JP2003520133A - Catalyst support with microstructured expandable sleeve - Google Patents

Catalyst support with microstructured expandable sleeve

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Publication number
JP2003520133A
JP2003520133A JP2001553511A JP2001553511A JP2003520133A JP 2003520133 A JP2003520133 A JP 2003520133A JP 2001553511 A JP2001553511 A JP 2001553511A JP 2001553511 A JP2001553511 A JP 2001553511A JP 2003520133 A JP2003520133 A JP 2003520133A
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JP
Japan
Prior art keywords
sleeve
honeycomb body
plate
jacket tube
shaped metal
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
JP2001553511A
Other languages
Japanese (ja)
Other versions
JP4809563B2 (en
Inventor
ナーゲル、トーマス
マウス、ヴォルフガング
ファウスト、ハンス‐ギュンター
ヴィーレス、ルートヴィッヒ
Original Assignee
エミテック ゲゼルシヤフト フユア エミツシオンス テクノロギー ミツト ベシユレンクテル ハフツング
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Application filed by エミテック ゲゼルシヤフト フユア エミツシオンス テクノロギー ミツト ベシユレンクテル ハフツング filed Critical エミテック ゲゼルシヤフト フユア エミツシオンス テクノロギー ミツト ベシユレンクテル ハフツング
Priority claimed from PCT/EP2001/000315 external-priority patent/WO2001053668A1/en
Publication of JP2003520133A publication Critical patent/JP2003520133A/en
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Publication of JP4809563B2 publication Critical patent/JP4809563B2/en
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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
    • F01N3/2839Arrangements for mounting catalyst support in housing, e.g. with means for compensating thermal expansion or vibration
    • F01N3/2842Arrangements 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
    • 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
    • F01N2260/00Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/10Exhaust treating devices having provisions not otherwise provided for for avoiding stress caused by expansions or contractions due to temperature variations
    • 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
    • F01N2330/42Honeycomb supports characterised by their structural details made of three or more different sheets, foils or plates stacked one on the other
    • 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
    • F01N2450/00Methods or apparatus for fitting, inserting or repairing different elements
    • F01N2450/02Fitting monolithic blocks into the housing
    • 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
    • F01N2450/00Methods or apparatus for fitting, inserting or repairing different elements
    • F01N2450/22Methods or apparatus for fitting, inserting or repairing different elements by welding or brazing
    • 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
    • F01N2450/00Methods or apparatus for fitting, inserting or repairing different elements
    • F01N2450/28Methods or apparatus for fitting, inserting or repairing different elements by using adhesive material, e.g. cement

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)
  • Exhaust Gas After Treatment (AREA)
  • Catalysts (AREA)

Abstract

(57)【要約】 板状金属層(2)から成るハニカム体(1)と、ハニカム体を少なくとも部分的に包囲する外被管(4)と、ハニカム体の軸方向長さ(9)より短い軸方向長さ(8)のスリーブ(7)とを備え、板状金属層の少なくとも一部が、ハニカム体が排気ガスの貫流可能な通路(3)を有するよう構成され、外被管が少なくとも1つの軸方向部分範囲(6)だけでハニカム体に接合技術的に結合され、スリーブの外周面(10)が外被管の内側壁(5)の部分に接触する触媒担体に関する。スリーブは、ハニカム体の外側範囲(11)の端面(12)近傍に配置され、スリーブの内周面(13)が、ハニカム体の板状金属層の端面側半径方向外側に位置する終端範囲(15)に、この終端範囲(15)のふらつきを防止すべく、接合技術的に結合される。触媒担体は、機械的および熱的に大きな交番荷重に対しても耐久性を有し、特にエンジン近傍への配置に適する。 (57) [Summary] From a honeycomb body (1) composed of a plate-shaped metal layer (2), a jacket tube (4) at least partially surrounding the honeycomb body, and an axial length (9) of the honeycomb body A sleeve (7) having a short axial length (8), at least a portion of the plate-like metal layer is configured such that the honeycomb body has a passage (3) through which exhaust gas can flow, and the jacket tube is formed. The invention relates to a catalyst carrier which is joined to the honeycomb body only in at least one axial subregion (6) by means of a joining technique and whose outer peripheral surface (10) of the sleeve contacts the inner wall (5) of the jacket tube. The sleeve is arranged near the end face (12) of the outer area (11) of the honeycomb body, and the end area (13) in which the inner peripheral surface (13) of the sleeve is located radially outside the end face side of the plate-shaped metal layer of the honeycomb body. In order to prevent the end area (15) from fluctuating, a joining technique is used. The catalyst carrier is durable against large alternating loads mechanically and thermally, and is particularly suitable for arrangement near the engine.

Description

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

【0001】 本発明は、ハニカム体と、外被管と、両者間に配置されたスリーブとを備えた
触媒コンバータ用の触媒担体とその製造方法に関する。そのような触媒コンバー
タは、内燃機関、特に自動車の排気装置に賞用されている。
The present invention relates to a catalyst carrier for a catalytic converter including a honeycomb body, a jacket tube, and a sleeve arranged between the honeycomb body and the method, and a method for manufacturing the same. Such catalytic converters are widely used in exhaust systems of internal combustion engines, especially motor vehicles.

【0002】 国際特許出願公表99/37896号明細書に、外被形ハニカム体の製造方法
が記載されている。その外被形ハニカム体は、ハニカム体が排気ガスの貫流可能
な通路を備えるよう、積層および/又は巻回により形成され、少なくとも部分的
に微細構造化された板状金属層を有している。ハニカム体は外被管により包囲さ
れている。ハニカム体と外被管は、それらの異なる材料特性および運転中の互い
に異なる温度に基づき、異なる熱膨張挙動を示す。従って、ハニカム体の少なく
とも片側終端範囲で、ハニカム体と外被管との固い結合を避けるよう配慮してい
る。この理由から、外被形ハニカム体にスリーブが設けられている。該スリーブ
は、外被管とハニカム体の製造上の公差にも係らず、ハニカム体の少なくとも片
側終端範囲におけるハニカム体と外被管との直接ろう付け結合が確実に避けられ
るようにしている。この種ハニカム体の製造時、ハニカム体とスリーブ間の幾つ
かの接触個所は、多少はたまたま相互に結合されても、大半の接触個所は結合さ
れないままである。そのようにして確かに、外被管とハニカム体の間の熱応力は
避けられるが、ハニカム体のスリーブへの所定の結合が達成されない。
International Patent Application Publication No. 99/37896 describes a method of manufacturing a jacket-shaped honeycomb body. The envelope-shaped honeycomb body has a plate-like metal layer which is formed by stacking and / or winding and is at least partially microstructured so that the honeycomb body has passages through which exhaust gas can flow. . The honeycomb body is surrounded by the jacket tube. Honeycomb bodies and jacket tubes exhibit different thermal expansion behaviors based on their different material properties and different temperatures during operation. Therefore, care is taken to avoid a firm bond between the honeycomb body and the jacket tube in at least one end region of the honeycomb body. For this reason, sleeves are provided on the envelope honeycomb body. The sleeve ensures that, regardless of the manufacturing tolerances of the jacket tube and the honeycomb body, direct brazing of the honeycomb body and the jacket tube in at least one end region of the honeycomb body is avoided. During the manufacture of this type of honeycomb body, some contact points between the honeycomb body and the sleeve happen to be bonded to each other, but most contact points remain unbonded. In that way, indeed, thermal stresses between the jacket tube and the honeycomb body are avoided, but the desired bonding of the honeycomb body to the sleeve is not achieved.

【0003】 排気装置で触媒担体として利用されるこの種外被形ハニカム体は、熱的負荷だ
けでなく、動的荷重をも受ける。これは、ハニカム体の移動可能に配置された終
端範囲が振動することを意味する。強固に固定されていない接触個所は緩み、固
定されていない板状金属端は自由にふらつき、その結果、触媒作用層が剥離して
しまう。更に、ハニカム体のこの自由にふらつく部分範囲が緩み、隣接する通路
を塞いだり、隣接する排気装置の構成要素を損傷したりする危険がある。
This type of envelope-shaped honeycomb body used as a catalyst carrier in an exhaust device receives not only thermal load but also dynamic load. This means that the movably arranged end area of the honeycomb body vibrates. The contact points that are not firmly fixed loosen, and the plate-shaped metal edges that are not fixed freely fluctuate, and as a result, the catalytic layer separates. Furthermore, there is the risk that this free-flickering part of the honeycomb body will loosen, blocking adjacent passages and damaging adjacent exhaust system components.

【0004】 本発明の課題は、大きな熱的交番荷重の下でさえ外被管とハニカム体の間の熱
応力を回避し、且つ例えば脈動する排気ガス流による動的荷重下での板状金属自
由端や波形板状金属のふらつきを回避できる触媒担体を提供することにある。
The object of the invention is to avoid thermal stresses between the jacket tube and the honeycomb body even under high thermal alternating loads, and for example sheet metal under dynamic loads due to pulsating exhaust gas flow. Another object of the present invention is to provide a catalyst carrier capable of avoiding free end and wavy plate-shaped metal wobble.

【0005】 本発明の課題は、更にそのような触媒担体の製造方法を提供することにある。[0005]   Another object of the present invention is to provide a method for producing such a catalyst carrier.

【0006】 本発明は、この課題を請求項1に記載の触媒担体および請求項14に記載の製
造方法によって解決する。有利な実施態様は各従属請求項に示す。
The present invention solves this problem by the catalyst carrier according to claim 1 and the manufacturing method according to claim 14. Advantageous embodiments are given in the respective dependent claims.

【0007】 本発明に基づく触媒担体は、板状金属層から成るハニカム体を備え、この板状
金属層は、ハニカム体が排気ガスの貫流可能な通路を形成するよう、少なくとも
一部が微細構造化される。ハニカム体は、少なくとも部分的に外被管で包囲され
る。その外被管は、少なくとも1つの軸方向部分範囲だけでハニカム体に接合法
で結合される。なお、接合法での結合とは、接着、ろう付け、溶接等による物質
的な結合を意味する。ハニカム体の軸方向長さより短寸のスリーブが、外被管の
内側壁の部分に接触する。スリーブは、ハニカム体外周の端面近傍に配置する。
スリーブの内周面は、本発明に基づき、その円周にわたり、ハニカム体の板状金
属層の端面側半径方向外側に位置する終端範囲に、この終端範囲のふらつきを防
止すべく接合法で結合する。板状金属層の半径方向外側に位置する終端範囲は、
スリーブとの結合に基づき、個別の振動を生じない。この結果、大きな動的荷重
下でも、触媒作用層はじっと動かないでいる。この終端範囲のハニカム体からの
緩みを阻止し、この結果、触媒担体は、有害物の発生に関して最良の効果を発揮
し、大きな寿命を示す。
The catalyst carrier according to the present invention comprises a honeycomb body composed of a plate-shaped metal layer, and the plate-shaped metal layer has at least a part of a fine structure so that the honeycomb body forms a passage through which exhaust gas can flow. Be converted. The honeycomb body is at least partially surrounded by a jacket tube. The jacket tube is joined to the honeycomb body in a joining method only in at least one axial subrange. The joining by the joining method means a physical joining by adhesion, brazing, welding or the like. A sleeve, which is shorter than the axial length of the honeycomb body, comes into contact with the inner wall portion of the jacket tube. The sleeve is arranged near the end face of the outer periphery of the honeycomb body.
According to the present invention, the inner peripheral surface of the sleeve is joined to the end area located radially outside the end surface side of the plate-shaped metal layer of the honeycomb body by the joining method in order to prevent the end area from wobbling. To do. The termination range located on the outer side in the radial direction of the plate-shaped metal layer is
Due to the coupling with the sleeve, no individual vibration occurs. As a result, the catalytic layer does not move even under a large dynamic load. The loosening of this end region from the honeycomb body is prevented, so that the catalyst carrier has the best effect on the generation of harmful substances and has a long life.

【0008】 本発明の他の実施態様で、触媒コンバータの触媒担体は、ハニカム体が外被管
に対し熱膨張した際、スリーブが移動可能な点で優れている。かくして、触媒担
体の熱的負荷の下での、外被管とハニカム体の異なる熱膨張を補償する。
In another embodiment of the present invention, the catalyst carrier of the catalytic converter is excellent in that the sleeve can move when the honeycomb body thermally expands with respect to the jacket pipe. Thus, different thermal expansions of the jacket tube and the honeycomb body are compensated for under the thermal loading of the catalyst support.

【0009】 スリーブを少なくともハニカム体の端面迄延ばし、板状金属層の終端範囲に結
合するとよい。この結果、板状金属層の終端範囲を特に強固に固定できる。
The sleeve may be extended at least up to the end face of the honeycomb body and bonded to the end region of the plate-shaped metal layer. As a result, the terminal area of the plate-shaped metal layer can be fixed particularly firmly.

【0010】 本発明の有利な実施態様では、スリーブが外被管の縁より突出し、スリーブの
辺が、外被管の縁に鍔状に接するよう、半径方向外側に折り曲げる。かくしてハ
ニカム体を挿入する際および/又は触媒担体の運転中に、ハニカム体が所定の挿
入深さを越えて外被管内に侵入するのを阻止するストッパが生ずる。
In an advantageous embodiment of the invention, the sleeve projects beyond the edge of the jacket tube and is bent radially outwards so that the sides of the sleeve bear against the edge of the jacket tube in a flanged manner. Thus, during insertion of the honeycomb body and / or during operation of the catalyst carrier, a stopper is provided which prevents the honeycomb body from penetrating into the jacket pipe beyond a predetermined insertion depth.

【0011】 本発明の他の実施形態では、スリーブは少なくとも1つの微細構造を持つ。こ
の結果、スリーブは外被管との小さな接触面を示す。これは特に、ハニカム体が
熱膨張した際、スリーブが外被管に対し小さな摩擦力のため容易に移動でき、外
被管とハニカム体との間の熱応力を特に良好に阻止できる点で有利である。この
微細構造は、スリーブの軸方向長さにわたり少なくとも部分的に延び、好適には
その全長にわたって形成される。
In another embodiment of the invention, the sleeve has at least one microstructure. As a result, the sleeve exhibits a small contact surface with the jacket tube. This is particularly advantageous in that when the honeycomb body thermally expands, the sleeve can easily move due to a small frictional force against the jacket pipe, and thermal stress between the jacket tube and the honeycomb body can be prevented particularly well. Is. The microstructure extends at least partially over the axial length of the sleeve and is preferably formed over its entire length.

【0012】 本発明の他の実施態様では、微細構造を環状に形成する。これは、微細構造を
スリーブに円周方向、軸縦方向又はスパイラル状に配置することを意味する。こ
の種微細構造は、例えばヨーロッパ特許第454712号明細書で公知である。
In another embodiment of the present invention, the microstructure is formed in an annular shape. This means arranging the microstructures on the sleeve in a circumferential, longitudinal or spiral fashion. Microstructures of this kind are known, for example, from EP 454712.

【0013】 本発明の他の実施態様では、例えば国際特許出願公表96/09892号明細
書で知られているように、複数の微細構造が交差している。
In another embodiment of the invention, a plurality of microstructures are intersected, as is known, for example, from WO 96/09892.

【0014】 特に、少なくとも1つの微細構造が、半径方向外側のみ、即ち外被管にしか向
かないようスリーブを形成するとよい。こうすると、部分的に単に点状の非常に
小さな接触面しか生じないので、外被管へのスリーブの固着を防止できる。加え
て、少なくとも部分的にハニカム体とスリーブの線状接触面が生じるので、スリ
ーブの内周面はハニカム体に良好にろう付けできる。
In particular, it is advantageous to form the sleeve such that the at least one microstructure only faces radially outwardly, ie towards the jacket tube. In this way, only a very small contact surface, which is simply spot-shaped, is partially produced, so that the sleeve is prevented from sticking to the jacket tube. In addition, since the linear contact surface between the honeycomb body and the sleeve is generated at least partially, the inner peripheral surface of the sleeve can be brazed to the honeycomb body well.

【0015】 板状金属層が両側板状金属端を備えた少なくとも1つの板状金属を有し、その
少なくとも1つの板状金属の少なくとも片側板状金属端がスリーブの内周面に接
触する触媒担体において、本発明の他の実施態様に基づき、スリーブの内周面を
それに接する少なくとも片側板状金属端に接合法で結合する。スリーブの内周面
は、それに接する全ての板状金属端に接合法で結合するとよい。
A catalyst in which the plate-shaped metal layer has at least one plate-shaped metal having two-sided plate-shaped metal ends, and at least one plate-shaped metal end of the at least one plate-shaped metal contacts the inner peripheral surface of the sleeve. In the carrier, according to another embodiment of the invention, the inner peripheral surface of the sleeve is joined to at least one plate-shaped metal end in contact with it by a joining method. The inner peripheral surface of the sleeve may be joined to all of the plate-shaped metal ends in contact with it by a joining method.

【0016】 ハニカム体の他の実施態様では、板状金属層が***部付きの微細構造化された
少なくとも1つの板状金属を有し、その少なくとも1つの板状金属が、その***
部でスリーブの内周面に接触する。本発明に基づき、スリーブの内周面に、それ
に接する***部を接合法で結合する。
In another embodiment of the honeycomb body, the plate-shaped metal layer comprises at least one microstructured plate-shaped metal with ridges, the at least one plate-shaped metal being sleeved at the ridges. Contact the inner surface of. According to the present invention, the inner peripheral surface of the sleeve is joined to the raised portion in contact with it by a joining method.

【0017】 本発明の他の実施態様では、スリーブとハニカム体との結合部は、製造条件に
伴いスリーブと外被管の間に生ずる結合より大きな強度を示す。この大きな強度
は、異なる熱膨張に基づき生ずる応力を、まずスリーブと外被管との結合を断つ
ことによって無くすることを保障する。スリーブと外被管との結合は、触媒担体
の製造時、特に外被管内におけるスリーブの予備固定或いは意図しない点状の固
着によって、意図的に或いは意図なしに生ずる。
In another embodiment of the invention, the joint between the sleeve and the honeycomb body exhibits greater strength than the joint that occurs between the sleeve and the jacket tube due to manufacturing conditions. This high strength ensures that the stresses caused by the different thermal expansions are eliminated by first breaking the connection between the sleeve and the jacket tube. The connection between the sleeve and the jacket tube occurs intentionally or unintentionally during the manufacture of the catalyst carrier, especially by pre-fixing or unintentional point-like fixing of the sleeve in the jacket tube.

【0018】 本発明の他の実施態様で、ハニカム体と外被管との間の接合による結合はろう
付け結合である。特にハニカム体を外被管に高温真空ろう付けするとよい。この
結合は、自動車の内燃機関の排気装置、特にエンジン近くに据え付けられた触媒
担体に生ずる、極端な熱的および機械的状態にも耐える点で優れている。
In another embodiment of the invention, the joining connection between the honeycomb body and the jacket tube is a brazing connection. In particular, it is advisable to braze the honeycomb body to the jacket tube at high temperature. This combination is advantageous in that it also withstands the extreme thermal and mechanical conditions that occur in exhaust systems of internal combustion engines of motor vehicles, in particular catalyst supports installed near the engine.

【0019】 本発明は他の観点から、ハニカム体と外被管とスリーブとを備えた触媒担体の
製造方法を提案する。まず、ハニカム体を、排気ガスが貫流する通路を形成する
ように、少なくとも部分的に微細構造化した板状金属層の積層および/又は巻回
により公知のように形成する。続いて、外被管内にスリーブを入れ、スリーブの
外周面を外被管の内側壁の部分に接触させる。その場合、スリーブが組立状態に
おいてハニカム体の端面範囲の近くに存在するよう、スリーブを外被管内に配置
するとよい。続いて、外被管の内側壁とスリーブの内周面の少なくとも1つの環
状円周範囲にろう材を付ける。次に、ハニカム体を外被管とスリーブ内に入れ、
ハニカム体の端面をスリーブ近傍で外被管の縁から突出させる。ハニカム体の突
出した端面とその突出端面近傍の外側範囲に接着剤を着ける。ハニカム体の軸方
向突出部分は、接着剤の塗布を容易にする。続いて、ハニカム体を外被管とスリ
ーブ内に完全に入れる。そして、ハニカム体の端面側にろう材料、特にろう粉末
を付着させ、ろう材を付ける。特にこの工程後、スリーブとハニカム体間でハニ
カム体の端面近傍の外側範囲にろう粉末が存在すると有利である。その後、ハニ
カム体と外被管およびハニカム体とスリーブをろう付け結合する。
From another point of view, the present invention proposes a method of manufacturing a catalyst carrier including a honeycomb body, a jacket tube, and a sleeve. First, a honeycomb body is formed in a known manner by laminating and / or winding at least partially microstructured plate-like metal layers so as to form passages through which exhaust gas flows. Then, the sleeve is put in the jacket tube, and the outer peripheral surface of the sleeve is brought into contact with the inner wall portion of the jacket tube. In that case, the sleeve may be arranged in the envelope tube so that it lies near the end face area of the honeycomb body in the assembled state. Subsequently, a brazing material is applied to at least one annular circumferential area of the inner wall of the jacket tube and the inner peripheral surface of the sleeve. Next, put the honeycomb body in the jacket tube and the sleeve,
The end face of the honeycomb body is made to project from the edge of the jacket pipe in the vicinity of the sleeve. An adhesive is applied to the protruding end surface of the honeycomb body and the outer area near the protruding end surface. The axially protruding portion of the honeycomb body facilitates application of the adhesive. Subsequently, the honeycomb body is completely put into the jacket tube and the sleeve. Then, a brazing material, particularly a brazing powder, is adhered to the end face side of the honeycomb body to attach the brazing material. Particularly after this step, it is advantageous for the wax powder to be present in the outer area between the sleeve and the honeycomb body in the vicinity of the end faces of the honeycomb body. After that, the honeycomb body and the jacket tube and the honeycomb body and the sleeve are brazed together.

【0020】 本発明に基づく方法の有利な実施態様では、スリーブをハニカム体の板状金属
層の終端範囲に高温真空ろう付けする。
In a preferred embodiment of the method according to the invention, the sleeve is hot vacuum brazed to the end regions of the plate-shaped metal layer of the honeycomb body.

【0021】 本発明に基づく方法の他の実施態様では、スリーブを、ハニカム体の挿入前に
外被管の内側壁に接着剤で接着する。そのために用いる接着剤は、ろう付け中に
少なくとも部分的に気化する。かくして、ハニカム体と外被管の異なる熱膨張に
基づき、スリーブが外被管の内側壁上を滑るのを保障する。
In another embodiment of the method according to the invention, the sleeve is glued to the inner wall of the jacket tube before insertion of the honeycomb body. The adhesive used for this at least partially vaporizes during brazing. Thus, the different thermal expansions of the honeycomb body and the jacket tube ensure that the sleeve slides on the inside wall of the jacket tube.

【0022】 特に、スリーブの辺をまず半径方向外側に曲げ、その曲げた辺を、ハニカム体
を外被管とスリーブ内に完全に挿入した後、外被管の縁に接触させるとよい。こ
れに伴い、外被管内でのハニカム体の、特に正確な軸方向固定が行える。
In particular, the sides of the sleeve may be first bent outward in the radial direction, and the bent sides may be brought into contact with the edges of the jacket tube after the honeycomb body is completely inserted into the jacket tube and the sleeve. Along with this, particularly accurate axial fixing of the honeycomb body in the jacket tube can be performed.

【0023】 以下図示の特に有利な実施例を参照して、本発明に基づく触媒担体とその製造
方法の他の利点および詳細を説明する。
Further advantages and details of the catalyst carrier according to the invention and the process for its preparation will be explained below with reference to the particularly preferred embodiments shown in the drawings.

【0024】 図1は、端面12と軸方向長さ9を持つハニカム体1を示す。ハニカム体1の
外側範囲11に軸方向部分範囲6があり、該範囲でハニカム体1は外被管5と接
合法で結合している。また該外側範囲11に、板状金属端17が見えている。
FIG. 1 shows a honeycomb body 1 having an end face 12 and an axial length 9. In the outer region 11 of the honeycomb body 1, there is an axial partial region 6 in which the honeycomb body 1 is joined to the jacket pipe 5 by a joining method. Further, the plate-shaped metal end 17 is visible in the outer region 11.

【0025】 更に、スリーブ7を示している。スリーブ7の軸方向長さ8は、ハニカム体1
の軸方向長さ9より短い。スリーブ7は、外周面10と内周面13と辺19とを
有している。スリーブ7をハニカム体1にその端面12の近くで固定するため、
スリーブ7の円周範囲20を利用する。
Furthermore, the sleeve 7 is shown. The axial length 8 of the sleeve 7 depends on the honeycomb body 1.
Is shorter than the axial length 9 of. The sleeve 7 has an outer peripheral surface 10, an inner peripheral surface 13 and a side 19. In order to fix the sleeve 7 to the honeycomb body 1 near its end face 12,
The circumferential range 20 of the sleeve 7 is utilized.

【0026】 外被管4は、内側壁5と端面側縁14を持つ。外被管4は、接合状態では、ス
リーブ7付きのハニカム体1を包囲する。
The jacket pipe 4 has an inner wall 5 and an end surface side edge 14. The jacket tube 4 surrounds the honeycomb body 1 with the sleeve 7 in the joined state.

【0027】 上述した触媒担体の製造は、第1工程で、ハニカム体1を板状金属層12(図
2参照)の積層および/又は巻回により製造することから始まる。スリーブ7を
外被管4内に入れ、その際、スリーブ7の外周面10を外被管4の内側壁5に接
触させる。外被管4の内側壁5およびスリーブ7の環状円周範囲20に、ろう材
を付ける。そして、ハニカム体1を外被管4およびスリーブ7内に入れる。その
場合、外被管4内でのスリーブ7の位置は、できるだけ不変であるようにせねば
ならない。ハニカム体1は部分的に外被管4の縁14から軸方向に突出する。ハ
ニカム体1の突出した端面12および該端面12近傍における外側範囲11に接
着剤を付ける。接着剤は、端面12並びに該端面12近くにおける板状金属端1
7の十分な固着を保障する。そしてハニカム体1を、外力を加えることで外被管
4およびスリーブ7内に完全に入れる。特に、ハニカム体1の端面12がスリー
ブ7の辺19と面一に続いていると有利である。次の工程で、ハニカム体1と外
被管4との間並びにハニカム体1とスリーブ7との間接合する。結合は、高温真
空ろう付けにより実行するのが好ましい。
The production of the catalyst carrier described above begins with the first step of producing the honeycomb body 1 by laminating and / or winding the plate-shaped metal layer 12 (see FIG. 2). The sleeve 7 is placed in the jacket tube 4, with the outer peripheral surface 10 of the sleeve 7 contacting the inner wall 5 of the jacket tube 4. A brazing material is applied to the inner side wall 5 of the jacket tube 4 and the annular circumferential area 20 of the sleeve 7. Then, the honeycomb body 1 is put into the jacket tube 4 and the sleeve 7. In that case, the position of the sleeve 7 within the jacket tube 4 should be as invariant as possible. The honeycomb body 1 partially projects in the axial direction from the edge 14 of the jacket tube 4. An adhesive is applied to the protruding end surface 12 of the honeycomb body 1 and the outer area 11 in the vicinity of the end surface 12. The adhesive is applied to the end face 12 and the plate-shaped metal end 1 near the end face 12.
Guarantee a sufficient fixation of 7. Then, the honeycomb body 1 is completely put into the jacket pipe 4 and the sleeve 7 by applying an external force. In particular, it is advantageous if the end face 12 of the honeycomb body 1 is flush with the side 19 of the sleeve 7. In the next step, the honeycomb body 1 and the jacket tube 4 and the honeycomb body 1 and the sleeve 7 are joined together. Bonding is preferably performed by high temperature vacuum brazing.

【0028】 図2は、外被管4と、スリーブ7と、板状金属層2から製造したハニカム体1
とから成る本発明に基づく触媒担体を端面図で示す。金属層2は、ハニカム体1
が排気ガスの貫流する通路3を形成すべく、積層および/又は巻回され、少なく
とも部分的に微細構造化された板状金属層2を備える。この金属層2は、例えば
板状金属16で形成する。その幾つかの板状金属16は***部18を有し、代表
的には通常のハニカム体と同様に波形板状金属の波山を持つ。板状金属層2は、
その半径方向外側に位置する終端範囲15でスリーブ7に接している。図示の実
施例では、板状金属16はその板状金属端17がスリーブ7に接している。特に
高温真空ろう付け過程後に、全ての板状金属端17がスリーブ7に結合している
と有利である。
FIG. 2 shows a honeycomb body 1 manufactured from a jacket tube 4, a sleeve 7, and a plate-shaped metal layer 2.
FIG. 3 shows an end view of a catalyst carrier according to the invention consisting of The metal layer 2 is the honeycomb body 1.
Comprises a plate-like metal layer 2 which is laminated and / or wound and at least partially microstructured to form a passage 3 through which the exhaust gas flows. The metal layer 2 is formed of, for example, a plate-shaped metal 16. Some of the plate-shaped metals 16 have a raised portion 18, and typically have a wave crest of a corrugated plate-shaped metal similar to a normal honeycomb body. The plate-shaped metal layer 2 is
It contacts the sleeve 7 in the end region 15 located radially outside thereof. In the illustrated embodiment, the sheet metal 16 has its sheet metal end 17 in contact with the sleeve 7. Particularly after the hot vacuum brazing process, it is advantageous if all the sheet metal ends 17 are connected to the sleeve 7.

【0029】 このように形成した触媒担体は、熱的負荷時のハニカム体1と外被管4の異な
る熱膨張を、スリーブ7がハニカム体1の端面側終端範囲15で外被管4の内側
壁5上を滑ることより補償する。終端範囲15とスリーブ7との接合法による結
合に基づき、板状金属層2のふらつきを防止できる。この結果、特にエンジン近
傍に据え付けた際に、特に荷重の印加が可能な触媒担体が生ずる。
In the catalyst carrier thus formed, the thermal expansion causes different thermal expansion of the honeycomb body 1 and the jacket pipe 4, and the sleeve 7 inside the jacket pipe 4 in the end surface side end region 15 of the honeycomb body 1. Compensate by sliding on the wall 5. It is possible to prevent the plate-shaped metal layer 2 from wobbling based on the connection between the end area 15 and the sleeve 7 by the joining method. This results in a catalyst carrier to which a load can be applied especially when installed near the engine.

【0030】 図3は、微細構造21を備えたスリーブ7を製造するための板状金属22を示
す。板状金属22をスリーブ7状に成形することで、互いに平行に延びる微細構
造21を適当に方向付け、膨張方向を任意に定めることができる。
FIG. 3 shows a sheet metal 22 for manufacturing the sleeve 7 with the microstructures 21. By molding the plate-shaped metal 22 in the shape of the sleeve 7, the microstructures 21 extending parallel to each other can be appropriately oriented and the expansion direction can be arbitrarily determined.

【0031】 図4および図5は、互いに相異なる微細構造21を備えたスリーブ用板状金属
22の、別個の実施例を示す。図6は、交差微細構造22を備えたスリーブ用板
状金属22を斜視図で示す。
FIGS. 4 and 5 show separate embodiments of the plate metal 22 for the sleeve with different microstructures 21. FIG. 6 shows a perspective view of a plate metal 22 for a sleeve provided with crossed microstructures 22.

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

【図1】 本発明に基づく触媒担体のハニカム体、スリーブおよび外被管の分解斜視図。[Figure 1]   FIG. 3 is an exploded perspective view of a honeycomb body, a sleeve and a jacket tube of the catalyst carrier according to the present invention.

【図2】 接合された状態にある本発明に基づく触媒担体の断面図。[Fig. 2]   FIG. 3 is a cross-sectional view of a catalyst carrier according to the present invention in a bonded state.

【図3】 微細構造を備えた板状金属の部分正面図。[Figure 3]   The partial front view of the plate-shaped metal provided with the fine structure.

【図4】 微細構造を備えた板状金属の実施例の断面図。[Figure 4]   Sectional drawing of the Example of the plate-shaped metal provided with a fine structure.

【図5】 微細構造を備えた板状金属の異なった実施例の断面図。[Figure 5]   Sectional drawing of the different Example of the plate-shaped metal provided with a microstructure.

【図6】 公差する微細構造を備えたスリーブ用板状金属の部分斜視図。[Figure 6]   FIG. 3 is a partial perspective view of a plate-shaped metal for a sleeve having a microstructure that is tolerated.

【符号の説明】 1 ハニカム体 2 板状金属層 3 通路 4 外被管 5 内側壁 6 部分範囲 7 スリーブ 8 スリーブ長さ 9 ハニカム体の軸方向長さ 10 スリーブの外周面 11 ハニカム体の外側範囲 12 ハニカム体の端面 13 スリーブの内周面 14 外被管の縁 15 ハニカム体の終端範囲 16 板状金属 17 板状金属端 18 ***部 19 スリーブの辺 20 円周範囲 21 微細構造 22 スリーブ板状金属[Explanation of symbols]   1 Honeycomb body   2 Plate metal layer   3 passages   4 jacket tube   5 Inner wall   6 partial range   7 sleeve   8 Sleeve length   9 Axial length of honeycomb 10 Outer peripheral surface of sleeve 11 Outside range of honeycomb body 12 End face of honeycomb 13 Inner surface of sleeve 14 Edge of jacket tube 15 End range of honeycomb 16 Plate metal 17 Plate metal edge 18 ridge 19 Sleeve side 20 circle range 21 Fine structure 22 Sleeve plate metal

───────────────────────────────────────────────────── フロントページの続き (81)指定国 EP(AT,BE,CH,CY, DE,DK,ES,FI,FR,GB,GR,IE,I T,LU,MC,NL,PT,SE,TR),OA(BF ,BJ,CF,CG,CI,CM,GA,GN,GW, ML,MR,NE,SN,TD,TG),AP(GH,G M,KE,LS,MW,MZ,SD,SL,SZ,TZ ,UG,ZW),EA(AM,AZ,BY,KG,KZ, MD,RU,TJ,TM),AE,AG,AL,AM, AT,AU,AZ,BA,BB,BG,BR,BY,C A,CH,CN,CR,CU,CZ,DE,DK,DM ,DZ,EE,ES,FI,GB,GD,GE,GH, GM,HR,HU,ID,IL,IN,IS,JP,K E,KG,KP,KR,KZ,LC,LK,LR,LS ,LT,LU,LV,MA,MD,MG,MK,MN, MW,MX,NO,NZ,PL,PT,RO,RU,S D,SE,SG,SI,SK,SL,TJ,TM,TR ,TT,TZ,UA,UG,US,UZ,VN,YU, ZA,ZW (72)発明者 ファウスト、ハンス‐ギュンター ドイツ連邦共和国 51143 ケルン ロー ゼンヒューゲル 76 (72)発明者 ヴィーレス、ルートヴィッヒ ドイツ連邦共和国 51491 オフェラート オッペルナー シュトラーセ 2 Fターム(参考) 3G091 AA02 AB01 BA39 GA08 GA16 HA27 HA31 HA44 4D048 BB02 BB11 EA06 4G069 AA01 AA08 CA03 DA06 EA20 EA26 ED10 ─────────────────────────────────────────────────── ─── Continued front page    (81) Designated countries EP (AT, BE, CH, CY, DE, DK, ES, FI, FR, GB, GR, IE, I T, LU, MC, NL, PT, SE, TR), OA (BF , BJ, CF, CG, CI, CM, GA, GN, GW, ML, MR, NE, SN, TD, TG), AP (GH, G M, KE, LS, MW, MZ, SD, SL, SZ, TZ , UG, ZW), EA (AM, AZ, BY, KG, KZ, MD, RU, TJ, TM), AE, AG, AL, AM, AT, AU, AZ, BA, BB, BG, BR, BY, C A, CH, CN, CR, CU, CZ, DE, DK, DM , DZ, EE, ES, FI, GB, GD, GE, GH, GM, HR, HU, ID, IL, IN, IS, JP, K E, KG, KP, KR, KZ, LC, LK, LR, LS , LT, LU, LV, MA, MD, MG, MK, MN, MW, MX, NO, NZ, PL, PT, RO, RU, S D, SE, SG, SI, SK, SL, TJ, TM, TR , TT, TZ, UA, UG, US, UZ, VN, YU, ZA, ZW (72) Inventor Faust, Hans-Günter             Federal Republic of Germany 51143 Cologne Roh             Zen Hugel 76 (72) Inventor Wiles, Ludwig             Germany 51491 Oferat               Opperner Strasse 2 F-term (reference) 3G091 AA02 AB01 BA39 GA08 GA16                       HA27 HA31 HA44                 4D048 BB02 BB11 EA06                 4G069 AA01 AA08 CA03 DA06 EA20                       EA26 ED10

Claims (17)

【特許請求の範囲】[Claims] 【請求項1】 板状金属層(2)から成るハニカム体(1)と、ハニカム体
(1)を少なくとも部分的に包囲する外被管(4)と、ハニカム体(1)の軸方
向長さ(9)より短い軸方向長さ(8)のスリーブ(7)とを備え、板状金属層
(2)の少なくとも一部は、ハニカム体(1)が排気ガスの貫流可能な通路(3
)を形成するよう構成され、外被管(4)が少なくとも1つの軸方向部分範囲(
6)だけでハニカム体(1)に接合法で結合され、スリーブ(7)の外周面(1
0)が外被管(4)の内側壁(5)の部分に接触する触媒担体において、スリー
ブ(7)がハニカム体(1)の外側範囲(11)に、その端面(12)に近接し
て配置され、スリーブ(7)の内周面(13)が、ハニカム体(1)の端面側半
径方向外側に位置する板状金属層(2)の終端範囲(15)に、この終端範囲(
15)のふらつきを防止すべく接合法で結合されたことを特徴とする触媒担体。
1. A honeycomb body (1) comprising a plate-shaped metal layer (2), a jacket pipe (4) at least partially surrounding the honeycomb body (1), and an axial length of the honeycomb body (1). A sleeve (7) having an axial length (8) shorter than the length (9), and at least a part of the plate-like metal layer (2) has a passage (3) through which the honeycomb body (1) can flow exhaust gas.
), Wherein the jacket tube (4) forms at least one axial subrange (
6) is bonded to the honeycomb body (1) by a bonding method alone, and the outer peripheral surface (1
In the catalyst carrier in which 0) is in contact with the portion of the inner wall (5) of the jacket pipe (4), the sleeve (7) is close to the outer region (11) of the honeycomb body (1) and its end face (12). And the inner peripheral surface (13) of the sleeve (7) is located in the end area (15) of the plate-shaped metal layer (2) located radially outside the end surface side of the honeycomb body (1).
A catalyst carrier characterized by being bonded by a bonding method so as to prevent the fluctuation of 15).
【請求項2】 ハニカム体(1)が外被管(4)に対して伸びた際、スリー
ブ(7)が移動することを特徴とする請求項1記載の担体。
2. A carrier as claimed in claim 1, characterized in that the sleeve (7) moves when the honeycomb body (1) extends relative to the jacket tube (4).
【請求項3】 スリーブ(7)が、少なくともハニカム体(1)の端面(1
2)迄延びることを特徴とする請求項1又は2記載の担体。
3. The sleeve (7) has at least an end face (1) of the honeycomb body (1).
Carrier according to claim 1 or 2, characterized in that it extends to 2).
【請求項4】 スリーブ(7)が外被管(4)の縁(14)から突出し、ス
リーブ(7)の辺(19)が、外被管(4)の縁(14)に鍔状に接するように
折り曲げられたことを特徴とする請求項1から3の1つに記載の担体。
4. The sleeve (7) projects from the edge (14) of the jacket tube (4), the side (19) of the sleeve (7) forming a collar on the edge (14) of the jacket tube (4). 4. The carrier according to claim 1, wherein the carrier is bent so as to be in contact with each other.
【請求項5】 スリーブ(7)が少なくとも1つの微細構造(21)を有す
ることを特徴とする請求項1から4の1つに記載の担体。
5. Carrier according to one of claims 1 to 4, characterized in that the sleeve (7) has at least one microstructure (21).
【請求項6】 少なくとも1つの微細構造(12)が環状に形成されたこと
を特徴とする請求項5記載の担体。
6. Carrier according to claim 5, characterized in that at least one microstructure (12) is formed in an annular shape.
【請求項7】 複数の微細構造(12)が交差することを特徴とする請求項
5又は6記載の担体。
7. Carrier according to claim 5 or 6, characterized in that a plurality of microstructures (12) intersect.
【請求項8】 少なくとも1つの微細構造(12)が、半径方向外方のみに
外被管(4)に向かうことを特徴とする請求項5から7の1つに記載の担体。
8. Carrier according to one of claims 5 to 7, characterized in that at least one microstructure (12) is directed only radially outwards to the jacket tube (4).
【請求項9】 板状金属層(2)が両側板状金属端(17)を備えた少なく
とも1つの板状金属(16)を有し、その少なくとも1つの板状金属(16)の
少なくとも片側板状金属端(17)が、スリーブ(7)の内周面(13)に接触
する請求項1から8の1つに記載の担体において、スリーブ(7)の内周面(1
3)が、それに接する少なくとも片側板状金属端(17)、好適にはそれに接す
る全ての板状金属端(17)に、接合法で結合されたことを特徴とする担体。
9. The plate-like metal layer (2) has at least one plate-like metal (16) with two-sided plate-like metal ends (17), at least one side of which is at least one plate-like metal (16). Carrier according to one of claims 1 to 8, characterized in that the plate-shaped metal end (17) contacts the inner peripheral surface (13) of the sleeve (7).
3) A carrier characterized in that 3) is bonded by a bonding method to at least one plate-shaped metal end (17) contacting it, preferably to all plate-shaped metal ends (17) contacting it.
【請求項10】 板状金属層が***部(18)付きの微細構造化された少な
くとも1つの板状金属(16)を有し、その少なくとも1つの板状金属(16)
がその***部(18)でスリーブ(7)の内周面(13)に接触する請求項1か
ら9の1つに記載の触媒担体において、スリーブ(7)の内周面(13)が、そ
れに接する***部(18)に接合法で結合されたことを特徴とする担体。
10. The plate-shaped metal layer comprises at least one microstructured plate-shaped metal (16) with a ridge (18), the at least one plate-shaped metal (16).
The catalyst carrier according to one of claims 1 to 9, wherein the ridges (18) contact the inner peripheral surface (13) of the sleeve (7), wherein the inner peripheral surface (13) of the sleeve (7) is A carrier characterized in that it is bonded to the raised portion (18) in contact with it by a bonding method.
【請求項11】 スリーブ(7)とハニカム体(1)の結合が、場合によっ
て製造上条件づけられるスリーブ(7)と外被管(4)の間の結合よりも大きな
強度を有することを特徴とする請求項1から10の1つに記載の担体。
11. The connection between the sleeve (7) and the honeycomb body (1) has a greater strength than the connection between the sleeve (7) and the jacket tube (4), which is optionally manufacturing-conditioned. The carrier according to one of claims 1 to 10, wherein
【請求項12】 ハニカム体(1)が外被管(4)にろう付け、好適には高
温真空ろう付けされたことを特徴とする請求項1から11の1つに記載の担体。
12. A carrier as claimed in claim 1, wherein the honeycomb body (1) is brazed to the jacket tube (4), preferably by high temperature vacuum brazing.
【請求項13】 板状金属層(2)の端面側半径方向外側に位置する終端範
囲(15)が、スリーブ(7)にその辺(19)の近くで、スリーブ内周面(1
3)の少なくとも1つの環状円周範囲(20)においてろう付け、好適には高温
真空ろう付けされたことを特徴とする請求項1から12の1つに記載の担体。
13. The inner peripheral surface (1) of the sleeve (7) has a terminal area (15) located radially outward of the end surface side of the plate-shaped metal layer (2) near the side (19) of the sleeve (7).
13. Carrier according to one of claims 1 to 12, characterized in that it is brazed in at least one annular circumference range (20) of 3), preferably hot vacuum brazed.
【請求項14】 板状金属層(2)から成るハニカム体(1)と、ハニカム
体(1)を少なくとも部分的に包囲する外被管(4)と、ハニカム体(1)の軸
方向長さ(9)より短い軸方向長さ(8)のスリーブ(7)とを備え、板状金属
層(2)の少なくとも一部を、ハニカム体(1)が排気ガスの貫流可能な通路(
3)を有するように構成し、外被管(4)を少なくとも1つの軸方向部分範囲(
6)だけでハニカム体(1)に固着し、スリーブ(7)の外周面(10)を外被
管(4)の内側壁(5)の部分に接触させる触媒担体の製造方法において、ハニ
カム体(1)を、これが排気ガスの貫流可能な通路(3)を持つように少なくと
も一部が微細構造化された板状金属層(2)の積層および/又は巻回により形成
し、外被管(4)内にスリーブ(7)を入れ、その際、スリーブ(7)の外周面
(10)を外被管(4)の内側壁(5)の部分に接触させ、外被管(4)の内側
壁(5)とスリーブ(7)の内周面(13)の少なくとも1つの環状円周範囲(
20)にろう材を付着させ、外被管(4)およびスリーブ(7)内にハニカム体
(1)を入れ、その際、ハニカム体(1)の端面(12)をスリーブ(7)の近
くで外被管(4)の縁(14)から突出させ、ハニカム体(1)の突出した端面
(12)およびその突出端面(12)の近傍の外側範囲(11)に接着剤を付け
、ハニカム体(1)を外被管(4)およびスリーブ(7)内に完全に入れ、ハニ
カム体(1)の端面側にろう粉末を着けることでろう材を着け、ハニカム体(1
)と外被管(4)との間およびハニカム体(1)とスリーブ(7)との間にろう
付け結合を形成することを特徴とする触媒担体の製造方法。
14. A honeycomb body (1) comprising a plate-shaped metal layer (2), a jacket pipe (4) at least partially surrounding the honeycomb body (1), and an axial length of the honeycomb body (1). A sleeve (7) having an axial length (8) shorter than the length (9), and the honeycomb body (1) passes through at least a part of the plate-shaped metal layer (2) through a passage (
3) and having a jacket tube (4) with at least one axial subrange (
In the method for producing a catalyst carrier, which is fixed to the honeycomb body (1) only by 6) and the outer peripheral surface (10) of the sleeve (7) is brought into contact with the inner wall (5) of the jacket pipe (4). (1) is formed by laminating and / or winding a plate-like metal layer (2) at least a part of which is microstructured so that it has a passage (3) through which exhaust gas can flow, and a jacket pipe The sleeve (7) is put into the (4), in which case the outer peripheral surface (10) of the sleeve (7) is brought into contact with the portion of the inner wall (5) of the jacket pipe (4) so that the jacket pipe (4) Of at least one annular circumference of the inner wall (5) of the sleeve and the inner peripheral surface (13) of the sleeve (7) (
20), a brazing filler metal is attached to the honeycomb body (1), and the honeycomb body (1) is placed in the jacket pipe (4) and the sleeve (7). And projecting it from the edge (14) of the jacket pipe (4) by applying an adhesive to the protruding end face (12) of the honeycomb body (1) and the outer range (11) in the vicinity of the protruding end face (12), The body (1) is completely put into the jacket tube (4) and the sleeve (7), and the brazing filler metal is applied to the end face side of the honeycomb body (1) to apply the brazing material,
) And the jacket tube (4) and between the honeycomb body (1) and the sleeve (7), a brazing bond is formed.
【請求項15】 スリーブ(7)を、ハニカム体(1)の板状金属層(2)
の終端範囲(15)に高温真空ろう付けすることを特徴とする請求項14記載の
方法。
15. A plate-shaped metal layer (2) for a honeycomb body (1), comprising a sleeve (7).
15. The method according to claim 14, characterized in that high-temperature vacuum brazing is carried out in the end region (15) of the.
【請求項16】 スリーブ(7)を、ハニカム体(1)の挿入前に、外被管
(4)の内側壁(5)に接着剤で接着し、該接着剤を、ろう付け中に少なくとも
部分的に気化し、これによってその後、スリーブ(7)を外被管(4)の内側壁
(5)上で滑動可能とすることを特徴とする請求項14又は15記載の方法。
16. A sleeve (7) is glued to the inner side wall (5) of the jacket pipe (4) before the insertion of the honeycomb body (1), said glue being at least during brazing. 16. Method according to claim 14 or 15, characterized in that it is partially vaporized, whereby the sleeve (7) is then slidable on the inner wall (5) of the jacket tube (4).
【請求項17】 スリーブ(7)の辺(19)をまず半径方向外側に曲げ、
ハニカム体(1)を外被管(4)およびスリーブ(7)内に完全に挿入した後、
前記曲げた辺(19)を外被管(4)の縁(14)に接触させることを特徴とす
る請求項14から16の1つに記載の方法。
17. A side (19) of the sleeve (7) is first bent outward in the radial direction,
After completely inserting the honeycomb body (1) into the jacket tube (4) and the sleeve (7),
17. Method according to one of claims 14 to 16, characterized in that the bent side (19) is brought into contact with the edge (14) of the jacket tube (4).
JP2001553511A 2000-01-17 2001-01-12 Catalyst support with microstructured expandable sleeve Expired - Fee Related JP4809563B2 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
DE10001639.1 2000-01-17
DE10001639 2000-01-17
DE10017839.1 2000-04-11
DE10017839A DE10017839A1 (en) 2000-01-17 2000-04-11 Catalyst carrier body with a stretch sleeve with microstructures
PCT/EP2001/000315 WO2001053668A1 (en) 2000-01-17 2001-01-12 Catalyst support comprising an expandable collar provided with microstructures

Publications (2)

Publication Number Publication Date
JP2003520133A true JP2003520133A (en) 2003-07-02
JP4809563B2 JP4809563B2 (en) 2011-11-09

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DE (1) DE10017839A1 (en)

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