JPH02102744A - Metallic base body for automobile catalyst having resistance to thermal fatigue - Google Patents
Metallic base body for automobile catalyst having resistance to thermal fatigueInfo
- Publication number
- JPH02102744A JPH02102744A JP63255003A JP25500388A JPH02102744A JP H02102744 A JPH02102744 A JP H02102744A JP 63255003 A JP63255003 A JP 63255003A JP 25500388 A JP25500388 A JP 25500388A JP H02102744 A JPH02102744 A JP H02102744A
- Authority
- JP
- Japan
- Prior art keywords
- honeycomb
- outer cylinder
- metal
- joined
- foil
- 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
- 239000003054 catalyst Substances 0.000 title abstract description 10
- 239000011888 foil Substances 0.000 claims abstract description 48
- 229910052751 metal Inorganic materials 0.000 claims description 35
- 239000002184 metal Substances 0.000 claims description 35
- 238000005304 joining Methods 0.000 claims description 10
- 239000000758 substrate Substances 0.000 claims description 6
- 238000005096 rolling process Methods 0.000 claims description 5
- 238000004804 winding Methods 0.000 abstract 2
- 241000264877 Hippospongia communis Species 0.000 description 78
- 239000007789 gas Substances 0.000 description 12
- 229910001220 stainless steel Inorganic materials 0.000 description 11
- 239000010935 stainless steel Substances 0.000 description 10
- 238000005219 brazing Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- 238000003466 welding Methods 0.000 description 6
- 238000001816 cooling Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 239000000969 carrier Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 230000005856 abnormality Effects 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 208000025599 Heat Stress disease Diseases 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 238000010420 art technique Methods 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052878 cordierite Inorganic materials 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910000510 noble metal Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust 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
- F01N3/24—Exhaust 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
- F01N3/28—Construction of catalytic reactors
- F01N3/2839—Arrangements for mounting catalyst support in housing, e.g. with means for compensating thermal expansion or vibration
- F01N3/2842—Arrangements for mounting catalyst support in housing, e.g. with means for compensating thermal expansion or vibration specially adapted for monolithic supports, e.g. of honeycomb type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust 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
- F01N3/24—Exhaust 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
- F01N3/28—Construction of catalytic reactors
- F01N3/2803—Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
- F01N3/2807—Metal other than sintered metal
- F01N3/281—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A50/00—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE in human health protection, e.g. against extreme weather
- Y02A50/20—Air quality improvement or preservation, e.g. vehicle emission control or emission reduction by using catalytic converters
Abstract
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ItlJ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ェライト等のセラミックハニカム
の上にpt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
こわ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
、その使用温度が低くめに制限される等の欠点があった
。[Prior Art] More than 10 years have passed since the automobile exhaust gas regulation ItlJ was implemented, and current exhaust gas countermeasures are taken by improving engines and purifying exhaust gas using catalysts. The mainstream catalysts for exhaust gas purification have a structure in which γ-alumina powder supporting a noble metal catalyst such as PT is supported on a ceramic honeycomb such as cordierite. However, the stiff ceramic honeycomb has a rather high exhaust resistance, and the temperature at which it can be used is low due to the heat resistance of the buffer stainless steel mesh inserted between the honeycomb and the outer cylinder to prevent it from breaking. There were disadvantages such as restrictions on
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2
図に断面図を示すように一般に金属担体は厚み50μ前
後のステンレス平箔と波型加工したステンレス波箔とを
重ねて円筒形又は楕円柱状に巻き込み、これを耐熱ステ
ンレス製の外i43に装入して平箔〜波箔〜外筒間を相
互にろう付けや抵抗溶接等により接合する。第3図はこ
れを模式的に表したもので、斜線8の部分と太線9の部
分はろう付けされてることを示す。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. Second
As shown in the cross-sectional view in the figure, metal carriers are generally made by stacking a stainless steel flat foil with a thickness of around 50 μm and a corrugated stainless steel corrugated foil, rolling it into a cylindrical or elliptical shape, and charging this into a heat-resistant stainless steel outer i43. Then, the flat foil, corrugated foil, and outer cylinder are joined together by brazing, resistance welding, or the like. FIG. 3 schematically shows this, and the diagonal line 8 and thick line 9 indicate that they are brazed.
金属担体が高温・高速の排気ガスに耐えるためには、耐
酸化性の良好なステンレス箔を用い平箔〜波箔〜外筒相
互の接合面積を増すことが有効であるが、それだけでは
激しい加熱・冷却に対しては耐えられない。すなわち自
動車エンジンに装着された金属担体ではエンジン始動か
ら走行開始時にハニカ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持
続し、この間燃料の供給をカットするタイプのものでは
ハニカムが外筒に先行して冷却され、外局とハニカム間
に大きな温度差が生じる。しかも加熱時と冷却時では温
度差の正負が入れ変わるためハニカムは外筒に近い部分
で熱疲労破壊を生じ、排気ガスの背圧によりハニカムが
風下方向に飛び出す等の不具合が生じる。In order for the metal carrier to withstand high-temperature and high-speed exhaust gas, it is effective to use stainless steel foil with good oxidation resistance and increase the bonding area between the flat foil, corrugated foil, and outer cylinder. - Cannot withstand cooling. In other words, in the case of a metal carrier installed in an automobile engine, the honeycomb portion is heated before the outer cylinder when the engine is started and the vehicle starts running.
In addition, on long downhill slopes, the engine brake state continues for a long time, and in types that cut off the fuel supply during this period, the honeycomb cools down before the outer tube, creating a large temperature difference between the outer tube and the honeycomb. Moreover, since the positive and negative temperature differences change between heating and cooling, the honeycomb suffers thermal fatigue failure at a portion close to the outer cylinder, causing problems such as the honeycomb flying out in the leeward direction due to the back pressure of the exhaust gas.
このように金属担体を固く接合した場合の不具合を防止
する先行技術として、ハニカムを機械的に固定する方法
が米国特許4,186,172号公報、特公昭60−2
7807号公報等に開示されている。またハニカムを部
分的に接合する方法が特開昭62−45345号公報お
よび特開昭61−19957号公報に開示されているが
、ハニカムと外筒との接合方法は明確に記述されておら
ず、ハニカムの外筒への接合強度と耐熱疲労性のすくな
くとも一方で充分な特性を示すものではない。As a prior art technique for preventing problems when metal carriers are firmly joined, a method for mechanically fixing honeycombs is disclosed in U.S. Pat. No. 4,186,172 and Japanese Patent Publication No. 60-2
It is disclosed in Publication No. 7807 and the like. Furthermore, methods for partially joining honeycombs are disclosed in JP-A-62-45345 and JP-A-61-19957, but the method for joining the honeycomb and the outer cylinder is not clearly described. However, the honeycomb does not exhibit sufficient properties in at least one of bonding strength to the outer cylinder and thermal fatigue resistance.
[発明が解決しようとする。課題]
本発明は上述した従来技術の欠点に鑑みてなされたもの
で、高温・高速の排気ガス流にも耐え、か、つ急速な加
熱・冷却にも耐える耐熱疲労性を有する金属基体を提供
するものである。[The invention attempts to solve the problem.] Problem] The present invention has been made in view of the above-mentioned drawbacks of the prior art, and provides a metal substrate that can withstand high-temperature and high-speed exhaust gas flows and has thermal fatigue resistance that can withstand rapid heating and cooling. It is something to do.
[課題を解決するための手段]
この目的を達成するため本発明はハニカムと外筒との間
に温度差が生じた場合でも熱疲労が生じにくい基体の構
成を考案したものであり、第1図は本発明のその一例で
ある。すなわち本発明は平らな金属箔(以下平箔と称す
る)と波型加工した金属箔(以下波箔と称する)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、ハニカムの少
なくとも中心軸方向両端部は平箔と波箔との接合が最外
周から最内周までなされ、且つ前記両端部では外筒とハ
ニカムとは接合されておらず、残りの部分のハニカムは
前記両端部の最外周から最内周まで接合されている部分
の中側端部から少なくとも5゛億m以上離れた場所で最
外周が外筒と接合され、且つ中心軸方向断面においては
面記外筒と接合されている部分と上記両端部との間は接
合されたハニカム部分を介して接続され、ざらに外筒と
の接合面で囲まれたハニカムでは中心軸に垂直なハニカ
ム断面においては、少なくとも接合されていない部分が
半径方向に分布していることを特徴とする耐熱疲労性を
有する自動車触媒用基体である。[Means for Solving the Problems] In order to achieve this object, the present invention has devised a base structure that is less likely to cause thermal fatigue even when a temperature difference occurs between the honeycomb and the outer cylinder. The figure is an example of the present invention. That is, the present invention provides a metal honeycomb for automobile catalysts consisting of a metal honeycomb formed by stacking and rolling together flat metal foil (hereinafter referred to as flat metal foil) and corrugated metal foil (hereinafter referred to as corrugated foil), and a metal outer cylinder surrounding them. In the base body, the flat foil and the corrugated foil are joined at least at both ends in the central axis direction of the honeycomb from the outermost circumference to the innermost circumference, and the outer tube and the honeycomb are not joined at both ends, and the remaining portion The honeycomb is such that the outermost periphery is joined to the outer cylinder at a distance of at least 5 billion meters from the middle end of the part where the ends are joined from the outermost periphery to the innermost periphery, and The part joined to the outer cylinder and the above two ends are connected via the joined honeycomb part, and the honeycomb that is roughly surrounded by the joint surface with the outer cylinder is perpendicular to the central axis. The present invention is a substrate for an automobile catalyst having heat fatigue resistance characterized in that, in a cross section, at least the unjoined portions are distributed in the radial direction.
[発明の図面に基く詳細説明]
次に本発明の詳細な説明する。第1図は本発明の金属基
体の中心軸方向の断面を示すものである。一般に金属基
体の排ガスの入側および出側のハニカム両端面は平箔〜
波箔間の接合をせずに使用すると、高速の排気ガスによ
って箔が振動して疲労破壊を生じる。したがってハニカ
ムの両端部付近1.2の波箔と平箔は相互に接合して個
々の振動を防止する必要がある。しかし接合を行った部
分のハニカムはひとつの剛体としてふる舞うため、この
部分の外筒に接する面を外筒3と接合すると、外筒3と
ハニカムの温度差が縁り返し変化する場合にハニカムの
外周部付近で熱疲労破壊を生じる。[Detailed Description of the Invention Based on Drawings] Next, the present invention will be described in detail. FIG. 1 shows a cross section of the metal base of the present invention in the central axis direction. Generally, both end faces of the honeycomb on the exhaust gas inlet and outlet sides of the metal base are made of flat foil.
If corrugated foils are used without bonding, the foils will vibrate due to high-speed exhaust gas and cause fatigue failure. Therefore, the corrugated foil and flat foil near both ends of the honeycomb 1.2 must be bonded to each other to prevent individual vibrations. However, since the honeycomb in the joined part behaves as one rigid body, if the surface in contact with the outer cylinder of this part is joined to the outer cylinder 3, the honeycomb Thermal fatigue failure occurs near the outer periphery.
このため本発明ではハニカムの最内周から最外周の全層
にわたって接合したハニカム部分(以下完全接合部)は
外筒3と接合しない構造とした。For this reason, in the present invention, a honeycomb portion (hereinafter referred to as a complete joint portion) that is joined over the entire layer from the innermost circumference to the outermost circumference of the honeycomb is not bonded to the outer cylinder 3.
しかしこれだけではハニカムを外筒に固定していないこ
とになるために、使用中にハニカムが排ガスの風下側に
飛び出してくる。したがってハニカムの完全接合部以外
でハニカムと外筒とを接合することが必要である。However, this alone means that the honeycomb is not fixed to the outer cylinder, so the honeycomb will pop out to the leeward side of the exhaust gas during use. Therefore, it is necessary to join the honeycomb and the outer cylinder at a point other than the completely joined portion of the honeycomb.
本発明者らはハニカムと外筒との接合部位について種々
検討した結果、耐熱疲労性のうえからハニカムと外筒と
の接合部6は両端部の完全接合部1.2の中側端部から
少なくとも5I1m以上離す必要があり(第1図(a)
の11およびり、)、これによって前記完全接合部1.
2と外筒との接合部6との間のハニカムの熱疲労破壊を
防止できること、またハニカムの外筒への接合強度のう
えからハニカムと外筒との接合部6と両端部の完全接合
部1.2との間は中心軸方向断面で見た場合に接合され
たハニカム部分く以下ハニカム接合部)4゜5゛を介し
て接続されている必要のあることを知見した。As a result of various studies by the present inventors regarding the joint portion between the honeycomb and the outer cylinder, we found that from the viewpoint of thermal fatigue resistance, the joint portion 6 between the honeycomb and the outer cylinder is connected from the middle end of the complete joint portion 1.2 at both ends. It is necessary to separate at least 5I1m (Figure 1 (a))
11 and 1), thereby forming the complete joint 1.
In order to prevent thermal fatigue failure of the honeycomb between the joint 6 of the honeycomb and the outer cylinder, and to improve the bonding strength of the honeycomb to the outer cylinder, it is necessary to completely connect the joint 6 of the honeycomb and the outer cylinder to both ends. It has been found that the honeycomb portions (hereinafter referred to as honeycomb joints) must be connected through 4° and 5° when viewed in cross section in the central axis direction.
さらにハニカムと外筒の接合面で囲まれたハニカム内部
では、耐熱疲労性のうえから、ハニカムの中心軸と垂直
な断面においては、少くともハニカム非接合部が半径方
向に分布していることが必要であることを知見した。断
面によっては、ハニカム非接合部とハニカム接合部とが
半径方向に分布することとなるが、この場合ハニカム非
接合部は、全断面積の20%以上を占めることが望まし
い。したがって、全断面が全断面積がハニカム非接合部
となる場合も含まれる。すなわち、第1図(b)は(a
)の八s−A+’の部分における中心軸断面を示してお
り、どの半径線上にもハニカム非接合部とハニカム接合
部も存在し、この面上の半径方向の熱応力が緩和される
。また第1図(a)の八、−A 、 j断面は全断面が
ハニカム非接合部であり、この面上の半径方向の熱応力
が緩和される。この断面のほとんど大部分がハニカム接
合部となフた場合、この面上の熱応力の緩和は困難とな
る。Furthermore, in the inside of the honeycomb, which is surrounded by the joint surface between the honeycomb and the outer cylinder, from the viewpoint of thermal fatigue resistance, at least the non-joint parts of the honeycomb are distributed in the radial direction in a cross section perpendicular to the central axis of the honeycomb. I found out that it is necessary. Depending on the cross section, the honeycomb non-bonded portion and the honeycomb bonded portion will be distributed in the radial direction, but in this case, it is desirable that the honeycomb non-bonded portion occupies 20% or more of the total cross-sectional area. Therefore, the case where the entire cross-sectional area is a honeycomb non-joined portion is also included. That is, FIG. 1(b) is (a
) shows a central axis cross section at the section 8s-A+', and there are honeycomb non-bonded parts and honeycomb joined parts on every radial line, and the thermal stress in the radial direction on this surface is relaxed. In addition, the entire cross section of the section 8, -A, j in FIG. If most of this cross section becomes a honeycomb joint, it will be difficult to alleviate the thermal stress on this surface.
本発明でいう接合とは、ろう付け、抵抗溶接、レーザー
溶接、電子ビーム溶接、アーク溶接等の方法で波箔〜平
箔〜外筒を相互に接合したものをいう。また本来接合す
べきでない部位にろう材やアーク等の一部がまわり込ん
で一部の接点を接合させている場合はここでは接合して
いるとはみなさない。さらに高真空又は低圧水素中でス
テンレス同志を接触させて加熱した場合柱々にして生じ
る拡散接合は、ハニカムの接点では接合強度が低いため
ここでいう接合には含めない。また本発明において波箔
の波型は正弦波、台形、矩形等のいずれでもよい。In the present invention, joining refers to joining corrugated foil, flat foil, and outer cylinder to each other by brazing, resistance welding, laser welding, electron beam welding, arc welding, or the like. In addition, if a part of the brazing material, arc, etc. goes around a part that should not originally be joined and joins some of the contacts, it is not considered to be joined here. Furthermore, diffusion bonding, which occurs when stainless steels are brought into contact with each other and heated in a high vacuum or low pressure hydrogen to form pillars, is not included in the term bonding here because the bonding strength is low at honeycomb contacts. Further, in the present invention, the waveform of the corrugated foil may be any one of a sine wave, a trapezoid, a rectangle, etc.
第4図から第6図は本発明の他の例を示すものである。4 to 6 show other examples of the present invention.
ここで1〜7の各部分の意味は夫々第1図のものと同じ
である。これらの接合構造を有するもの)製造方法はろ
う付けの場合あらかじめ箔を巻き込む前に各ろう付はパ
ターンに従って展開図を画いておき、それらにしたがっ
てろう材のバインダーを塗布し、平箔と波箔を巻き込ん
だ後にろう材を塗布すれば良い。また他の接合方法はい
ずれも箔を巻き込む過程でこれらの展開図に従って接合
すれば良い。Here, the meanings of each part 1 to 7 are the same as in FIG. 1. The manufacturing method for products with these joint structures is brazing. Before wrapping the foil in advance, draw a developed diagram according to the pattern for each brazing joint, apply a binder of the brazing material according to the pattern, and then combine the flat foil and corrugated foil. You can apply the brazing filler metal after rolling it in. In addition, in any other joining method, joining may be performed in accordance with these developed diagrams during the process of rolling the foil.
[実施例]
実施例−1
第1図は本発明のひとつの実施態様を示すもので、第1
図(a)は内径100+n111、厚さ1.5mm 、
長さ100I!Imのステンレス外筒と、厚さ50μの
20Cr−5A4のステンレス波箔と平箔を36巻きし
て作られたハニカムで構成された金属基体の中心軸方向
断面である。ハニカム部の両端面1.2の部分は両端部
から厚さI OIamまで波箔と平箔が最外周がら最内
周までろう付けされているか、この部分では、箔がステ
ンレス製外WJ3に接する面は外筒とはろう付けされて
いない。さらにハニカムと外筒との接合部6は1,2の
中側端部からl0IIIIa内方へ離れた(Llおよび
L2)ところから中央部に位置している。該接合部6と
1.2の間はハニカム内の平箔と波箔の接合部分(ハニ
カム接合部)4.5を介して接続されている。このとき
、第1図(a)の6の上端部又は下端部での中心軸に垂
直な断面においては、第1図(b)に示すようにハニカ
ム非接合部とハニカム接合部が半径方向に分布し、全断
面積に対するハニカム非接合部の割合は約3196であ
った。[Example] Example-1 Figure 1 shows one embodiment of the present invention.
Diagram (a) shows inner diameter 100+n111, thickness 1.5mm,
Length 100I! This is a cross section in the central axis direction of a metal base made of a stainless steel outer cylinder of Im and a honeycomb made by 36 turns of 20Cr-5A4 stainless steel corrugated foil and flat foil with a thickness of 50μ. On both end faces 1.2 of the honeycomb part, corrugated foil and flat foil are brazed from the outermost circumference to the innermost circumference from both ends to a thickness of IOIam, or the foil contacts the stainless steel outer WJ3 in this part. The surface is not brazed to the outer cylinder. Furthermore, the joining portion 6 between the honeycomb and the outer cylinder is located in the center from a point 10IIIa inwardly away from the middle end portions 1 and 2 (Ll and L2). The joint parts 6 and 1.2 are connected via a joint part (honeycomb joint part) 4.5 between the flat foil and the corrugated foil in the honeycomb. At this time, in a cross section perpendicular to the central axis at the upper end or lower end of 6 in Fig. 1(a), the honeycomb non-joined part and the honeycomb joined part are radially aligned as shown in Fig. 1(b). The ratio of honeycomb non-bonded parts to the total cross-sectional area was about 3196.
第3図は比較例で、第1図のものと同材質、同一サイズ
の金属基体であるが、ハニカム内部8は全体的に波箔と
平箔がろう付けされ、また最外周9は全面にわたって外
筒3とろう付けされた。上記2種の金属基体にpt触媒
を担持させたγ−アルミナ粉を焼き付けたうえ、排気3
12000ccのエンジンに搭載しベンチテストにより
800℃以上1分。Figure 3 shows a comparative example, which has a metal base made of the same material and the same size as the one in Figure 1, but the inside of the honeycomb 8 is entirely brazed with corrugated foil and flat foil, and the outermost periphery 9 is entirely covered. Brazed to outer cylinder 3. After baking the γ-alumina powder supporting the PT catalyst on the above two types of metal substrates,
Mounted on a 12,000cc engine and tested over 800℃ for 1 minute.
150℃以下1分、合計!サイクル15分の冷熱試験を
繰り返した。1 minute below 150℃, total! The cold test was repeated with a 15 minute cycle.
その結果比較例は80サイクル後にハニカムの最外周か
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ガスの風下側に約2
0mm飛び出していた。一方、本発明(第1図)のもの
は冷熱+200サイクル後も何等異常は認められなかっ
た。As a result, in the comparative example, after 80 cycles, any one of the first to third layer honeycombs from the outermost periphery of the honeycomb was broken over the entire circumference, and the honeycombs on the inner periphery were approximately 2
It was protruding by 0mm. On the other hand, in the case of the present invention (FIG. 1), no abnormality was observed even after 200 cycles of cooling and heating.
実施例−2
第4図は本発明の別の実施態様を示すもので、第1図の
ものと同じ材質と寸法の金属基体の中心軸、および中心
軸に垂直な断面を示す。1.2は外筒と接合されておら
ず且つハニカムの全層の接点が箔を巻き込む段階で抵抗
溶接により接合されている部分で両端面より厚さ14m
mである。(100φx14f)、3はステンレス製外
筒、4は1.2の中心部30φの部分からハニカムとの
接合部6へ接続するハニカム内のろう付は部分、すなわ
ちハニカム接合部である。この例では6は1.2の中側
端部か614mm (Ll、L2)離れたところからハ
ニカム中央部に位置している。第4図(b)は同図(a
)のB−B’部分の中心軸直角断面で、全ハニカム断面
積の30%が非接合部であった。Example 2 FIG. 4 shows another embodiment of the present invention, showing the central axis of a metal base made of the same material and dimensions as those in FIG. 1, and a cross section perpendicular to the central axis. 1.2 is a part that is not joined to the outer cylinder and is joined by resistance welding at the stage where the contact points of all layers of the honeycomb are wrapped around the foil, and the thickness is 14 m from both end faces.
It is m. (100φ x 14f), 3 is a stainless steel outer cylinder, and 4 is a brazed portion within the honeycomb that connects the 30φ central portion of 1.2 to the joint 6 with the honeycomb, that is, the honeycomb joint. In this example, 6 is located in the center of the honeycomb from the middle edge of 1.2 614 mm (Ll, L2) away. Figure 4(b) is
), 30% of the total honeycomb cross-sectional area was a non-bonded part.
第5図は第4図のものと同材質、同寸法の基体で、更に
細かくハニカム接合部とハニカム非接合部をハニカム内
に分散させて耐熱疲労性を持たせたもので、両端部の完
全接合部1.2は両端面より厚さ8mn+で(100φ
x8j2)、外筒との接合部6と1.2の中側端部との
間隔り、、t、2は7ffIII+である。Figure 5 shows a base made of the same material and the same dimensions as the one in Figure 4, but with more finely dispersed honeycomb bonded areas and honeycomb non-bonded areas within the honeycomb to provide thermal fatigue resistance. The joint part 1.2 has a thickness of 8mm+ from both end faces (100φ
x8j2), the distance between the joint 6 with the outer cylinder and the middle end of 1.2, t,2 is 7ffIII+.
第6図と第7図は第1図と同材質、同寸法の金属基体の
中心軸での断面の接合状況を示すもので、1.2は完全
接合部であり外筒と接合されていない部分で両端面より
厚さ100101 (100φXl0fl)、4.5は
1,2の中心部の外径70φ、内径35φの部分からハ
ニカムと外筒との接合部6へ接続するハニカム接合部分
で、6は1.2の中側端部から10mm離れたところか
ら中央部に位置している(Ll、L2=10I1m)。Figures 6 and 7 show the joint state of the cross section at the central axis of the metal base made of the same material and the same dimensions as in Figure 1, and 1.2 is a complete joint and is not joined to the outer cylinder. The thickness is 100101 mm (100 φ is located at the center from a distance of 10 mm from the middle end of 1.2 (Ll, L2=10I1m).
これらの場合の4,5の断面は形状は曲線である。これ
ら3種の金属基体を実施例−1と同様にしてエンジンベ
ンチによる冷熱試験に供したところ、冷熱1200回後
も構造上の異常はみられなかった。In these cases, the cross sections 4 and 5 have curved shapes. When these three types of metal substrates were subjected to a thermal test on an engine bench in the same manner as in Example 1, no structural abnormality was observed even after 1200 thermal cycles.
[発明の効果]
以上説明したように本発明においては、最外周から最内
周までの全層にわたって接合されているハニカムは外筒
の拘束を受けることなく、ハニカムの温度変化に伴って
自由に膨張収縮し得る。[Effects of the Invention] As explained above, in the present invention, the honeycomb, which is bonded over all layers from the outermost periphery to the innermost periphery, is not constrained by the outer cylinder and can freely move as the honeycomb temperature changes. It can expand and contract.
方性筒に接合されている面に囲まれるハニカムは少なく
とも接合されていない部分が半径方向に分布しているた
め、ハニカム内部で熱疲労破壊を生じることなく外筒と
ハニカムの接合が維持され、エンジン排ガスの風圧によ
ってもズレを生じることなく、はげしい温度変化に対し
ても長期にわたって耐え得る。Since at least the unbonded portions of the honeycomb surrounded by the surfaces joined to the oriented cylinder are distributed in the radial direction, the bond between the outer cylinder and the honeycomb is maintained without causing thermal fatigue failure inside the honeycomb. It does not shift due to the wind pressure of engine exhaust gas, and can withstand severe temperature changes for a long period of time.
第1図は本発明による金属基体の断面の接合状況を示す
図で、第2図は従来の金属基体の断面、第3図は第2図
の金属基体の接合状況を示す模式図、第4図〜7図は本
発明による金属基体の断面の接合状況を示す図である。
1.2−・・ハニカムの両端部、3・・・外筒、4.5
・・・ハニカム接合部、6・・・接合部、7・・・非接
合部。FIG. 1 is a diagram showing a state of joining of a cross section of a metal base according to the present invention, FIG. 2 is a cross section of a conventional metal base, FIG. 3 is a schematic diagram showing a state of joining of the metal base of FIG. 2, and FIG. FIGS. 7 to 7 are diagrams showing the bonding state of the cross section of the metal base according to the present invention. 1.2--Both ends of the honeycomb, 3...Outer cylinder, 4.5
...Honeycomb joint, 6: Joint, 7: Non-joint.
Claims (1)
以下波箔)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、 前記ハニカムの少なくとも中心軸方向両端部は平箔と波
箔との接合が最外周から最内周までなされ、且つ前記両
端部では外筒とハニカムとは接合されておらず、残りの
部分のハニカムは、前記最外周から最内周まで接合され
ている部分の中側端部から少なくとも5mm以上離れた
場所で外筒と接合され、且つ中心軸方向断面においては
前記外筒と接合されている部分と前記両端部の間はハニ
カム内の接合されている部分を介して接続され、さらに
外筒との接合面で囲まれたハニカムでは中心軸に垂直な
ハニカム断面においては、少なくとも接合されていない
部分が半径方向に分布していることを特徴とする耐熱疲
労性を有する自動車触媒用金属基体。 2、外筒と接合されているハニカム断面におけるハニカ
ム非接合部の半径方向分布が全断面積の20%以上を占
めることを特徴とする請求項1記載の自動車触媒用金属
基体。[Claims] 1. Flat metal foil (hereinafter referred to as flat foil) and corrugated metal foil (
In a metal base for an autocatalyst, which is composed of a metal honeycomb formed by stacking and rolling up a metal honeycomb (hereinafter referred to as "corrugated foil") and a metal outer cylinder surrounding them, at least at both ends in the central axis direction of the honeycomb, the joining of the flat foil and the corrugated foil starts from the outermost periphery. The outer tube and the honeycomb are not joined to each other at both ends, and the remaining portion of the honeycomb extends from the middle end of the joined portion from the outermost periphery to the innermost periphery at least. It is joined to the outer cylinder at a distance of 5 mm or more, and in the cross section in the central axis direction, the part joined to the outer cylinder and the both ends are connected via the joined part in the honeycomb, and A metal for an autocatalyst having thermal fatigue resistance, characterized in that in a honeycomb surrounded by a joint surface with an outer cylinder, at least unjoined portions are distributed in the radial direction in the honeycomb cross section perpendicular to the central axis. Base. 2. The metal substrate for an autocatalyst according to claim 1, wherein the radial distribution of the non-bonded portion of the honeycomb in the cross section of the honeycomb joined to the outer cylinder occupies 20% or more of the total cross-sectional area.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63255003A JPH0611405B2 (en) | 1988-10-12 | 1988-10-12 | Metal base for automobile catalysts with heat fatigue resistance |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63255003A JPH0611405B2 (en) | 1988-10-12 | 1988-10-12 | Metal base for automobile catalysts with heat fatigue resistance |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH02102744A true JPH02102744A (en) | 1990-04-16 |
JPH0611405B2 JPH0611405B2 (en) | 1994-02-16 |
Family
ID=17272850
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63255003A Expired - Lifetime JPH0611405B2 (en) | 1988-10-12 | 1988-10-12 | Metal base for automobile catalysts with heat fatigue resistance |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0611405B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1996016735A1 (en) * | 1994-12-02 | 1996-06-06 | Usui Kokusai Sangyo Kaisha, Ltd. | Metal honeycomb body |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62194436U (en) * | 1986-06-02 | 1987-12-10 | ||
JPS6397235A (en) * | 1986-10-08 | 1988-04-27 | エミテク・ゲゼルシャフト・フュール・エミシオーンテクノロギー・ミット・ベシュレンクテル・ハフツング | Matrix for catalytic reactor for purifying exhaust gas |
-
1988
- 1988-10-12 JP JP63255003A patent/JPH0611405B2/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62194436U (en) * | 1986-06-02 | 1987-12-10 | ||
JPS6397235A (en) * | 1986-10-08 | 1988-04-27 | エミテク・ゲゼルシャフト・フュール・エミシオーンテクノロギー・ミット・ベシュレンクテル・ハフツング | Matrix for catalytic reactor for purifying exhaust gas |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1996016735A1 (en) * | 1994-12-02 | 1996-06-06 | Usui Kokusai Sangyo Kaisha, Ltd. | Metal honeycomb body |
GB2310385A (en) * | 1994-12-02 | 1997-08-27 | Usui Kokusai Sangyo Kk | Metal honeycomb body |
GB2310385B (en) * | 1994-12-02 | 1998-12-09 | Usui Kokusai Sangyo Kk | Metal honeycomb core body |
US5853902A (en) * | 1994-12-02 | 1998-12-29 | Usui Kokusai Sangyo Kaisha, Ltd. | Metal honeycomb core body |
Also Published As
Publication number | Publication date |
---|---|
JPH0611405B2 (en) | 1994-02-16 |
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