JPH02171237A - Ceramic and metallic couple - Google Patents
Ceramic and metallic coupleInfo
- Publication number
- JPH02171237A JPH02171237A JP32692888A JP32692888A JPH02171237A JP H02171237 A JPH02171237 A JP H02171237A JP 32692888 A JP32692888 A JP 32692888A JP 32692888 A JP32692888 A JP 32692888A JP H02171237 A JPH02171237 A JP H02171237A
- Authority
- JP
- Japan
- Prior art keywords
- ceramic
- intermediate member
- metal
- ceramic member
- fitting
- 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
- 239000000919 ceramic Substances 0.000 title claims abstract description 29
- 229910052751 metal Inorganic materials 0.000 claims description 20
- 239000002184 metal Substances 0.000 claims description 20
- 239000002905 metal composite material Substances 0.000 claims description 13
- 230000007423 decrease Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 9
- 238000005219 brazing Methods 0.000 abstract description 4
- 238000003466 welding Methods 0.000 abstract description 3
- 230000002093 peripheral effect Effects 0.000 abstract 2
- 238000000926 separation method Methods 0.000 abstract 1
- 238000005304 joining Methods 0.000 description 9
- 238000005452 bending Methods 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- 239000011295 pitch Substances 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 238000005336 cracking Methods 0.000 description 3
- 210000001503 joint Anatomy 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 229910052581 Si3N4 Inorganic materials 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000004881 precipitation hardening Methods 0.000 description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910001141 Ductile iron Inorganic materials 0.000 description 1
- 241001446276 Helia <angisperm> Species 0.000 description 1
- 229910001240 Maraging steel Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- QQHSIRTYSFLSRM-UHFFFAOYSA-N alumanylidynechromium Chemical compound [Al].[Cr] QQHSIRTYSFLSRM-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- VNTLIPZTSJSULJ-UHFFFAOYSA-N chromium molybdenum Chemical compound [Cr].[Mo] VNTLIPZTSJSULJ-UHFFFAOYSA-N 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- -1 sialon Chemical compound 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
Abstract
Description
【発明の詳細な説明】
［産業上の利用分野］
本発明はセラミック部材と金属部材とを中間部材を介し
て嵌合することよりなるセラミックス・金属結合体に関
するもので、特に熱膨張の異なる部材、例えば、セラミ
ック部材と金属部材との結合に好適な構造のセラミック
ス・金属結合体に関するものである。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a ceramic-metal composite formed by fitting a ceramic member and a metal member through an intermediate member, and particularly relates to a ceramic-metal composite body that is formed by fitting a ceramic member and a metal member through an intermediate member, and particularly relates to a ceramic-metal composite body that is formed by fitting a ceramic member and a metal member through an intermediate member. For example, the present invention relates to a ceramic-metal composite having a structure suitable for joining a ceramic member and a metal member.
［従来の技術］
従来、熱膨張率の相違する部材を突き合わせて接着する
ことにより結合体を得る方法としては、両者を直接圧接
して結合する方法や両者の界面に別体の中間層を設けて
接合する方法か知られている。例えば、実開閉５９−１
６０５３”１号公報においては、セラミックスと金属と
の接合構造として両者の界面にＷ材又はＭＯ材よりなる
クラツド材を介在させて接合する方法が開示されている
。[Prior Art] Conventionally, methods for obtaining a bonded body by butting and gluing members with different coefficients of thermal expansion include methods of directly pressing and bonding the two, and providing a separate intermediate layer at the interface between the two. There are known methods of joining. For example, actual opening/closing 59-1
6053'' No. 1 discloses a method of bonding a ceramic and a metal by interposing a cladding material made of a W material or an MO material at the interface between the two.
［発明が解決しようとする課題］
しかしながら、上述した従来方法では、熱膨張差により
結合界面に残留応力が生じ七分な結合強度が得られなか
った。[Problems to be Solved by the Invention] However, in the conventional method described above, residual stress was generated at the bonding interface due to the difference in thermal expansion, and a sufficient bonding strength could not be obtained.
また、中間層としてＷ材またはＭＯ材よりなるクラツド
材を使用した場合は、上述した直接に両者を加圧接合等
の方法で接合する場合と比較しである程゛度は残留応力
か除去されるものの、この中間層の目的か接合界面にお
ける残留応力の除去てはないため、接合界面における剥
離やセラミック部材の割れをなくすことばてきなかった
。In addition, when a clad material made of W material or MO material is used as the intermediate layer, the residual stress is removed to a certain extent compared to the case where the two are directly joined by a method such as pressure joining as described above. However, since the purpose of this intermediate layer is not to eliminate residual stress at the bonding interface, it has not been possible to eliminate peeling at the bonding interface or cracking of the ceramic member.
［課題を解決するための手段］
本発明の目的は上述した従来方法の不具合を解消して、
界面の剥離やセラミック部材の割れを有効に除去可能な
セラミックス・金属結合体を提供しようとするものであ
る。[Means for Solving the Problems] The purpose of the present invention is to solve the above-mentioned problems of the conventional method,
The present invention aims to provide a ceramic-metal composite that can effectively eliminate interface peeling and cracking of ceramic members.
そして、上記の［目的は、本発明によれば、セラミック
部材と金属部材とを中間部材を介して嵌合することによ
り構成したセラミックス・金属結合体であって、該中間
部材がハニカム構造であることを特徴とするセラミック
ス・金属結合体、により達成することかてきる。According to the present invention, there is provided a ceramic-metal composite body constructed by fitting a ceramic member and a metal member through an intermediate member, the intermediate member having a honeycomb structure. This can be achieved by using a ceramic-metal composite body characterized by the following.
また、このセラミックス・金属結合体においては、中間
部材の剛性な嵌合端に向って低くすることにより、残留
応力か残り易い部分程剛性を小さくでき、好ましい。In addition, in this ceramic-metal composite, it is preferable that the intermediate member is made lower toward the rigid fitting end, since the rigidity can be reduced in the portion where residual stress is more likely to remain.
ここでハニカム構造とは、はちの巣状の直線的な隔壁に
より構成されたものたけてはなく、平面または曲面の板
材より構成された構造をいうものである。The term "honeycomb structure" as used herein refers to a structure composed of planar or curved plates, rather than a straight honeycomb-like partition wall.
［作用］
本発明のセラミックス・金属結合体においてはセラミッ
ク部材と金属部材とを中間部材を介して嵌合することに
より構成している。従って、単なる突合せ結合と異なり
、セラミック部材と金属部材の接合面植を大きくでき、
接合強度を高めることかてきる。[Function] The ceramic-metal composite of the present invention is constructed by fitting a ceramic member and a metal member through an intermediate member. Therefore, unlike a simple butt joint, the joint surface of the ceramic member and the metal member can be increased,
It can increase the bonding strength.
さらに、中間部材をハニカム構造としてその剛性を低下
させたので接合時の接合温度から室温まての降温時に生
じるセラミック部材と金属部材との熱膨張差を吸収し、
セラミック部材中の嵌合端に発生する残留応力を除去す
るとともに、接着すべき部材間の接着性を悪化させるこ
ともない。Furthermore, since the intermediate member has a honeycomb structure to reduce its rigidity, it absorbs the difference in thermal expansion between the ceramic member and the metal member that occurs when the temperature drops from the joining temperature to room temperature.
This eliminates the residual stress generated at the fitting end of the ceramic member, and does not deteriorate the adhesion between the members to be bonded.
以上の結果、接着性を犠牲にすることなく界面の剥離や
セラミック部材の割れを除去することが可能となる。As a result of the above, it becomes possible to remove interfacial peeling and cracks in the ceramic member without sacrificing adhesiveness.
また、中間部材としてのハニカム構造において嵌合端に
向う程剛性を小さくすると、すなわち例えば円柱と環状
体間の嵌合の場合であれば、円柱の環状体の先端部へい
く程剛性を小さくすれば、残留応力が残りやすい部分程
剛性を小さくてきより好適である。In addition, in a honeycomb structure as an intermediate member, if the rigidity is decreased toward the fitting end, for example, in the case of fitting between a cylinder and an annular body, the rigidity can be decreased toward the tip of the annular body of the cylinder. For example, it is more preferable to reduce the rigidity of a portion where residual stress tends to remain.
なお、ハニカムの厚さとしては０．５ｍｍ以上あればよ
く、１．０ｍｍ以上あればより好ましい。The thickness of the honeycomb may be 0.5 mm or more, and more preferably 1.0 mm or more.
［実施例］
以下、本発明を図示の実施例に基づいてさらに詳細に説
明するが１本発明はこれらの実施例に限られるものでは
ない。[Examples] Hereinafter, the present invention will be described in more detail based on illustrated embodiments, but the present invention is not limited to these embodiments.
第１図は本発明の結合体の一実施例を示す断面図である
。この場合、先端部か円柱状のセラミック部材ｌと、セ
ラミック部材ｌの先端部をハニカム構造のＴｉ、Ａｉ等
からなる管状の中間部材３を介して外周より金属部材２
により嵌合し、各部材間をろう付、溶接等の方法により
一体に接着した例を示している。FIG. 1 is a sectional view showing an embodiment of the combined body of the present invention. In this case, the tip of the ceramic member l is cylindrical, and the tip of the ceramic member l is connected to the metal member 2 from the outer periphery via a tubular intermediate member 3 made of Ti, Ai, etc. with a honeycomb structure.
The figure shows an example in which the members are fitted together and bonded together by brazing, welding, or other methods.
この中間部材３は例えば第２図（ａ） （ｂ）に示すよ
うに、金属薄板７を格子状で且つ放射状にＭｌ立て、内
周側を円筒板５にて、外周側を円筒板６にて構成したも
のである。第３図及び第４図は中間部材３の他の実施例
を示しており、中間部材３を周方向に一部切断した部分
断面図である。第３図（ａ）〜（Ｃ）はそれぞれ嵌合底
８側から嵌合端４側へ剛性を等しくした構成であり、一
方、第４図（ａ）〜（Ｃ）はそれぞれ嵌合底８側から嵌
合端４側へ行くに従って低剛性となるように形成されて
いる構成例を示す。この構成は１例えば第４図（ａ）の
ように、嵌合底８から嵌合端４に近ずく程ハニカム構造
の格子間間隔を粗にする方法などにより作製することが
できる。このように構成することにより、４６６部にお
ける残留応力の影響をより効果的に緩和することかでき
る。また、第５図は中間部材３のさらに別の実施例を示
す斜視図で、一定間隔毎にで箱型状の凹凸をずらして設
けた形状のものを示す。For example, as shown in FIGS. 2(a) and 2(b), this intermediate member 3 consists of thin metal plates 7 arranged in a lattice pattern and arranged radially, with a cylindrical plate 5 on the inner periphery and a cylindrical plate 6 on the outer periphery. It is composed of 3 and 4 show other embodiments of the intermediate member 3, and are partial cross-sectional views of the intermediate member 3 partially cut in the circumferential direction. 3(a) to 3(C) each have a configuration in which the rigidity is equalized from the fitting bottom 8 side to the fitting end 4 side, while FIGS. An example of a configuration is shown in which the rigidity becomes lower as it goes from the side to the fitting end 4 side. This structure can be manufactured by, for example, a method in which the lattice spacing of the honeycomb structure is made coarser as it approaches the fitting end 4 from the fitting bottom 8, as shown in FIG. 4(a). With this configuration, the influence of residual stress at the 466 portion can be more effectively alleviated. FIG. 5 is a perspective view showing still another embodiment of the intermediate member 3, in which box-shaped unevenness is provided at regular intervals.
本発明に用いられるセラミック部材としては窒化珪素、
炭化珪素、サイアロン、ジルコニア、ムライト、アルミ
ナ、へりリア等か使用でき、また金属部材としては、炭
素鋼、ステンレス鋼、球状黒鉛鋳鉄、ニッケル・クロム
・そリブデン鋼、クロム・モリブデン鋼、アルミニウム
・クロム・モリブデン鋼、マルエージング鋼、析出硬化
型合金等が使用てきる。また、金属部材としてはその−
部あるいは全部に析出硬化処理、窒化処理または高周波
焼入れ処理等の硬化処理か行なわれていると好適である
。さらに、中間部材としてはステンレス鋼あるいは７ｉ
、 Ｎｉ、 Ｗ、 Ｎｂ、 Ｃｕ、 Ｔａ及びその合金
等が使用できる。The ceramic member used in the present invention includes silicon nitride,
Silicon carbide, sialon, zirconia, mullite, alumina, helia, etc. can be used, and metal parts include carbon steel, stainless steel, spheroidal graphite cast iron, nickel-chromium-solid steel, chromium-molybdenum steel, aluminum-chromium.・Molybdenum steel, maraging steel, precipitation hardening alloy, etc. can be used. In addition, as a metal member,
It is preferable that a hardening treatment such as a precipitation hardening treatment, a nitriding treatment, or an induction hardening treatment is performed on some or all of the parts. Furthermore, as the intermediate member, stainless steel or 7i
, Ni, W, Nb, Cu, Ta and their alloys can be used.
また、各部材間の接合方法としてはろう付け、拡散接合
、溶融接合などによる接合あるいはこれらの組合せによ
る接合を用いることかできる。Further, as a joining method between each member, joining by brazing, diffusion joining, fusion joining, etc., or joining by a combination of these can be used.
以下、具体的な実施結果を示す。Specific implementation results are shown below.
（実施例１）
第６図に示す先端部か直径２０量■φの外径を有する窒
化珪素からなるセラミック部材ｌの先端部外周を、厚さ
２ｍｍのＴｉ製中間部材３を介して炭素鋼（３４５Ｇ）
からなる金属部材２にて囲繞して嵌合し、銀ろうによる
ろう付により接合した。中間部材３の形状は第２図に示
すように、厚み０．２■のＴｉ板７により円筒板５にお
ける軸方向ピッチｔで放射状に円筒板６に取付けてなる
管状のハニカム構造体〔嵌合幅（第６図の文３）は３０
■〕をスポット溶接により作製し、その内面および外面
を厚さ０．２ＨのＴｉ製の円筒板５および円筒板６にて
ろう付して構成した。(Example 1) The outer periphery of the tip of a ceramic member l made of silicon nitride having an outer diameter of 20 mm in diameter as shown in FIG. (345G)
They were surrounded and fitted together with a metal member 2 consisting of the following, and joined by brazing with silver solder. As shown in FIG. 2, the shape of the intermediate member 3 is a tubular honeycomb structure [fitting The width (text 3 in Figure 6) is 30
(2) was manufactured by spot welding, and its inner and outer surfaces were brazed with Ti cylindrical plates 5 and 6 having a thickness of 0.2H.
このように構成したセラミックス・金属結合体において
、ピッチｔをすべて２■とした場合（本発明（１））と
、嵌合端４側の６■のピ・ンチｔを３１１１１とし、そ
れ以外のピッチｔを２ｍｍとした場合（本発明（２））
と、嵌合端４側の１２ｍ−のピッチｔを４ｍｍとし、そ
れ以外のピッチｔを２ｍｍとした場合（本発明（３））
と、ハニカム構造ではなく厚さ２■のＴｉ板で中間部材
を構成した場合（比較例）を準備し、第６図において文
、＝７０ ｍｍ、 ｌ ２＝４０１となるようにに’ｉ
Ｎした結合体を曲げ試験装置に組み付け、セラミック部
材ｌに対し荷重Ｐを鉛直方向にかけることにより各結合
体の曲げ強度試験を実施した。結果を第７図に示す。な
お、第７図に示す曲げ強度は、比較例の曲げ強度を基準
として示している。In the ceramic-metal composite body constructed in this way, when all the pitches t are 2■ (the present invention (1)), the pinch t of 6■ on the fitting end 4 side is 31111, and the other cases are as follows. When pitch t is 2 mm (present invention (2))
In the case where the pitch t of 12 m on the fitting end 4 side is 4 mm, and the other pitch t is 2 mm (present invention (3))
Then, we prepared a case (comparative example) in which the intermediate member was made of a Ti plate with a thickness of 2 mm instead of a honeycomb structure, and in Fig. 6, we prepared
The bonded bodies were assembled into a bending test device, and a bending strength test was conducted on each bonded body by applying a load P to the ceramic member 1 in the vertical direction. The results are shown in FIG. The bending strength shown in FIG. 7 is based on the bending strength of the comparative example.
第７図から明らかなように、本発明の結合体、特に嵌合
端に向って低剛性とした結合体は、比較例に比し高い曲
げ強度を有することがわかる。As is clear from FIG. 7, it can be seen that the combined body of the present invention, particularly the combined body with lower rigidity toward the fitting end, has higher bending strength than the comparative example.
［発明の効果］
以上説明した通り、本発明のセラミックス・金属結合体
は、セラミック部材と金属部材とをハニカム構造を形成
する中間部材を介して嵌合しているため、接合面積を大
きくてき、高い接合強度を有するとともに、接合時のセ
ラミック部材と金属部材との熱膨張差による残留応力を
除去でき、界面の剥離やセラミック部材の割れを防止す
ることかできる。従って、ガスタービン静翼接合部、ガ
スタービン燃焼器などのセラミックスと金属とからなる
結合体に好適に利用てきる。[Effects of the Invention] As explained above, in the ceramic-metal composite of the present invention, since the ceramic member and the metal member are fitted through the intermediate member forming a honeycomb structure, the bonding area can be increased. In addition to having high bonding strength, it is possible to remove residual stress due to the difference in thermal expansion between the ceramic member and the metal member during bonding, and it is possible to prevent peeling at the interface and cracking of the ceramic member. Therefore, it can be suitably used for joints made of ceramics and metal, such as gas turbine stationary blade joints and gas turbine combustors.
第１図は本発明の結合体の一実施例を示す断面図、第２
図（ａ）は中間部材の一例を概略的に示す説明図て、第
２図（ｂ）は第２図（ａ）のＡ−Ａ断面図である。３図
（ａ）〜（Ｃ）および第４図（ａ）〜（Ｃ）は中間部材
の他の例を示す部分断面図、第５図は中間部材のさらに
別の例を示す斜視図、第６図は結合体を曲げ強度試験に
適用した例を示す概略図、第７図は結合体の曲げ強度試
験結果を示すグラフである。
ｌ・・・セラミックス、２・・・金属、３・・・中間部
材、４・・・嵌合端、５・・・円筒板、６・・・円筒板
、７・・・金属薄板、８・・・嵌合底。FIG. 1 is a sectional view showing one embodiment of the combined body of the present invention, and FIG.
FIG. 2(a) is an explanatory diagram schematically showing an example of the intermediate member, and FIG. 2(b) is a sectional view taken along the line AA in FIG. 2(a). 3(a)-(C) and FIG. 4(a)-(C) are partial sectional views showing other examples of the intermediate member, FIG. 5 is a perspective view showing still another example of the intermediate member, and FIG. FIG. 6 is a schematic diagram showing an example in which the combined body is applied to a bending strength test, and FIG. 7 is a graph showing the results of the bending strength test of the combined body. l... Ceramics, 2... Metal, 3... Intermediate member, 4... Fitting end, 5... Cylindrical plate, 6... Cylindrical plate, 7... Metal thin plate, 8... ...Mating bottom.
Claims (2)
嵌合することにより構成したセラミックス・金属結合体
であって、該中間部材がハニカム構造であることを特徴
とするセラミックス・金属結合体。(1) A ceramic-metal composite body constructed by fitting a ceramic member and a metal member through an intermediate member, the intermediate member having a honeycomb structure.
項１記載のセラミックス・金属結合体。(2) The ceramic-metal composite according to claim 1, wherein the intermediate member has a rigidity that decreases toward the fitting end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63326928A JPH0628939B2 (en) | 1988-12-24 | 1988-12-24 | Ceramics / metal combination |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63326928A JPH0628939B2 (en) | 1988-12-24 | 1988-12-24 | Ceramics / metal combination |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH02171237A true JPH02171237A (en) | 1990-07-02 |
| JPH0628939B2 JPH0628939B2 (en) | 1994-04-20 |
Family
ID=18193330
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63326928A Expired - Fee Related JPH0628939B2 (en) | 1988-12-24 | 1988-12-24 | Ceramics / metal combination |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0628939B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3747590A1 (en) * | 2019-06-07 | 2020-12-09 | Commissariat à l'énergie atomique et aux énergies alternatives | Method for assembling a ceramic part with a metal part |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102991093B (en) * | 2012-12-28 | 2015-02-18 | 江阴东大新材料研究院 | Reaction hot pressing method for manufacturing honeycomb ceramic interlayer composite plate on surface of steel plate |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63231928A (en) * | 1987-03-20 | 1988-09-28 | 日本碍子株式会社 | Bonding body |
-
1988
- 1988-12-24 JP JP63326928A patent/JPH0628939B2/en not_active Expired - Fee Related
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63231928A (en) * | 1987-03-20 | 1988-09-28 | 日本碍子株式会社 | Bonding body |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3747590A1 (en) * | 2019-06-07 | 2020-12-09 | Commissariat à l'énergie atomique et aux énergies alternatives | Method for assembling a ceramic part with a metal part |
| FR3096915A1 (en) * | 2019-06-07 | 2020-12-11 | Commissariat A L'energie Atomique Et Aux Energies Alternatives | Assembly process of a ceramic part with a metal part |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0628939B2 (en) | 1994-04-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5161908A (en) | Joined structure comprising members of different coefficients of thermal expansion and joining method thereof | |
| JPS62104696A (en) | Metallic ceramics junction body and metallic ceramics coupling body formed by using said body | |
| JPH0516382B2 (en) | ||
| JPH0444631B2 (en) | ||
| US4865896A (en) | Composite joined bodies including an intermediate member having a honeycomb structure | |
| JPH0454825B2 (en) | ||
| US4959258A (en) | Joined metal-ceramic assembly method of preparing the same | |
| US5076484A (en) | Joining structure of a turbine rotor | |
| JPH01240714A (en) | Metallic carrier body | |
| JPH02171237A (en) | Ceramic and metallic couple | |
| JPH0339991B2 (en) | ||
| JP2537199Y2 (en) | Exhaust gas purification catalyst carrier | |
| JPH063171B2 (en) | Ceramic-Metal Friction Welding Body and Ceramic Casting Piston Composed of It | |
| JPH01219072A (en) | Metal-ceramic joined body | |
| JPH0976079A (en) | Method for joining low alloy steel shaft or steel shaft with rotary body made of titanium aluminide | |
| JP3056747B2 (en) | Exhaust gas purification device | |
| JPH02126942A (en) | Metallic carrier base for carrying exhaust gas purifying catalyst | |
| JP2003170277A (en) | Connected member composed of both heat-resistant metallic member and complex member and their connecting method | |
| JP2639993B2 (en) | Manufacturing method of metal carrier | |
| JPS6247113B2 (en) | ||
| JPH01282167A (en) | Joined body of members different in coefficient of thermal expansion | |
| JPS62159707A (en) | Rocker arm | |
| JPH0234269A (en) | Ceramic cast-in piston and production thereof | |
| JPH0448754B2 (en) | ||
| JPS63235068A (en) | Jig for brazing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |