JPH0256191B2 - - Google Patents

Info

Publication number
JPH0256191B2
JPH0256191B2 JP28956186A JP28956186A JPH0256191B2 JP H0256191 B2 JPH0256191 B2 JP H0256191B2 JP 28956186 A JP28956186 A JP 28956186A JP 28956186 A JP28956186 A JP 28956186A JP H0256191 B2 JPH0256191 B2 JP H0256191B2
Authority
JP
Japan
Prior art keywords
plate
layer
thickness
cold
diffusion annealing
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
JP28956186A
Other languages
Japanese (ja)
Other versions
JPS63140782A (en
Inventor
Shigemichi Sugiura
Masaaki Ishio
Hiroshi Miura
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.)
Proterial Ltd
Original Assignee
Sumitomo Special Metals 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 Sumitomo Special Metals Co Ltd filed Critical Sumitomo Special Metals Co Ltd
Priority to JP28956186A priority Critical patent/JPS63140782A/en
Publication of JPS63140782A publication Critical patent/JPS63140782A/en
Publication of JPH0256191B2 publication Critical patent/JPH0256191B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/017Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of aluminium or an aluminium alloy, another layer being formed of an alloy based on a non ferrous metal other than aluminium

Landscapes

  • Pressure Welding/Diffusion-Bonding (AREA)

Description

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

利用産業分野 この発明は、熱交換器等、特に苛酷な環境条件
にて使用される熱交換器部材として、軽量でかつ
耐食性にすぐれた2層または3層クラツド板を品
質良好かつ効率よく製造できる製造方法に関す
る。 背景技術 最近の宇宙開発の進歩と共に、人口衛星にも
種々の熱交換器が使用されている。一般に、熱交
換器用部材としては、軽量化の目的でAl材が使
用されている。 この人口衛星等に用いる熱交換器用の部材とし
ては、軽量かつ苛酷な雰囲気条件下で長寿命の熱
交換器用材料が要望されてきたが、従来の如く、
その構造部材にAlを使用する場合、苛酷な環境
条件下にては、生成される水分等により、Alは
孔食をおこし易く、孔食がAl部材を貫通した場
合は冷却流体が他室に漏洩する恐れがあり、その
信頼性に大きな問題を生ずる。 そのため、熱交換器用部材として、軽量、耐食
性及び機械的強度の大きなTi板の片面、あるい
は両面にAl板を被覆したAl―Ti2層クラツド板、
あるいはAl―Ti―Al3層クラツド板が提案されて
いるが、その製造法は熱間プレスにより得られる
ため、その生産性に問題があり、安価に前記クラ
ツド板を提供できない問題があつた。 生産性を向上させるため、クラツド板の一般的
な製造方法である冷間圧接、拡散焼鈍による方法
が考えられるが、心材となるTi板と被着材とな
るAl板は、冷間圧接後の拡散焼鈍条件によつて
は、圧接界面にlTi、TiAl3等の金属間化合物の
成長により、圧接界面が脆弱となり、その接着強
度が低下する恐れがあつた。 また、製品クラツド板の板厚、用途、機械的性
質により、拡散焼鈍度、冷間圧延あるいはさらに
中間焼鈍、仕上圧延等を施す必要があるが、クラ
ツド板を構成するAl板、Ti板の冷間圧接前の板
厚比率が適当な比率でなければ、冷間圧接時ある
いは冷間圧延時、心材のTi板に亀裂、引き裂れ
割れを生じ、品質良好なる2層あるいは3層クラ
ツド板を得ることができなかつた。 発明の目的 この発明は、従来のAl―Tiクラツド板の問題
点を解消し、心材のTiに亀裂などの発生がなく、
高品質でかつ安価に製造できる多層クラツド板の
製造方法を目的としている。 発明の構成と効果 この発明は、表面を清浄化したTi板の片面あ
るいは両面に、 クラツド板の上記Ti層、Al層の層厚比が 1:0.01〜4なる如く、 予めその板厚を設定したAl板を対向し、前記
Ti板と重ね合せた後、冷間にて圧下率30〜70%
で圧接し、 Al―Ti2層クラツド板の場合は、真空中で 500℃〜600℃、1Hr〜6Hrの条件にて拡散焼鈍
を行い、 また、Al―Ti―Al3層クラツド板の場合は、真
空中あるいはN2、Arガス等の不活性ガス中で 500℃〜600℃、1Hr〜6Hrの条件にて拡散焼鈍
して、2層または3層の多層クラツド板を得る製
造方法である。 この発明の製造方法により、lとTiの圧接界
面に金属間化合物を生成することなく、高い圧着
強度を得ることができ、かつ所要の機械的性質を
有する多層クラツド板を効率よく製造できる。 発明の図面に基づく開示 この発明によるAl―Ti―Al3層クラツド板の製
造方法を第1図に基づいて説明する。 コイル状のT板1を巻戻しながら、表面を機械
的にあるいは化学的に清浄化し、図において右方
向走行させた前記Ti板1の両面に、Al板2,3
のそれぞれを対向し、重ね合せて圧接ロール4に
て、30%〜70%の圧下率にて冷間圧接する。 この際、前記Al板2,は、Ti板の板厚に対し
て0.01〜4の板厚比を有する。 前記の冷間圧接後、連続焼鈍炉5において、真
空中または不活性ガス中にて500℃〜600℃、1Hr
〜6Hrの拡散焼鈍を施し、必要により圧延機6に
て冷間圧延し、軟化処理炉7にて軟化処理、また
は中間冷延、中間焼鈍、仕上冷延、または更に軟
化処理し、Al―Ti―Al3層クラツド板を得る。 発明の好ましい実施態様 この発明において、冷間圧接前のAl板、Ti板
の板厚比を0.01〜4:1に限定した理由は、Tiに
対する板厚比が0.01未満では、極薄板となつて移
送と、冷間圧接時あるいは後続の冷間圧延時に、
Tiに割れや亀裂の発生を惹起するので好ましく
ない。 また、冷間圧接の圧下率が30%未満では十分な
る接ができず、圧下率が70%を超えるとTi板の
割れ亀裂の発生が起るため好ましくない。 拡散焼鈍条件は、500℃未満、1Hr未満ではTi
板の軟化が不十分であり、また600℃の超えると
圧接界面の金属間化合物の成長が著しく好ましく
なく、また6Hrを超えると拡散焼鈍効果は飽和
し、かつAl粒の粗大化を招来し好ましくない。 また拡散焼鈍時の雰囲気としては、Tiは酸素、
窒素、水素ガスを吸蔵しやすく、Tiの性質を大
きく変動するため、真空中での熱処理が好ましい
が、Ti板の両面にAl板にて被覆する場合も、も
しくは後続工程にて曲げ加工、絞り加工をしない
で、圧延ままの平板にて使用する場合は、Naガ
ス等不活性ガスにて拡散焼鈍してもよい。 拡散焼鈍後の冷間圧延の圧下率は、製品クラツ
ド板の所要板厚、使用条件、所要の機械的性質に
よつて、適宜選択されるが、圧下率は70%を超え
るとTi板の割れ、亀裂を招来するので好ましく
ない。 また冷間圧延後の軟化処理条件は雰囲気、温
度、時間共、拡散焼鈍と同一条件でよい。 実施例 実施例 1 巻戻しローラーより巻戻しされ、表面をバフ研
摩された板厚2mm×幅300mmのTi板の平面に、板
厚2mm×幅300mmのAl板を、前記Ti板に対向させ
ながら走行させ、両板を重ね合せて、圧下率50%
にて冷間圧接して、板厚2mmの2相クラツド板に
作製した。 その後、真空炉中で、250℃、300℃、350℃、
450℃、500℃、550℃、600℃、650℃の各温度、
1Hrの拡散焼鈍を行い、2mm×10mm×100mm寸法
の試験片を得た。 前記試験片を第2図に示す如く、圧接面にて離
反方向に折り曲げて略T字型となし、その硬度を
測定し、また試験片の圧接面の顕微鏡観察を行な
い、界面にAlTi金属間化合物の生成の有無を調
べた。その結果を第1表に示す。
Field of application: This invention enables the efficient production of lightweight, highly corrosion-resistant, two- or three-layer clad plates of good quality and as heat exchanger components used in particularly harsh environmental conditions, such as heat exchangers. Regarding the manufacturing method. BACKGROUND ART With recent advances in space development, various heat exchangers are also being used in artificial satellites. Generally, Al material is used as a heat exchanger member for the purpose of weight reduction. There has been a demand for materials for heat exchangers that are lightweight and have a long life under harsh atmospheric conditions, but as in the past,
When Al is used for structural members, under harsh environmental conditions, Al is prone to pitting corrosion due to generated moisture, and if pitting corrosion penetrates the Al member, the cooling fluid will leak into other rooms. There is a risk of leakage, which poses a major problem with its reliability. Therefore, as a heat exchanger component, we use an Al-Ti two-layer clad plate, which is a Ti plate coated with an Al plate on one or both sides, which is lightweight, has high corrosion resistance, and has high mechanical strength.
Alternatively, an Al--Ti--Al three-layer clad plate has been proposed, but since it is manufactured by hot pressing, there is a problem in its productivity, and the clad plate cannot be provided at a low price. In order to improve productivity, methods such as cold pressure welding and diffusion annealing, which are common manufacturing methods for clad plates, can be considered. Depending on the diffusion annealing conditions, the growth of intermetallic compounds such as lTi and TiAl 3 at the welded interface may make the welded interface brittle and reduce its adhesive strength. In addition, depending on the thickness, purpose, and mechanical properties of the product clad plate, it is necessary to perform diffusion annealing, cold rolling, intermediate annealing, finish rolling, etc. If the plate thickness ratio before welding is not appropriate, cracks and tearing will occur in the core Ti plate during cold welding or cold rolling, making it difficult to produce good-quality two- or three-layer clad plates. I couldn't get it. Purpose of the invention This invention solves the problems of conventional Al-Ti clad plates, and eliminates the occurrence of cracks in the Ti core material.
The objective is to provide a method for manufacturing multilayer cladding boards that can be manufactured at high quality and at low cost. Structure and Effects of the Invention This invention sets the thickness of the clad plate on one or both sides of the Ti plate whose surface has been cleaned so that the thickness ratio of the Ti layer and the Al layer is 1:0.01 to 4. Place the aluminum plates facing each other and
After stacking with Ti plate, rolling reduction rate is 30-70% in cold.
In the case of an Al-Ti two-layer clad plate, diffusion annealing is performed in a vacuum at 500℃ to 600℃ for 1 to 6 hours, and in the case of an Al-Ti-Al three-layer clad plate, a vacuum annealing is performed. This is a manufacturing method in which a two-layer or three-layer multilayer clad plate is obtained by diffusion annealing at 500° C. to 600° C. for 1 hour to 6 hours in an inert gas such as N 2 or Ar gas. By the manufacturing method of the present invention, it is possible to obtain high pressure bonding strength without forming intermetallic compounds at the pressure contact interface between L and Ti, and to efficiently produce a multilayer clad plate having the required mechanical properties. Disclosure of the Invention Based on Drawings The method for manufacturing an Al--Ti--Al three-layer clad plate according to the present invention will be explained with reference to FIG. While unwinding the coiled T plate 1, the surface is mechanically or chemically cleaned, and Al plates 2 and 3 are placed on both sides of the Ti plate 1, which is run rightward in the figure.
are placed on top of each other and cold welded using a pressure roll 4 at a reduction rate of 30% to 70%. At this time, the Al plate 2 has a thickness ratio of 0.01 to 4 with respect to the thickness of the Ti plate. After the above-mentioned cold pressure welding, in a continuous annealing furnace 5, it is heated at 500°C to 600°C for 1 hour in a vacuum or an inert gas.
After diffusion annealing for ~6 hours, if necessary, cold rolling in a rolling mill 6, softening treatment in a softening furnace 7, or intermediate cold rolling, intermediate annealing, finish cold rolling, or further softening treatment, Al-Ti - Obtain an Al three-layer clad plate. Preferred Embodiment of the Invention In this invention, the reason why the thickness ratio of the Al plate and the Ti plate before cold welding is limited to 0.01 to 4:1 is that if the thickness ratio to Ti is less than 0.01, the plate becomes extremely thin. during transport and during cold welding or subsequent cold rolling.
This is not preferable because it causes cracks and cracks in Ti. Furthermore, if the rolling reduction ratio of cold welding is less than 30%, sufficient welding cannot be achieved, and if the rolling reduction ratio exceeds 70%, cracks may occur in the Ti plate, which is not preferable. Diffusion annealing conditions are less than 500℃ and less than 1 hour.
The softening of the plate is insufficient, and if the temperature exceeds 600℃, the growth of intermetallic compounds at the weld interface will be extremely undesirable.If the temperature exceeds 6Hr, the diffusion annealing effect will be saturated and the Al grains will become coarser, which is not desirable. do not have. In addition, the atmosphere during diffusion annealing is oxygen for Ti,
Since it easily absorbs nitrogen and hydrogen gas and greatly changes the properties of Ti, heat treatment in a vacuum is preferable, but it is also possible to coat both sides of the Ti plate with Al plates, or bending or drawing in the subsequent process. When using a flat plate as rolled without processing, diffusion annealing may be performed using an inert gas such as Na gas. The reduction rate of cold rolling after diffusion annealing is selected appropriately depending on the required thickness of the product clad plate, usage conditions, and required mechanical properties, but if the reduction rate exceeds 70%, the Ti plate may crack. , which is undesirable because it causes cracks. Further, the softening treatment conditions after cold rolling may be the same as those for diffusion annealing in terms of atmosphere, temperature, and time. Examples Example 1 An Al plate with a thickness of 2 mm and a width of 300 mm is placed on the plane of a Ti plate with a thickness of 2 mm and a width of 300 mm, which has been rewound by an unwinding roller and whose surface has been buffed, while facing the Ti plate. Run it, overlap both plates, and reduce the reduction rate to 50%.
A two-phase clad plate with a thickness of 2 mm was produced by cold welding. Then, in a vacuum furnace at 250℃, 300℃, 350℃,
Each temperature of 450℃, 500℃, 550℃, 600℃, 650℃,
Diffusion annealing was performed for 1 hour to obtain a test piece with dimensions of 2 mm x 10 mm x 100 mm. As shown in Figure 2, the test piece was bent in the direction of separation at the pressure contact surface to form a roughly T-shape, and its hardness was measured.The pressure contact surface of the test piece was also observed under a microscope. The presence or absence of compound formation was investigated. The results are shown in Table 1.

【表】 実施例 2 巻戻しローラーより巻戻しされ、表面をバフ研
摩された板厚1mm×幅300mmのTi板の両面に、板
厚0.5mm×幅300mmのAl板を、前記Ti板に対向さ
せながら走行させ、各板を重ね合せて、圧下率60
%にて冷間圧接して、板厚0.8mmの3層クラツド
板に作製した。 その後、真空炉中で550℃、3Hrの拡散焼鈍を
行つた後、圧下率60%にて劣冷間圧延を行つて、
3層クラツド板を得た。 前記クラツド板より試験片を採取して、引張強
さ、伸び、ヤング率、体積抵抗率、比重、及び構
成各層の層厚を測定して、その結果を第2表に示
す。
[Table] Example 2 An Al plate of 0.5 mm in thickness x 300 mm in width was placed on both sides of a Ti plate of 1 mm in thickness x 300 mm in width, which had been rewound by an unwind roller and had its surface buffed, facing the Ti plate. Run it while moving, overlap each plate, and reduce the rolling reduction rate to 60.
A three-layer clad plate with a thickness of 0.8 mm was fabricated by cold pressure welding at 0.8 mm. After that, after diffusion annealing at 550℃ for 3 hours in a vacuum furnace, cold rolling was performed at a reduction rate of 60%.
A three-layer clad board was obtained. A test piece was taken from the clad plate, and the tensile strength, elongation, Young's modulus, volume resistivity, specific gravity, and layer thickness of each layer were measured. The results are shown in Table 2.

【表】【table】

【表】【table】 【図面の簡単な説明】[Brief explanation of drawings]

第1図はこの発明による製造方法を示す説明図
である。第2図は試験片の説明図である。 1……Ti板、2,3……Al板、4……圧接ロ
ーラ、5……連続焼鈍炉、6……圧延ローラ、7
……軟化処理炉。
FIG. 1 is an explanatory diagram showing the manufacturing method according to the present invention. FIG. 2 is an explanatory diagram of the test piece. 1... Ti plate, 2, 3... Al plate, 4... Pressure roller, 5... Continuous annealing furnace, 6... Rolling roller, 7
...Softening treatment furnace.

Claims (1)

【特許請求の範囲】 1 表面を清浄化したTi板の片面あるいは両面
に、 クラツド板の上記Ti層、Al層の層厚比が 1:0.01〜4なる如く、予めその板厚を設定し
たAl板を対向し、前記Ti板と重ね合せた後、冷
間にて圧下率30%〜70%で圧接し、 その後、不活性ガス、あるいは真空中にて 500℃〜600℃、1Hr〜6Hrの条件で拡散焼鈍を
施すことを特徴とする多層クラツド板の製造方
法。
[Claims] 1. On one or both sides of a Ti plate whose surface has been cleaned, an Al plate whose thickness is set in advance such that the thickness ratio of the Ti layer and Al layer of the cladding plate is 1:0.01 to 4. After stacking the plates facing each other on the Ti plate, they are cold welded at a reduction rate of 30% to 70%, and then heated in an inert gas or vacuum at 500℃ to 600℃ for 1Hr to 6Hr. A method for manufacturing a multilayer clad plate, characterized by performing diffusion annealing under certain conditions.
JP28956186A 1986-12-04 1986-12-04 Production of multi-layered clad plate Granted JPS63140782A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP28956186A JPS63140782A (en) 1986-12-04 1986-12-04 Production of multi-layered clad plate

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP28956186A JPS63140782A (en) 1986-12-04 1986-12-04 Production of multi-layered clad plate

Publications (2)

Publication Number Publication Date
JPS63140782A JPS63140782A (en) 1988-06-13
JPH0256191B2 true JPH0256191B2 (en) 1990-11-29

Family

ID=17744824

Family Applications (1)

Application Number Title Priority Date Filing Date
JP28956186A Granted JPS63140782A (en) 1986-12-04 1986-12-04 Production of multi-layered clad plate

Country Status (1)

Country Link
JP (1) JPS63140782A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10103169B4 (en) * 2001-01-25 2005-09-01 Deutsche Titan Gmbh A method of manufacturing a molded component using a roll-plated titanium sheet
CN1241732C (en) 2001-02-27 2006-02-15 特里尔人轧钢技术有限公司 Method of manufacturing metallic composite material
JP2008006445A (en) * 2006-06-27 2008-01-17 Tohoku Univ Method of joining titanium alloy and aluminum material
DE102006031469B4 (en) * 2006-07-05 2008-04-30 Wickeder Westfalenstahl Gmbh Method for producing a component from a titanium flat product for high-temperature applications
ITRM20120168A1 (en) * 2012-04-19 2013-10-20 Ct Sviluppo Materiali Spa PROCEDURE FOR THE PRODUCTION OF A COMPOSITE MULTI-LAYER WITH A REINFORCED AND MULTI-LAYING COMPOSITE METALLIC MATRIX.
CN104209659B (en) * 2013-05-31 2016-08-24 宝山钢铁股份有限公司 The implementation method of vacuum during the welding of a kind of composite billet assembly
CN113909717B (en) * 2021-11-02 2022-12-02 中国人民解放军陆军工程大学 Titanium/aluminum/titanium double-sided multilayer composite material fusion brazing method

Also Published As

Publication number Publication date
JPS63140782A (en) 1988-06-13

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