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JPS6353477B2 - - Google Patents
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JPS6353477B2 - - Google Patents

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Publication number
JPS6353477B2
JPS6353477B2 JP53090297A JP9029778A JPS6353477B2 JP S6353477 B2 JPS6353477 B2 JP S6353477B2 JP 53090297 A JP53090297 A JP 53090297A JP 9029778 A JP9029778 A JP 9029778A JP S6353477 B2 JPS6353477 B2 JP S6353477B2
Authority
JP
Japan
Prior art keywords
fin
weight
manganese
cross
thickness
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.)
Expired
Application number
JP53090297A
Other languages
Japanese (ja)
Other versions
JPS5517072A (en
Inventor
Akira Kuboki
Nobuyuki Matsuzoe
Hideki Hoshino
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.)
Mitsubishi Chemical Corp
MA Aluminum Corp
Original Assignee
Mitsubishi Aluminum Co Ltd
Kasei Naoetsu Industries 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 Mitsubishi Aluminum Co Ltd, Kasei Naoetsu Industries Ltd filed Critical Mitsubishi Aluminum Co Ltd
Priority to JP9029778A priority Critical patent/JPS5517072A/en
Publication of JPS5517072A publication Critical patent/JPS5517072A/en
Publication of JPS6353477B2 publication Critical patent/JPS6353477B2/ja
Granted legal-status Critical Current

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Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は熱交換器用クロス・フイン材の製造法
に関する。詳しくは、0.1〜2重量%のマンガン
を含むアルミニウム合金を用いて、強度およびフ
イン加工性を向上させた熱交換器用クロス・フイ
ン材を製造する方法に関する。 従来、ルームクーラー、冷蔵庫などには、厚さ
0.15〜0.3mmの薄板にカラー状の立上りを有する
直径5〜15mmの孔を穿設し(フイン加工)、この
孔に、冷却媒体を通過させるための管を挿通させ
てなる熱交換器が用いられている。この熱交換器
で用いられ、上記フイン加工を施した薄板は一般
にクロス・フインと呼ばれている。冷却媒体の熱
は管、およびカラー状の立上りを経てクロス・フ
インに伝導され、広表面積のクロス・フインから
有効に外部に放散される。 このクロス・フイン用材料(以下、クロス・フ
イン材という)としては上記フイン加工の容易な
JIS 1050、JIS 1100、JIS 1200などの純アルミニ
ウムまたはJIS 3003などのアルミニウム―マンガ
ン合金が用いられている。 クロス・フイン材は、一般には、上記純アルミ
ニウムまたはアルミニウム―マンガン合金の溶湯
を半連続鋳造法により鋳造してスラブとし、これ
を熱間圧延して厚さ3〜10mmの帯状板を得、次い
でこれをさらに冷間圧延して薄板としたのち、焼
鈍処理を施すことによつて製造されている。 近年、コストダウンを目的として、クロス・フ
インの薄肉化が望まれているがクロス・フインを
薄肉化すれば、それだけフインの強度が低下する
ので、フインのカラー状の立上り部と管との密着
性が不十分となり、この結果、管内の冷却媒体と
フインとの間の熱伝導効率が低下する。 そこで、本発明者らは、フイン加工が容易で、
かつ、高い強度を有するクロス・フイン材を得る
ために検討した結果、直接連続鋳造圧延法、すな
わち、アルミニウム―マンガン合金の溶湯を回転
する1対のロールにより構成される鋳型に導入
し、この鋳型によつて冷却および圧延する方法に
より、合金の溶湯から直接前記帯状板を製造すれ
ば、得られるクロス・フイン材は優れたフイン加
工性とともに高い強度を有することを見出し、本
発明に到達した。 すなわち、本発明の目的は、優れたフイン加工
性および高い強度を有するクロス・フイン材を製
造することであり、この目的は、0.1〜2重量%
のマンガンを含むアルミニウム合金の溶湯を連続
的に鋳造圧延して直接、3〜10mmの帯状板とな
し、次いでこの帯状板を冷間圧延して厚さ0.05〜
0.15mmの薄板とし、その後、これに焼鈍処理を施
すことによつて達成される。 次に、本発明を詳細に説明する。 本発明方法において、クロス・フイン材は0.1
〜2重量%のマンガンを含むアルミニウム合金を
用いて製造する。 マンガンは上記範囲でアルミニウム中に含有さ
れて、フインの耐食性および加工性を損わずに、
強度を向上させる。マンガン含有量が2.5重量%
を超えるとフイン材の耐食性が低下する。また、
鋳造時にマンガンを含む金属間化合物が粗大に晶
出するため、加工性も低下するので、フイン材に
フイン加工を施すと、フインのカラー状立上り部
に一部割れが発生する。また、マンガン含有量が
0.1重量%より少なければ、フインの強度を向上
させることができないのでマンガン含有量は0.1
〜2.5重量%、好ましくは0.3〜2重量%である。 マンガン含有量が0.3重量%より少ないときは、
フイン材の強度を向上させるため必要に応じて
0.05〜0.2重量%のジルコニウムを合金に含有さ
せることもできる。 アルミニウム合金中には、鉄、銅、マグネシウ
ム、珪素などの不純物が含まれているが、本発明
のフイン材において鉄は鋳造時、マンガンを含む
金属間化合物の晶出を促進し、フイン加工性を低
下させ、銅は、耐食性を低下させる。 また、珪素はフイン加工性および強度を低下さ
せる。 従つて、鉄は0.5重量%以下、とくに、0.3重量
%以下、銅は0.2重量%以下、とくに、0.1重量%
以下そして珪素は0.4重量%以下、とくに0.2重量
%以下とすることが好ましい。 マグネシウムは0.5重量%を超えるとフイン加
工が困難となるので0.5重量%以下好ましくは0.3
重量%以下とする。 本発明方法では上記0.1〜2重量%のマンガン
を含むアルミニウム合金の溶湯を連続的に鋳造圧
延して直接、厚さ3〜10mmの帯状板を得、これを
冷間圧延して厚さ0.05〜0.15mmの薄板とする。 上記の連続的な鋳造圧延によつて得られる帯状
板の板厚3〜10mmとは、マンガン、鉄、珪素など
の合金中の成分元素のアルミニウム中への強制固
溶が十分に行なわれて連続的な鋳造圧延の効果が
十分に生かされる板厚、即ち溶湯の冷却が均一か
つ急速に行なわれるような鋳造圧延状態の得られ
る板厚である。3mm未満という余りに薄い板厚の
帯状板を溶湯から連続的な鋳造圧延により直接得
ることは技術的な困難が大きく、他方、10mmを上
回るような厚い板厚では溶湯の冷却を均一かつ急
速に行なうことに技術的困難がある。 また、上記の冷間圧延によつて得られる薄板の
板厚0.05〜0.15mmとは、熱交換器用クロス・フイ
ン材として要求されるフイン加工性及び機械的強
度等の特性が十分に得られるための板厚である。
0.05mm未満という余りに薄い板厚に冷間圧延する
と、熱交換器用クロス・フイン材として十分な機
械的強度を得ることが困難であり、他方、0.15mm
を上回るような厚い板厚では、コスト的に不利で
あると共に熱交換の効率が悪化する。 合金の溶湯を連続的に鋳造圧延するには、2個
の回転する鋳造用ロールまたは走行する鋳造用ベ
ルトなどで構成される鋳型の間に配置されたノズ
ルを経て合金溶湯を上記鋳型間に導入し、鋳型で
冷却しながら同時に圧延すればよい。 上記方法は、直接連続鋳造圧延法として知られ
ている。この方法により、厚さ3〜10mmの帯状板
を製造すれば、鋳造時にマンガンの強制固溶量が
増加するため、マンガン、鉄、珪素などの元素の
含有量が少ない場合には、マンガンを含む金属間
化合物などはほとんど晶出せず、逆にこれらの元
素の含有量が多い場合でも、その晶出物の量が少
なく、かつ、そのサイズも小さいので、得られる
フイン材のフイン加工性が損われることがない。 直接連続鋳造圧延法では、鋳造速度(帯状板の
進行速度)は0.8〜1.4m/分、溶湯温度は680〜
710℃の範囲が適当である。 このようにして得られた帯状板は冷間圧延によ
り薄板となし、その後、これに焼鈍処理を施す。 冷間圧延における加工度は高いほど、焼鈍処理
後の薄板の組織をより均一微細にすることができ
るので、加工度は95%以上とすることが好まし
い。 焼鈍条件は、合金中のマンガン量などによつて
種々異なるが、焼鈍温度は200〜350℃焼鈍時間は
1〜2時間の範囲から適宜選ばれる。 本発明方法で得られるクロス・フイン材は、優
れたフイン加工性を有し、かつ、フイン加工して
得られるクロス・フインは優れた耐食性および大
きな引張強度を有する。 クロス・フイン材のフイン加工は常法に従つて
行なうことができる。 すなわち、フイン材に孔を穿ち、その後、円柱
状のポンチを挿入してカラー状の立上りを孔の周
囲に形成させるか、あるいは、フイン材を張出加
工してカツプ状の突起を形成させ、次いでその底
部を打ち抜く方法などによつて行なわれる。 以上、詳細に説明したように、本発明方法によ
れば、フイン加工性、耐食性および引張強度の優
れたクロス・フイン材を製造することができ、ま
た、本発明方法により得られるフイン材を用いる
ことにより、クロス・フインの薄肉化が可能とな
る。 次に、本発明を実施例により具体的に説明する
が本発明はその要旨を超えない限り以下の実施例
に限定されるものではない。 実施例1〜4および比較例1〜4 下記表1に示す各種組成のアルミニウム合金を
それぞれガス炉で溶解し、溶解後溶湯温度を750
℃とし、これによく乾燥させた塩素と窒素の混合
ガスを吹き込み、脱ガス処理を行なつた。その
後、これらの溶湯にアルミニウム―チタン―ホウ
素母合金(チタン含有量5重量%、ホウ素含有量
1重量%)をチタン含有量が0.02重量%となるよ
うに添加し、次いでこれから直接連続鋳造圧延法
または縦型半連続鋳造法および熱間圧延によりそ
れぞれ、厚さ5mmの帯状板を製造した。 直接連続鋳造圧延法では、駆動鋳型として半径
30cmの2個のロールを用い、また、鋳造速度は
130cm/分であつた。 一方、縦型半連続鋳造法では、鋳造速度4cm/
分で断面9cm×20cmのスラブを鋳造し、これを
400〜500℃で熱間圧延により帯状板とした。 次に、得られた帯状板を冷間圧延して最終的に
厚さ0.1mmの薄板とし(冷間加工度98%)、下記表
1に示す温度で2時間焼鈍を行なつたのち、フイ
ン加工性試験、引張強度試験および耐食性試験に
供した。 フイン加工性試験は、打抜ダイスを用いて薄板
に直径12mmの孔をあけ、次いで、直径16.5mmの円
柱状ポンチを孔に挿入してカラー状立上りを形成
させ、これを5回繰り返すことにより行なつた。
この結果、いずれのフイン材にも形成されたカラ
ー状立上り部に亀裂の発生が全く認められず、フ
イン加工性は良好であつた。 引張強度試験は平行部長さ60mm巾10mmの試験片
を用い、引張速度10mm/分で行なつた。 耐食性試験はJIS Z 2371の方法に準拠して3
週間の塩水噴霧試験を行ない、薄板の腐食減量
(試験前および試験後における厚さ0.1mmの薄板の
1dm2あたりの腐食による重量差mg/dm2)により
表示した。 これらの結果を表1に示す。
The present invention relates to a method for manufacturing a cross fin material for a heat exchanger. Specifically, the present invention relates to a method of manufacturing a cross fin material for a heat exchanger with improved strength and fin workability using an aluminum alloy containing 0.1 to 2% by weight of manganese. Traditionally, room coolers, refrigerators, etc.
A heat exchanger is used in which a hole with a diameter of 5 to 15 mm with a collar-like rise is bored in a thin plate of 0.15 to 0.3 mm (fin processing), and a tube for passing the cooling medium is inserted into this hole. It is being The thin plate used in this heat exchanger and subjected to the above-mentioned fin processing is generally called a cross fin. The heat of the cooling medium is conducted to the cross fins through the tubes and collar-like rises, and is effectively dissipated to the outside through the large surface area of the cross fins. The material for this cross fin (hereinafter referred to as cross fin material) is one that is easy to process.
Pure aluminum such as JIS 1050, JIS 1100, and JIS 1200 or aluminum-manganese alloy such as JIS 3003 is used. Cross fin materials are generally made by casting the above-mentioned molten aluminum or aluminum-manganese alloy into a slab using a semi-continuous casting method, hot rolling it to obtain a strip plate with a thickness of 3 to 10 mm, and then casting it into a slab. After further cold rolling this into a thin plate, it is manufactured by subjecting it to annealing treatment. In recent years, there has been a desire to make cross fins thinner in order to reduce costs, but thinner cross fins also reduce the strength of the fins, so it is important to make sure that the collar-shaped rising part of the fins is in close contact with the pipe. This results in insufficient heat transfer efficiency between the cooling medium in the tube and the fins. Therefore, the present inventors found that fin processing is easy and
In order to obtain a cross fin material with high strength, we conducted a direct continuous casting and rolling method, in which molten aluminum-manganese alloy was introduced into a mold consisting of a pair of rotating rolls, and the mold was The present inventors have discovered that if the strip plate is produced directly from the molten alloy by cooling and rolling, the resulting cross-fin material has excellent fin workability and high strength, and has thus arrived at the present invention. That is, an object of the present invention is to produce a cross fin material having excellent fin processability and high strength, and this purpose is to
A molten aluminum alloy containing manganese is continuously cast and rolled directly into a strip of 3 to 10 mm, and then this strip is cold rolled to a thickness of 0.05 to 10 mm.
This is achieved by making a 0.15 mm thin plate and then annealing it. Next, the present invention will be explained in detail. In the method of the present invention, the cross fin material is 0.1
Manufactured using an aluminum alloy containing ~2% by weight manganese. Manganese is contained in aluminum within the above range, without impairing the corrosion resistance and workability of the fin.
Improve strength. Manganese content 2.5% by weight
If it exceeds this, the corrosion resistance of the fin material will decrease. Also,
During casting, manganese-containing intermetallic compounds crystallize coarsely, which reduces workability, so when fin processing is applied to fin material, some cracks occur in the collar-shaped rising portions of the fins. In addition, the manganese content
If it is less than 0.1% by weight, the strength of the fin cannot be improved, so the manganese content should be 0.1% by weight.
-2.5% by weight, preferably 0.3-2% by weight. When the manganese content is less than 0.3% by weight,
If necessary to improve the strength of the fin material
The alloy can also contain 0.05-0.2% by weight of zirconium. Aluminum alloys contain impurities such as iron, copper, magnesium, and silicon, but in the fin material of the present invention, iron promotes the crystallization of intermetallic compounds including manganese during casting, and improves fin workability. Copper reduces corrosion resistance. Silicon also reduces fin processability and strength. Therefore, iron is 0.5% by weight or less, especially 0.3% by weight or less, and copper is 0.2% by weight or less, especially 0.1% by weight.
The content of silicon is preferably 0.4% by weight or less, particularly 0.2% by weight or less. Magnesium becomes difficult to process if it exceeds 0.5% by weight, so it should be less than 0.5% by weight, preferably 0.3%.
% by weight or less. In the method of the present invention, a molten aluminum alloy containing 0.1 to 2% by weight of manganese is continuously cast and rolled to directly obtain a strip plate with a thickness of 3 to 10 mm, which is then cold rolled to a thickness of 0.05 to 10 mm. A thin plate of 0.15mm. The plate thickness of the strip plate obtained by the above continuous casting and rolling process is 3 to 10 mm, which means that the component elements of the alloy such as manganese, iron, and silicon are sufficiently forced to form a solid solution in the aluminum. This is the thickness that allows the effects of casting and rolling to be fully utilized, that is, the thickness that allows casting and rolling to be achieved in which the molten metal is uniformly and rapidly cooled. It is technically difficult to directly obtain a strip plate with an extremely thin plate thickness of less than 3 mm from the molten metal by continuous casting and rolling.On the other hand, with a thick plate of more than 10 mm, it is difficult to cool the molten metal uniformly and rapidly. There are particular technical difficulties. In addition, the thickness of the thin plate obtained by the above-mentioned cold rolling is 0.05 to 0.15 mm because it provides sufficient properties such as fin workability and mechanical strength required as a cross fin material for heat exchangers. The plate thickness is .
If the plate is cold rolled to a thickness that is too thin (less than 0.05 mm), it will be difficult to obtain sufficient mechanical strength as cross fin material for heat exchangers;
If the plate thickness is greater than 100 mm, it is disadvantageous in terms of cost and the efficiency of heat exchange deteriorates. To continuously cast and roll a molten alloy, the molten alloy is introduced between the molds through a nozzle placed between the molds, which are composed of two rotating casting rolls or a running casting belt. Then, it may be rolled at the same time while being cooled in a mold. The above method is known as the direct continuous casting and rolling method. If a strip plate with a thickness of 3 to 10 mm is manufactured using this method, the amount of forced solid solution of manganese will increase during casting, so if the content of elements such as manganese, iron, and silicon is low, it may contain manganese. Almost no intermetallic compounds crystallize, and conversely, even if the content of these elements is high, the amount of crystallized substances is small and their size is small, so the fin processability of the resulting fin material is impaired. Never get caught. In the direct continuous casting and rolling method, the casting speed (progress speed of the strip plate) is 0.8 to 1.4 m/min, and the molten metal temperature is 680 to 680 m/min.
A range of 710°C is appropriate. The strip plate thus obtained is cold rolled into a thin plate, and then annealed. The higher the working degree in cold rolling, the more uniform and fine the structure of the thin plate after annealing treatment can be made, so the working degree is preferably 95% or more. The annealing conditions vary depending on the amount of manganese in the alloy, etc., but the annealing temperature is appropriately selected from the range of 200 to 350°C and the annealing time of 1 to 2 hours. The cross fin material obtained by the method of the present invention has excellent fin processability, and the cross fin obtained by fin processing has excellent corrosion resistance and high tensile strength. Fin processing of the cross fin material can be carried out according to a conventional method. That is, a hole is punched in the fin material, and then a cylindrical punch is inserted to form a collar-shaped rise around the hole, or the fin material is stretched to form a cup-shaped protrusion. This is then done by punching out the bottom. As explained above in detail, according to the method of the present invention, it is possible to produce a cross fin material with excellent fin processability, corrosion resistance, and tensile strength, and the fin material obtained by the method of the present invention can be used. This allows the cross fin to be made thinner. Next, the present invention will be specifically explained with reference to examples, but the present invention is not limited to the following examples unless it exceeds the gist thereof. Examples 1 to 4 and Comparative Examples 1 to 4 Aluminum alloys having various compositions shown in Table 1 below were melted in a gas furnace, and the molten metal temperature after melting was set to 750°C.
℃, and a well-dried mixed gas of chlorine and nitrogen was blown thereto for degassing. After that, an aluminum-titanium-boron mother alloy (titanium content: 5% by weight, boron content: 1% by weight) was added to these molten metals so that the titanium content was 0.02% by weight, and then directly cast and rolled using the continuous casting and rolling method. Alternatively, a strip plate with a thickness of 5 mm was produced by vertical semi-continuous casting and hot rolling, respectively. In the direct continuous casting rolling method, the radius is used as the driving mold.
Two 30cm rolls were used, and the casting speed was
It was 130cm/min. On the other hand, in the vertical semi-continuous casting method, the casting speed is 4 cm/
A slab with a cross section of 9 cm x 20 cm was cast in minutes, and this
A strip plate was formed by hot rolling at 400 to 500°C. Next, the obtained strip plate was cold-rolled into a thin plate with a final thickness of 0.1 mm (cold working degree 98%), and after annealing for 2 hours at the temperature shown in Table 1 below, the fin It was subjected to a processability test, a tensile strength test and a corrosion resistance test. The fin workability test was performed by punching a hole with a diameter of 12 mm in a thin plate using a punching die, then inserting a cylindrical punch with a diameter of 16.5 mm into the hole to form a collar-like rise, and repeating this 5 times. I did it.
As a result, no cracks were observed in the collar-shaped rising portions formed on any of the fin materials, and the fin processability was good. The tensile strength test was conducted using a test piece with a parallel length of 60 mm and a width of 10 mm at a tensile speed of 10 mm/min. Corrosion resistance test was conducted in accordance with JIS Z 2371 method.
A salt spray test was conducted for a week, and the corrosion loss of the thin plate (before and after the test)
The weight difference due to corrosion per 1 dm 2 (mg/dm 2 ) is expressed. These results are shown in Table 1.

【表】【table】

【表】 比較例 5〜8 比較例1〜4において各焼鈍温度を、それぞれ
表2に示すように実施例1〜4に対応するものと
したのち、フイン加工性試験及び引張強度試験を
行なつた。 その結果、いずれもフイン材のカラー状立上が
り部1か所当たり1〜10ケの亀裂の発生が認めら
れた。引張強度試験結果を実施例1〜4のものと
併せて表2に示す。
[Table] Comparative Examples 5 to 8 In Comparative Examples 1 to 4, each annealing temperature was set to correspond to Examples 1 to 4 as shown in Table 2, and then a fin workability test and a tensile strength test were conducted. Ta. As a result, the occurrence of 1 to 10 cracks per collar-like rising portion of the fin material was observed in all cases. The tensile strength test results are shown in Table 2 together with those of Examples 1 to 4.

【表】 比較例 9〜12 比較例1〜4において、夫々、同一の合金組成
を有する実施例1〜4のものと引張強度がほぼ同
様となる焼鈍温度条件を求め、該温度で焼鈍され
たものについてフイン加工性試験及び引張試験を
行なつた。 その結果、いずれもフイン材のカラー状立上が
り部に亀裂が認められた。引張試験の結果を実施
例1〜4のものと併せて表3に示す。
[Table] Comparative Examples 9 to 12 In Comparative Examples 1 to 4, the annealing temperature conditions were determined so that the tensile strength was almost the same as that of Examples 1 to 4 having the same alloy composition, and the annealing temperature conditions were determined. A fin processability test and a tensile test were conducted on the product. As a result, cracks were found in the collar-shaped rising portions of the fin materials in all cases. The results of the tensile test are shown in Table 3 together with those of Examples 1 to 4.

【表】【table】

Claims (1)

【特許請求の範囲】[Claims] 1 0.1〜2重量%のマンガンを含むアルミニウ
ム合金の溶湯を連続的に鋳造圧延して直接厚さ3
〜10mmの帯状板となし、次いでこの帯状板を冷間
圧延して厚さ0.05〜0.15mmの薄板とし、その後、
これに焼鈍処理を施すことを特徴とする熱交換器
用クロス・フイン材の製造法。
1 A molten aluminum alloy containing 0.1 to 2% by weight of manganese is continuously cast and rolled to a thickness of 3
A strip of ~10 mm is then cold rolled into a thin sheet of 0.05 to 0.15 mm thick, and then
A method for producing a cross fin material for a heat exchanger, which comprises subjecting the material to an annealing treatment.
JP9029778A 1978-07-24 1978-07-24 Heat exchanger cross fin material Granted JPS5517072A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9029778A JPS5517072A (en) 1978-07-24 1978-07-24 Heat exchanger cross fin material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9029778A JPS5517072A (en) 1978-07-24 1978-07-24 Heat exchanger cross fin material

Publications (2)

Publication Number Publication Date
JPS5517072A JPS5517072A (en) 1980-02-06
JPS6353477B2 true JPS6353477B2 (en) 1988-10-24

Family

ID=13994594

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9029778A Granted JPS5517072A (en) 1978-07-24 1978-07-24 Heat exchanger cross fin material

Country Status (1)

Country Link
JP (1) JPS5517072A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1045012C (en) * 1995-06-09 1999-09-08 三菱铝株式会社 Aluminum alloy processing superior strength and workability for use in forming fin, and manufacturing method for same

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56142844A (en) * 1980-04-09 1981-11-07 Showa Alum Corp Aluminum alloy for plate excellent in formability and corrosion resistance
JPS5722870A (en) * 1980-07-16 1982-02-05 Furukawa Alum Co Ltd Flux brazing method for heat exchanger made of aluminum
JPS63157842A (en) * 1986-12-22 1988-06-30 Sumitomo Light Metal Ind Ltd Manufacture of aluminum alloy stock for heat-exchanger fin excellent in strength at high temperature
JPH02243734A (en) * 1989-10-25 1990-09-27 Sky Alum Co Ltd Aluminum alloy for vacuum brazing sheet corrugated fin core material

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5934782B2 (en) * 1976-02-18 1984-08-24 古河アルミニウム工業株式会社 Manufacturing method of droop-resistant aluminum alloy plate

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1045012C (en) * 1995-06-09 1999-09-08 三菱铝株式会社 Aluminum alloy processing superior strength and workability for use in forming fin, and manufacturing method for same

Also Published As

Publication number Publication date
JPS5517072A (en) 1980-02-06

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