JPH02273545A - Thermal fatigue-resistant metal support for automotive catalyst and its preparation - Google Patents

Thermal fatigue-resistant metal support for automotive catalyst and its preparation

Info

Publication number
JPH02273545A
JPH02273545A JP1093043A JP9304389A JPH02273545A JP H02273545 A JPH02273545 A JP H02273545A JP 1093043 A JP1093043 A JP 1093043A JP 9304389 A JP9304389 A JP 9304389A JP H02273545 A JPH02273545 A JP H02273545A
Authority
JP
Japan
Prior art keywords
foil
metal
corrugated
thermal fatigue
honeycomb
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
Application number
JP1093043A
Other languages
Japanese (ja)
Other versions
JPH0611406B2 (en
Inventor
Masayuki Tento
雅之 天藤
Mikio Yamanaka
幹雄 山中
Shigeru Ogawa
茂 小川
Kazuo Nakamura
和男 中村
Satoru Matoba
哲 的場
Yoshio Nishizawa
西沢 良雄
Akihiko Kasahara
笠原 昭彦
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.)
Nippon Steel Corp
Nippon Kinzoku Co Ltd
Original Assignee
Nippon Steel Corp
Nippon Kinzoku 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 Nippon Steel Corp, Nippon Kinzoku Co Ltd filed Critical Nippon Steel Corp
Priority to JP1093043A priority Critical patent/JPH0611406B2/en
Publication of JPH02273545A publication Critical patent/JPH02273545A/en
Publication of JPH0611406B2 publication Critical patent/JPH0611406B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/24Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
    • F01N3/28Construction of catalytic reactors
    • F01N3/2803Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
    • F01N3/2807Metal other than sintered metal
    • F01N3/281Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2330/00Structure of catalyst support or particle filter
    • F01N2330/02Metallic plates or honeycombs, e.g. superposed or rolled-up corrugated or otherwise deformed sheet metal
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2330/00Structure of catalyst support or particle filter
    • F01N2330/30Honeycomb supports characterised by their structural details
    • F01N2330/32Honeycomb supports characterised by their structural details characterised by the shape, form or number of corrugations of plates, sheets or foils

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Catalysts (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Exhaust Gas Treatment By Means Of Catalyst (AREA)

Abstract

PURPOSE:To absorb thermal stress caused by temperature difference in a honeycomb part and to obtain a catalyst which is not broken by thermal fatigue by shaping a wavy foil to be a wavy shape having bending parts. CONSTITUTION:A bending part B is formed between joining points A and C of platy foils 1, 3 and a wavy foil 2. A bending part D bent in the opposite direction of the part B is formed between the joining point C and neighboring joining point E and thus a nonsymmetrical trapezoidal shape is formed by repeating formation of bending parts in this way. The length A-B-C of the wavy foil is made sufficiently long against the distance between the joining points A, C. With this structure, a catalyst having enough durability to high temperature and high speed exhaust gas flow and high resistance to thermal fatigue even when temperature difference is caused between a honeycomb part and an outer cylinder is obtained.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は自動車触媒用の金属基体に関する。[Detailed description of the invention] [Industrial application field] The present invention relates to metal substrates for automotive catalysts.

[従来の技術] 自動車の排気ガス規制が実施されて10年以上経過する
が、現在の排気ガス対策はエンジンの改良と触媒による
排気ガスの浄化によって行われている。排気ガス浄化用
の触媒はコージライト等のセラミックハニカムの上にp
tなどの貴金属触媒を担持したγ−アルミナ粉を担持す
る構造のものが主流を占めている。さりながらこれらの
セラミックハニカムは排気抵抗がやや高く、またハニカ
ムの破壊を防止するために外筒との間に挿入する緩衝用
のステンレスメツシュの耐熱性の制約などから、その使
用温度が低めに制限される等の欠点があった。
[Prior Art] More than 10 years have passed since automobile exhaust gas regulations were implemented, and current exhaust gas countermeasures are taken by improving engines and purifying exhaust gas using catalysts. The catalyst for exhaust gas purification is placed on a ceramic honeycomb such as cordierite.
The mainstream is one having a structure in which γ-alumina powder supporting a noble metal catalyst such as T is supported. However, these ceramic honeycombs have somewhat high exhaust resistance, and the temperature at which they can be used is rather low due to the heat resistance of the buffer stainless steel mesh that is inserted between the honeycomb and the outer cylinder to prevent it from breaking. There were drawbacks such as restrictions.

これらの欠点を改善するものとして近年ステンレス箔か
らなる金属担体が注目されている。これら金属担体は当
然反応中の高温かつ高速の排気ガスに耐える耐熱性と激
しい加熱・冷却に耐える耐熱疲労性が要求される。第4
図に示すように一般に金属担体は厚み50ua+前後の
ステンレス平箔lOと波へり加工したステンレス波箔9
とを重ね”【゛円筒jfツまI、−は楕円杆状に削き込
みハ、″:カム体8とし、4−tを耐熱ステンレス製の
外筒7に挿久し下平箔−波箔〜4筒間を相Tiにろう付
しりやド(抗溶接等により接合−4゛る。
In recent years, metal carriers made of stainless steel foil have attracted attention as a means of improving these drawbacks. These metal carriers are naturally required to have heat resistance to withstand high temperature and high velocity exhaust gas during the reaction and thermal fatigue resistance to withstand intense heating and cooling. Fourth
As shown in the figure, the metal carrier is generally a stainless steel flat foil 10 with a thickness of about 50 ua+ and a stainless steel corrugated foil 9 with a corrugated edge.
``Cylinder jf knob I, - is cut into an oval rod shape ``: cam body 8, 4-t is inserted into the heat-resistant stainless steel outer cylinder 7, and the lower flat foil - corrugated foil -4 cylinders are joined to the phase Ti by brazing, doweling, etc.

τ針属世体が高温・高速の排気ガスに耐えるために冒ま
、耐酸化性の良好なステンレス箔を用い平箔−・−・波
箔−・外筒相〃の接合面積を増すことがllr効である
が、−モ゛、t1だ0では激しい加熱・冷却に対しては
耐えら木lない。すなわち自動巾丁ンジンに装着さ21
k上属4f1体ではJ゛ンジン始動ら走行開始時Lmハ
ーニfJム部が外筒に先行して加熱され、また長い下り
坂では長時間エンジンブレーキの状態が特記1;1、・
2.二の間燃料の供給を力・/1・するタイプのもので
はハニカムか外筒に先行して冷却さ第11、ハ、−。
In order to withstand high temperature and high speed exhaust gas, stainless steel foil with good oxidation resistance is used to increase the bonding area of flat foil, corrugated foil, and outer cylinder phase. However, when the temperature is -Mo, t1 is 0, it cannot withstand intense heating and cooling. In other words, it is attached to an automatic kitchen knife 21
In the 4F1 model of the K upper class, when the J engine starts and the running starts, the Lm honeycomb fJ part heats up before the outer cylinder, and it is noted that the engine brake is on for a long time on long downhill slopes.
2. In the case of the type that supplies fuel between two times, the honeycomb or outer cylinder is cooled in advance.

カム内の内側と外側あるいは夕(筒とハニカム部の間V
大きな温度差か生じる。しかも加熱時と冷却では、温度
差の111負か入れ変わるためハニカムはや・)筒に近
い部分で熱疲労破壊を生じ、υ[気ガスの■圧によりハ
ニカムが風)プ)向に飛び出1゛等の不具合が/ノもじ
る。
Inside and outside of the cam (V between the cylinder and the honeycomb part)
A large temperature difference will occur. Moreover, due to the temperature difference of 111 during heating and cooling, thermal fatigue failure occurs in the part of the honeycomb near the cylinder, and the honeycomb flies out in the wind direction due to the pressure of air gas. Problems such as ゛ occur.

このような熱線′カ破壊を防止する光性技術と1.2て
7金属箔同志あるいは外筒との接僑を部分的1、゛行う
ことを、特開昭62−830’14、西独特、XT公開
会報3312944に開示されているか、製造F桿が複
雑1になり′:〕ストもト昇する一方、効果%〉−7−
分と(1ま8“j′;ない。
Japanese Patent Application Laid-Open No. 1983-830'14, a patent application published in 1983-830'14, describes optical technology to prevent such heat ray damage and 1.2 to partially contact the metal foils or the outer cylinder. , as disclosed in XT Public Bulletin No. 3312944, the production F rod becomes complicated 1':] While the strike also increases, the effect %〉-7-
Minute (1 or 8 "j'; no.

[発明が解決しようどする課題] 本発明は−に述しまた従来技術の欠点に鑑み”〔なτ゛
(才またもので、高温・高速の排気ガス流にも耐1式。
[Problems to be Solved by the Invention] The present invention has been proposed in view of the drawbacks of the prior art as described above.

かつ急速な加熱・冷却にも耐オる耐熱疲労性を41する
金属基体を提伊するものである。
The present invention also proposes a metal substrate that has a thermal fatigue resistance of 41 and is resistant to rapid heating and cooling.

「課題を解決するためのt段〕 この1]的を達成するため本発明はハニカム内の内側と
りl側、およびハニーカム部と外筒との間(6テ温度差
が生じた場合でも熱疲労を生じにくい波箔の形状を発明
したもので、温度差によ・・)て住1、・六−熱応力を
波箔の形状によって緩和することができる。すなわち平
らな金属箔(以下Y箔と称する)と波型加工した金属箔
(以下波箔と称1−る)4・市ね1′へき込んて゛なる
仝属ハーゴ、カムどこれらを囲む金属外筒からなる自動
中触媒用金属基体におい(、・P−箔との接庁点間に交
η虹曲げ))向の異なる屈曲部を配置する波形状(以下
)1対称台形と称する)ン打1−る葭記1波箔と15.
て、ガス流に直角方向に′牛1.た熱歪をこの波箔に形
成した屈曲点の角度の′1化に−よって吸収さセること
かできる。千1ノて核;)点ならびに゛P箔1ζノ1し
る熱応力を低減させ、破l輿を防1)−することかii
J能となった。
"T step to solve the problem" In order to achieve this goal (1), the present invention is designed to prevent thermal fatigue even when a temperature difference of 6 degrees occurs between the inner side of the honeycomb and between the honeycomb part and the outer cylinder. The shape of the corrugated foil was invented, and the shape of the corrugated foil made it possible to alleviate the thermal stress caused by temperature differences (...) by the shape of the corrugated foil. A metal base for automatic catalysts consisting of a corrugated metal foil (hereinafter referred to as corrugated foil) (hereinafter referred to as corrugated foil) 4, a metal outer cylinder that surrounds a metal outer tube, a cam, etc. A wave shape (hereinafter referred to as a 1-symmetrical trapezoid) in which bent parts with different directions are arranged (cross η rainbow bending between the contact points with the P-foil) 15.
1. In the direction perpendicular to the gas flow. The thermal strain caused by this can be absorbed by making the angle of the bending point formed in the corrugated foil narrower. It is possible to reduce the thermal stress at the 1,1 point core;
It became J-Noh.

;\1)k:木9明名らは、50%以」−の圧F率で冷
間J1−延l、2て作fyJlッだ金属箔を波付加工す
ること、あるいは箔の成形方向と逆り向に 1〜10k
g/wlI[12の張)Jを1]1j犬ながら波(・t
 JJln−Ixすることにより、1記のJ1χ、を称
台形の形状を4rする波箔を容易に製造することができ
ることも砧出し、1.記の自動中触媒用仝・属担体の1
1業的生産がlIT能どなった。
\1) k:K9 Akina et al. Cold-rolled and 2-rolled metal foil at a pressure rate of 50% or more, or corrugated the metal foil, or in the forming direction of the foil. 1-10k in the opposite direction
g/wlI [12 no Zhang) J 1] 1j dog wave (・t
It is also clear that by using JJln-Ix, it is possible to easily manufacture corrugated foil in which J1χ in 1 has a trapezoidal shape of 4r. Part 1 of the above-mentioned support for automatic catalysts
Industrial production has become less efficient.

1イ1川] 次に本発明の詳細な説明rる。第1図は本発明の非吋称
台形の波形状を11“する波箔と平箔を重ねた断面?示
すものである。一般に金属基体中を流1″L?1榎気カ
スによってハニカム部か加熱・冷JJI 、’≦iする
場合、ガス流中東部と外側、特に外筒部イ・t iUr
での温度差か大きくなり、排気ガス流に対して面角方向
、つまり第1図中の矢印の方向に熱歪か牛し・る。本発
明ではこの熱歪を吸収するために、第1図に示す如くモ
箔1.3と波箔2の接り点AI)よびCの間に屈曲点B
を形成し、そしてその晴りの接合点CおよびEの間には
BとはJ5i対ツノ゛向に′曲げた屈曲点りを形成させ
、こオ′1を繰り返す訓対称台形波形状とした。上、紀
屈曲点での角度の変化、つまり波形状の変化により矢印
の方向に生1.゛5る熱歪を吸収することができる。
1] Next, a detailed explanation of the present invention will be given. Fig. 1 shows a cross-section of a 11" corrugated foil and a flat foil stacked together to form an asymmetrical trapezoidal wave shape of the present invention. In general, a flow of 1"L in a metal substrate is shown. 1. If the honeycomb part is heated or cooled due to air scum, '≦i, the middle eastern part of the gas flow and the outside, especially the outer cylinder part.
The temperature difference at the exhaust gas flow increases, causing thermal strain in the plane angle direction with respect to the exhaust gas flow, that is, in the direction of the arrow in Figure 1. In the present invention, in order to absorb this thermal strain, as shown in FIG.
, and between the clear junction points C and E, a bend point bent in the direction of the J5i horn is formed, and a symmetrical trapezoidal wave shape is formed by repeating this process. . Above, due to the change in the angle at the bend point, that is, the change in the wave shape, a wave is generated in the direction of the arrow 1. It is possible to absorb thermal strain of 5.

熱歪を効果的に吸収し、耐熱疲労性を確保J゛るために
は、接合点Aと接合点Co1中νに対l7.2て、波箔
の長さABCが1分長い必要がある。実際j(はABC
の長さがACの長ざよりも銚以上、−4”’ 1.”<
わち1805倍以)−長いことが望ましい、ま1.−・
(・″箔1と波箔BCとの角度F、および’I’ 7i
3と波71I) h゛との角度Gは5′以上どすること
か9まし7い。−F記角度か小さいと熱53によって波
形状か変化し1′、:場合、波箔が平箔と接触し十分な
耐熱疲労性を確保できなくなる。また波の頂点と頂点と
の間において、前記BとDのごとく交互に曲げ方向を変
えるのは、波箔と平箔に囲まれたガスが流れる空間の形
状を一様にし、ガス流を均一にするためである。
In order to effectively absorb thermal strain and ensure thermal fatigue resistance, the length ABC of the corrugated foil needs to be 1 minute longer than ν between the junction A and the junction Co1, with respect to l7.2. . Actually j (is ABC
The length of the AC is longer than the length of the AC, -4"'1."<
(i.e., 1805 times or more) - preferably longer, or 1. −・
(・Angle F between foil 1 and corrugated foil BC, and 'I' 7i
3 and wave 71I) The angle G between h゛ should be 5' or more. -F If the angle is small, the wave shape will change due to the heat 53. In the case 1', the corrugated foil will come into contact with the flat foil, making it impossible to ensure sufficient thermal fatigue resistance. Also, between the crests of the waves, the bending direction is alternately changed as shown in B and D above to make the shape of the space surrounded by the corrugated foil and the flat foil into which the gas flows uniform, and to make the gas flow uniform. This is for the purpose of

平箔と波箔の接合には、ろう付け、抵抗溶接、レーザー
溶接、電子ビーム溶接、アーク溶接、拡散接合等が行わ
れるが、接合面積は小さい方が望ましい。ろう材やアー
ク等が拡がり接合面積が大きくなると波箔の動きを束縛
し、熱歪を吸収する効果が減少する。また本発明におい
て、平箔と波箔の全ての接点において接合させる必要は
ない。
Brazing, resistance welding, laser welding, electron beam welding, arc welding, diffusion bonding, etc. are used to join flat foil and corrugated foil, but it is desirable that the joining area be small. When the brazing filler metal, arc, etc. spread and the bonding area becomes larger, the movement of the corrugated foil is restricted and the effect of absorbing thermal strain is reduced. Further, in the present invention, it is not necessary to join the flat foil and the corrugated foil at all contact points.

次に耐熱疲労性を有する上述のような非対称台形波型を
加工するには、波型ロールを用いるのが最も一般的であ
る。ここでまず第1に50%以上の圧下率にて冷間圧延
して作製した金属箔5を使用すると、第2図に示す如く
台形波型ロール4によって非対称台形波形状に加工する
ことが可能である。つまり冷間圧延を行うことにより金
属箔を加工硬化させ、波付は加工直後のスプリング・バ
ック現象により金属箔はロールと同じ台形波型には加工
されず、第1図に示す非対称台形の波形状に加工される
。これにより従来の波型加工用の装置がそのまま使用で
きるため好都合である。第2は上記の如く硬質化されて
いない金属箔に波付加工を行う場合、加工される金属箔
に張力を1−10kg/lllm2付加することによっ
ても台形波型ロールで非対称台形波形状に加工すること
が可能である。これは第3図に示すように矢印の方向の
張力により波の前後で加工条件がことなり、より張力を
付加されながら加工される波の後部の方がより大きく曲
げられ、結果的に非対称台形波形状となる。上記2つの
いずれかの方法により台形波型ロールで非対称台形波形
状に加工することができ、耐熱疲労性を有する金属担体
用波箔を容易に製造することが可能である。上記2つの
方法を用いない場合は1例えば第5図に示す如くロール
と同じ対称な台形波型となり、耐熱疲労性を発揮しない
Next, in order to process the above-mentioned asymmetric trapezoidal corrugation having heat fatigue resistance, it is most common to use a corrugation roll. First of all, if a metal foil 5 produced by cold rolling is used at a reduction rate of 50% or more, it can be processed into an asymmetrical trapezoidal wave shape using a trapezoidal wave roll 4 as shown in FIG. It is. In other words, the metal foil is work-hardened by cold rolling, and due to the spring-back phenomenon immediately after the corrugation, the metal foil is not processed into the same trapezoidal wave shape as the roll, and the asymmetrical trapezoidal wave shape shown in Figure 1. Processed into shape. This is advantageous because conventional corrugation processing equipment can be used as is. Second, when corrugating metal foil that has not been hardened as described above, applying tension of 1-10 kg/llm2 to the metal foil to be processed can also process it into an asymmetrical trapezoidal wave shape using a trapezoidal wave roll. It is possible to do so. This is because, as shown in Figure 3, the processing conditions are different at the front and back of the wave due to the tension in the direction of the arrow, and the rear part of the wave that is processed under more tension is bent more, resulting in an asymmetrical trapezoid shape. It becomes a wave shape. By using either of the above two methods, it is possible to process the foil into an asymmetrical trapezoidal wave shape using a trapezoidal wave roll, and it is possible to easily produce a corrugated foil for a metal carrier having thermal fatigue resistance. If the above two methods are not used, the material will have the same symmetrical trapezoidal wave shape as the roll, as shown in FIG. 5, for example, and will not exhibit thermal fatigue resistance.

[実施例] 実施例−1 204kCr−5!kA4で0.4a+−厚さ、100
m+−幅のステンレス鋼板を厚さ50μ履まで冷間圧延
を施し、第2図に示す台形波型ロールで波付加工を行っ
た。この波箔と波付加工を行わなかった同材質の平箔と
を重ね、36巻きしてハニカムを構成させ、さらにその
外側に内径100+sm 、厚さ1.5gIm 、長さ
lOt)amのフェライト系ステンレス外筒で囲んだ。
[Example] Example-1 204kCr-5! kA4 0.4a+-thickness, 100
A stainless steel plate having a width of m+- was cold rolled to a thickness of 50 μm, and corrugated using a trapezoidal corrugated roll shown in FIG. This corrugated foil and a flat foil made of the same material that was not corrugated were layered and wound 36 times to form a honeycomb, and then on the outside was a ferritic foil with an inner diameter of 100+sm, a thickness of 1.5gIm, and a length of lOt)am. Surrounded by a stainless steel outer cylinder.

第1図は上記の如く作製した金属担体の平箔と波箔を重
ねた形態を示す、本発明のひとつの実施態様である。
FIG. 1 shows one embodiment of the present invention, showing a configuration in which a flat foil and a corrugated foil of the metal carrier produced as described above are stacked.

波型形状は非対称台形を示し、FおよびGの角度は10
°、ABCおよびCDHの長さはACおよびCEの長さ
に対していずれも1.1倍でありた。平箔と波箔との接
合およびハニカム部と外筒との接合は、Ni基ろうによ
るろう付けを行った。また比較例として、同じ材質、サ
イズの金属箔を焼鈍し、軟質化させたものを同じ台形波
型ロールで波付加工を行った。その後前記と同じ方法で
金属担体を作製した。この比較例の平箔と波箔を重ねた
形態を示したのが第5図である。
The wave shape shows an asymmetric trapezoid, and the angles of F and G are 10
°, the lengths of ABC and CDH were all 1.1 times the lengths of AC and CE. The flat foil and the corrugated foil were joined together, and the honeycomb part and the outer cylinder were joined together by brazing using Ni-based brazing. As a comparative example, a metal foil of the same material and size was annealed and softened, and then corrugated using the same trapezoidal corrugated roll. Thereafter, a metal carrier was produced in the same manner as above. FIG. 5 shows a configuration in which flat foil and corrugated foil of this comparative example are stacked.

上記の2種の金属担体に白金触媒を担持させたγ−アル
ミナ粉を焼き付けたうえ、排気N2000ccのエンジ
ンに搭載し、ベンチテストにより800℃以上で1分、
150℃以下で1分、合計lサイクル15分の冷熱試験
を繰り返した。
After baking the γ-alumina powder with platinum catalyst supported on the above two types of metal carriers, it was installed in an engine with an exhaust N2000cc, and a bench test was conducted at 800℃ or higher for 1 minute.
The thermal test was repeated for 1 minute at 150° C. or lower for a total of 1 cycle of 15 minutes.

その結果、比較例は100サイクル後に金属ハニカム部
の径が釣軸I収縮し、最外周から1〜3層目のいずれか
のハニカムが全周にわたって破断し、それより内周のハ
ニカムが排気ガスの風下側に約2(1wm飛び出してい
た。一方、本発明(第1図)のものは冷熱1200サイ
クル後も何ら異常は認められなかった。
As a result, in the comparative example, after 100 cycles, the diameter of the metal honeycomb part contracted by the angle I, one of the first to third layer honeycombs from the outermost periphery was broken over the entire circumference, and the honeycombs on the inner periphery were broken due to exhaust gas. On the other hand, in the case of the present invention (Fig. 1), no abnormality was observed even after 1200 cycles of heating and cooling.

実施例−2 実施例−1と同じ材質、サイズの金属箔を焼鈍し、軟質
化させたものに、3kg/1trta2の張力を付加さ
せて上記と同じ台形波型ロールで波付加工を行った。波
付加工の形態を示したのが第3図である。このように作
製した波箔と平箔から実施例−!と同じ方法で金属担体
を構成した。ただし抵抗溶接により平箔と波箔およびハ
ニカム部と外筒の接へ・・・ν行った。その上jo二自
白金触媒担持さゼたγ−アルミナ粉を焼きイζ」けた。
Example-2 A metal foil made of the same material and size as in Example-1 was annealed and softened, and a tension of 3 kg/1 trta2 was added to it, and corrugated processing was performed using the same trapezoidal corrugated roll as above. . FIG. 3 shows the form of corrugated processing. Examples from the corrugated foil and flat foil produced in this way! The metal support was constructed in the same manner as described above. However, resistance welding was used to connect the flat foil to the corrugated foil and the honeycomb part to the outer cylinder. Furthermore, the γ-alumina powder supported on the platinum catalyst was baked.

そして排気12000ccのエンジンにIみ載しベンチ
テストにより8(10℃以Vで1分、150℃以ドで1
分、合シ11サイクル■5分の冷熱試験を実施した。
Then, I was installed on an engine with an exhaust of 12,000 cc, and a bench test showed 8 (1 minute at V above 10 degrees Celsius, 1 at V above 150 degrees Celsius).
A thermal test was conducted for 5 minutes and 11 cycles.

千の結果、]−記担体は冷熱1200サイクル後も何ら
異常は認めらオ]、なかった。
As a result, no abnormality was observed in the carrier even after 1200 cycles of cooling and heating.

[発明の効果] 以l−説明したように本発明においては、波箔を屈曲部
を4Tする波形状(非対称台形波)にすることに:より
、ハニカム部の温度差から発生1また熱歪を吸収するこ
とかでき、熱疲労による破壊を生じさセない自動jtJ
触媒用金属担体が実現した。
[Effects of the Invention] As explained below, in the present invention, the corrugated foil is made into a wave shape (asymmetrical trapezoidal wave) with a bent portion of 4T. automatic jtj that can absorb heat and not cause damage due to thermal fatigue.
A metal carrier for catalysts has been realized.

4 、 図面ノ@ Il、 fax説明第1図は本発明
により波箔と平箔を重ねた断面を小すものである。第2
図は冷間圧延を施した金属箔を用い°C非対称台形の波
形状の加工している状況を示す。第3図は金属箔に張力
を付加させて非村称台形の波形状に加工している状況を
ボす。
4. Drawings @ Il, fax Explanation Fig. 1 shows a cross-section of a corrugated foil and a flat foil overlapped according to the present invention. Second
The figure shows a situation in which cold-rolled metal foil is processed into a °C asymmetric trapezoidal wave shape. Figure 3 shows the situation in which tension is applied to the metal foil and it is processed into a non-symmetrical trapezoidal wave shape.

1g4図は一般的な金属担体のMI#造を示す。第5図
は従来からの波形状の波箔ど平箔?屯ねた断面を示′1
−0 1.3.1111. 1+、  +a・=r箔、2.9
、l 2 ・= trli箔、4・・・台形波望V1−
ル、5・・・加工硬化し/、二金属箔、6・・・加]、
硬化1ノでいない金属箔、7・・・外筒78・・・ハニ
カム部、A、C,E・・・平箔と波箔の接合点、B、D
・・・屈曲部、E、F・・・接合部に、h ciろ゛(
′−箔と波箔の接触角度。
Figure 1g4 shows the MI# structure of a general metal support. Figure 5 shows the conventional wave-shaped wavy foil Doheihaku? Showing the vertical cross section'1
-0 1.3.1111. 1+, +a・=r foil, 2.9
, l 2 ・= trli foil, 4... trapezoidal waveform V1-
Le, 5... work hardening/, bimetallic foil, 6... addition],
Metal foil that has not been cured 1, 7... Outer cylinder 78... Honeycomb part, A, C, E... Junction point of flat foil and corrugated foil, B, D
... bending part, E, F ... joint part, hciro (
′−Contact angle between foil and corrugated foil.

Claims (1)

【特許請求の範囲】 1、平らな金属箔(平箔)と波型加工した金属箔(波箔
)を重ねて巻き込んでなる金属ハニカムとこれらを囲む
金属外筒からなる自動車触媒用金属基体において、波箔
の波の頂点と頂点との間において交互に曲げ方向が異な
る屈曲部を設けることを特徴とする自動車触媒金属担体
。 2、50%以上冷間圧延して作製した金属箔を波付加工
して波箔を製造することを特徴とする請求項1記載の自
動車触媒用金属担体の製造方法。 3、金属箔を波型ロールにて波箔を製造する際、金属箔
にロール成形方向と逆方向に1〜10kg/mm^2の
張力を加えることを特徴とする請求項1記載の自動車触
媒用金属担体の製造方法。
[Scope of Claims] 1. In a metal substrate for an autocatalyst consisting of a metal honeycomb formed by overlapping and rolling together a flat metal foil (flat foil) and a corrugated metal foil (corrugated foil) and a metal outer cylinder surrounding them. An automobile catalyst metal carrier characterized in that bent portions having different bending directions are provided alternately between the crests of the waves of the corrugated foil. 2. The method for producing a metal carrier for an automobile catalyst according to claim 1, wherein the corrugated foil is produced by corrugating a metal foil produced by cold rolling 50% or more. 3. The autocatalyst according to claim 1, characterized in that when the corrugated foil is produced using a corrugated roll, a tension of 1 to 10 kg/mm^2 is applied to the metal foil in a direction opposite to the roll forming direction. Method for producing metal carrier for use.
JP1093043A 1989-04-14 1989-04-14 Metal support for automobile catalyst having heat fatigue resistance and method for producing the same Expired - Fee Related JPH0611406B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1093043A JPH0611406B2 (en) 1989-04-14 1989-04-14 Metal support for automobile catalyst having heat fatigue resistance and method for producing the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1093043A JPH0611406B2 (en) 1989-04-14 1989-04-14 Metal support for automobile catalyst having heat fatigue resistance and method for producing the same

Publications (2)

Publication Number Publication Date
JPH02273545A true JPH02273545A (en) 1990-11-08
JPH0611406B2 JPH0611406B2 (en) 1994-02-16

Family

ID=14071478

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1093043A Expired - Fee Related JPH0611406B2 (en) 1989-04-14 1989-04-14 Metal support for automobile catalyst having heat fatigue resistance and method for producing the same

Country Status (1)

Country Link
JP (1) JPH0611406B2 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63104653A (en) * 1986-10-22 1988-05-10 Calsonic Corp Metal honeycomb carrier
JPS63299875A (en) * 1987-05-29 1988-12-07 Aichi Steel Works Ltd Method for joining metal structural body

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63104653A (en) * 1986-10-22 1988-05-10 Calsonic Corp Metal honeycomb carrier
JPS63299875A (en) * 1987-05-29 1988-12-07 Aichi Steel Works Ltd Method for joining metal structural body

Also Published As

Publication number Publication date
JPH0611406B2 (en) 1994-02-16

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