JPH07268476A - Cooling method after joining heat treatment for metal honeycomb structure - Google Patents

Cooling method after joining heat treatment for metal honeycomb structure

Info

Publication number
JPH07268476A
JPH07268476A JP6517994A JP6517994A JPH07268476A JP H07268476 A JPH07268476 A JP H07268476A JP 6517994 A JP6517994 A JP 6517994A JP 6517994 A JP6517994 A JP 6517994A JP H07268476 A JPH07268476 A JP H07268476A
Authority
JP
Japan
Prior art keywords
heat treatment
cooling
honeycomb
temperature
honeycomb structure
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
JP6517994A
Other languages
Japanese (ja)
Other versions
JP3498994B2 (en
Inventor
Mikio Yamanaka
幹雄 山中
Masuhiro Fukaya
益啓 深谷
Yasushi Ishikawa
泰 石川
Hitoshi Ota
仁史 太田
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 JP06517994A priority Critical patent/JP3498994B2/en
Publication of JPH07268476A publication Critical patent/JPH07268476A/en
Application granted granted Critical
Publication of JP3498994B2 publication Critical patent/JP3498994B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Pressure Welding/Diffusion-Bonding (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

PURPOSE:To secure both the material and productivity of a honeycomb by joining heat treatment for a honeycomb product. CONSTITUTION:In a cooling stage after heat treatment for joining a honeycomb structure constituted of the thin steel or foil of a ferritic stainless steel in which a gamma phase is formed at a high temp., cooling is executed for >=7min from 850 to 700 deg.C, or soaking is executed for >=2min from 800 to 700 deg.C. Thus, joining heat treatment with high productivity can be executed to a honeycomb while its good material is maintained without forming a martensitic phase thereon.

Description

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

【0001】[0001]

【産業上の利用分野】本発明は熱交換器や自動車触媒用
に供せられるメタルハニカム構造体の製造方法に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for manufacturing a metal honeycomb structure used for heat exchangers and automobile catalysts.

【0002】[0002]

【従来の技術】近年、熱交換器や自動車排気ガス浄化用
の触媒装置として、耐熱金属からなる平板と波板を交互
に積層し、あるいは巻回したハニカム体を外筒に収納し
たものが種々開発され、既に一部実用化されている。そ
して前記平板と波板間、およびハニカム体外周面と外筒
内表面との接合手段としては、特開昭61−19057
4号公報などに記載のろう付け、特開昭64−4018
0号公報の記載にある抵抗溶接、特開昭54−1346
2号公報の記載にあるレーザービーム溶接や電子ビーム
溶接、米国特許第4300956号明細書や特開平1−
270947号公報の記載に示されている拡散接合が一
般的である。
2. Description of the Related Art In recent years, there have been various heat exchangers and catalyst devices for purifying exhaust gas from automobiles, in which flat plates made of heat-resistant metal and corrugated plates are alternately laminated or wound, and a honeycomb body is housed in an outer cylinder. It has been developed and has already been partially put into practical use. Further, as a joining means between the flat plate and the corrugated plate and between the outer peripheral surface of the honeycomb body and the inner surface of the outer cylinder, there is disclosed in JP-A-61-19057.
Brazing described in Japanese Patent Laid-Open No. 4-4018
Resistance welding described in Japanese Patent Laid-Open No. 0-134346.
Laser beam welding and electron beam welding described in Japanese Patent No. 2300952, U.S. Pat.
The diffusion bonding shown in the description of Japanese Patent No. 270947 is common.

【0003】また耐熱金属材料としては特公昭58−2
3138号公報、特公昭54−15035号公報、特開
昭56−96726号公報などに開示されている耐酸化
性の優れたFe−Cr−Al系合金箔が使われてきた。
これらのFe−Cr−Al系合金鋼はその製造性に難が
あって一般的に高価なものになるため、特に高度の耐熱
性が要求される環境以外で使用されるものについては、
より低廉なCr系又はCr−Si系のステンレス鋼が使
用され始めている。本発明者らは先にCr−Si系のス
テンレス鋼を用いて拡散接合によりハニカム体を得る技
術を特願平05−24517号公報で提案したところで
ある。
As a heat-resistant metal material, Japanese Patent Publication No. 58-2
Fe-Cr-Al alloy foils having excellent oxidation resistance, which are disclosed in Japanese Patent No. 3138, Japanese Patent Publication No. 54-15035, Japanese Patent Laid-Open No. 56-96726, etc., have been used.
Since these Fe-Cr-Al alloy steels are difficult to manufacture and generally expensive, for those used in environments other than those requiring high heat resistance,
The cheaper Cr-based or Cr-Si-based stainless steels are beginning to be used. The present inventors have previously proposed a technique for obtaining a honeycomb body by diffusion bonding using Cr—Si type stainless steel in Japanese Patent Application No. 05-24517.

【0004】これらハニカム体に用いられるステンレス
鋼はろう付けや拡散接合のための熱処理で1000℃以
上の温度に加熱されるが、低廉型材料であるCr系〜C
r−Si系の耐熱ステンレス鋼ではこの温度領域でα−
γの二相組織になるものがある。これらの接合は通常工
程費のかさむ真空炉を使って行われるが、製造能率を上
げるため接合が終了した後は真空炉内にHe,Ar,N
2 などの冷却ガスを導入して急冷される。
The stainless steel used for these honeycomb bodies is heated to a temperature of 1000 ° C. or higher by a heat treatment for brazing or diffusion bonding, but it is a low-cost material such as Cr-C.
In the temperature range of r-Si heat-resistant stainless steel, α-
Some have a two-phase structure of γ. These joinings are usually performed using a vacuum furnace, which requires a high process cost, but after the joining is completed, He, Ar, and N are placed in the vacuum furnace to increase manufacturing efficiency.
It is cooled rapidly by introducing cooling gas such as 2 .

【0005】前記の高温で二相組織になる材料で構成さ
れたハニカム構造体を真空炉で急冷するとその金属組織
はマルテンサイト相を含むものになり、ハニカム構造体
は硬くて脆いものになり、後工程でわずかな機械的な変
形を加えても亀裂の発生をみる等の不具合が生じる。こ
れを避けるために接合温度から徐冷をすると冷却に時間
がかゝり生産性を損う。
When a honeycomb structure made of the above-mentioned material having a two-phase structure at a high temperature is rapidly cooled in a vacuum furnace, its metal structure contains a martensite phase, and the honeycomb structure becomes hard and brittle. Even if a slight mechanical deformation is applied in the subsequent process, defects such as cracks will occur. In order to avoid this, if cooling is gradually performed from the bonding temperature, it takes time to cool and the productivity is impaired.

【0006】[0006]

【発明が解決しようとする課題】本発明は上記のような
接合熱処理後の冷却過程において材質上有害なマルテン
サイト相を発生させることなく、しかも冷却時間をそれ
ほど長くしない能率の良い冷却方法を提供するものであ
る。
DISCLOSURE OF THE INVENTION The present invention provides an efficient cooling method which does not generate a martensite phase harmful to the material in the cooling process after the above-mentioned joining heat treatment and does not prolong the cooling time so much. To do.

【0007】[0007]

【課題を解決するための手段】上記の課題を解決するた
めになされた本発明は、高温でγ相を生じるフェライト
系ステンレス鋼の薄板ないし箔よりなるハニカム構造体
を接合するための熱処理後の冷却過程において850℃
の温度から700℃の温度までの間を7分以上かけて冷
却することを特徴とするハニカム構造体の冷却方法であ
る。そして実際の熱処理炉に於いて大量のハニカム構造
体にこの処理をより確実に行わしめる方法として、該冷
却過程の800〜700℃の間に2分以上の保定を行う
均熱処理を施すことが有効で、この温度間以外の温度に
おいては導入ガスによる急冷を行ってよい。
DISCLOSURE OF THE INVENTION The present invention made to solve the above-mentioned problems is to provide a structure after a heat treatment for joining a honeycomb structure made of a ferritic stainless steel thin plate or foil that produces a γ phase at high temperature. 850 ℃ in the cooling process
The method for cooling a honeycomb structure is characterized in that the cooling from the temperature of 1 to the temperature of 700 ° C. is performed over 7 minutes or more. Then, as a method for more reliably performing this treatment on a large amount of honeycomb structures in an actual heat treatment furnace, it is effective to carry out soaking for 2 minutes or more during the cooling process at 800 to 700 ° C. Then, at a temperature other than this temperature, quenching with the introduced gas may be performed.

【0008】このように冷却することにより、ろう付け
や拡散接合のための1000℃以上の高温で生じたγ相
は850℃から700℃の間にα相とCr炭化物に全て
分解するため、この後Ms点以下の温度にまでやゝ大き
な速度で冷却されてもマルテンサイト相を生じることな
く、メタルハニカムの脆化は避けられる。こゝで850
℃から700℃までの間を緩冷却するように選んだ理由
は、850℃超ではγ相がα相とCr炭化物へ変態する
駆動力が弱くて変態に長時間を要し、また700℃未満
では原子振動が不活発になり、平衡状態であるα+炭化
物への移行に時間がかゝるようになるからである。
By cooling in this way, the γ phase generated at a high temperature of 1000 ° C. or higher for brazing and diffusion bonding is completely decomposed into α phase and Cr carbide between 850 ° C. and 700 ° C. Even if the steel is cooled to a temperature below the Ms point at a high speed, a martensite phase does not occur, and brittleness of the metal honeycomb can be avoided. 850 here
The reason why we chose to cool slowly between ℃ and 700 ℃ is that if the temperature exceeds 850 ℃, the driving force to transform the γ phase into α phase and Cr carbide is weak and it takes a long time to transform. Then, atomic vibration becomes inactive, and it takes time to transfer to α + carbide which is in the equilibrium state.

【0009】また、上記温度範囲の降温時間を7分以上
にしたのは確実にγ相をα相とCr炭化物に分解するた
めであり、上限は特に定めないが、1時間以内とするこ
とが能率上好ましい。また、上記温度範囲内の所定温度
に2分以上保定する均熱処理を施すことで上記と同様の
効果を得ることができるが、その上限の時間は能率上1
時間以内とすることが好ましい。
Further, the reason why the temperature lowering time in the above temperature range is set to 7 minutes or more is to surely decompose the γ phase into the α phase and the Cr carbide, and the upper limit is not particularly specified, but it may be within 1 hour. It is preferable for efficiency. Further, the same effect as described above can be obtained by performing soaking for holding at a predetermined temperature within the above temperature range for 2 minutes or more, but the upper limit time is 1 for efficiency.
It is preferably within the time.

【0010】次に実施例により、本発明の具体例を説明
する。
Next, specific examples of the present invention will be described with reference to examples.

【0011】[0011]

【実施例】【Example】

実施例1 表1に化学組成を示したステンレス鋼の50μm厚の箔
を作成し、平箔とこれをコルゲート加工したものを重ね
合せたものを巻回し100φ×90lのハニカムを形成
した。これを19%Cr鋼の1.5tの厚さの外筒に圧
入し、ハニカム同士とハニカムと外筒間を拡散接合する
ために真空中で1200℃に加熱し、40分間均熱した
後に冷却した。冷却はArガスを真空炉に流入させ、温
度の上ったガスを炉外に設けたガス冷却装置に導いて再
度真空炉にガスをもどすことによりガスを循環させて行
った。ここで1200℃から850℃までは11分かけ
て冷却し、850℃から700℃までの温度域は冷却ガ
スの流量を減らして表2に示す各時間で冷却し、700
℃からは再度冷却ガス流量を多くして150℃まで23
分で冷却し、大気中に取り出した。取り出したハニカム
を切断して樹脂にうめ込み研磨して金属組織を観察し、
マルテンサイト相の有無を調べ、結果を表2に示した。
表2に示すように850℃から700℃までを7分以上
かけて冷却したものではマルテンサイト相はなく、7分
未満の時間で冷却したものにはマルテンサイト相が認め
られた。またマルテンサイト相の生じた試料No. Aのハ
ニカムと生じなかった試料No. Eのハニカムを機械的な
押し出し試験により強制的にハニカム中央を押して外筒
から押し出したところ、試料No. Aのハニカムは脆性破
壊を示し、試料No. Eのものは延性破壊を示した。
Example 1 A stainless steel foil having a chemical composition shown in Table 1 and having a thickness of 50 μm was prepared, and a flat foil and a corrugated flat foil were superposed and wound to form a 100φ × 90 l honeycomb. This was press-fitted into an outer cylinder of 19% Cr steel having a thickness of 1.5 tons, heated to 1200 ° C. in vacuum for diffusion bonding between the honeycombs and between the honeycomb and the outer cylinder, soaked for 40 minutes, and then cooled. did. Cooling was performed by flowing Ar gas into a vacuum furnace, introducing a gas whose temperature had risen to a gas cooling device provided outside the furnace, and returning the gas to the vacuum furnace again to circulate the gas. Here, 1200 ° C. to 850 ° C. is cooled over 11 minutes, and in the temperature range from 850 ° C. to 700 ° C., the flow rate of the cooling gas is reduced and cooling is performed at each time shown in Table 2.
From ℃, increase the cooling gas flow rate again to 150 ℃ 23
It was cooled in minutes and taken out into the atmosphere. The honeycomb taken out is cut, embedded in resin and polished to observe the metal structure,
The presence or absence of a martensite phase was examined, and the results are shown in Table 2.
As shown in Table 2, there was no martensite phase in the one cooled from 850 ° C to 700 ° C over 7 minutes, and the martensite phase was recognized in the one cooled in less than 7 minutes. When the honeycomb of sample No. A in which the martensite phase was generated and the honeycomb of sample No. E in which the martensite phase was not generated were forced out of the outer cylinder by forcibly pushing the center of the honeycomb by a mechanical extrusion test, the honeycomb of sample No. A was found. Indicates brittle fracture, and sample No. E exhibits ductile fracture.

【0012】[0012]

【表1】 [Table 1]

【0013】[0013]

【表2】 [Table 2]

【0014】実施例2 実施例1と同じく平箔とコルゲート箔を重ね合わせたも
のを巻回し、19Cr鋼の外筒に挿入したものを多数作
成して、大量の担体の熱処理試験を行った。大型の真空
熱処理炉を用い、60ケづつの担体をトレイに並べてこ
れを4段重ねにして合計240ケの担体を真空中で12
00℃に加熱し、60分間均熱した。その後Arガスに
より表3に示す各温度まで急冷を行い、各温度で1分、
2分、5分間の均熱を行った後再度急冷した。各条件で
熱処理した担体を各トレイから5ケづつ取り出して前記
の機械的な押し出し試験を行い、脆性破壊の有無を調べ
た。それらの結果は表3に示す通り800℃、750
℃、700℃で2分以上均熱したものが延性破壊を示
し、他のものは脆性破壊を示した。
Example 2 Similar to Example 1, a flat foil and a corrugated foil were superposed and wound, and a large number of them were inserted into an outer cylinder of 19Cr steel, and a large amount of carriers were subjected to a heat treatment test. Using a large-sized vacuum heat treatment furnace, 60 carriers are arranged in a tray and these are stacked in 4 layers to make a total of 240 carriers in a vacuum.
It heated at 00 degreeC and soaked for 60 minutes. After that, it was rapidly cooled to each temperature shown in Table 3 by Ar gas, and at each temperature for 1 minute,
After soaking for 2 minutes and 5 minutes, it was rapidly cooled again. Five pieces of the carrier heat-treated under each condition were taken out from each tray and the above mechanical extrusion test was performed to examine the presence or absence of brittle fracture. The results are shown in Table 3 at 800 ° C. and 750
Those that were soaked at ℃ and 700 ℃ for 2 minutes or more showed ductile fracture, and others showed brittle fracture.

【0015】[0015]

【表3】 [Table 3]

【0016】[0016]

【発明の効果】以上の実施例が示す通り、本発明方法は
高温でγ相を生じるメタルハニカムの接合の熱処理後の
冷却において、850〜700℃の間のみを緩冷却又は
800〜700℃で短時間の均熱を行うことにより、他
の温度域では急冷してもマルテンサイト相を生じること
なく、冷却時間を短かくすることを可能ならしめ、生産
性の高いメタルハニカムの製造法を提供することができ
る。
As shown in the above examples, in the method of the present invention, in the cooling after the heat treatment of the joining of the metal honeycombs that produce the γ phase at a high temperature, the cooling is performed only between 850 and 700 ° C or at 800 to 700 ° C. By performing soaking for a short time, it is possible to shorten the cooling time without producing a martensite phase even in rapid cooling in other temperature ranges, and to provide a highly productive method for manufacturing metal honeycombs. can do.

フロントページの続き (72)発明者 太田 仁史 愛知県東海市東海町5−3 新日本製鐵株 式会社名古屋製鐵所内Front Page Continuation (72) Inventor Hitoshi Ota 5-3 Tokai-cho, Tokai-shi, Aichi Nippon Steel Co., Ltd. Nagoya Steel Works

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 高温でγ相を生じるフェライト系ステン
レス鋼の薄板ないし箔よりなるハニカム構造体を接合す
るための熱処理を施した後、該熱処理温度から冷却する
過程において、850℃の温度から700℃の温度まで
の間を7分以上かけて冷却することを特徴とするハニカ
ム構造体の冷却方法。
1. A heat treatment for joining a honeycomb structure made of a ferritic stainless steel thin plate or foil which produces a γ phase at a high temperature, and then cooling from the heat treatment temperature, at a temperature of 850 ° C. to 700 ° C. A method for cooling a honeycomb structure, comprising cooling to a temperature of ° C over 7 minutes or more.
【請求項2】 800℃の温度から700℃の温度まで
の間に2分以上の均熱処理を施すことを特徴とする請求
項1に記載の冷却方法。
2. The cooling method according to claim 1, wherein a soaking treatment is performed for 2 minutes or more between a temperature of 800 ° C. and a temperature of 700 ° C.
JP06517994A 1994-04-01 1994-04-01 Cooling method after bonding heat treatment of metal honeycomb structure Expired - Lifetime JP3498994B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP06517994A JP3498994B2 (en) 1994-04-01 1994-04-01 Cooling method after bonding heat treatment of metal honeycomb structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP06517994A JP3498994B2 (en) 1994-04-01 1994-04-01 Cooling method after bonding heat treatment of metal honeycomb structure

Publications (2)

Publication Number Publication Date
JPH07268476A true JPH07268476A (en) 1995-10-17
JP3498994B2 JP3498994B2 (en) 2004-02-23

Family

ID=13279433

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JP3498994B2 (en)

Also Published As

Publication number Publication date
JP3498994B2 (en) 2004-02-23

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