CN101798645B true CN101798645B (en) | 2012-01-04 |
Family
ID=42594488
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201010149085 Active CN101798645B (en) | 2010-04-17 | 2010-04-17 | Aluminum alloy for heat exchanger fins and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101798645B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102011032A (en) * | 2010-12-30 | 2011-04-13 | 上海交通大学 | Heat-resisting aluminum alloy for heat exchangers and preparation method thereof |
CN103540877B (en) * | 2013-10-31 | 2016-03-02 | 银邦金属复合材料股份有限公司 | A kind of aluminum alloy fin complete processing improving resist collapse performance after soldering |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1473949A (en) * | 2003-07-29 | 2004-02-11 | 沈健生 | Aluminium alloy foil and its producing method |
CN1505692A (en) * | 2001-04-04 | 2004-06-16 | 1 | Method of manufacturing AIMn strip or sheet |
CN1973056A (en) * | 2004-05-26 | 2007-05-30 | 克里斯铝轧制品有限公司 | Process for producing an aluminium alloy brazing sheet, aluminium alloy brazing sheet |
EP1918394A2 (en) * | 2006-10-13 | 2008-05-07 | Sapa Heat Transfer AB | High strength and sagging resistant fin material |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH05169133A (en) * | 1991-12-19 | 1993-07-09 | Furukawa Alum Co Ltd | Manufacture of aluminum alloy tube for heat exchanger |
-
2010
- 2010-04-17 CN CN 201010149085 patent/CN101798645B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1505692A (en) * | 2001-04-04 | 2004-06-16 | 1 | Method of manufacturing AIMn strip or sheet |
CN1473949A (en) * | 2003-07-29 | 2004-02-11 | 沈健生 | Aluminium alloy foil and its producing method |
CN1973056A (en) * | 2004-05-26 | 2007-05-30 | 克里斯铝轧制品有限公司 | Process for producing an aluminium alloy brazing sheet, aluminium alloy brazing sheet |
EP1918394A2 (en) * | 2006-10-13 | 2008-05-07 | Sapa Heat Transfer AB | High strength and sagging resistant fin material |
Non-Patent Citations (1)
Title |
---|
JP特开平5-169133A 1993.07.09 |
Also Published As
Publication number | Publication date |
---|---|
CN101798645A (en) | 2010-08-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101186986B (en) | Manufacture method of high-intensity aluminum manganese alloy for heat exchanger | |
CN102286679A (en) | Rare earth aluminum alloy used for heat exchanger and preparation method thereof | |
CN101927588B (en) | Novel compound brazed aluminum alloy material for heat exchanger of automobile | |
JP6751713B2 (en) | Aluminum alloy for heat exchanger fins | |
JP4408567B2 (en) | Method of manufacturing aluminum alloy fin material | |
CN102641889B (en) | A kind of preparation method of brazing composite aluminum foil | |
CN103818051B (en) | A kind of aluminium alloy compound foil and preparation method thereof | |
CN1914340A (en) | High strength aluminum alloy fin material for heat exchanger and method for production thereof | |
CN109797321A (en) | A kind of no layer soldering aluminium alloy heat sink material and preparation method thereof | |
CN104342586B (en) | Heat exchanger multicomponent microalloying high-performance brazed aluminum alloy material | |
JP6838079B2 (en) | Aluminum composite with corrosion protection layer | |
CN108220699B (en) | Preparation method of high-strength and high-plasticity aluminum alloy double-layer composite sheet for body structural parts | |
CN111086289A (en) | Water-cooling plate, manufacturing method thereof, battery comprising water-cooling plate and new energy automobile | |
CN108220698B (en) | A kind of preparation method of high formability aluminum alloy composite plate for car body outer panel | |
CN110408819B (en) | Inflation type water cooling plate and preparation method of composite plate used by inflation type water cooling plate | |
CN101308001A (en) | High-performance aluminum alloy composite foil for heat exchanger and manufacturing method thereof | |
CN110983115B (en) | Improved 3003 aluminum alloy strip and preparation method and application thereof | |
CN105331852A (en) | Ultrathin high-strength aluminum alloy fin material and preparation method and application thereof | |
CN102286680A (en) | Rare earth aluminum alloy used for heat exchanger fin and preparation method thereof | |
CN102534319A (en) | Aluminium alloy composite material for laminated heat exchanger of automobile air conditioner and preparation method of aluminium alloy composite material | |
CN109720036A (en) | High Alcoa brazing sheet and its heat treatment process | |
CN101798645B (en) | Aluminum alloy for heat exchanger fins and preparation method thereof | |
CN101775528B (en) | Aluminum alloy for heat exchange fin and preparation method thereof | |
CN110356069B (en) | Composite aluminum foil and preparation method thereof | |
CN106498241B (en) | A kind of fin material and its production method |
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: 20180813 Address after: 201507 1111 Yue Gong Road, Jinshan District, Shanghai Patentee after: HUAFON NIKKEI ALUMINIUM CORPORATION Address before: 200240 No. 800, Dongchuan Road, Shanghai, Minhang District Co-patentee before: Huafon Aluminum Co., Ltd. Patentee before: Shanghai Jiao Tong University |
|
TR01 | Transfer of patent right | ||
CP01 | Change in the name or title of a patent holder |
Address after: 201507 1111 Yue Gong Road, Jinshan District, Shanghai Patentee after: Shanghai Huafeng Aluminum Co., Ltd. Address before: 201507 1111 Yue Gong Road, Jinshan District, Shanghai Patentee before: HUAFON NIKKEI ALUMINIUM CORPORATION |
|
CP01 | Change in the name or title of a patent holder |