JPH08266905A - Metal carrier - Google Patents

Metal carrier

Info

Publication number
JPH08266905A
JPH08266905A JP7076853A JP7685395A JPH08266905A JP H08266905 A JPH08266905 A JP H08266905A JP 7076853 A JP7076853 A JP 7076853A JP 7685395 A JP7685395 A JP 7685395A JP H08266905 A JPH08266905 A JP H08266905A
Authority
JP
Japan
Prior art keywords
metal carrier
intermediate body
honeycomb body
outer cylinder
joined
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
JP7076853A
Other languages
Japanese (ja)
Other versions
JP3667811B2 (en
Inventor
Yasushi Ishikawa
泰 石川
Tadayuki Otani
忠幸 大谷
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
Original Assignee
Nippon Steel Corp
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 filed Critical Nippon Steel Corp
Priority to JP07685395A priority Critical patent/JP3667811B2/en
Publication of JPH08266905A publication Critical patent/JPH08266905A/en
Application granted granted Critical
Publication of JP3667811B2 publication Critical patent/JP3667811B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Exhaust Gas After Treatment (AREA)
  • Exhaust Gas Treatment By Means Of Catalyst (AREA)
  • Laminated Bodies (AREA)
  • Catalysts (AREA)

Abstract

PURPOSE: To provide a metal carrier having high freedom by a simple method by providing an intermediate body between an outer cylinder and a honeycomb body in a structure in which the honeycomb body of the metal carrier is bonded entirely or the temperature variation of exhaust gas is large and high durability is not obtained. CONSTITUTION: As a metal carrier of good durability, plane foils and corrugated foils are wound or laminated alternately to form a honeycomb body 4, and then a sheet of same thickness as that of foils or thicker is wound on the outside of the body twice or more to form an intermediate body 5. The inner face of the intermediate body 5 and the outer face of the honeycomb body 1 are continuously or intermittently bonded one round, and the outer face of the intermediate body 5 is bonded with an outer cylinder 6 within one round, and also an unbonded layer of one round or more is formed in the intermediate body 5.

Description

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

【0001】[0001]

【産業上の利用分野】本発明は、自動車エンジン等の内
燃機関から排出される排ガスを浄化するためのメタル担
体に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a metal carrier for purifying exhaust gas discharged from an internal combustion engine such as an automobile engine.

【0002】[0002]

【従来の技術】従来排気ガスを浄化するための触媒コン
バータにはセラミックスメタル担体が使用されたが、耐
熱性、低圧損および搭載性の点より最近はメタル担体の
使用が増加している。
2. Description of the Related Art Conventionally, a ceramic metal carrier has been used for a catalytic converter for purifying exhaust gas, but recently, the use of the metal carrier has been increasing in view of heat resistance, low pressure loss and mountability.

【0003】メタル担体は厚さ50μm程度の耐熱性の
あるフェライト系ステンレス鋼等の金属よりなる平箔
と、この平箔をコルゲート加工した波箔とを渦巻状に巻
回してハニカム体を形成し、これを同じく耐熱性のある
フェライト系ステンレス鋼等の耐蝕、耐熱性金属で製造
された外筒に収納し、ロウ付け等により相互に接合して
構成されている。
The metal carrier is formed by spirally winding a flat foil made of a metal such as ferritic stainless steel having a heat resistance of about 50 μm and a corrugated corrugated corrugated foil into a honeycomb body. This is housed in an outer cylinder made of a corrosion-resistant and heat-resistant metal such as ferritic stainless steel, which also has heat resistance, and is joined to each other by brazing or the like.

【0004】このメタル担体は白金、パラジウム、ロジ
ウム等の排ガス浄化用の触媒を担持された後、例えば自
動車エンジンの排ガス系に搭載使用される。そのため、
本メタル担体は運転状況の変化に伴う激しい温度変化、
振動を受けるが、もし損傷すると浄化性能が落ちるばか
りか、排気系の閉鎖あるいはエンジン損傷を引き起こす
ため特に高い耐久性が要求される。
This metal carrier is loaded with a catalyst for purifying exhaust gas such as platinum, palladium and rhodium, and then mounted and used in an exhaust gas system of an automobile engine, for example. for that reason,
This metal carrier has severe temperature changes due to changes in operating conditions,
It suffers from vibration, but if damaged, not only the purification performance will deteriorate, but also exhaust system closure or engine damage will be required, so particularly high durability is required.

【0005】メタル担体に作用する熱応力は、温度差の
大きい外筒とハニカム体間では特に大きく従来からその
応力を緩和するため、様々な接合構造が提案されてい
る。例えば、特開平4−148016号公報に示される
ように、ハニカム体内部の接合構造およびハニカム体と
外筒の接合箇所を特定し、熱変形に対する自由度を上
げ、いわゆる柔構造とし、熱応力を下げる方法、あるい
は、特開平3−157139号公報、特開平2−298
620号公報に示されるように、筒状の中間体をハニカ
ム体と外筒の間に配置し、内側でハニカム体と、外側で
外筒と接合するが、その両接合箇所を軸方向に一致させ
ないことにより、同じく熱変形に対する自由度を上げる
方法がある。
The thermal stress acting on the metal carrier is particularly large between the outer cylinder and the honeycomb body having a large temperature difference, and various bonding structures have conventionally been proposed in order to reduce the stress. For example, as disclosed in Japanese Patent Application Laid-Open No. 4-148016, the joint structure inside the honeycomb body and the joint portion between the honeycomb body and the outer cylinder are specified to increase the degree of freedom with respect to thermal deformation so that a so-called flexible structure can be obtained, and thermal stress The lowering method, or JP-A-3-157139 and JP-A-2-298.
As disclosed in Japanese Patent Laid-Open No. 620, a tubular intermediate body is arranged between a honeycomb body and an outer cylinder, and is joined to the honeycomb body on the inner side and the outer cylinder on the outer side. There is also a method of increasing the degree of freedom with respect to thermal deformation by not allowing it.

【0006】従来の方法は、ハニカム体内部および外筒
とハニカム体間の接合構造を合理化したり、また中間体
を設けることにより、熱変形に対する自由度を高め、良
好な耐久性を確保しているが、製造が複雑で生産性が低
くなり、コスト高になる問題があった。またハニカム体
を拡散接合する場合は、特別な対策を講じなければ平箔
と波箔の接触箇所は全て接合されるが、このようにハニ
カム体が全体接合された場合は、外筒とハニカム体間の
変形に対する自由度をさらに高める必要があるが、従来
の方法では不足し、ハニカム体支持部が破損し終わりに
は、ずれてしまう問題があった。
In the conventional method, the degree of freedom with respect to thermal deformation is improved and good durability is ensured by rationalizing the joining structure between the inside of the honeycomb body and the outer cylinder and the honeycomb body and providing an intermediate body. However, there is a problem that manufacturing is complicated, productivity is low, and cost is high. When the honeycomb body is diffusion-bonded, all contact points between the flat foil and the corrugated foil are bonded unless special measures are taken, but when the honeycomb body is entirely bonded in this way, the outer cylinder and the honeycomb body are bonded together. Although it is necessary to further increase the degree of freedom with respect to deformation, there is a problem in that the conventional method is insufficient, and the honeycomb body supporting portion is damaged and is displaced at the end.

【0007】[0007]

【発明が解決しようとする課題】本発明は、メタル担体
のハニカム体が全体接合されたり、排気ガスの温度変化
が大きく、従来の方法ではハニカム体と外筒間の変形に
対する自由度が不足するため、高い耐久性が得られない
場合、外筒とハニカム体間に中間を設けることにより高
い自由度を簡便な方法で付与したメタル担体を提供する
ものである。
DISCLOSURE OF THE INVENTION According to the present invention, the honeycomb bodies of the metal carrier are wholly joined or the temperature of the exhaust gas changes greatly, and the conventional method lacks the degree of freedom for deformation between the honeycomb body and the outer cylinder. Therefore, when high durability cannot be obtained, a metal carrier is provided in which a high degree of freedom is provided by a simple method by providing an intermediate between the outer cylinder and the honeycomb body.

【0008】[0008]

【課題を解決するための手段】すなわち本発明は、耐久
性のあるメタル担体として、(1)平箔と波箔を交互に
巻回あるいは積層したハニカム体を形成した後、その外
側に箔と同じあるいはそれよりも厚い薄板を2回以上巻
回して中間体を形成し、その中間体の内面とハニカム対
外面とは連続的に、あるいは間欠的に一周、中間体の外
面においては外筒と一周以内接合し、さらに中間体内部
においては一周以上の非接合層を設けたことを特徴とす
るメタル担体、(2)ハニカム体内部を全体接合したこ
とを特徴とする前(1)項記載のメタル担体、(3)中
間体をコルゲート加工していない平板とすることを特徴
とする前(1)あるいは(2)項記載のメタル担体、
(4)中間体をコルゲート加工した波板とすることを特
徴とする前(1)から(3)の何れかに記載のメタル担
体、および(5)中間体とハニカム体は上流側で、中間
体と外筒とは下流側で接合することを特徴とする前
(1)から(4)の何れかに記載のメタル担体である。
Means for Solving the Problems That is, the present invention provides, as a durable metal carrier, (1) after forming a honeycomb body in which flat foil and corrugated foil are alternately wound or laminated, and then a foil is formed on the outside thereof. The same or thicker thin plate is wound two or more times to form an intermediate body, and the inner surface of the intermediate body and the honeycomb-to-outer surface continuously or intermittently make one round, and the outer surface of the intermediate body forms an outer cylinder. A metal carrier characterized by being joined within one round and further provided with a non-joining layer of one round or more inside the intermediate body, (2) The inside of the honeycomb body being wholly joined, A metal carrier, (3) the metal carrier according to the above (1) or (2), characterized in that the intermediate body is a flat plate that is not corrugated.
(4) The metal carrier according to any one of (1) to (3) above, wherein the intermediate body is a corrugated corrugated plate, and (5) the intermediate body and the honeycomb body are on the upstream side, and are intermediate. The body and the outer cylinder are joined on the downstream side, which is the metal carrier as described in any of the above (1) to (4).

【0009】以下本発明を詳細に説明する。図1は本発
明のメタル担体1の外観図である。平箔2と波箔3を巻
回あるいは積層して形成されたハニカム体4の外側に、
2回以上巻回した中間体5が、さらにその外側に外筒6
が配置されている。同構成においてハニカム体4は中間
体5の内面と接合し、また中間体5の外面は、外筒6の
内面と接合されている。しかし、多重に巻回されている
中間体5の内部は接合されていない。
Hereinafter, the present invention will be described in detail. FIG. 1 is an external view of a metal carrier 1 of the present invention. Outside the honeycomb body 4 formed by winding or laminating the flat foil 2 and the corrugated foil 3,
The intermediate body 5 wound twice or more is further provided with an outer cylinder 6 on the outer side thereof.
Is arranged. In the same structure, the honeycomb body 4 is joined to the inner surface of the intermediate body 5, and the outer surface of the intermediate body 5 is joined to the inner surface of the outer cylinder 6. However, the inside of the intermediate body 5 wound in multiple layers is not joined.

【0010】また中間体5の板厚は、外筒6より薄く、
ハニカム体を構成している平箔2、波箔3より厚く設定
されている。中間体5は、ハニカム体4とは連続的にあ
るいは間欠的に一周分で接合し、外筒6とは一周分以内
で、連続的あるいは間欠的に接合されている。
The plate thickness of the intermediate body 5 is thinner than that of the outer cylinder 6,
It is set thicker than the flat foil 2 and the corrugated foil 3 which form the honeycomb body. The intermediate body 5 is joined to the honeycomb body 4 continuously or intermittently for one round, and is joined to the outer cylinder 6 within one round continuously or intermittently.

【0011】従って、本発明のメタル担体1の中間体5
は、熱応力的には内周でハニカム体4を保持し、その外
面で外筒6に結合しているコイルバネのような役割を有
し、半径方向の変位に対して容易に追従でき、また熱伝
導的には、中間体5内部の非接合層が断熱層として作用
し、ハニカム体4と中間体5の温度差が小さくなり、同
時に中間体5と外筒6間の温度差も小さくなり、ハニカ
ム体4と外筒6間で発生する応力を小さくできる。
Therefore, the intermediate 5 of the metal carrier 1 of the present invention
In terms of thermal stress, has a role like a coil spring that holds the honeycomb body 4 on the inner circumference and is connected to the outer cylinder 6 on the outer surface, and can easily follow radial displacement. In terms of heat conduction, the non-bonding layer inside the intermediate body 5 acts as a heat insulating layer, and the temperature difference between the honeycomb body 4 and the intermediate body 5 becomes small, and at the same time, the temperature difference between the intermediate body 5 and the outer cylinder 6 also becomes small. The stress generated between the honeycomb body 4 and the outer cylinder 6 can be reduced.

【0012】ハニカム体4には、触媒が塗布されている
ので、その反応熱が発生し軸方向に熱応力が発生する。
しかし、ハニカム体4が全体接合されているため、その
軸方向の変位は、強制的に拘束されるので変位量が小さ
くなり、良好な耐久性を確保できる。
Since the catalyst is applied to the honeycomb body 4, reaction heat of the catalyst is generated and thermal stress is generated in the axial direction.
However, since the entire honeycomb body 4 is bonded, the displacement in the axial direction is forcibly restrained, so that the displacement amount becomes small and good durability can be secured.

【0013】図2は本発明のメタル担体1の構成を示す
図である。(a)図には平箔2と波箔3が巻回され形成
されたハニカム体4の外観を示し、(b)図にそのハニ
カム体4を巻き込み包む中間体5の外観を示すが、2回
以上カールされている。また図2では中間体は平坦な薄
板で示しているが、コルゲート加工した波箔を同様に2
回以上カールしても良い。(c)図にはハニカム体4と
中間筒5を収納する外筒6の外観を示す。これらの接触
面には、例えばロウ付けする場合は相互に接合するため
のロウ材、あるいは拡散接合する場合は界面接合を清浄
にし接合できる準備がなされ、また逆に接合しない部位
については接合防止剤等が塗布された後、必要な加圧力
が付加され密着するように組み立てられる。
FIG. 2 is a diagram showing the structure of the metal carrier 1 of the present invention. The appearance of the honeycomb body 4 formed by winding the flat foil 2 and the corrugated foil 3 is shown in (a), and the appearance of the intermediate body 5 that wraps the honeycomb body 4 is shown in (b). It has been curled more than once. Although the intermediate body is shown as a flat thin plate in FIG. 2, a corrugated corrugated foil is similarly used.
You may curl more than once. (C) shows the outer appearance of the outer cylinder 6 that houses the honeycomb body 4 and the intermediate cylinder 5. For these contact surfaces, for example, when brazing, a brazing material for joining to each other, or in the case of diffusion joining, preparation is made so that the interface joining can be cleaned and joined. After being coated, etc., they are assembled so that the necessary pressing force is applied and they are in close contact.

【0014】以下本発明のメタル担体における各種の接
合構造を示す。図3から図6までは、メタル担体縦断面
における接合構造の実施例を示し、図7から図10は各
メタル担体横断面の接合構造を示す。なお、これらの縦
断面の接合構造と横断面の接合構造は、特定の組み合わ
せはなく、適宜、組み合わせて使用できるものである。
Various bonding structures in the metal carrier of the present invention will be shown below. 3 to 6 show an embodiment of the joint structure in the vertical cross section of the metal carrier, and FIGS. 7 to 10 show the joint structure in the horizontal cross section of each metal carrier. There is no specific combination of the joining structure of the vertical cross section and the joining structure of the cross section, and they can be appropriately combined and used.

【0015】図3は、ハニカム体4は斜線で示す範囲が
例えば拡散接合あるいはロウ付けにより、平箔と波箔の
全ての接点が、原則的に接合されている。5は中間体で
あるが、その内面のハニカム体4の外面と接するの部位
7(点で示している範囲の部位)は軸方向に全長接合し
ている。同様に中間体5の外面と外筒6の内面と接する
部位8(点で示している範囲の部位)は軸方向に全長接
合している。しかし、中間体5の内外面以外の、中間層
9は接合されない。
In FIG. 3, in the honeycomb body 4, all the contact points of the flat foil and the corrugated foil are bonded in principle by, for example, diffusion bonding or brazing in a shaded area. Reference numeral 5 denotes an intermediate body, and a portion 7 (a portion within a range indicated by a dot) on the inner surface of the intermediate body, which is in contact with the outer surface of the honeycomb body 4, is joined in the entire length in the axial direction. Similarly, a portion 8 (a portion within a range indicated by a dot) in contact with the outer surface of the intermediate body 5 and the inner surface of the outer cylinder 6 is joined to the entire length in the axial direction. However, the intermediate layer 9 other than the inner and outer surfaces of the intermediate body 5 is not joined.

【0016】図4は、中間体5の自由度を最大に利用す
る時に採用するが、同様にハニカム体4は斜線で示す範
囲が例えば拡散接合あるいはロウ付けにより、平箔と波
箔の全ての接点が、原則的に接合されている。中間体5
の内面のハニカム体4の外面と接するの部位7は軸方向
に、例えば排気ガスの入側の特定範囲を接合し、外筒6
の内面と接する部位8は軸方向に、例えば排気ガス出側
の特定範囲を接合している。しかし、部位7,8以外の
点で示していない範囲の部位、および同じく中間体5の
内外面以外の、中間層9は接合されない。
FIG. 4 is adopted when the degree of freedom of the intermediate body 5 is utilized to the maximum. Similarly, in the honeycomb body 4, the range indicated by diagonal lines is, for example, by diffusion bonding or brazing, so that all of the flat foil and the corrugated foil can be obtained. The contacts are in principle joined. Intermediate 5
The portion 7 of the inner surface of the honeycomb body 4 that contacts the outer surface of the honeycomb body 4 is joined in the axial direction, for example, in a specific range on the exhaust gas inlet side,
The portion 8 in contact with the inner surface of is joined in the axial direction, for example, in a specific range on the exhaust gas outlet side. However, the intermediate layer 9 is not joined except for the parts other than the parts 7 and 8 which are not shown and the inner and outer surfaces of the intermediate body 5.

【0017】図5は、例えば中間体5のハニカム体4お
よび外筒6との接合部を、高温の排気ガスから保護する
場合に採用するが、ハニカム体4は斜線で示す範囲が例
えば拡散接合あるいはロウ付けにより、平箔と波箔の全
ての接点が、原則的に接合されている。中間体5の内面
のハニカム体4の外面と接する部位7は軸方向に、例え
ば排気ガスの出側の特定範囲を接合し、外筒6の内面と
接する部位8は軸方向に、例えば排気ガス出側の特定範
囲を接合している。しかし、同じく中間体5の内外面以
外の、中間層9は接合されない。なお中間体5の長さ
は、図5では接合範囲に留めているが、接合長よりも長
くしても支障ない。
FIG. 5 is used when, for example, the joint portion of the intermediate body 5 with the honeycomb body 4 and the outer cylinder 6 is protected from high-temperature exhaust gas. Alternatively, by brazing, all the contacts of the flat foil and the corrugated foil are basically joined. A portion 7 of the inner surface of the intermediate body 5 which is in contact with the outer surface of the honeycomb body 4 is joined in the axial direction, for example, a specific range on the exhaust gas outlet side, and a portion 8 of which is in contact with the inner surface of the outer cylinder 6 is in the axial direction, for example the exhaust gas. The specified area on the output side is joined. However, the intermediate layer 9 other than the inner and outer surfaces of the intermediate body 5 is not joined. Although the length of the intermediate body 5 is limited to the joining range in FIG. 5, there is no problem if it is longer than the joining length.

【0018】図6は、例えばハニカム体5の長さが短い
ため、使用中に外筒6の中で傾くのを防止する場合に採
用する。同図においてハニカム体4の長さは短いが、中
間体5および外筒6は、ハニカム体4より長く、使用中
に変形が発生しても、その姿勢を維持できる長さを有し
ている。ハニカム体4は、上記と同様に斜線で示す範囲
が例えば拡散接合あるいはロウ付けにより、平箔と波箔
の全ての接点が、原則的に接合されている。中間体5の
内面のハニカム体4の外面と接する部位7は軸方向に、
例えば全長接合し、外筒6の内面と接する部位8は軸方
向に、例えば全長接合している。しかし、同じく中間体
5の内外面以外の中間層9は接合されない。
FIG. 6 is used to prevent the honeycomb body 5 from tilting in the outer cylinder 6 during use because the honeycomb body 5 has a short length, for example. In the figure, the honeycomb body 4 has a short length, but the intermediate body 5 and the outer cylinder 6 are longer than the honeycomb body 4 and have such a length that the posture thereof can be maintained even if deformation occurs during use. . In the honeycomb body 4, all the contact points of the flat foil and the corrugated foil are bonded in principle by, for example, diffusion bonding or brazing in the shaded area as in the above. The portion 7 of the inner surface of the intermediate body 5 which is in contact with the outer surface of the honeycomb body 4 is in the axial direction,
For example, the portion 8 that is joined over the entire length and is in contact with the inner surface of the outer cylinder 6 is joined over the entire length in the axial direction. However, similarly, the intermediate layer 9 other than the inner and outer surfaces of the intermediate body 5 is not joined.

【0019】図7において、ハニカム体4は斜線で示す
範囲の平箔と波箔の接点が全て接合され、中間体5の内
面とは全周(点で示される範囲の部位)で接合され、ま
た中間体5の外面は外筒6と全周(点で示される範囲の
部位)で接合されている。しかし、中間体5の中間層9
は接合されていない。
In FIG. 7, in the honeycomb body 4, all the contact points of the flat foil and the corrugated foil in the shaded area are joined, and the inner surface of the intermediate body 5 is joined along the entire circumference (the portion in the area indicated by the dots). Further, the outer surface of the intermediate body 5 is joined to the outer cylinder 6 along the entire circumference (a portion within a range indicated by a dot). However, the intermediate layer 9 of the intermediate 5
Are not joined.

【0020】図8においては、中間体5と外筒6は、ハ
ニカム体4の箔よりも厚いため全周接合する必要がない
場合に採用する接合構造である。ハニカム体4内部の接
合およびハニカム体4と中間体5との接合は図7の場合
と同じであるが、中間体5の外面と外筒6の内面は全周
でない、一部に留め、他の点で示していない範囲の部位
は接合されていない。なおこの場合、中間体5の非接合
部が1周以上必要ない場合は、本発明の応用として中間
体5のカールする範囲を2周以下とし、中間体5を節約
することができる。
In FIG. 8, the intermediate body 5 and the outer cylinder 6 are thicker than the foil of the honeycomb body 4 and are a joining structure adopted when it is not necessary to join them all around. The joining of the inside of the honeycomb body 4 and the joining of the honeycomb body 4 and the intermediate body 5 are the same as in the case of FIG. 7, but the outer surface of the intermediate body 5 and the inner surface of the outer cylinder 6 are not the entire circumference, only a part of them is Areas not shown by the points are not joined. In this case, if the non-bonded portion of the intermediate body 5 is not required to make one round or more, the curling range of the intermediate body 5 may be set to two or less as an application of the present invention, and the intermediate body 5 can be saved.

【0021】図9は、中間体5と外筒6間の接合材を節
約する場合に採用する構造を示す。すなわち中間体5と
外筒6間の点で示す範囲の部位は接合し、点で示されな
い範囲の接合しない部位を交互に配置する。中間体5の
内部の層を接合しないのは上記と同じである。
FIG. 9 shows a structure adopted to save the bonding material between the intermediate body 5 and the outer cylinder 6. That is, the parts in the range shown by the points between the intermediate body 5 and the outer cylinder 6 are joined, and the parts not joined in the ranges not shown by the points are alternately arranged. As in the above, the layers inside the intermediate body 5 are not joined.

【0022】図10はさらにハニカム体4と中間体5
間、および中間体5と外筒6間の接合材を節約する場合
に採用する構造である。同図で点で示す範囲の部位は接
合し、表示していない範囲の部位は接合しない。すなわ
ちハニカム体4は全体的に接合し、ハニカム体4と中間
体5とは間欠的に、また中間体5は外筒6とはその一部
で接合している。
FIG. 10 further shows a honeycomb body 4 and an intermediate body 5.
This structure is used when saving the space between the intermediate body 5 and the outer cylinder 6. In the figure, parts in the range shown by dots are joined, and parts in the range not shown are not joined. That is, the honeycomb body 4 is entirely joined, the honeycomb body 4 and the intermediate body 5 are joined intermittently, and the intermediate body 5 and the outer cylinder 6 are joined at a part thereof.

【0023】上記の応用として、公知の内部の特定箇所
に非接合部を設けたハニカム体を、本発明のメタル担体
に採用することは、耐久性をさらに向上し可能である。
しかし製造コストから本発明のように、全体的に接合し
たハニカム体を採用した方が有利である。
As the above-mentioned application, it is possible to further improve the durability by adopting a known honeycomb body having a non-bonded portion at a specific location inside thereof in the metal carrier of the present invention.
However, in terms of manufacturing cost, it is advantageous to adopt a honeycomb body that is wholly bonded as in the present invention.

【0024】本発明のメタル担体1は、従来の公知のメ
タル担体と同様に、例えば排気ガス浄化用の白金、パラ
ジウム、ロジウム等の貴金属を担持された後、例えば自
動車の排気系に取り付け使用される。同箇所ではメタル
担体は激しい温度変化を受けるため、半径方向の大きい
温度差が発生し、外筒6はハニカム体4に強い圧縮引張
り力が作用する。
The metal carrier 1 of the present invention is used in the same manner as a conventionally known metal carrier after being loaded with a noble metal such as platinum, palladium or rhodium for purifying exhaust gas, and then attached to an exhaust system of an automobile, for example. It Since the metal carrier undergoes a drastic temperature change at the same location, a large temperature difference occurs in the radial direction, and the outer cylinder 6 exerts a strong compressive tensile force on the honeycomb body 4.

【0025】ハニカム体4は熱膨張により、中間体5を
介して外筒6に押し付けられるが、1回目の熱膨張によ
り、ハニカム体4は外層が若干押し潰され外径が小さく
なり、以降の熱膨張では圧縮応力は殆ど作用しなくな
る。一方熱収縮による引張り力は、熱膨張と熱収縮が熱
サイクル毎に繰り返され発生する。しかし、内部の層が
接合されていない中間体5が配設されているので、変形
が吸収されハニカム体4に発生する応力が大幅に低減さ
れる。さらに同中間体5の非接合層により、外筒と断熱
されるため、ハニカム体に発生する温度分布が改善さ
れ、耐久性が向上する。次に本発明の実施例について述
べる。
The honeycomb body 4 is pressed against the outer cylinder 6 through the intermediate body 5 by thermal expansion, but the first thermal expansion causes the outer layer of the honeycomb body 4 to be slightly crushed to reduce the outer diameter. The thermal expansion causes almost no compressive stress. On the other hand, the tensile force due to thermal contraction is generated by repeating thermal expansion and thermal contraction in each thermal cycle. However, since the intermediate body 5 in which the inner layers are not joined is arranged, the deformation is absorbed and the stress generated in the honeycomb body 4 is significantly reduced. Furthermore, since the non-bonding layer of the intermediate body 5 is thermally insulated from the outer cylinder, the temperature distribution generated in the honeycomb body is improved and the durability is improved. Next, examples of the present invention will be described.

【0026】[0026]

【実施例】図3に本発明の実施例のメタル担体Aを示
す。横断面の接合構造を図7に示す。外筒6は19Cr
−0.4Nbを合金成分とするフェライト系ステンレス
鋼で、外径は100mm、長さは110mm、厚さは1.5
mmである。ハニカム体4は20Cr−5Aを合金成分と
するフェライト系ステンレス鋼で、外径は96.4で、
厚さ50μmの平箔4と波箔5で構成されている。ハニ
カム体4のセル密度は、400セル/平方インチであ
る。中間体5は20Cr−5Alを合金成分とするフィ
ライト系ステンレンス鋼で、その長さは100mmで、2
回カールされ外径は97mmで、その厚さは150μmで
ある。
EXAMPLE FIG. 3 shows a metal carrier A according to an example of the present invention. The junction structure of the cross section is shown in FIG. Outer cylinder 6 is 19Cr
A ferritic stainless steel containing -0.4 Nb as an alloy component, with an outer diameter of 100 mm, a length of 110 mm, and a thickness of 1.5.
mm. The honeycomb body 4 is a ferritic stainless steel having an alloy component of 20Cr-5A and an outer diameter of 96.4.
It is composed of a flat foil 4 and a corrugated foil 5 having a thickness of 50 μm. The cell density of the honeycomb body 4 is 400 cells / square inch. Intermediate 5 is a phyllite stainless steel containing 20Cr-5Al as an alloy component, and its length is 100 mm.
It is curled once and has an outer diameter of 97 mm and a thickness of 150 μm.

【0027】またハニカム体4の内部の接合はロウ付け
あるいは拡散接合により、ハニカム体4と中間体5の接
合および中間体5と外筒6の接合は、Niを主成分とす
るNiロウ材で接合されている。
The inside of the honeycomb body 4 is joined by brazing or diffusion joining. The joining of the honeycomb body 4 and the intermediate body 5 and the joining of the intermediate body 5 and the outer cylinder 6 are made of Ni brazing material containing Ni as a main component. It is joined.

【0028】図4は本発明の別の実施例のメタル担体B
を示す。その横断面の接合構造を図7に示す。外筒6、
ハニカム体4および中間体5の材質、寸法および接合方
法はメタル担体Aと同じである。ハニカム体4と中間体
5は担体入側端面から50mmの範囲を、また中間体5と
外筒6は担体中央から出側端面までの50mmの範囲をロ
ウ材で接合している。
FIG. 4 shows a metal carrier B according to another embodiment of the present invention.
Indicates. The junction structure of the cross section is shown in FIG. Outer cylinder 6,
The material, dimensions and joining method of the honeycomb body 4 and the intermediate body 5 are the same as those of the metal carrier A. The honeycomb body 4 and the intermediate body 5 are joined with a brazing filler metal within a range of 50 mm from the carrier entrance side end face, and the intermediate body 5 and the outer cylinder 6 are joined with a brazing filler metal within a range of 50 mm from the carrier center to the exit side end face.

【0029】図5は本発明の別の実施例のメタル担体C
を示す。その横断面の接合構造は図7に示す。外筒6、
長さが50mmとなった以外は中間体5も、ハニカム体4
の材質、寸法および接合方法はメタル担体Aと同じであ
る。中間体5はメタル担体の中央より出側に配置され、
ハニカム体4と中間体5は軸方向に全長、中間体5と外
筒6は軸方向に全長ロウ付けされている。
FIG. 5 shows a metal carrier C according to another embodiment of the present invention.
Indicates. The junction structure of the cross section is shown in FIG. Outer cylinder 6,
The intermediate body 5 and the honeycomb body 4 are the same except that the length is 50 mm.
The material, dimensions, and joining method of are the same as those of the metal carrier A. The intermediate body 5 is arranged on the exit side from the center of the metal carrier,
The honeycomb body 4 and the intermediate body 5 are brazed in the entire length in the axial direction, and the intermediate body 5 and the outer cylinder 6 are brazed in the entire length in the axial direction.

【0030】図6は本発明の別の実施例のメタル担体D
を示す。その横断面の接合構造は図7に示す。外筒6、
中間体5、ハニカム体4も長さが50mmとなった以外は
材質、寸法および接合方法はメタル担体Aと同じであ
る。ハニカム体4は担体の入側に配置され、ハニカム体
4と中間体5は軸方向に全長、中間体5と外筒6は軸方
向に全長ロウ付けされている。
FIG. 6 shows a metal carrier D according to another embodiment of the present invention.
Indicates. The junction structure of the cross section is shown in FIG. Outer cylinder 6,
The material, dimensions, and joining method of the intermediate body 5 and the honeycomb body 4 are the same as those of the metal carrier A, except that the length is 50 mm. The honeycomb body 4 is arranged on the inlet side of the carrier, the honeycomb body 4 and the intermediate body 5 are brazed in the entire length in the axial direction, and the intermediate body 5 and the outer cylinder 6 are brazed in the entire length in the axial direction.

【0031】図11は、本発明のメタル担体と比較する
ための公知のメタル担体Eである。メタル担体各部の寸
法、材質は同じであるが、ハニカム体4の外径は、中間
体がないため、97mmである。ハニカム体10の内部は
斜線の範囲がロウ付けで接合されている。ハニカム体1
0と外筒6は、メタル担体の出側近傍の点で示される範
囲の部位11でロウ付けされており、温度変化の大きい
排気ガスによる半径方向および軸方向の熱膨張収縮に対
して、自由に変形できるので、ハニカム体10と外筒6
の間に大きい熱応力が発生することは殆どなく、高い耐
久性が確保される。しかし、ハニカム体10内部の接合
を、図のようにパターン化するには複雑な製造工程が必
要で、製造コストが掛かる問題がある。
FIG. 11 shows a known metal carrier E for comparison with the metal carrier of the present invention. The dimensions and material of each part of the metal carrier are the same, but the outer diameter of the honeycomb body 4 is 97 mm because there is no intermediate body. The inside of the honeycomb body 10 is joined by brazing in the shaded area. Honeycomb body 1
0 and the outer cylinder 6 are brazed at a portion 11 in the range indicated by a point near the exit side of the metal carrier, and are free from thermal expansion and contraction in the radial direction and the axial direction due to exhaust gas having a large temperature change. Since it can be transformed into a honeycomb body 10 and an outer cylinder 6
A large thermal stress is hardly generated between the two, and high durability is secured. However, in order to pattern the bonding inside the honeycomb body 10 as shown in the figure, a complicated manufacturing process is required, and there is a problem that the manufacturing cost is increased.

【0032】図12は、本発明のメタル担体と比較する
ための公知のメタル担体Fである。外筒6、ハニカム体
4、中間体12の材質は同じである。外筒6のサイズは
メタル担体Aと同じであるが、中間体12は厚さは15
0μmであるが、ハニカム体4の周りを一周しているの
みである。ハニカム体4の内部は同様に斜線を施してい
る範囲を拡散接合あるいはロウ付けで全体接合されてい
るが、ハニカム体4と中間体12は担体の入側近傍部1
3で、中間体11と外筒6は出側近傍部14で接合され
ている。排気ガスの温度変化による、メタル担体Fのハ
ニカム体4の半径方向の熱膨張収縮を、中間体12の撓
みで逃げる構造となっている。
FIG. 12 shows a known metal carrier F for comparison with the metal carrier of the present invention. The outer cylinder 6, the honeycomb body 4, and the intermediate body 12 are made of the same material. The outer cylinder 6 has the same size as the metal carrier A, but the intermediate body 12 has a thickness of 15
Although it is 0 μm, it only makes one round around the honeycomb body 4. Similarly, the inside of the honeycomb body 4 is entirely joined by diffusion joining or brazing in the shaded area.
In FIG. 3, the intermediate body 11 and the outer cylinder 6 are joined at the outlet-side vicinity portion 14. The structure is such that the thermal expansion and contraction in the radial direction of the honeycomb body 4 of the metal carrier F due to the temperature change of the exhaust gas escapes by the bending of the intermediate body 12.

【0033】これらの各種メタル担体の製造コストを相
対比較すると共に、耐久性を評価するため排気量200
0ccの、4サイクルエンジンの出側に取付け、図13の
ような熱サイクル試験を実施した。同図で縦軸は温度、
横軸は時間を表し、測温はメタル担体の上流側端面から
20mmの位置で行い、Temp1 =150℃、Temp2 =90
0℃、T1 =10min 、T2 =10min である。達成す
べき試験サイクル数は、1000サイクルであるが、耐
久性を相対評価するため試験サイクル数を1500サイ
クルまで延長し評価した。
To compare the manufacturing costs of these various metal carriers relative to each other and to evaluate the durability, the displacement of 200
A 0 cc 4-cycle engine was mounted on the outlet side and a thermal cycle test as shown in FIG. 13 was performed. In the figure, the vertical axis is temperature,
The horizontal axis represents time, and the temperature was measured at a position 20 mm from the upstream end surface of the metal carrier, Temp1 = 150 ° C, Temp2 = 90
0 ° C., T1 = 10 min, T2 = 10 min. The number of test cycles to be achieved is 1000, but in order to relatively evaluate durability, the number of test cycles was extended to 1500 and evaluated.

【0034】その製造コスト比較と耐久試験結果を表1
に示す。外筒からハニカム体が外れるまでのサイクル数
を示す。なお、判定は1000サイクル耐えれば合格と
した。
The production cost comparison and the durability test result are shown in Table 1.
Shown in The number of cycles until the honeycomb body is removed from the outer cylinder is shown. In addition, the judgment was passed if it survived 1000 cycles.

【0035】[0035]

【表1】 [Table 1]

【0036】以上のように、本発明の各種メタル担体お
よび比較の従来の各種メタル担体は何れも、耐久試験に
合格したが、従来のメタル担体Fは中間体の変形自由度
が不足し相対的に耐久度が低い。またメタル担体Eは良
好な耐久性を示したが、製造プロセスが複雑なため、製
造コストが高くなる短所がある。それに比べ本発明のメ
タル担体A〜Dは、耐久性および製造コストのバランス
がとれ、従来のメタル担体より総合的に優秀である。
As described above, each of the various metal carriers of the present invention and the conventional various metal carriers for comparison passed the endurance test. The durability is low. Further, although the metal carrier E showed good durability, it has a disadvantage that the manufacturing cost becomes high because the manufacturing process is complicated. On the other hand, the metal carriers A to D of the present invention have a good balance of durability and manufacturing cost and are generally superior to the conventional metal carriers.

【0037】[0037]

【発明の効果】以上説明したように、本発明によれば、
メタル担体の構造を合理化することにより、低コストで
耐久性の優れたメタル担体を供給できることが判明し
た。
As described above, according to the present invention,
It was found that by rationalizing the structure of the metal carrier, it is possible to supply a metal carrier that is low in cost and excellent in durability.

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

【図1】本発明のメタル担体の外観を示す斜視図。FIG. 1 is a perspective view showing the appearance of a metal carrier of the present invention.

【図2】本発明のメタル担体の各構成要素の一例を示す
外観斜視図。
FIG. 2 is an external perspective view showing an example of each component of the metal carrier of the present invention.

【図3】本発明の実施例(メタル担体A)を示す断面
図。
FIG. 3 is a sectional view showing an embodiment (metal carrier A) of the present invention.

【図4】本発明の実施例(メタル担体B)を示す断面
図。
FIG. 4 is a sectional view showing an embodiment (metal carrier B) of the present invention.

【図5】本発明の実施例(メタル担体C)を示す断面
図。
FIG. 5 is a sectional view showing an embodiment (metal carrier C) of the present invention.

【図6】本発明の実施例(メタル担体D)を示す断面
図。
FIG. 6 is a sectional view showing an embodiment (metal carrier D) of the present invention.

【図7】本発明の実施例を示すメタル担体の横断面図。FIG. 7 is a cross-sectional view of a metal carrier showing an example of the present invention.

【図8】本発明の実施例を示すメタル担体の横断面図。FIG. 8 is a cross-sectional view of a metal carrier showing an embodiment of the present invention.

【図9】本発明の実施例を示すメタル担体の横断面図。FIG. 9 is a cross-sectional view of a metal carrier showing an embodiment of the present invention.

【図10】本発明の実施例を示すメタル担体の横断面
図。
FIG. 10 is a cross-sectional view of a metal carrier showing an example of the present invention.

【図11】本発明のメタル担体と比較するための公知の
メタル担体Eの縦断面図。
FIG. 11 is a vertical sectional view of a known metal carrier E for comparison with the metal carrier of the present invention.

【図12】本発明のメタル担体と比較するための公知の
メタル担体Fの縦断面図。
FIG. 12 is a longitudinal sectional view of a known metal carrier F for comparison with the metal carrier of the present invention.

【図13】各種メタル担体の耐久性を評価するための熱
サイクルパターンを示す図。
FIG. 13 is a diagram showing a thermal cycle pattern for evaluating durability of various metal carriers.

【符号の説明】[Explanation of symbols]

1 メタル担体 2 平箔 3 波箔 4 ハニカム体 5 中間体 6 外筒 7 ハニカム体と中間体との接合部 8 中間体と外筒の接合部 9 中間体の非接合部 10 接合部位をパターン化したハニカム体 11 ハニカム体と外筒の接合部 12 中間体 13 ハニカム体と中間体の接合部 14 中間体と外筒の接合部 DESCRIPTION OF SYMBOLS 1 Metal carrier 2 Flat foil 3 Corrugated foil 4 Honeycomb body 5 Intermediate body 6 Outer cylinder 7 Joining part between honeycomb body and intermediate body 8 Joining part between intermediate body and outer cylinder 9 Non-bonding part of intermediate body 10 Patterning bonding part Formed honeycomb body 11 joined portion between honeycomb body and outer cylinder 12 intermediate body 13 joined portion between honeycomb body and intermediate body 14 joined portion between intermediate body and outer cylinder

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】 平箔と波箔を交互に巻回あるいは積層し
たハニカム体を形成した後、その外側に箔と同じあるい
はそれよりも厚い薄板を2回以上巻回して中間体を形成
し、その中間体の内面とハニカム対外面とは連続的ある
いは間欠的に一周、中間体の外面においては外筒と一周
以内接合し、さらに中間体内部においては一周以上の非
接合層を設けたことを特徴とするメタル担体。
1. After forming a honeycomb body in which flat foil and corrugated foil are alternately wound or laminated, a thin plate which is the same as or thicker than the foil is wound two or more times on the outside thereof to form an intermediate body, The inner surface of the intermediate body and the honeycomb-to-outer surface are continuously or intermittently made one round, the outer surface of the intermediate body is joined to the outer cylinder within one round, and further, at least one round of non-bonding layer is provided inside the intermediate body. Characteristic metal carrier.
【請求項2】 ハニカム体内部を全体接合したことを特
徴とする請求項1記載のメタル担体。
2. The metal carrier according to claim 1, wherein the entire inside of the honeycomb body is joined.
【請求項3】 中間体をコルゲート加工していない平板
とすることを特徴とする請求項1あるいは2記載のメタ
ル担体。
3. The metal carrier according to claim 1, wherein the intermediate body is a flat plate that is not corrugated.
【請求項4】 中間体をコルゲート加工した波板とする
ことを特徴とする請求項1から3の何れかに記載のメタ
ル担体。
4. The metal carrier according to claim 1, wherein the intermediate is a corrugated corrugated plate.
【請求項5】 中間体とハニカム体は上流側で、中間体
と外筒とは下流側で接合することを特徴とする請求項1
から4の何れかに記載のメタル担体。
5. The intermediate body and the honeycomb body are bonded on the upstream side, and the intermediate body and the outer cylinder are bonded on the downstream side.
The metal carrier according to any one of 1 to 4.
JP07685395A 1995-03-31 1995-03-31 Metal carrier Expired - Fee Related JP3667811B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP07685395A JP3667811B2 (en) 1995-03-31 1995-03-31 Metal carrier

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP07685395A JP3667811B2 (en) 1995-03-31 1995-03-31 Metal carrier

Publications (2)

Publication Number Publication Date
JPH08266905A true JPH08266905A (en) 1996-10-15
JP3667811B2 JP3667811B2 (en) 2005-07-06

Family

ID=13617219

Family Applications (1)

Application Number Title Priority Date Filing Date
JP07685395A Expired - Fee Related JP3667811B2 (en) 1995-03-31 1995-03-31 Metal carrier

Country Status (1)

Country Link
JP (1) JP3667811B2 (en)

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* Cited by examiner, † Cited by third party
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US6267932B1 (en) * 1997-03-21 2001-07-31 Kemira Metalkat Oy Catalytic reactors
CN1096542C (en) * 1997-03-21 2002-12-18 凯米拉梅塔尔卡特公司 Improvements in catalytic reactors
EP1329603A1 (en) * 2002-01-10 2003-07-23 Calsonic Kansei Corporation Metal substrate for carrying catalyst and method for manufacturing the same
JP2005522324A (en) * 2002-04-18 2005-07-28 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 Catalyst carrier with corrugated cylinder and manufacturing method thereof
JP2008132497A (en) * 2008-02-14 2008-06-12 Ecocat Oy Improved catalytic reactor
US8661673B2 (en) 2010-09-30 2014-03-04 Tenneco Automotive Operating Company Inc. Method of installing a multi-layer batt, blanket or mat in an exhaust gas aftertreatment or acoustic device

Cited By (9)

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US6267932B1 (en) * 1997-03-21 2001-07-31 Kemira Metalkat Oy Catalytic reactors
CN1096542C (en) * 1997-03-21 2002-12-18 凯米拉梅塔尔卡特公司 Improvements in catalytic reactors
EP1329603A1 (en) * 2002-01-10 2003-07-23 Calsonic Kansei Corporation Metal substrate for carrying catalyst and method for manufacturing the same
US6821639B2 (en) * 2002-01-10 2004-11-23 Calsonic Kansei Corporation Metal substrate for carrying catalyst and method for manufacturing the same
JP2005522324A (en) * 2002-04-18 2005-07-28 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 Catalyst carrier with corrugated cylinder and manufacturing method thereof
JP4751021B2 (en) * 2002-04-18 2011-08-17 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 Catalyst carrier with corrugated cylinder and manufacturing method thereof
JP2008132497A (en) * 2008-02-14 2008-06-12 Ecocat Oy Improved catalytic reactor
US8661673B2 (en) 2010-09-30 2014-03-04 Tenneco Automotive Operating Company Inc. Method of installing a multi-layer batt, blanket or mat in an exhaust gas aftertreatment or acoustic device
US8752290B2 (en) 2010-09-30 2014-06-17 Tenneco Automotive Operating Company Inc. Method of installing a longitudinally offset multi-layer mat in an exhaust gas aftertreatment or acoustic device

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