JPH08243734A - Production of aluminum base product - Google Patents
Production of aluminum base productInfo
- Publication number
- JPH08243734A JPH08243734A JP5298795A JP5298795A JPH08243734A JP H08243734 A JPH08243734 A JP H08243734A JP 5298795 A JP5298795 A JP 5298795A JP 5298795 A JP5298795 A JP 5298795A JP H08243734 A JPH08243734 A JP H08243734A
- Authority
- JP
- Japan
- Prior art keywords
- brazing
- alloy
- minutes
- heat treatment
- phase
- 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
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 21
- 229910052782 aluminium Inorganic materials 0.000 title abstract description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title description 2
- 238000005219 brazing Methods 0.000 claims abstract description 89
- 238000010438 heat treatment Methods 0.000 claims abstract description 24
- 239000000956 alloy Substances 0.000 claims abstract description 19
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 18
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 10
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 9
- 239000012535 impurity Substances 0.000 claims abstract description 6
- 239000000463 material Substances 0.000 claims description 37
- 239000011162 core material Substances 0.000 claims description 25
- 229910000838 Al alloy Inorganic materials 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 9
- 229910006776 Si—Zn Inorganic materials 0.000 claims description 8
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- 229910052726 zirconium Inorganic materials 0.000 claims description 3
- 229910052797 bismuth Inorganic materials 0.000 claims description 2
- 239000002245 particle Substances 0.000 claims description 2
- 229910018125 Al-Si Inorganic materials 0.000 claims 1
- 229910018523 Al—S Inorganic materials 0.000 claims 1
- 229910018520 Al—Si Inorganic materials 0.000 claims 1
- 229910001297 Zn alloy Inorganic materials 0.000 claims 1
- 229910052748 manganese Inorganic materials 0.000 claims 1
- 238000005260 corrosion Methods 0.000 abstract description 56
- 230000007797 corrosion Effects 0.000 abstract description 56
- 229910052751 metal Inorganic materials 0.000 abstract description 4
- 239000002184 metal Substances 0.000 abstract description 4
- 239000000945 filler Substances 0.000 abstract description 3
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 abstract description 2
- 230000004907 flux Effects 0.000 abstract description 2
- 238000005253 cladding Methods 0.000 abstract 1
- 239000011261 inert gas Substances 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 239000012071 phase Substances 0.000 description 29
- 230000005496 eutectics Effects 0.000 description 16
- 239000007787 solid Substances 0.000 description 15
- 238000001816 cooling Methods 0.000 description 4
- 239000013078 crystal Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 230000004580 weight loss Effects 0.000 description 2
- 239000002023 wood Substances 0.000 description 2
- 229910018131 Al-Mn Inorganic materials 0.000 description 1
- 229910018461 Al—Mn Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000003487 electrochemical reaction Methods 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、Al−Si−Zn系合
金をろう材として用いた熱交換器等の製品の製造方法に
関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method of manufacturing a product such as a heat exchanger using an Al-Si-Zn alloy as a brazing material.
【0002】[0002]
【発明の背景】芯材の表面にろう材が貼り合わされたブ
レージングシートを用いてフィン(あるいはチューブ)
を作製し、このフィンとチューブとを組み合わし、ろう
付けすることによって熱交換器が製造されている。この
熱交換器に要求されている特性の一つとして耐蝕性に富
むことが挙げられる。すなわち、腐食環境下に置かれて
いると、徐々に腐食が進行する。この為、各種の耐蝕性
技術が提案されている。しかし、更なる耐蝕性技術が求
められている。BACKGROUND OF THE INVENTION Fins (or tubes) using a brazing sheet in which a brazing material is attached to the surface of a core material
Is manufactured, the fins and tubes are combined, and brazing is performed to manufacture a heat exchanger. One of the characteristics required for this heat exchanger is that it has excellent corrosion resistance. That is, when placed in a corrosive environment, the corrosion gradually progresses. Therefore, various corrosion resistance techniques have been proposed. However, further corrosion resistance technology is required.
【0003】[0003]
【発明の開示】前記の問題点に対する研究が本発明者に
よって鋭意押し進められた。先ず、従来の製品について
の検討が行われた。すなわちアルミニウム又はアルミニ
ウム合金製(Al製)熱交換器において、ブレージング
シートを用いて構成したフィンとチューブとを結合して
いるろう材(Al−Si−Zn系合金)が如何なる状態
にあるかを検討した。ろう付けに際して溶融したAl−
Si−Zn系合金は冷却する過程において、先ず、初晶
α相が析出し、成長する。そして、共晶温度に至った時
点で液相が凝固し、共晶相が形成され、そして室温まで
冷却される。この時、理論的には、初晶α相のSi固溶
度と共晶α相のSi固溶度とは同じである。しかし、凝
固後の冷却過程で、共晶α相のSiは析出し易く、この
ため共晶α相のSi固溶度は初晶α相のSi固溶度より
低くなっていることが判って来た。ところで、共晶α相
のSi固溶度が初晶α相のSi固溶度より低いと言うこ
とは、共晶α相は初晶α相よりも電気化学的に卑な状態
にある。この為、腐食環境下にあると、共晶α相が優先
的に溶解してしまい、残った初晶α相が脱落し、この脱
落による減量が溶解減量よりも大きく寄与し、腐食速度
が高くなると考えられた。この結果、フィンとチューブ
とが外れてしまい易くなる。DISCLOSURE OF THE INVENTION The inventors of the present invention have enthusiastically investigated the above problems. First, the conventional products were examined. That is, in a heat exchanger made of aluminum or an aluminum alloy (made of Al), the state of the brazing filler metal (Al-Si-Zn alloy) connecting the fin and the tube formed by using the brazing sheet is examined. did. Al-melted during brazing
In the process of cooling the Si-Zn alloy, first, the primary crystal α phase is precipitated and grows. Then, when the eutectic temperature is reached, the liquid phase is solidified to form a eutectic phase and cooled to room temperature. At this time, theoretically, the Si solid solubility of the primary crystal α phase and the Si solid solubility of the eutectic α phase are the same. However, in the cooling process after solidification, Si in the eutectic α phase is likely to precipitate, and therefore, the Si solid solubility in the eutectic α phase is lower than the Si solid solubility in the primary α phase. I came. By the way, the fact that the solid solubility of the eutectic α phase is lower than that of the primary α phase means that the eutectic α phase is electrochemically more base than the primary α phase. Therefore, when in a corrosive environment, the eutectic α phase is preferentially dissolved, and the remaining primary α phase is removed, and the weight loss due to this loss contributes more than the dissolution weight loss, and the corrosion rate is high. Was thought to be. As a result, the fin and the tube are likely to come off.
【0004】又、前記のような腐食(粒界腐食)が進行
して行くと、ブレージングシートの芯材が露出し、孔食
が芯材にまで進み易く、貫通孔が形成され易い。これが
チューブの場合には致命的なものとなる。そして、ろう
材と芯材との関係を鑑みると、芯材内部との電位差が最
も大きいのは共晶α相であるが、この共晶α相における
Si固溶度は充分に小さいものではないから前記電位差
が充分なものとは言えない。この為、ろう材に充分な犠
牲陽極効果を期待することは出来ない。Further, when the above-mentioned corrosion (grain boundary corrosion) progresses, the core material of the brazing sheet is exposed, pitting corrosion easily progresses to the core material, and through holes are easily formed. If this is a tube, it is fatal. Considering the relationship between the brazing material and the core material, the eutectic α phase has the largest potential difference from the inside of the core material, but the Si solid solubility in this eutectic α phase is not sufficiently small. Therefore, the potential difference cannot be said to be sufficient. Therefore, the brazing material cannot be expected to have a sufficient sacrificial anode effect.
【0005】このようなことから、初晶α相のSi固溶
度と共晶α相のSi固溶度とを同等にすることが大事で
あると考えられた。特に、初晶α相のSi固溶度と共晶
α相のSi固溶度とを同等にし、かつ、Si固溶量を低
くすることが好ましいことが判って来た。すなわち、斯
の如くにしていると、ろう材のα相における電気化学的
特性が等しくなり、初晶α相と共晶α相とは略同時に溶
解し、全面溶解となって粒界腐食が起き難いものとな
る。更には、α相は内部の芯材に対して大きな電位差を
持つ卑なものとなり、犠牲陽極効果が発揮され、芯材の
孔食が起き難いものとなる。From the above, it was considered important to make the solid solubility of the primary α phase and the solid solubility of the eutectic α phase equal. In particular, it has been found that it is preferable to make the Si solid solubility of the primary crystal α phase and the Si solid solubility of the eutectic α phase equal and to reduce the Si solid solution amount. That is, in this way, the electrochemical characteristics of the α phase of the brazing material become equal, the primary α phase and the eutectic α phase are dissolved almost at the same time, and the entire surface is dissolved to cause intergranular corrosion. It will be difficult. Further, the α phase becomes a base material having a large potential difference with respect to the core material inside, the sacrificial anode effect is exerted, and pitting corrosion of the core material hardly occurs.
【0006】このような状態を達成する為には、ろう付
け作業後に熱処理を施せば良いことが判った。すなわ
ち、ろう付け作業後に熱処理を施すと、初晶α相に固溶
したSi量と共晶α相に固溶したSi量とが同等に、か
つ、Si固溶量が低くなり、電気化学的特性は均等に、
かつ、芯材に対して卑なものとなる。このような知見を
基にして本発明が達成されたものであり、耐蝕性に優れ
たAl系製品を提供することを目的とする。In order to achieve such a state, it has been found that heat treatment should be performed after the brazing work. That is, when heat treatment is performed after the brazing operation, the amount of Si dissolved in the primary crystal α phase and the amount of Si dissolved in the eutectic α phase are equal and the amount of Si solid solution is low, resulting in an electrochemical reaction. The characteristics are even,
Moreover, it becomes base on the core material. The present invention has been achieved based on such knowledge, and an object thereof is to provide an Al-based product having excellent corrosion resistance.
【0007】この本発明の目的は、芯材の表面に少なく
ともSi及びZnを含むAl−Si−Zn系合金ろう材
が設けられたAl材料が用いられた製品の製造方法であ
って、前記ろう材によるろう付け作業の後、100〜4
00℃の温度で3分以上の熱処理を行うことを特徴とす
るAl系製品の製造方法によって達成される。又、少な
くともMnを含むAl合金からなる芯材の表面に少なく
ともSi及びZnを含むAl−Si−Zn系合金ろう材
が設けられたAl材料が用いられた製品の製造方法であ
って、前記ろう材によるろう付け作業の後、100〜4
00℃の温度で3分以上の熱処理を行うことを特徴とす
るAl系製品の製造方法によって達成される。An object of the present invention is a method for producing a product using an Al material in which an Al-Si-Zn alloy brazing material containing at least Si and Zn is provided on the surface of a core material, and the brazing material is used. After brazing work with wood, 100-4
This is achieved by a method for manufacturing an Al-based product, which is characterized by performing heat treatment for 3 minutes or more at a temperature of 00 ° C. A method for producing a product using an Al material, in which an Al-Si-Zn alloy brazing material containing at least Si and Zn is provided on the surface of a core material made of an Al alloy containing at least Mn, the method comprising: After brazing work with wood, 100-4
This is achieved by a method for manufacturing an Al-based product, which is characterized by performing heat treatment for 3 minutes or more at a temperature of 00 ° C.
【0008】又、Cu,Si,Zr,Tiの群の中から
選ばれる少なくとも一種、及びMnを含むAl合金から
なる芯材の表面に少なくともSi及びZnを含むAl−
Si−Zn系合金ろう材が設けられたAl材料が用いら
れた製品の製造方法であって、前記ろう材によるろう付
け作業の後、100〜400℃の温度で3分以上の熱処
理を行うことを特徴とするAl系製品の製造方法によっ
て達成される。Further, at least one selected from the group consisting of Cu, Si, Zr, and Ti, and an Al-containing at least Si and Zn on the surface of a core material made of an Al alloy containing Mn.
A method of manufacturing a product using an Al material provided with a Si-Zn alloy brazing material, wherein a heat treatment is performed for 3 minutes or more at a temperature of 100 to 400 ° C after the brazing operation with the brazing material. And an Al-based product manufacturing method.
【0009】尚、上記Al材料は、芯材の表面(片面ま
たは両面)にろう材が貼り合わされた(クラッドされ
た)ブレージングシートであったり、芯材の表面にろう
材粉末(粒子)を溶射若しくはバインダによって付けた
シートが挙げられる。このようなシートを用いてフィン
を成形したりチューブを成形する。本発明におけるろう
材はAl−Si−Zn系合金である。特に、Si含有量
が3〜15wt%(より好ましくは3〜11wt%、も
っと好ましくは5〜10wt%)、Zn含有量が0.1
〜15wt%(より好ましくは0.1〜10wt%、も
っと好ましくは1〜10wt%)、残部がAlと不可避
不純物とからなる。又、更に、0.001〜0.1wt
%のIn、0.01〜0.07wt%のBe、0.02
〜0.20wt%のBi等を含んでいても良い。The Al material is a brazing sheet in which a brazing material is bonded (clad) on the surface (one surface or both surfaces) of the core material, or a brazing material powder (particles) is sprayed on the surface of the core material. Alternatively, a sheet attached with a binder may be used. Fins or tubes are formed using such a sheet. The brazing material in the present invention is an Al-Si-Zn based alloy. In particular, the Si content is 3 to 15 wt% (more preferably 3 to 11 wt%, more preferably 5 to 10 wt%), and the Zn content is 0.1.
-15 wt% (more preferably 0.1-10 wt%, more preferably 1-10 wt%), the balance consisting of Al and unavoidable impurities. In addition, 0.001 to 0.1 wt
% In, 0.01-0.07 wt% Be, 0.02
˜0.20 wt% Bi and the like may be included.
【0010】芯材としては純AlあるいはAl合金であ
る。機械的強度が要求されない場合には純Alでも良
い。しかしながら、機械的強度を要求されることが多
く、このような場合にはAl合金が用いられる。特に、
Mn含有量が0.1〜1.5wt%のAl合金が用いら
れる。又、0.05〜0.5wt%のCu、0.3〜
1.2wt%のSi、0.01〜0.15wt%のZ
r、0.01〜0.2wt%のTiの中の一種または二
種以上と0.1〜1.5wt%のMnとを少なくとも含
有するAl合金が用いられる。このようなAl−Mn系
合金あるいはAl−Mn−X系合金を用いることによっ
て、芯材として必要な機械的強度が確保される。The core material is pure Al or Al alloy. Pure Al may be used if mechanical strength is not required. However, mechanical strength is often required, and in such a case, an Al alloy is used. In particular,
An Al alloy having a Mn content of 0.1 to 1.5 wt% is used. Also, 0.05 to 0.5 wt% Cu, 0.3 to
1.2 wt% Si, 0.01 to 0.15 wt% Z
An Al alloy containing at least one of r and 0.01 to 0.2 wt% of Ti, and 0.1 to 1.5 wt% of Mn is used. By using such an Al-Mn-based alloy or Al-Mn-X-based alloy, the mechanical strength required as the core material is secured.
【0011】上記Al材料で作製されたシートを用いて
構成した熱媒体の流路である管(チューブ、パテプ)と
Al製フィンとを組み合わし、ろう付けした後、冷却す
る。この冷却後の製品を100〜400℃の温度で3分
以上(好ましくは10分以上)熱処理する。熱処理温度
が低い場合には、初晶α相のSiの固溶度と共晶α相の
Siの固溶度との差をなくすことが出来なかったことよ
り、100℃以上とした。逆に、高くなり過ぎると、冷
却時の析出過程において同じような固溶度差が生じ、本
発明の熱処理の意味がなくなることから、400℃以下
とした。尚、好ましい熱処理温度は200〜300℃で
ある。又、熱処理時間が短い場合には、初晶α相のSi
の固溶度と共晶α相のSiの固溶度との差をなくすこと
が出来なかったことより、3分以上とした。熱処理時間
は長くても差し支えなかったが、生産効率を考えると1
0時間以内である。好ましい熱処理時間は10分〜10
時間である。[0011] A tube (tube or putty), which is a flow path for a heat medium formed by using a sheet made of the above-mentioned Al material, and an Al fin are combined, brazed, and then cooled. The cooled product is heat-treated at a temperature of 100 to 400 ° C. for 3 minutes or longer (preferably 10 minutes or longer). When the heat treatment temperature was low, it was not possible to eliminate the difference between the solid solubility of Si in the primary α phase and the solid solubility of Si in the eutectic α phase. On the contrary, if the temperature is too high, the same solid solubility difference occurs in the precipitation process during cooling, and the heat treatment of the present invention is meaningless. The preferable heat treatment temperature is 200 to 300 ° C. Also, when the heat treatment time is short, the primary α-phase Si
Since it was not possible to eliminate the difference between the solid solubility of Si and the solid solubility of Si in the eutectic α phase, it was set to 3 minutes or more. The heat treatment time can be long, but considering the production efficiency, 1
Within 0 hours. The preferable heat treatment time is 10 minutes to 10 minutes.
Time.
【0012】以下、具体的な実施例を挙げて説明する。A specific embodiment will be described below.
【0013】[0013]
〔実施例1〕不可避不純物しか含まない純Alからなる
芯材の両面に、Siが8wt%、Znが3wt%で、残
部がAlと不可避不純物からなるAl−8Si−3Zn
合金ろう材をクラッド(クラッド率は片面10%)した
0.4mm厚のブレージングシートを用意した。そし
て、このブレージングシートを用いてチューブを構成し
た。[Example 1] Al-8Si-3Zn in which Si is 8 wt% and Zn is 3 wt% and the balance is Al and inevitable impurities on both surfaces of a core material made of pure Al containing only inevitable impurities.
A brazing sheet having a thickness of 0.4 mm, in which a brazing alloy material was clad (the clad ratio was 10% on one side) was prepared. Then, a tube was constructed using this brazing sheet.
【0014】このチューブとAl製フィンとを組み合わ
せ、不活性雰囲気下においてフッ化物系のフラックスを
用いたろう付け手段により600℃、3分間のろう付け
を実施し、チューブとフィンとを結合した。この熱交換
器を表−1に示す条件で熱処理し、この後は空冷によっ
て徐々に室温まで冷却し、耐蝕性テストを行ったので、
その結果を表−1に示す。This tube was combined with an Al fin, and brazing was performed at 600 ° C. for 3 minutes by a brazing means using a fluoride-based flux in an inert atmosphere to bond the tube and the fin. This heat exchanger was heat-treated under the conditions shown in Table-1, and then gradually cooled to room temperature by air cooling, and a corrosion resistance test was conducted.
The results are shown in Table-1.
【0015】 表−1熱処理条件 ろう材電位(mVvsSCE) 耐蝕性 熱処理なし(ろう付のまま) −870 やや局部腐食型 孔食深さ0.12mm ろう付後50℃で50時間 −875 やや局部腐食型 孔食深さ0.12mm ろう付後130℃で5時間 −960 全面腐食型 孔食深さ0.04mm ろう付後200℃で3時間 −955 全面腐食型 孔食深さ0.04mm ろう付後300℃で1時間 −950 全面腐食型 孔食深さ0.05mm ろう付後300℃で30分間 −950 全面腐食型 孔食深さ0.05mm ろう付後300℃で10分間 −948 全面腐食型 孔食深さ0.06mm ろう付後400℃で3分間 −920 全面腐食型 孔食深さ0.07mm ろう付後450℃で10分間 −900 やや局部腐食型 孔食深さ0.13mm *耐蝕性テストは、酸性塩水噴霧試験を1日間実施し、ろう材の腐食形態を調 べると共に、同様の試験を30日間実施し、孔食深さを調べた。Table-1 Heat treatment conditions Brazing potential (mVvsSCE) Corrosion resistance No heat treatment (as brazing) -870 Some local corrosion type Pit depth 0.12mm 50 hours after brazing at 50 ° C -875 Some local corrosion type Pitting depth 0.12mm 5 hours at 130 ° C after brazing −960 General corrosion type Pitting depth 0.04mm 3 hours at 200 ° C after brazing −955 General corrosion type Pitting depth 0.04mm At 300 ° C after brazing 1 hour -950 General corrosion type pitting corrosion depth 0.05mm 30 minutes after brazing at 300 ° C -950 General corrosion type pitting corrosion depth 0.05mm 10 minutes after brazing at 300 ° C -948 General corrosion type pitting depth 0.06 mm After brazing at 400 ° C for 3 minutes −920 General corrosion type pitting depth 0.07mm After brazing at 450 ° C for 10 minutes −900 Slightly localized corrosion type pitting depth 0.13mm * Corrosion resistance test is acid salt spray test For 1 day to check the corrosion morphology of the brazing material and Such a test was carried out for 30 days, and the pitting depth was examined.
【0016】〔実施例2〕実施例1において、芯材とし
てAl−1.2Mn−0.15Cu合金を用い、かつ、
ろう材としてAl−8Si−1Zn合金を用いた他は同
様に行い、耐蝕性テストを行ったので、その結果を表−
2に示す。 表−2熱処理条件 ろう材電位(mVvsSCE) 耐蝕性 熱処理なし(ろう付のまま) −760 やや局部腐食型 孔食深さ0.15mm ろう付後50℃で50時間 −763 やや局部腐食型 孔食深さ0.15mm ろう付後130℃で5時間 −910 全面腐食型 孔食深さ0.03mm ろう付後200℃で3時間 −906 全面腐食型 孔食深さ0.04mm ろう付後300℃で1時間 −900 全面腐食型 孔食深さ0.03mm ろう付後300℃で30分間 −900 全面腐食型 孔食深さ0.04mm ろう付後300℃で10分間 −900 全面腐食型 孔食深さ0.02mm ろう付後400℃で3分間 −890 全面腐食型 孔食深さ0.02mm ろう付後450℃で10分間 −878 やや局部腐食型 孔食深さ0.14mm 〔実施例3〕実施例1において、芯材としてAl−1.
2Mn−0.5Cu−0.6Si−0.1Zr合金を用
い、かつ、ろう材としてAl−8Si−1Zn合金を用
いた他は同様に行い、耐蝕性テストを行ったので、その
結果を表−3に示す。Example 2 In Example 1, an Al-1.2Mn-0.15Cu alloy was used as the core material, and
Corrosion resistance test was conducted in the same manner except that Al-8Si-1Zn alloy was used as the brazing material.
It is shown in FIG. Table-2 Heat treatment conditions Brazing potential (mVvsSCE) Corrosion resistance No heat treatment (as brazing ) -760 Some local corrosion pitting depth 0.15mm 50 hours after brazing at 50 ° C -763 Some local corrosion pitting depth 0.15mm 5 hours at 130 ° C after brazing −910 General corrosion type pitting depth 0.03mm 3 hours at 200 ° C after brazing −906 General corrosion type pitting depth 0.04mm 1 hour at 300 ° C after brazing − 900 General corrosion type pitting depth 0.03mm After brazing at 300 ° C for 30 minutes −900 General corrosion type pitting depth 0.04mm After brazing at 300 ° C for 10 minutes −900 General corrosion type pitting depth 0.02mm Brazing After that, 400 ° C. for 3 minutes −890 general corrosion type pitting depth 0.02 mm After brazing for 10 minutes at −878 slightly local corrosion type pitting depth 0.14 mm [Example 3] In Example 1, as a core material Al-1.
2Mn-0.5Cu-0.6Si-0.1Zr alloy was used, and Al-8Si-1Zn alloy was used as the brazing material, and the same corrosion resistance test was performed. 3 shows.
【0017】 表−3熱処理条件 ろう材電位(mVvsSCE) 耐蝕性 熱処理なし(ろう付のまま) −750 やや局部腐食型 孔食深さ0.15mm ろう付後50℃で50時間 −690 やや局部腐食型 孔食深さ0.13mm ろう付後130℃で5時間 −915 全面腐食型 孔食深さ0.04mm ろう付後200℃で3時間 −909 全面腐食型 孔食深さ0.06mm ろう付後300℃で1時間 −900 全面腐食型 孔食深さ0.05mm ろう付後300℃で30分間 −900 全面腐食型 孔食深さ0.05mm ろう付後300℃で10分間 −902 全面腐食型 孔食深さ0.05mm ろう付後400℃で3分間 −880 全面腐食型 孔食深さ0.06mm ろう付後450℃で10分間 −860 やや局部腐食型 孔食深さ0.14mm 〔比較例〕実施例1において、芯材としてAl−1.2
Mn−0.15Cu合金を用い、かつ、ろう材としてA
l−8Si合金を用いた他は同様に行い、耐蝕性テスト
を行ったので、その結果を表−4に示す。Table-3 Heat treatment conditions Brazing potential (mVvsSCE) Corrosion resistance No heat treatment (as brazing) -750 Some local corrosion type Pit depth 0.15mm 50 hours after brazing at 50 ° C-690 Some local corrosion type Pitting depth 0.13mm 5 hours at 130 ° C after brazing −915 General corrosion type Pitting depth 0.04mm 3 hours at 200 ° C after brazing −909 General corrosion type Pitting depth 0.06mm At 300 ° C after brazing 1 hour -900 General corrosion type pitting corrosion depth 0.05mm After brazing at 300 ° C for 30 minutes -900 General corrosion type pitting corrosion depth 0.05mm After brazing at 300 ° C for 10 minutes -902 General corrosion type pitting corrosion depth 0.05 mm After brazing at 400 ° C. for 3 minutes −880 General corrosion type pitting depth 0.06 mm After brazing at 450 ° C. for 10 minutes −860 Slightly localized corrosion type pitting depth 0.14 mm [Comparative Example] In Example 1, Al-1.2 as material
A Mn-0.15Cu alloy is used and A is used as a brazing filler metal.
A corrosion resistance test was conducted in the same manner except that the 1-8Si alloy was used, and the results are shown in Table-4.
【0018】 表−4熱処理条件 ろう材電位(mVvsSCE) 耐蝕性 熱処理なし(ろう付のまま) −740 孔食深さ0.40mm ろう付後50℃で50時間 −740 孔食深さ0.35mm ろう付後130℃で5時間 −740 孔食深さ0.32mm ろう付後200℃で3時間 −750 孔食深さ0.34mm ろう付後300℃で1時間 −760 孔食深さ0.36mm ろう付後300℃で30分間 −755 孔食深さ0.37mm ろう付後300℃で10分間 −753 孔食深さ0.35mm ろう付後400℃で3分間 −762 孔食深さ0.34mm ろう付後450℃で10分間 −745 孔食深さ0.35mmTable-4 Heat treatment conditions Brazing potential (mVvsSCE) Corrosion resistance No heat treatment (as brazing) -740 Pitting depth 0.40mm After brazing at 50 ° C for 50 hours -740 Pitting depth 0.35mm Brazing After 5 hours at 130 ℃ -740 Pitting depth 0.32mm After brazing 3 hours at 200 ℃ -750 Pitting depth 0.34mm After brazing at 1 hour at 300 ℃ -760 Pitting depth 0.36mm After brazing 300 30 minutes at ℃ −755 Pitting depth 0.37mm After brazing at 300 ℃ for 10 minutes −753 Pitting depth 0.35mm After brazing at 400 ℃ for 3 minutes −762 Pitting depth 0.34mm At 450 ℃ after brazing 10 minutes -745 Pitting depth 0.35mm
【0019】[0019]
【効果】本発明によれば、耐蝕性に優れたAl製熱交換
器などの製品が得られる。According to the present invention, products such as Al heat exchangers having excellent corrosion resistance can be obtained.
Claims (8)
含むAl−Si−Zn系合金ろう材が設けられたAl材
料が用いられた製品の製造方法であって、前記ろう材に
よるろう付け作業の後、100〜400℃の温度で3分
以上の熱処理を行うことを特徴とするAl系製品の製造
方法。1. A method of manufacturing a product using an Al material in which an Al—Si—Zn alloy brazing material containing at least Si and Zn is provided on the surface of a core material, the brazing operation using the brazing material. After that, a heat treatment is performed for 3 minutes or more at a temperature of 100 to 400 ° C., a manufacturing method of an Al-based product.
芯材の表面に少なくともSi及びZnを含むAl−Si
−Zn系合金ろう材が設けられたAl材料が用いられた
製品の製造方法であって、前記ろう材によるろう付け作
業の後、100〜400℃の温度で3分以上の熱処理を
行うことを特徴とするAl系製品の製造方法。2. An Al—Si containing at least Si and Zn on the surface of a core material made of an Al alloy containing at least Mn.
A method for manufacturing a product using an Al material provided with a Zn-based alloy brazing material, comprising performing a heat treatment for 3 minutes or more at a temperature of 100 to 400 ° C. after brazing with the brazing material. A method for producing a characteristic Al-based product.
ばれる少なくとも一種、及びMnを含むAl合金からな
る芯材の表面に少なくともSi及びZnを含むAl−S
i−Zn系合金ろう材が設けられたAl材料が用いられ
た製品の製造方法であって、前記ろう材によるろう付け
作業の後、100〜400℃の温度で3分以上の熱処理
を行うことを特徴とするAl系製品の製造方法。3. An Al—S containing at least Si and Zn on the surface of a core material made of an Al alloy containing Mn and at least one selected from the group consisting of Cu, Si, Zr and Ti.
A method of manufacturing a product using an Al material provided with an i-Zn alloy brazing material, wherein after the brazing operation with the brazing material, a heat treatment is performed at a temperature of 100 to 400 ° C for 3 minutes or more. A method for producing an Al-based product, comprising:
合わされたものであることを特徴とする請求項1〜請求
項3いずれかのAl系製品の製造方法。4. The method for producing an Al-based product according to claim 1, wherein the Al material is a brazing material bonded to the surface of a core material.
設けられたものであることを特徴とする請求項1〜請求
項3いずれかのAl系製品の製造方法。5. The method for producing an Al-based product according to claim 1, wherein the Al material comprises a brazing material particle provided on a surface of a core material.
%、Zn含有量が0.1〜15wt%、必要に応じてI
nを0.001〜0.1wt%、Beを0.01〜0.
07wt%、及びBiを0.02〜0.20wt%、そ
して残部がAlと不可避不純物であることを特徴とする
請求項1〜請求項5いずれかのAl系製品の製造方法。6. The brazing material has a Si content of 3 to 15 wt.
%, Zn content of 0.1 to 15 wt%, I if necessary
n is 0.001 to 0.1 wt% and Be is 0.01 to 0.
The method for producing an Al-based product according to any one of claims 1 to 5, wherein 07 wt% and Bi are 0.02 to 0.20 wt% and the balance is Al and inevitable impurities.
量が0.1〜1.5wt%であることを特徴とする請求
項2又は請求項3のAl系製品の製造方法。7. The method for producing an Al-based product according to claim 2, wherein the Mn content in the core material made of an Al alloy is 0.1 to 1.5 wt%.
有した場合のCu含有量は0.05〜0.5wt%、S
iを含有した場合のSi含有量は0.3〜1.2wt
%、Zrを含有した場合のZr含有量は0.01〜0.
15wt%、Tiを含有した場合のTi含有量は0.0
1〜0.2wt%であることを特徴とする請求項3のA
l系製品の製造方法。8. The Cu content in the core material made of an Al alloy when it contains Cu is 0.05 to 0.5 wt%, S
Si content when i is included is 0.3 to 1.2 wt.
%, Zr content in the case of containing Zr is 0.01-0.
15wt%, Ti content when Ti is included is 0.0
A of claim 3 wherein the content is 1 to 0.2 wt%.
Method for manufacturing l-based product.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5298795A JP3549028B2 (en) | 1995-03-13 | 1995-03-13 | Manufacturing method of Al-based products |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5298795A JP3549028B2 (en) | 1995-03-13 | 1995-03-13 | Manufacturing method of Al-based products |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH08243734A true JPH08243734A (en) | 1996-09-24 |
| JP3549028B2 JP3549028B2 (en) | 2004-08-04 |
Family
ID=12930280
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5298795A Expired - Fee Related JP3549028B2 (en) | 1995-03-13 | 1995-03-13 | Manufacturing method of Al-based products |
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| Country | Link |
|---|---|
| JP (1) | JP3549028B2 (en) |
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|---|---|---|---|---|
| JP2009179830A (en) * | 2008-01-29 | 2009-08-13 | Mitsubishi Alum Co Ltd | Brazing sheet for heat exchanger, heat exchanger |
| JP2009179829A (en) * | 2008-01-29 | 2009-08-13 | Mitsubishi Alum Co Ltd | Brazing sheet for heat exchanger, heat exchanger |
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| JP2012097320A (en) * | 2010-11-02 | 2012-05-24 | Furukawa-Sky Aluminum Corp | Heat exchanger made from aluminum and manufacturing method thereof |
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1995
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Cited By (9)
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|---|---|---|---|---|
| JP2009179830A (en) * | 2008-01-29 | 2009-08-13 | Mitsubishi Alum Co Ltd | Brazing sheet for heat exchanger, heat exchanger |
| JP2009179829A (en) * | 2008-01-29 | 2009-08-13 | Mitsubishi Alum Co Ltd | Brazing sheet for heat exchanger, heat exchanger |
| JP2010209426A (en) * | 2009-03-11 | 2010-09-24 | Kobe Steel Ltd | Aluminum alloy brazed body, method for heat-treating the same, and heat exchanger |
| CN101839665A (en) * | 2009-03-13 | 2010-09-22 | 古河Sky株式会社 | Thin brazing sheet fin member for high-temperature brazing and method of manufacturing heat exchanger using same |
| CN101839666A (en) * | 2009-03-13 | 2010-09-22 | 古河Sky株式会社 | Thin brazing sheet fin member for high-temperature brazing and method of manufacturing heat exchanger using same |
| CN101839666B (en) | 2009-03-13 | 2012-07-18 | 古河Sky株式会社 | Thin brazing sheet fin component for high temperature brazing and method for manufacturing heat exchanger using the same |
| JP2012097320A (en) * | 2010-11-02 | 2012-05-24 | Furukawa-Sky Aluminum Corp | Heat exchanger made from aluminum and manufacturing method thereof |
| JP2014074226A (en) * | 2012-09-12 | 2014-04-24 | Uacj Corp | Aluminum alloy clad plate |
| JP2017164780A (en) * | 2016-03-16 | 2017-09-21 | 三菱アルミニウム株式会社 | Aluminum alloy brazing sheet and method for brazing aluminum alloy brazing sheet |
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| Publication number | Publication date |
|---|---|
| JP3549028B2 (en) | 2004-08-04 |
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