JPH0940476A - Joined body of aluminum alloy member and ceramic member - Google Patents

Joined body of aluminum alloy member and ceramic member

Info

Publication number
JPH0940476A
JPH0940476A JP11015296A JP11015296A JPH0940476A JP H0940476 A JPH0940476 A JP H0940476A JP 11015296 A JP11015296 A JP 11015296A JP 11015296 A JP11015296 A JP 11015296A JP H0940476 A JPH0940476 A JP H0940476A
Authority
JP
Japan
Prior art keywords
aluminum alloy
ceramic
joined body
thickness
ceramic member
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.)
Pending
Application number
JP11015296A
Other languages
Japanese (ja)
Inventor
Masaya Ito
正也 伊藤
Tomoo Tanaka
智雄 田中
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.)
Niterra Co Ltd
Original Assignee
NGK Spark Plug 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 NGK Spark Plug Co Ltd filed Critical NGK Spark Plug Co Ltd
Priority to JP11015296A priority Critical patent/JPH0940476A/en
Publication of JPH0940476A publication Critical patent/JPH0940476A/en
Pending legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To obtain a joined body securely joined with a high-strength aluminum alloy member and a ceramic member by joining the age hardening type aluminum alloy member and the ceramic member via an intermediate member consisting of a non-heat treatment type aluminum alloy. SOLUTION: A round bar (a diameter 10mm and length 10mm) made of Si3 N4 , ZrO2 or Al2 O3 is prepd. as, for example, the ceramic member 2 and an Al film 5 of a thickness 1μm is formed by a vapor deposition method on one side end face which is a joint surface. A round bar (a diameter 10mm and length 10mm) made of the material meeting the requirements specified in JIS(Japanese Industrial Standards) 2024, 7075 is prepd. as the Al alloy member 3. A disk (a diameter 10mm and thickness 0.5mm) made of the material meeting the requirements specified in JIS 1050, 5052 is prepd. as the intermediate member 4 made of the non-heat treatment type Al alloy. Alloy foil (diameter 10mm, thickness 0.05mm) of 58% Zn-30%Al-10%Cu-2%Si is prepd. as a brazing filler metal 6. These materials are superposed on each other in order shown in Fig., are set in jigs and are brazed while being held for two hours at 470 deg.C in the nitrogen in a heating furnace.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、アルミニウム合金部材
とセラミックス部材との接合体に関し、更に詳しくは自
動車、航空機、鉄道車両等に用いられる構造部材や超音
波加工に用いられるホーンに代表される加工工具等の産
業部品に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a joined body of an aluminum alloy member and a ceramic member, and more specifically, it is represented by a structural member used in automobiles, aircrafts, railway vehicles and the like, and a horn used in ultrasonic machining. Related to industrial parts such as processing tools.

【0002】[0002]

【従来の技術】アルミニウム又はその合金は、一般の鉄
系材料に比べて軽量、高熱伝導、高電気伝導、高耐食性
などの利点を有する。特に時効硬化型アルミニウム合金
であるJIS2000系のアルミニウム合金、JIS6
000系のアルミニウム合金、JIS7000系のアル
ミニウム合金は熱処理により高い材料強度が得られるた
め、構造部材として広く用いられている。一方、セラミ
ックス材料は耐摩耗性、耐食性、耐熱性に優れるためア
ルミニウム合金と複合化することにより優れた機能を具
備せしめることが可能となる。かかる複合化の手段とし
ては、鋳ぐるみやろう付接合が一般的に知られている。
2. Description of the Related Art Aluminum or its alloy has advantages such as light weight, high heat conduction, high electric conduction and high corrosion resistance as compared with general iron-based materials. In particular, JIS2000 series aluminum alloy, JIS6, which is an age hardening type aluminum alloy.
000 series aluminum alloys and JIS 7000 series aluminum alloys are widely used as structural members because high material strength can be obtained by heat treatment. On the other hand, ceramic materials are excellent in wear resistance, corrosion resistance, and heat resistance, so that they can be provided with excellent functions by combining with an aluminum alloy. As a means for forming such a composite, cast dolls and brazing are generally known.

【0003】[0003]

【発明が解決しようとする課題】しかし、セラミックス
部材を鋳ぐるみした複合体は、アルミニウム合金が鋳造
のまま用いられるのでアルミニウム合金自体の強度が低
い。また、一般に鋳ぐるみしたものは圧延等の加工によ
り高強度となるが、セラミックス部材を既に鋳ぐるみし
たものは加工が困難である。一方、ろう付接合によれば
アルミニウム合金とセラミックス部材との複合化は可能
であるが、通常ろう付け接合は400℃以上で行なわれ
るためアルミニウム合金自体が鈍ってしまい、やはりア
ルミニウム合金自体の強度が低い。このためろう付接合
の終了後に溶体化処理及び時効処理が必要となるが、通
常溶体化は450℃から550℃の温度範囲から水焼入
れすることにより行なわれ、このときアルミニウム合金
が一層硬化する。これに伴って発生する熱応力(熱膨張
差に起因する残留応力)によりセラミックス部材にクラ
ックが発生したり、接合面が剥離する等の不具合が生じ
ることがあった。この熱応力は、セラミックス材料がア
ルミニウム合金に比べ、熱膨張係数が小さいためであ
る。
However, since the aluminum alloy is used as it is in the casting, the strength of the aluminum alloy itself is low. Further, in general, cast products have high strength by processing such as rolling, but it is difficult to process cast ceramic products that have already been cast. On the other hand, by brazing, an aluminum alloy and a ceramic member can be composited, but since the brazing is usually performed at 400 ° C. or higher, the aluminum alloy itself becomes dull, and the strength of the aluminum alloy itself is also low. Low. For this reason, solution treatment and aging treatment are required after the completion of brazing, but solution treatment is usually performed by water quenching from a temperature range of 450 ° C to 550 ° C, at which time the aluminum alloy is further hardened. Due to the thermal stress (residual stress resulting from the difference in thermal expansion) generated along with this, a crack may occur in the ceramic member, or a joint surface may be peeled off. This thermal stress is because the ceramic material has a smaller coefficient of thermal expansion than the aluminum alloy.

【0004】本発明の課題は、高強度なアルミニウム合
金部材とセラミックス部材とが強固に接合された接合体
を提供することである。
An object of the present invention is to provide a joined body in which a high-strength aluminum alloy member and a ceramic member are firmly joined.

【0005】[0005]

【課題を解決するための手段及び作用】その第1の手段
は、時効硬化型アルミニウム合金部材とセラミックス部
材とが非熱処理型アルミニウム合金からなる中間部材を
介して接合されているアルミニウム合金部材とセラミッ
クス部材との接合体である。第1の手段の接合体は、溶
体化処理(焼入れ)により又は使用時の熱間において
も、時効硬化型アルミニウム合金は硬化するが非熱処理
型アルミニウム合金は硬化しない。従って非熱処理型ア
ルミニウム合金からなる中間部材は、時効処理型アルミ
ニウム合金部材とセラミックス部材との間で応力緩衝層
として有効に機能する。更に部材間に生ずる各部材の熱
膨張係数の差に起因するセラミックス部材に発生するク
ラックや、中間部材とセラミックス部材との接合面の剥
離を防止することができる。その第2の手段は、時効硬
化型アルミニウム合金部材とセラミックス部材とが非熱
処理型アルミニウム合金からなる中間部材を2以上介し
て接合されているアルミニウム合金部材とセラミックス
部材との接合体である。第2の手段の接合体は、第1の
手段の接合体と同様の作用を有する他に中間部材の数が
多い分、更に中間部材が応力緩衝層として有効に機能
し、部材間に生ずる各部材の熱膨張係数の差に起因する
セラミックス部材に発生するクラックや、中間部材とセ
ラミックス部材との接合面の剥離を防止することができ
る。
[Means and Action for Solving the Problems] The first means thereof is an aluminum alloy member and a ceramic in which an age hardening type aluminum alloy member and a ceramic member are joined via an intermediate member made of a non-heat treatment type aluminum alloy. It is a joined body with a member. In the joined body of the first means, the age hardening type aluminum alloy is hardened but the non-heat treatment type aluminum alloy is not hardened by solution treatment (quenching) or even during hot use. Therefore, the intermediate member made of the non-heat treatment type aluminum alloy effectively functions as a stress buffer layer between the aging treatment type aluminum alloy member and the ceramic member. Further, it is possible to prevent cracks occurring in the ceramic member due to the difference in the thermal expansion coefficient of each member between the members and peeling of the joint surface between the intermediate member and the ceramic member. The second means is a joined body of an aluminum alloy member and a ceramic member in which the age hardening type aluminum alloy member and the ceramic member are joined via two or more intermediate members made of a non-heat treatment type aluminum alloy. The joined body of the second means has the same function as that of the joined body of the first means, and in addition to the large number of intermediate members, the intermediate member effectively functions as a stress buffer layer, and each of the members generated between the members. It is possible to prevent cracks occurring in the ceramic member due to the difference in the coefficient of thermal expansion of the members and peeling of the joint surface between the intermediate member and the ceramic member.

【0006】ここで時効硬化型アルミニウム合金は、例
えばJIS2000系に規定されるAl−Cu系、JI
S6000系に規定されるAl−Mg−Si系、JIS
7000系に規定されるAl−Zn−Mg系、あるいは
JISAC2A、JISAC4A等に代表される合金鋳
物,ADC10等に代表されるダイキャスト合金等のア
ルミニウム合金である。即ち、例えば、400〜600
℃程度の接合熱処理により、材料の硬さが低下し、再度
溶体化及び時効硬化処理を必要とするようなアルミニウ
ム合金である。また非熱処理型アルミニウム合金は、例
えばJIS1000系に規定される純Al系、JIS3
000系に規定されるAl−Mn系、JIS4000系
に規定されるAl−Si系、JIS5000系に規定さ
れるAl−Mg系のアルミニウム合金である。前記非熱
処理型アルミニウム合金は、Al−Mg系合金であるこ
とが好ましい。それは、例えばJIS5000系のAl
−Mg系アルミニウム合金は、例えばJIS3000系
のAl−Mn系アルミニウム合金に比して強度が高いの
で耐力を向上させつつ応力緩和機能を維持できるからで
ある。また、前記非熱処理型アルミニウム合金は、Al
を99重量%以上含有すること、いわゆる純Al系アル
ミニウムが好ましい。それは、Alを99重量%以上含
有する純Al系アルミニウムは、軟質であり応力緩和に
大きく寄与するからである。
Here, the age hardening type aluminum alloy is, for example, Al-Cu system or JI system defined in JIS2000 system.
Al-Mg-Si system specified by S6000 system, JIS
It is an Al-Zn-Mg system defined in 7000 series, an alloy casting represented by JISAC2A, JISAC4A, etc., or an aluminum alloy such as a die cast alloy represented by ADC10, etc. That is, for example, 400 to 600
It is an aluminum alloy whose hardness is lowered by the joining heat treatment at about ° C, and which requires solution treatment and age hardening treatment again. Further, the non-heat treatment type aluminum alloy is, for example, pure Al based on JIS1000, JIS3 based.
Al-Mn-based aluminum alloys defined in 000 series, Al-Si systems defined in JIS 4000 series, and Al-Mg series aluminum alloys defined in JIS 5000 series. The non-heat treatment type aluminum alloy is preferably an Al-Mg based alloy. It is, for example, JIS 5000 series Al
This is because the -Mg-based aluminum alloy has a higher strength than, for example, the JIS3000-based Al-Mn-based aluminum alloy, and thus can improve the proof stress and maintain the stress relaxation function. The non-heat treatment type aluminum alloy is Al
Of 99% by weight or more, that is, so-called pure Al-based aluminum is preferable. This is because pure Al-based aluminum containing 99% by weight or more of Al is soft and greatly contributes to stress relaxation.

【0007】前記中間部材の厚さは、0.1〜2.0m
mであることが好ましい。0.1mm未満では応力緩和
機能に乏しく、2.0mmを越えると効果があまり変わ
らないばかりか接合体に負荷が生じた時に中間部材に降
伏が起きることがあり好ましくない。また、前記中間部
材の厚さが、0.1〜1.0mmであることが好まし
い。0.1mm未満では上記と同様に応力緩和機能に乏
しく、1mm以下であれば上記の2mm以下の場合に比
し、更に中間部材に降伏が起こりにくい。前記時効硬化
型アルミニウム合金部材の硬さがHv100以上である
接合体が好ましい。Hv100以上とすることにより耐
力250MPa程度の材料強度を確保できる。ここで、
「中間部材の厚さ」は、第1の手段及び第2の手段とも
に一つの中間部材の厚さを意味する。
The thickness of the intermediate member is 0.1 to 2.0 m.
m is preferable. If it is less than 0.1 mm, the stress relaxation function is poor, and if it exceeds 2.0 mm, not only the effect does not change significantly, but also the intermediate member may yield when a load is applied to the bonded body, which is not preferable. Further, the thickness of the intermediate member is preferably 0.1 to 1.0 mm. If it is less than 0.1 mm, the stress relaxation function is poor as in the above case, and if it is 1 mm or less, yielding is less likely to occur in the intermediate member as compared with the case of 2 mm or less. A joined body in which the age-hardening aluminum alloy member has a hardness of Hv100 or more is preferable. By setting the Hv to 100 or more, a material strength with a yield strength of about 250 MPa can be secured. here,
The "thickness of the intermediate member" means the thickness of one intermediate member for both the first means and the second means.

【0008】ところで、第2の手段のように2以上の中
間部材を介した接合体は、個々の中間部材の厚みが2.
0mm以下であっても、合計した中間部材の厚みが2.
0mmを越える場合がある。この場合には、個々の中間
部材が応力緩衝層として個々に機能し、部材間に生ずる
各部材の熱膨張係数の差に起因するセラミックス部材に
発生するクラックや、中間部材とセラミックス部材との
接合面の剥離を防止することができる。即ち、合計した
中間部材の厚みが2.0mmを越えた場合は、個々の中
間部材の厚みが2.0mmを越えた場合に比べ、中間部
材同士の接合界面が更に応力緩衝層として機能する。ま
た、第2の手段のように2以上の中間部材を介した接合
体の好ましい態様の中間部材の厚さを0.1〜1.0m
mとした場合であっても、同様である。つまり、個々の
中間部材の厚みが1.0mm以下であっても、合計した
中間部材の厚みが1.0mmを越える場合がある。この
場合には、個々の中間部材が応力緩衝層として個々に機
能し、部材間に生ずる各部材の熱膨張係数の差に起因す
るセラミックス部材に発生するクラックや、中間部材と
セラミックス部材との接合面の剥離を防止することがで
きる。即ち、合計した中間部材の厚みが1.0mmを越
えた場合は、個々の中間部材の厚みが1.0mmを越え
た場合に比べ、中間部材同士の接合界面が更に応力緩衝
層として機能する。またセラミックスは、例えば、Al
23、ZrO2、Si34 、AlN、SiC或いはこれ
らの複合材、又は超硬、サーメット等の低膨張焼結材料
等周知の材料が使用可能である。ここで、溶体化処理と
は、高温に加熱して析出相を母相中に溶かし込み、これ
を急冷する処理をいう。
By the way, in the joined body having two or more intermediate members as in the second means, the thickness of each intermediate member is 2.
Even if it is 0 mm or less, the total thickness of the intermediate members is 2.
It may exceed 0 mm. In this case, each intermediate member individually functions as a stress buffer layer, and cracks are generated in the ceramic member due to the difference in thermal expansion coefficient between the members that occurs between the members, and the joining of the intermediate member and the ceramic member. The peeling of the surface can be prevented. That is, when the total thickness of the intermediate members exceeds 2.0 mm, the joint interface between the intermediate members further functions as a stress buffer layer as compared with the case where the thickness of each intermediate member exceeds 2.0 mm. Further, the thickness of the intermediate member in a preferred embodiment of the joined body having two or more intermediate members as in the second means is 0.1 to 1.0 m.
The same applies when m is set. That is, even if the thickness of each intermediate member is 1.0 mm or less, the total thickness of the intermediate members may exceed 1.0 mm. In this case, each intermediate member individually functions as a stress buffer layer, and cracks are generated in the ceramic member due to the difference in thermal expansion coefficient between the members that occurs between the members, and the joining of the intermediate member and the ceramic member. The peeling of the surface can be prevented. That is, when the total thickness of the intermediate members exceeds 1.0 mm, the joint interface between the intermediate members further functions as a stress buffer layer as compared with the case where the thickness of each intermediate member exceeds 1.0 mm. Further, the ceramic is, for example, Al
Well-known materials such as 2 O 3 , ZrO 2 , Si 3 N 4 , AlN, SiC or composite materials thereof, or low expansion sintered materials such as cemented carbide and cermet can be used. Here, the solution treatment is a treatment in which the precipitation phase is melted in the mother phase by heating it at a high temperature, and this is rapidly cooled.

【0009】[0009]

【発明の実施の形態】本発明の一の実施の形態を図1
(図2)に示す。アルミニウム合金部材とセラミックス
部材との接合体1は、図1に示すように時効硬化型アル
ミニウム合金部材3とセラミックス部材2とが非熱処理
型アルミニウム合金からなる中間部材4を介して接合さ
れている。本発明の他の実施の形態である接合体の接合
する直前の状態を図3に示す。アルミニウム合金部材と
セラミックス部材との接合体1は、時効硬化型アルミニ
ウム合金部材3とセラミックス部材2とを非熱処理型ア
ルミニウム合金からなる中間部材4及び中間部材8を介
して接合することにより得ることができる。本発明の他
の実施の形態である接合体の接合する直前の状態を図4
に示す。アルミニウム合金部材とセラミックス部材との
接合体1は、時効硬化型アルミニウム合金部材3とセラ
ミックス部材2とを非熱処理型アルミニウム合金からな
る中間部材4、中間部材8及び中間部材10を介して接
合することにより得ることができる。その具体的な接合
方法は、ろう付けによる接合が好ましいが、拡散接合、
摩擦圧接、はんだ付けも可能である。また、接合後に溶
体化処理、または溶体化処理及び時効硬化処理すること
により更に強固な接合体を得ることができる。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT FIG. 1 shows an embodiment of the present invention.
(FIG. 2). As shown in FIG. 1, a joined body 1 of an aluminum alloy member and a ceramic member is joined with an age hardening type aluminum alloy member 3 and a ceramic member 2 via an intermediate member 4 made of a non-heat treatment type aluminum alloy. FIG. 3 shows a state immediately before joining of a joined body which is another embodiment of the present invention. The joined body 1 of the aluminum alloy member and the ceramic member is obtained by joining the age hardening type aluminum alloy member 3 and the ceramic member 2 via the intermediate member 4 and the intermediate member 8 made of the non-heat treatment type aluminum alloy. it can. FIG. 4 shows a state immediately before joining of a joined body according to another embodiment of the present invention.
Shown in The joined body 1 of the aluminum alloy member and the ceramic member is formed by joining the age hardening type aluminum alloy member 3 and the ceramic member 2 via the intermediate member 4, the intermediate member 8 and the intermediate member 10 made of the non-heat treatment type aluminum alloy. Can be obtained by The specific joining method is preferably joining by brazing, but diffusion joining,
Friction welding and soldering are also possible. Further, a stronger joint can be obtained by performing solution treatment or solution treatment and age hardening treatment after joining.

【0010】ー実験例1ー セラミックス部材2として表1に示す各種セラミックス
よりなる丸棒(直径10mm、長さ10mm)を用意
し、接合面となる片側端面に蒸着法により厚さ1μmの
Al膜5を成膜した。アルミニウム合金部材3として表
1に示すJISに規格する材料よりなる丸棒(直径10
mm、長さ50mm)を用意した。また非熱処理型アル
ミニウム合金からなる中間部材4として表1に示すJI
Sに規格する材料よりなる円板(直径10mm、厚さ
0.5mm)を準備した。ろう材6として、58%Zn
−30%Al−10%Cuー2%Siの合金箔(直径1
0mm、厚さ0.05mm)を準備し、これらを図2に
示す順番に重ね合せ、図示しない治具にセットした。こ
れらを加熱炉中にセットして窒素中にて、470℃で2
時間保持してろう付を行なった。得られた接合体1に溶
体化処理を行なった後、時効処理を行なった。溶体化処
理は、表1に記載の各温度に1時間保持したのち直ちに
図5に示す様にアルミニウム合金部材3の丸棒部分のみ
を水焼入れすることにより行なった。
--Experimental Example 1-- As a ceramic member 2, a round bar (diameter 10 mm, length 10 mm) made of various ceramics shown in Table 1 was prepared, and an Al film having a thickness of 1 μm was formed on one end surface to be a joint surface by vapor deposition. 5 was deposited. As the aluminum alloy member 3, a round bar (diameter 10
mm, length 50 mm). The JI shown in Table 1 as the intermediate member 4 made of a non-heat treatment type aluminum alloy.
A disk (diameter 10 mm, thickness 0.5 mm) made of a material specified by S was prepared. As the brazing material 6, 58% Zn
-30% Al-10% Cu-2% Si alloy foil (diameter 1
0 mm, thickness 0.05 mm) were prepared, these were piled up in the order shown in FIG. 2 and set on a jig (not shown). Set these in a heating furnace and place in nitrogen at 470 ° C for 2
Brazing was performed while holding the time. The obtained joined body 1 was subjected to solution treatment and then subjected to aging treatment. The solution treatment was carried out by holding each temperature shown in Table 1 for 1 hour and then immediately water quenching only the round bar portion of the aluminum alloy member 3 as shown in FIG.

【00011】なお比較例として、中間部材を用いずに
直接両部材を接合したもの(No.14)についても同
様に溶体化処理後に時効処理を行なった。時効処理を完
了した接合体の少なくとも接合部の外周を直径9mmと
なるまで円筒研削し、図6に示す様にアルミニウム合金
部材3側をクランプしてセラミックス部材2に荷重をか
ける片持曲げ試験にて接合強度を評価した。また、評価
終了後にアルミニウム合金部材3の丸棒を切断してビッ
カース硬度を測定した。結果を表1に示す。
As a comparative example, the one in which both members were directly joined without using the intermediate member (No. 14) was similarly subjected to the solution treatment and then the aging treatment. In a cantilever bending test in which at least the outer periphery of the joined portion of the joined body that has been aged is cylindrically ground to a diameter of 9 mm, and the aluminum alloy member 3 side is clamped to apply a load to the ceramic member 2 as shown in FIG. And the bonding strength was evaluated. After the evaluation, the round bar of the aluminum alloy member 3 was cut to measure the Vickers hardness. The results are shown in Table 1.

【0012】[0012]

【表1】 [Table 1]

【0013】本発明の実施例の接合体は、いずれもセラ
ミックス部材にクラックや部材同士の剥離の発生がなく
良好な接合強度を有したが、中間部材を用いない比較例
の接合体(No.13、No.14)は溶体化処理の際に
セラミックス部材にクラックが発生していた。結果から
分かるように中間部材が軟質で厚さが厚くなることによ
り、接合体の応力緩和が十分に行われていた。よって、
接合強度が上昇し、軟質である中間部材が変形するに至
ったと考えられる。中間部材が厚い分、変形の度合いが
大きかった(No.5、No.7、No.12)。
The joints of the examples of the present invention all had good joint strength without cracks in the ceramic members or separation of the members from each other, but the joints of the comparative example (No. No. 13, No. 14) had cracks in the ceramic member during the solution treatment. As can be seen from the results, the intermediate member was soft and had a large thickness, whereby the stress of the bonded body was sufficiently relaxed. Therefore,
It is considered that the joint strength increased and the soft intermediate member was deformed. The thicker the intermediate member, the greater the degree of deformation (No. 5, No. 7, No. 12).

【0014】ー実験例2ー セラミックス部材2として表2に示す各種セラミックス
よりなる丸棒(直径10mm、長さ10mm)を用意
し、接合面となる片側端面に蒸着法により厚さ1μmの
Al膜5を成膜した。アルミニウム合金部材3として表
2に示すJISに規格する材料よりなる丸棒(直径10
mm、長さ50mm)を用意した。また非熱処理型アル
ミニウム合金からなる中間部材4、中間部材8として表
2に示すJISに規格する材料よりなる円板(直径10
mm、厚さ0.5mm)を準備した。ろう材6として、
58%Zn−30%Al−10%Cuー2%Siの合金
箔(直径10mm、厚さ0.05mm)を準備し、これ
らを図3に示す順番に重ね合せ、図示しない治具にセッ
トした。これらを加熱炉中にセットして窒素中にて、4
70℃で2時間保持してろう付を行なった。得られた接
合体1に溶体化処理を行なった後、時効処理を行なっ
た。溶体化処理は、表2に記載の各温度に1時間保持し
たのち直ちに図5に示す様にアルミニウム合金部材3の
丸棒部分のみを水焼入れすることにより行なった。時効
処理を完了した接合体の少なくとも接合部の外周を直径
9mmとなるまで円筒研削し、図6に示す様にアルミニ
ウム合金部材3側をクランプしてセラミックス部材2に
荷重をかける片持曲げ試験にて接合強度を評価した。ま
た、評価終了後にアルミニウム合金部材3の丸棒を切断
してビッカース硬度を測定した。結果を表2に示す。
--Experimental Example 2-- As a ceramic member 2, a round bar (diameter 10 mm, length 10 mm) made of various ceramics shown in Table 2 was prepared, and an Al film having a thickness of 1 μm was formed on one end surface to be a joint surface by vapor deposition. 5 was deposited. As the aluminum alloy member 3, a round bar (diameter 10
mm, length 50 mm). Further, as the intermediate member 4 and the intermediate member 8 made of the non-heat treatment type aluminum alloy, a disk (diameter 10
mm, thickness 0.5 mm) was prepared. As brazing material 6,
An alloy foil of 58% Zn-30% Al-10% Cu-2% Si (diameter 10 mm, thickness 0.05 mm) was prepared, these were stacked in the order shown in FIG. 3, and set on a jig (not shown). . Set these in a heating furnace and place in nitrogen for 4
Brazing was performed by holding at 70 ° C. for 2 hours. The obtained joined body 1 was subjected to solution treatment and then subjected to aging treatment. The solution treatment was performed by holding each temperature shown in Table 2 for 1 hour and then immediately water quenching only the round bar portion of the aluminum alloy member 3 as shown in FIG. In a cantilever bending test in which at least the outer periphery of the joined portion of the joined body that has been aged is cylindrically ground to a diameter of 9 mm, and the aluminum alloy member 3 side is clamped to apply a load to the ceramic member 2 as shown in FIG. And the bonding strength was evaluated. After the evaluation, the round bar of the aluminum alloy member 3 was cut to measure the Vickers hardness. Table 2 shows the results.

【0015】[0015]

【表2】 [Table 2]

【0016】本発明の実施例の接合体は、いずれもセラ
ミックス部材にクラックや部材同士の剥離の発生がなく
良好な接合強度を有した。結果から分かるように中間部
材が軟質で厚さが厚くなることにより、接合体の応力緩
和が十分に行われていた。よって、接合強度が上昇し、
軟質である中間部材が変形するに至ったと考えられる。
中間部材が厚い分、変形の度合いが大きかった(No.
22)。また、実施例1に比べ、中間部材の数に起因
し、全体的に接合強度が高かった。
All of the joined bodies of the examples of the present invention had good joining strength without cracks in the ceramic members or peeling of the members from each other. As can be seen from the results, the intermediate member was soft and had a large thickness, whereby the stress of the bonded body was sufficiently relaxed. Therefore, the bonding strength increases,
It is considered that the soft intermediate member has been deformed.
The thicker the intermediate member, the greater the degree of deformation (No.
22). In addition, due to the number of intermediate members, the bonding strength was higher overall as compared with Example 1.

【0017】−実験例3− セラミックス部材2として表3に示すセラミックスより
なる丸棒(直径10mm、長さ10mm)を用意し、接
合面となる片側端面に蒸着法により厚さ1μmのAl膜
5を成膜した。アルミニウム合金部材3として表3に示
すJISに規格する材料よりなる丸棒(直径10mm、
長さ50mm)を用意した。また非熱処理型アルミニウ
ム合金からなる中間部材4、中間部材8、中間部材10
として表3に示すJISに規格する材料よりなる円板
(直径10mm、厚さ0.5mm)を準備した。ろう材
6として、58%Zn−30%Al−10%Cuー2%
Siの合金箔(直径10mm、厚さ0.05mm)を準
備し、これらを図4に示す順番に重ね合せ、図示しない
治具にセットした。これらを加熱炉中にセットして窒素
中にて、470℃で2時間保持してろう付を行なった。
得られた接合体1に溶体化処理を行なった後、時効処理
を行なった。溶体化処理は、表3に記載の各温度に1時
間保持したのち直ちに図5に示す様にアルミニウム合金
部材3の丸棒部分のみを水焼入れすることにより行なっ
た。時効処理を完了した接合体の少なくとも接合部の外
周を直径9mmとなるまで円筒研削し、図6に示す様に
アルミニウム合金部材3側をクランプしてセラミックス
部材2に荷重をかける片持曲げ試験にて接合強度を評価
した。また、評価終了後にアルミニウム合金部材3の丸
棒を切断してビッカース硬度を測定した。結果を表3に
示す。
Experimental Example 3 As the ceramic member 2, a round bar (diameter 10 mm, length 10 mm) made of ceramics shown in Table 3 was prepared, and an Al film 5 having a thickness of 1 μm was formed on one end face to be a joint surface by vapor deposition. Was deposited. As the aluminum alloy member 3, a round bar (diameter 10 mm, made of a material specified in JIS shown in Table 3
(Length 50 mm). Further, the intermediate member 4, the intermediate member 8 and the intermediate member 10 made of a non-heat treatment type aluminum alloy.
A disk (diameter: 10 mm, thickness: 0.5 mm) made of a JIS standard material shown in Table 3 was prepared. As the brazing material 6, 58% Zn-30% Al-10% Cu-2%
Alloy foils of Si (diameter 10 mm, thickness 0.05 mm) were prepared, these were stacked in the order shown in FIG. 4, and set on a jig (not shown). These were set in a heating furnace and held in nitrogen at 470 ° C. for 2 hours for brazing.
The obtained joined body 1 was subjected to solution treatment and then subjected to aging treatment. The solution treatment was carried out by holding each temperature shown in Table 3 for 1 hour and then immediately water quenching only the round bar portion of the aluminum alloy member 3 as shown in FIG. In a cantilever bending test in which at least the outer periphery of the joined portion of the joined body that has been aged is cylindrically ground to a diameter of 9 mm, and the aluminum alloy member 3 side is clamped to apply a load to the ceramic member 2 as shown in FIG. And the bonding strength was evaluated. After the evaluation, the round bar of the aluminum alloy member 3 was cut to measure the Vickers hardness. The results are shown in Table 3.

【0018】[0018]

【表3】 [Table 3]

【0019】本発明の実施例の接合体は、いずれもセラ
ミックス部材にクラックや部材同士の剥離の発生がなく
良好な接合強度を有した。結果から分かるように中間部
材が軟質で厚さが厚くなることにより、接合体の応力緩
和が十分に行われていた。よって、接合強度が上昇し、
軟質である中間部材が変形するに至ったと考えられる。
中間部材が厚い分、変形の度合いが大きかった(No.
23)。また、実施例1及び実施例2に比べ、中間部材
の数に起因し、全体的に接合強度が高かった。
All of the bonded bodies of the examples of the present invention had good bonding strength without cracks in the ceramic members or peeling of the members from each other. As can be seen from the results, the intermediate member was soft and had a large thickness, whereby the stress of the bonded body was sufficiently relaxed. Therefore, the bonding strength increases,
It is considered that the soft intermediate member has been deformed.
The thicker the intermediate member, the greater the degree of deformation (No.
23). Moreover, compared with Examples 1 and 2, due to the number of intermediate members, the overall bonding strength was high.

【0020】[0020]

【発明の効果】本発明による構造の接合体とすることに
より、高強度なアルミニウム合金部材とセラミックス部
材とが強固に接合された接合体を得ることができる。
EFFECTS OF THE INVENTION By using the joined body having the structure according to the present invention, a joined body in which a high-strength aluminum alloy member and a ceramic member are firmly joined can be obtained.

【図面の簡単な説明】[Brief description of drawings]

【図1】実験例1の本発明のアルミニウム合金部材とセ
ラミックス部材との接合体の斜視図である。
FIG. 1 is a perspective view of a joined body of an aluminum alloy member of the present invention and a ceramic member of Experimental Example 1.

【図2】実験例1の本発明のアルミニウム合金部材とセ
ラミックス部材との接合体の両部材を接合する直前の状
態を示す正面図である。
FIG. 2 is a front view showing a state immediately before joining both members of the joined body of the aluminum alloy member of the present invention and the ceramic member of Experimental Example 1.

【図3】実験例2の本発明のアルミニウム合金部材とセ
ラミックス部材との接合体の両部材を接合する直前の状
態を示す正面図である。
FIG. 3 is a front view showing a state immediately before joining both members of a joined body of an aluminum alloy member of the present invention and a ceramic member of Experimental Example 2.

【図4】実験例3の本発明のアルミニウム合金部材とセ
ラミックス部材との接合体の両部材を接合する直前の状
態を示す正面図である。
FIG. 4 is a front view showing a state immediately before joining both members of a joined body of an aluminum alloy member of the present invention and a ceramic member of Experimental Example 3.

【図5】溶体化処理の方法を示す正面図である。FIG. 5 is a front view showing a solution treatment method.

【図6】接合強度を評価する方法を示す正面図である。FIG. 6 is a front view showing a method for evaluating bonding strength.

【符号の説明】[Explanation of symbols]

1 ・・・ アルミニウム合金部材とセラミックス部材
との接合体 2 ・・・ セラミックス部材 3 ・・・ アルミニウム合金部材 4 ・・・ 中間部材 5 ・・・ Al膜 6 ・・・ ろう材 7 ・・・ 水 8 ・・・ 中間部材 10・・・ 中間部材
1 ... Joined body of aluminum alloy member and ceramics member 2 ... Ceramics member 3 ... Aluminum alloy member 4 ... Intermediate member 5 ... Al film 6 ... Brazing material 7 ... Water 8 ... Intermediate member 10 ... Intermediate member

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】 時効硬化型アルミニウム合金部材とセラ
ミックス部材とが非熱処理型アルミニウム合金からなる
中間部材を介して接合されていることを特徴とするアル
ミニウム合金部材とセラミックス部材との接合体。
1. A joined body of an aluminum alloy member and a ceramic member, wherein the age hardening type aluminum alloy member and the ceramic member are joined via an intermediate member made of a non-heat treatment type aluminum alloy.
【請求項2】 時効硬化型アルミニウム合金部材とセラ
ミックス部材とが非熱処理型アルミニウム合金からなる
中間部材を2以上介して接合されていることを特徴とす
るアルミニウム合金部材とセラミックス部材との接合
体。
2. A joined body of an aluminum alloy member and a ceramic member, wherein the age hardening type aluminum alloy member and the ceramic member are joined via two or more intermediate members made of a non-heat treatment type aluminum alloy.
【請求項3】 前記非熱処理型アルミニウム合金がAl
−Mg系合金であることを特徴とする請求項1又は2に
記載のアルミニウム合金部材とセラミックス部材との接
合体。
3. The non-heat treatment type aluminum alloy is Al
A joined body of the aluminum alloy member and the ceramic member according to claim 1 or 2, which is a Mg-based alloy.
【請求項4】 前記非熱処理型アルミニウム合金がAl
を99重量%以上含有することを特徴とする請求項1又
は2に記載のアルミニウム合金部材とセラミックス部材
との接合体。
4. The non-heat treatment type aluminum alloy is Al
99% by weight or more is contained, The joined body of the aluminum alloy member and the ceramic member of Claim 1 or 2 characterized by the above-mentioned.
【請求項5】 前記中間部材の厚さが0.1〜2.0m
mであることを特徴とする請求項1〜4のいずれかに記
載のアルミニウム合金部材とセラミックス部材との接合
体。
5. The intermediate member has a thickness of 0.1 to 2.0 m.
The bonded body of the aluminum alloy member and the ceramic member according to any one of claims 1 to 4, wherein m is m.
【請求項6】 前記中間部材の厚さが0.1〜1.0m
mであることを特徴とする請求項1〜4のいずれかに記
載のアルミニウム合金部材とセラミックス部材との接合
体。
6. The intermediate member has a thickness of 0.1 to 1.0 m.
The bonded body of the aluminum alloy member and the ceramic member according to any one of claims 1 to 4, wherein m is m.
【請求項7】 時効硬化型アルミニウム合金部材の硬さ
がHv100以上であることを特徴とする請求項1〜6
のいずれかに記載のアルミニウム合金部材とセラミック
ス部材との接合体。
7. The age hardening type aluminum alloy member has a hardness of Hv100 or more.
A joined body of the aluminum alloy member and the ceramic member according to any one of 1.
JP11015296A 1995-05-22 1996-04-04 Joined body of aluminum alloy member and ceramic member Pending JPH0940476A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11015296A JPH0940476A (en) 1995-05-22 1996-04-04 Joined body of aluminum alloy member and ceramic member

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP14817895 1995-05-22
JP7-148178 1995-05-22
JP11015296A JPH0940476A (en) 1995-05-22 1996-04-04 Joined body of aluminum alloy member and ceramic member

Publications (1)

Publication Number Publication Date
JPH0940476A true JPH0940476A (en) 1997-02-10

Family

ID=26449829

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11015296A Pending JPH0940476A (en) 1995-05-22 1996-04-04 Joined body of aluminum alloy member and ceramic member

Country Status (1)

Country Link
JP (1) JPH0940476A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007111056A1 (en) * 2006-03-28 2007-10-04 Ngk Insulators, Ltd. Honeycomb structure and method for producing same
JP2016052979A (en) * 2014-09-04 2016-04-14 国立研究開発法人産業技術総合研究所 Method for bonding ceramic member and aluminum member
JP2017094390A (en) * 2015-10-19 2017-06-01 株式会社神戸製鋼所 Aluminum structural member
WO2017213258A1 (en) * 2016-06-09 2017-12-14 国立研究開発法人産業技術総合研究所 Method for producing conjugate, and conjugate
EP3584492A4 (en) * 2017-02-15 2021-03-17 Bogachek, Oleg Evgenievich Vessel made of thermally non-hardenable aluminum alloy and method for the production thereof

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007111056A1 (en) * 2006-03-28 2007-10-04 Ngk Insulators, Ltd. Honeycomb structure and method for producing same
US7947103B2 (en) 2006-03-28 2011-05-24 MGK Insulators, Ltd. Honeycomb structure and method for producing same
JP5103377B2 (en) * 2006-03-28 2012-12-19 日本碍子株式会社 Honeycomb structure and manufacturing method thereof
JP2016052979A (en) * 2014-09-04 2016-04-14 国立研究開発法人産業技術総合研究所 Method for bonding ceramic member and aluminum member
JP2017094390A (en) * 2015-10-19 2017-06-01 株式会社神戸製鋼所 Aluminum structural member
WO2017213258A1 (en) * 2016-06-09 2017-12-14 国立研究開発法人産業技術総合研究所 Method for producing conjugate, and conjugate
JPWO2017213258A1 (en) * 2016-06-09 2019-03-07 国立研究開発法人産業技術総合研究所 Manufacturing method of joined body and joined body
EP3584492A4 (en) * 2017-02-15 2021-03-17 Bogachek, Oleg Evgenievich Vessel made of thermally non-hardenable aluminum alloy and method for the production thereof
US11644151B2 (en) 2017-02-15 2023-05-09 Oleg Evgenievich BOGACHEK Vessel made of thermally non-hardenable aluminum alloy and method for the production thereof

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