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JP2006239580A - Method for manufacturing metallic carrier - Google Patents

Method for manufacturing metallic carrier Download PDF

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JP2006239580A
JP2006239580A JP2005059240A JP2005059240A JP2006239580A JP 2006239580 A JP2006239580 A JP 2006239580A JP 2005059240 A JP2005059240 A JP 2005059240A JP 2005059240 A JP2005059240 A JP 2005059240A JP 2006239580 A JP2006239580 A JP 2006239580A
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core
winding
core part
flat plate
manufacturing
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Japanese (ja)
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Tamotsu Sugimoto
保 杉本
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Marelli Corp
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Calsonic Kansei Corp
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a method for manufacturing a metallic carrier, which comprises the steps of manufacturing a core part having high dimensional accuracy while detecting the time when the winding work of the core part is completed by a simple method without using an advanced arithmetic circuit and press-injecting the manufactured core part into an outer cylinder without enlarging the outer cylinder while leaving no space between the core part and the outer cylinder. <P>SOLUTION: The method for manufacturing the metallic carrier comprises the steps of: manufacturing the core part 4 having a honeycomb structure by winding a long flat plate 1 and a long corrugated plate 2 around a winding core 3 while superimposing the flat plate on the corrugated plate; press-injecting the manufactured core part 4 into the outer cylinder; and joining/integrating the injected core part to/with the outer cylinder. A marker 6 and a mark detector 7 are arranged respectively at a start point and an end point the distance between which is one-fourth length obtained by equally quartering the final peripheral length when the winding work of the core part 4 is completed. A mark 10 is put on the flat plate 1 by the marker 6. The mark 10 is detected by the mark detector 7. A winding angle of the flat plate to the winding core 3 is measured when the mark is detected. When the measured winding angle is smaller than 90°, the winding work is completed. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

本発明は、メタル担体の製造方法に関する。   The present invention relates to a method for producing a metal carrier.

メタル担体は、平板と波板を重ねて巻芯に巻回し、その巻回したコア部の周長が最終周長となった時点で巻き上げ動作を終了し、その後、コア部を外筒に圧入しロウ付け或いは拡散接合して接合一体化することで製造される。   The metal carrier is wound around the core with a flat plate and corrugated plate, and when the circumference of the wound core reaches the final circumference, the winding operation is completed, and then the core is press-fitted into the outer cylinder. It is manufactured by brazing or diffusion bonding and integrating them.

ところで、コア部が外筒よりも大きいと、当該コア部を外筒に挿入することができず、また、コア部が外筒よりも小さすぎると、外筒との接触不良が発生し、接合強度が不十分となる。   By the way, if the core part is larger than the outer cylinder, the core part cannot be inserted into the outer cylinder, and if the core part is too small than the outer cylinder, poor contact with the outer cylinder occurs, and Insufficient strength.

このように、コア部の最終周長は生産性に大きく影響することから、そのコア部の最終周長を制御する方法が従来より提案されている(例えば、特許文献1参照)。   Thus, since the final circumference of a core part has big influence on productivity, the method of controlling the final circumference of the core part is proposed conventionally (for example, refer to patent documents 1).

特許文献1に記載の方法は、コア部の一周を複数に分割して定められた設定回転角に対応して決められたスタートタイミングで、移動される波板素材の山数をそれぞれ計数し、各スタートタイミングに対応して波板素材の山数/設定回転角をそれぞれ演算し、各スタートタイミングに対応して、波板素材の山数/設定回転角と波板素材のピッチを乗算し、コア部の一周分に換算することによりコア部の仮想的な周長変数を算出し、各スタートタイミングに対応するコア部の仮想的な周長変数がコア部の設定周長と同じになったときに波板素材と平板素材とを切断するようにしている。   The method described in Patent Document 1 counts the number of crests of the corrugated material to be moved at each start timing determined in accordance with a set rotation angle determined by dividing the circumference of the core portion into a plurality of parts, Corrugated sheet crest / set rotation angle is calculated corresponding to the start timing, and corrugated sheet crest / setting rotation angle is multiplied by the corrugated sheet pitch corresponding to each start timing. The virtual circumference variable of the core part is calculated by converting to one round, and when the virtual circumference variable of the core part corresponding to each start timing becomes the same as the set circumference of the core part, the corrugated plate The material and the flat material are cut.

要するに、特許文献1に記載の方法は、一定の回転角度で巻き上げた長さを全周分合計し、一定値に達成したときに巻き上げを終了する方法である。
特許第3431040号(第4頁から第7頁、図1、図3及び図4)
In short, the method described in Patent Document 1 is a method of summing up the lengths wound up at a constant rotation angle for the entire circumference, and ending the winding up when reaching a constant value.
Patent No. 3431040 (pages 4 to 7, FIG. 1, FIG. 3 and FIG. 4)

しかしながら、特許文献1に記載の方法では、設定角度での長さを測定し、その都度、長さを積算する高度な演算回路が必要になる。そのため、メタル担体を製造するコストが高くなる。   However, the method described in Patent Document 1 requires an advanced arithmetic circuit that measures the length at a set angle and integrates the length each time. Therefore, the cost for manufacturing the metal carrier increases.

そこで、本発明は、上述の実状に鑑みてなされたものであり、高度な演算回路を必要とすることなく、簡単な方法でコア部の巻き上げ動作終了時を検知して製品寸法精度の高いコア部を製造し、そのコア部を大きすぎること無く且つ隙間なく外筒に圧入し得るメタル担体の製造方法を提供することを目的とする。   Therefore, the present invention has been made in view of the above-described actual situation, and without requiring an advanced arithmetic circuit, a core with high product dimensional accuracy by detecting the end of the winding operation of the core portion by a simple method. An object of the present invention is to provide a method of manufacturing a metal carrier that can be press-fitted into an outer cylinder without producing a core portion and without making the core portion too large.

請求項1に記載の発明は、長尺状の平板と波板を重ねて巻芯に巻回することでハニカム構造のコア部を製造し、そのコア部を外筒に圧入して接合一体化してなるメタル担体の製造方法において、前記コア部を巻き終えたときの最終周長をN分割した1/N長さの開始点と終了点に刻印器と刻印検出器を設置し、前記刻印器で前記平板に刻印を付け、その刻印を前記刻印検出器で検出し、その検出時における前記巻芯の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を終了することを特徴とする。   The invention according to claim 1 is to manufacture a core part of a honeycomb structure by overlapping a long flat plate and a corrugated sheet and winding them around a winding core, and press-fitting the core part into an outer cylinder so as to be joined and integrated. In the metal carrier manufacturing method, a stamper and a stamp detector are installed at the start and end points of 1 / N length obtained by dividing the final circumference when the core portion is finished into N, and the stamper The flat plate is marked with a mark, the mark is detected by the marking detector, the winding angle of the core is measured at the time of detection, and the winding operation is performed when the winding angle is less than 360 degrees / N. It is characterized by terminating.

請求項2に記載の発明は、長尺状の平板と波板を重ねて巻芯に巻回することでハニカム構造のコア部を製造し、そのコア部を外筒に圧入して接合一体化してなるメタル担体の製造方法において、前記平板を前記巻芯へと送り出す途中に、該平板の送り長さを測定する測長器を設け、前記コア部を巻き終えたときの最終周長をN分割した1/N長さを、前記測長器で測長し、その測長時における前記巻芯の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を終了することを特徴とする。   The invention according to claim 2 is a method of manufacturing a core part of a honeycomb structure by overlapping a long flat plate and a corrugated sheet and winding them around a winding core, and press-fitting the core part into an outer cylinder so as to be joined and integrated. In the metal carrier manufacturing method, a length measuring device for measuring the feeding length of the flat plate is provided in the middle of feeding the flat plate to the winding core, and the final circumference when the winding of the core portion is finished is defined as N. The divided 1 / N length is measured with the length measuring device, the winding angle of the winding core during the length measurement is measured, and the winding operation is performed when the winding angle is less than 360 degrees / N. It is characterized by terminating.

請求項3に記載の発明は、請求項1または請求項2に記載のメタル担体の製造方法であって、前記コア部の周長が、前記最終周長mの概ね95%程度まで高速で巻き上げ動作を行い、その後、前記刻印器で刻印する、または、前記測長器で測長することを特徴とする。   Invention of Claim 3 is a manufacturing method of the metal support | carrier of Claim 1 or Claim 2, Comprising: The circumference of the said core part winds up at high speed to about 95% of the said final circumference m. An operation is performed, and thereafter, the marking is performed by the marking device, or the length is measured by the length measuring device.

請求項1に記載の発明によれば、コア部を巻き終えたときの最終周長をN分割した1/N長さの開始点と終了点に刻印器と刻印検出器を設置し、刻印器で前記平板に刻印を付け、その刻印を該刻印検出器で検出し、その検出時における巻芯の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を終了すれば、常に最終周長となったコア部を得ることができる。   According to the first aspect of the present invention, the stamper and the stamp detector are installed at the start point and the end point of the 1 / N length obtained by dividing the final circumference when the core portion has been wound into N, and the stamper The plate is engraved with a mark, the marking is detected by the marking detector, the winding angle of the winding core is measured at the time of detection, and the winding operation is finished when the winding angle is less than 360 degrees / N. By doing so, it is possible to always obtain the core portion having the final circumference.

したがって、本発明によれば、最終周長よりも長くなることも短くなることもなくコア部を製造できるので、そのコア部を外筒に対して隙間なく圧入させることができ、それらの間の接合強度を充分確保することができる。   Therefore, according to the present invention, since the core portion can be manufactured without being longer or shorter than the final circumference, the core portion can be pressed into the outer cylinder without any gap, A sufficient bonding strength can be secured.

請求項2に記載の発明によれば、平板を巻芯へと送り出す途中に、該平板の送り長さを測定する測長器を設け、コア部を巻き終えたときの最終周長をN分割した1/N長さを、測長器で測長し、その測長時における前記巻芯の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を終了すれば、常に最終周長となったコア部を得ることができる。   According to the second aspect of the present invention, a length measuring device for measuring the feed length of the flat plate is provided in the middle of feeding the flat plate to the winding core, and the final circumference when the core portion is finished is divided into N Measure the 1 / N length with a length measuring instrument, measure the winding angle of the core during the measurement, and terminate the winding operation when the winding angle is less than 360 degrees / N. In this case, the core portion that is always the final circumference can be obtained.

したがって、本発明によれば、最終周長よりも長くなることも短くなることもなくコア部を製造できるので、コア部を外筒に対して隙間なく圧入させることができ、それらの間の接合強度を充分確保することができる。   Therefore, according to the present invention, the core part can be manufactured without becoming longer or shorter than the final circumference, so that the core part can be press-fitted into the outer cylinder without a gap, and the joint between them can be produced. Sufficient strength can be secured.

請求項3に記載の発明によれば、コア部の周長が最終周長mの概ね95%程度まで高速で巻き上げ動作を行い、その後、刻印器で刻印する、または、測長器で測長するようにしたので、コア部を製造するスピードを向上させることができ、生産性を高めることができる。   According to the invention described in claim 3, the core part is wound up at a high speed up to about 95% of the final circumference m, and then engraved with a stamp, or length measured with a length meter. Since it did it, the speed which manufactures a core part can be improved, and productivity can be improved.

以下、本発明を適用した具体的な実施の形態について、図面を参照しながら詳細に説明する。   Hereinafter, specific embodiments to which the present invention is applied will be described in detail with reference to the drawings.

「第1の実施の形態」
図1は円筒形状としたメタル担体の製造方法の一例を示す概略図、図2は製造されたコア部を外筒に圧入し接合一体化してなるメタル担体の斜視図である。
“First Embodiment”
FIG. 1 is a schematic view showing an example of a method for producing a cylindrical metal carrier, and FIG. 2 is a perspective view of a metal carrier obtained by press-fitting the produced core part into an outer cylinder and integrating them.

メタル担体を製造するには、先ず、図1に示すように、一方向から供給される長尺状の平板1と、他方向から供給される長尺状の波板2を重ねるようにして円柱状の巻芯3に巻回してハニカム構造のコア部4を形成する。   To manufacture the metal carrier, first, as shown in FIG. 1, a long flat plate 1 supplied from one direction and a long corrugated plate 2 supplied from the other direction are overlapped to form a circle. A core portion 4 having a honeycomb structure is formed by winding around a columnar core 3.

かかるコア部4を形成するには、コア部製造装置を使用する。コア部製造装置は、巻芯3と、この巻芯3の巻き上げ角度を検出する巻き上げ角度検出手段5と、平板1を巻芯3に巻回する前の段階で該平板1に刻印を付ける刻印器6と、その刻印を検出する刻印検出器7と、コア部4が最終周長(製品周長)となったときに平板1及び波板2を切断する平板切断機8及び波板切断機9とを備える。   In order to form the core part 4, a core part manufacturing apparatus is used. The core part manufacturing apparatus includes a winding core 3, a winding angle detection means 5 that detects a winding angle of the winding core 3, and a stamp that marks the flat plate 1 at a stage before winding the flat plate 1 around the winding core 3. 6, a marking detector 7 for detecting the marking, and a flat plate cutting machine 8 and a corrugated sheet cutting machine for cutting the flat plate 1 and the corrugated plate 2 when the core portion 4 reaches the final circumferential length (product circumferential length). 9.

巻芯3は、所定の直径とされた円柱形状をなし、図示を省略するステッピングモータによりその回転数が制御されて回転駆動するようになっている。この巻芯3には、コア部4を構成する平板1と波板2とがその表面に巻回される。   The winding core 3 has a cylindrical shape with a predetermined diameter, and is driven to rotate by controlling its rotation speed by a stepping motor (not shown). A flat plate 1 and a corrugated plate 2 constituting the core portion 4 are wound around the surface of the core 3.

平板1と波板2は、例えば自動車用の触媒コンバータに使用されるメタル担体を構成する金属材料からなる。波板2は、平らな金属材料をコルゲート加工することにより波形に形成される。   The flat plate 1 and the corrugated plate 2 are made of a metal material constituting a metal carrier used in, for example, an automobile catalytic converter. The corrugated plate 2 is formed into a corrugated shape by corrugating a flat metal material.

巻き上げ角度検出手段5は、巻芯3の回転角度を検出する。この巻き上げ角度検出手段5としては、例えばエンコーダなどから構成される。   The winding angle detection means 5 detects the rotation angle of the winding core 3. The winding angle detection means 5 is composed of, for example, an encoder.

刻印器6は、平板1が巻芯3に巻回される手前に設けられ、当該平板1の表面1aに刻印10を付ける。かかる刻印器6としては、例えばレーザ装置やインク塗布装置或いは引っ掻き傷付与装置などが使用できる。レーザ装置を使用した場合は、レーザによる焦げ或いは小穴が刻印10となる。インク塗布装置を使用した場合は、インク滴が刻印10となる。引っ掻き傷付与装置を使用した場合は、引っ掻き傷が刻印10となる。   The stamp 6 is provided before the flat plate 1 is wound around the core 3, and the stamp 10 is attached to the surface 1a of the flat plate 1. For example, a laser device, an ink application device, or a scratching device can be used as the marking device 6. When a laser device is used, the laser burns or a small hole becomes the marking 10. When the ink application device is used, the ink droplet becomes the stamp 10. When the scratch imparting device is used, the scratch becomes the stamp 10.

刻印検出器7は、刻印器6によって平板1の表面1aに付けられた刻印10を検出する。刻印器6と刻印検出器7は、コア部4を巻き終えたときの最終周長をN分割した1/N長さの開始点と終了点にそれぞれ設置されている。本実施の形態では、前記コア部4の最終周長を4分割した1/4長さ(以下、これを1/4周長という)の位置に、前記刻印器6と刻印検出器7とをそれぞれ配置した。   The stamp detector 7 detects the stamp 10 attached to the surface 1 a of the flat plate 1 by the stamper 6. The stamp 6 and the stamp detector 7 are respectively installed at a start point and an end point of 1 / N length obtained by dividing the final circumference when the core portion 4 is wound into N parts. In the present embodiment, the marking device 6 and the marking detector 7 are placed at a position of a quarter length (hereinafter referred to as a quarter circumference) obtained by dividing the final circumference of the core portion 4 into four. Arranged respectively.

このコア部製造装置を用いてコア部4を製造するには、一方向から巻芯3へと繰り出される平板1と、これとは逆方向である他方向から巻芯3へと繰り出される波板2とを、前記巻芯3を回転させることでその周面に巻回させて行く。そして、コア部4の周長が最終周長mの概ね95%程度までこれら平板1と波板2を高速で巻き上げる。   In order to manufacture the core part 4 using this core part manufacturing apparatus, the flat plate 1 drawn out from one direction to the core 3 and the corrugated sheet drawn out from the other direction, which is the opposite direction, to the core 3. 2 is wound around the peripheral surface by rotating the winding core 3. Then, the flat plate 1 and the corrugated plate 2 are wound up at a high speed until the peripheral length of the core portion 4 is approximately 95% of the final peripheral length m.

このように、最終周長mの概ね95%程度まで高速で平板1と波板2を巻芯3に巻回すれば、コア部4の製造効率を高めることができる。   Thus, if the flat plate 1 and the corrugated plate 2 are wound around the core 3 at a high speed up to about 95% of the final circumferential length m, the manufacturing efficiency of the core portion 4 can be increased.

そして、最終周長mの概ね95%程度まで平板1と波板2を巻芯3に巻回させたら、刻印器6で平板1の表面1aに刻印10を付ける。次に、この刻印器6から1/4周長離れた位置に設けられた刻印検出器7で前記刻印10を検出する。刻印検出器7で前記刻印10が検出されたら、前記した巻き上げ角度検出手段5によってそのときの巻芯3の巻き上げ角度を測定する。   Then, when the flat plate 1 and the corrugated plate 2 are wound around the core 3 to about 95% of the final circumference m, the stamp 10 marks the surface 1a of the flat plate 1 with the stamp 6. Next, the marking 10 is detected by a marking detector 7 provided at a position one quarter circumference away from the stamp 6. When the marking 10 is detected by the marking detector 7, the winding angle detection means 5 measures the winding angle of the core 3 at that time.

巻き上げ角度検出手段5によって検出された巻き上げ角度が360度/4(90度)未満となったときに巻き上げ動作を終了する。すなわち、コア部4の周長が最終周長に満たなければ、平板1を1/4周長送っても巻き上げ角度は90度を超えるが、コア部4の周長が最終周長となったときは、巻き上げ角度は90度となる。   When the winding angle detected by the winding angle detection means 5 becomes less than 360 degrees / 4 (90 degrees), the winding operation is terminated. That is, if the peripheral length of the core portion 4 is less than the final peripheral length, the winding angle exceeds 90 degrees even if the flat plate 1 is fed by a quarter peripheral length, but the peripheral length of the core portion 4 becomes the final peripheral length. When the winding angle is 90 degrees.

したがって、巻芯3の巻き上げ角度が90度を超える場合は、次の1/4周長で再び刻印器6で平板1の表面1aに刻印10を付ける。そして、その刻印10を1/4周長離れた位置に設けた刻印検出器7にて検出し、そのときの巻芯3の巻き上げ角度を前記巻き上げ角度検出手段5で測定する。巻き上げ角度が90度未満であることが検出されたら巻き上げ動作を終了し、平板切断機8で平板1を切断すると共に、波板切断機9で波板2を切断する。   Therefore, when the winding angle of the core 3 exceeds 90 degrees, the stamp 10 is again marked on the surface 1a of the flat plate 1 by the stamper 6 at the next quarter circumference. Then, the marking 10 is detected by a marking detector 7 provided at a position separated by a quarter circumference, and the winding angle of the winding core 3 at that time is measured by the winding angle detecting means 5. When it is detected that the winding angle is less than 90 degrees, the winding operation is terminated, the flat plate 1 is cut by the flat plate cutting machine 8, and the corrugated plate 2 is cut by the corrugated plate cutting machine 9.

そして、巻芯3を回転させて平板1と波板2を切断端面まで巻き上げた後、得られたハニカム構造のコア部4を、図2に示す円筒形状の外筒11の中に圧入する。その後、これらコア部4と外筒11をロウ付けまたは拡散接合することによってメタル担体12を完成させる。   And after rotating the winding core 3 and winding up the flat plate 1 and the corrugated sheet 2 to a cut end surface, the core part 4 of the obtained honeycomb structure is press-fitted in the cylindrical outer cylinder 11 shown in FIG. Thereafter, the metal carrier 12 is completed by brazing or diffusion bonding the core portion 4 and the outer cylinder 11.

以上のように、本実施の形態によれば、巻き上げ角度が90度未満となったときに、巻き上げ動作を終了することで、常に最終周長となったコア部4を得ることができる。したがって、本発明方法を採用することで、最終周長よりも長くなることも短くなることもなくコア部4を製造でき、コア部4を外筒11に対して隙間なく圧入させることができ、それらの間の接合強度を充分確保することができる。   As described above, according to the present embodiment, when the winding angle becomes less than 90 degrees, the core portion 4 always having the final circumference can be obtained by terminating the winding operation. Therefore, by adopting the method of the present invention, the core part 4 can be manufactured without becoming longer or shorter than the final circumference, and the core part 4 can be press-fitted into the outer cylinder 11 without a gap, A sufficient bonding strength between them can be ensured.

また、本実施の形態によれば、巻き上げ角度検出手段5で検出した巻き上げ角度を演算することもないので、高度な演算回路を使用することなく、確実に最終周長のコア部4を得ることができ、製造コストも大幅に低減させることができる。   Further, according to the present embodiment, since the winding angle detected by the winding angle detection means 5 is not calculated, the core portion 4 having the final circumference can be obtained reliably without using an advanced calculation circuit. And manufacturing costs can be greatly reduced.

また、本実施の形態によれば、コア部4の周長が最終周長mの概ね95%程度まで高速で巻き上げ動作を行うようにしたので、コア部4を製造するスピードを向上させることができ、生産性を高めることができる。   Further, according to the present embodiment, since the winding operation is performed at a high speed up to the peripheral length of the core portion 4 being approximately 95% of the final peripheral length m, the speed of manufacturing the core portion 4 can be improved. And increase productivity.

「第2の実施の形態」
図3は楕円形状としたメタル担体の製造方法の一例を示す概略図、図4は巻き上げ動作を示す動作図、図5は製造されたコア部を外筒に圧入し接合一体化してなるメタル担体の斜視図である。
“Second Embodiment”
FIG. 3 is a schematic diagram showing an example of a manufacturing method of an elliptical metal carrier, FIG. 4 is an operation diagram showing a winding operation, and FIG. 5 is a metal carrier formed by press-fitting the manufactured core portion into an outer cylinder and joining them together. FIG.

第2の実施の形態では、巻芯13を楕円形状とし、その楕円形状とした巻芯3に平板1と波板2を重ねるようにして巻回させることでコア部14を形成する。かかるコア部14は、楕円形状としている点と、波板2を平板1と同一方向から巻芯3へ送っている点が、第1の実施の形態とは相違する。その他の構成は、第1の実施の形態と同一であるため、同一の符号を付すと共にその説明は省略するものとする。   In 2nd Embodiment, the core part 14 is formed by making the winding core 13 into an ellipse shape, and winding the flat plate 1 and the corrugated sheet 2 on the elliptical winding core 3 so that it may overlap. The core portion 14 is different from the first embodiment in that the core portion 14 has an elliptical shape and the corrugated plate 2 is fed to the core 3 from the same direction as the flat plate 1. Since the other configuration is the same as that of the first embodiment, the same reference numerals are given and the description thereof is omitted.

巻芯3を楕円形状とした場合でも、巻芯3を円筒形状としたときと同様に、コア部14の最終周長をN分割した1/N長さの開始点と終了点に刻印器6と刻印検出器7を設置し、その刻印器6で平板1に刻印(図示は省略する)を付け、その刻印を刻印検出器7で検出し、その検出時における巻芯3の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を行えば、常に最終周長となったコア部14を得ることができる。   Even when the core 3 has an elliptical shape, as in the case where the core 3 has a cylindrical shape, the stamper 6 is marked at the start and end points of the 1 / N length obtained by dividing the final circumference of the core portion 14 into N. The stamp detector 7 is installed, the flat plate 1 is marked with the stamp 6 (not shown), the stamp is detected by the stamp detector 7, and the winding angle of the core 3 at the time of detection is measured. If the winding operation is performed when the winding angle is less than 360 degrees / N, the core portion 14 always having the final circumference can be obtained.

したがって、本発明方法を採用することで、最終周長よりも長くなることも短くなることもなくコア部14を製造でき、そのコア部14を外筒15に対して隙間なく圧入させることができ、それらの間の接合強度を充分確保し得るメタル担体16を製造できる。   Therefore, by adopting the method of the present invention, the core portion 14 can be manufactured without becoming longer or shorter than the final circumference, and the core portion 14 can be press-fitted into the outer cylinder 15 without a gap. The metal carrier 16 that can sufficiently secure the bonding strength between them can be manufactured.

また、巻芯13を楕円形状とした場合でも、第1の実施の形態と同様、コア部4の周長が最終周長の概ね95%程度まで高速で巻き上げ動作を行うようにすることで、コア部4を製造するスピードを向上させることができ、生産性を高めることができる。   Further, even when the winding core 13 has an elliptical shape, as in the first embodiment, by performing the winding operation at a high speed up to about 95% of the final circumferential length of the core portion 4, The speed which manufactures the core part 4 can be improved, and productivity can be improved.

「第3の実施の形態」
図6はコア部を巻き終えたときの最終周長をN分割した1/N長さを測長器で測長する例を示す概略図である。
“Third Embodiment”
FIG. 6 is a schematic diagram showing an example in which a length measuring device measures the 1 / N length obtained by dividing the final circumference when the core portion is wound into N parts.

第1及び第2の実施の形態では、刻印器6と刻印検出器7を用いて1/N周長を検出するようにしたが、第3の実施の形態では、平板1を挟んで上下に設けた一対のロール状の測長器17で、前記1/N周長を測長する。   In the first and second embodiments, the 1 / N circumference is detected using the stamp 6 and the stamp detector 7, but in the third embodiment, the plate 1 is sandwiched up and down. The 1 / N circumference is measured with a pair of roll-shaped length measuring devices 17 provided.

この第3の実施の形態では、第1及び第2の実施の形態と同様、コア部4、14を巻き終えたときの最終周長をN分割した1/N長さを、前記測長器17で測長し、その測長時における前記巻芯3、13の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を終了する。   In the third embodiment, as in the first and second embodiments, the length measuring device is obtained by calculating the 1 / N length obtained by dividing the final circumference when the core portions 4 and 14 are wound into N by N. The length is measured at 17, and the winding angle of the winding cores 3 and 13 at the time of the measurement is measured. When the winding angle is less than 360 degrees / N, the winding operation is finished.

このようにすれば、常に最終周長となったコア部4、14を得ることができ、その寸法精度の高いコア部4、14を外筒11、15に隙間なく圧入させることができ、それらの間の接合強度を充分確保することができる。   In this way, it is possible to obtain the core portions 4 and 14 that always have the final circumference, and the core portions 4 and 14 having high dimensional accuracy can be press-fitted into the outer cylinders 11 and 15 without gaps, It is possible to ensure a sufficient bonding strength between the two.

円筒形状としたメタル担体の製造方法の一例を示す概略図である。It is the schematic which shows an example of the manufacturing method of the metal carrier made into the cylindrical shape. 製造されたコア部を外筒に圧入し接合一体化してなるメタル担体の斜視図である。It is a perspective view of the metal carrier formed by press-fitting the manufactured core part into the outer cylinder and joining and integrating them. 楕円形状としたメタル担体の製造方法の一例を示す概略図である。It is the schematic which shows an example of the manufacturing method of the metal carrier made into the ellipse shape. 巻き上げ動作を示す動作図である。It is an operation | movement figure which shows winding-up operation | movement. 製造されたコア部を外筒に圧入し接合一体化してなるメタル担体の斜視図である。It is a perspective view of the metal carrier formed by press-fitting the manufactured core part into the outer cylinder and joining and integrating them. コア部を巻き終えたときの最終周長をN分割した1/N長さを測長器で測長する例を示す概略図である。It is the schematic which shows the example which measures the 1 / N length which divided the final circumference at the time of finishing a core part into N with a length measuring device.

符号の説明Explanation of symbols

1…平板
2…波板
3、13…巻芯
4、14…コア部
5…巻き上げ角度検出手段
6…刻印器
7…刻印検出器
8…平板切断機
9…波板切断機
10…刻印
11、15…外筒
12、16…メタル担体
DESCRIPTION OF SYMBOLS 1 ... Flat plate 2 ... Corrugated sheet 3, 13 ... Core core 4, 14 ... Core part 5 ... Winding angle detection means 6 ... Stamping machine 7 ... Stamping detector 8 ... Flat plate cutting machine 9 ... Corrugated sheet cutting machine 10 ... Stamping 11, 15 ... outer cylinder 12, 16 ... metal carrier

Claims (3)

長尺状の平板と波板を重ねて巻芯に巻回することでハニカム構造のコア部を製造し、そのコア部を外筒に圧入して接合一体化してなるメタル担体の製造方法において、
前記コア部を巻き終えたときの最終周長をN分割した1/N長さの開始点と終了点に刻印器と刻印検出器を設置し、
前記刻印器で前記平板に刻印を付け、その刻印を前記刻印検出器で検出し、その検出時における前記巻芯の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を終了する
ことを特徴とするメタル担体の製造方法。
In the manufacturing method of a metal carrier formed by stacking a long flat plate and a corrugated sheet to be wound around a core to produce a core part of a honeycomb structure, and press-fitting the core part into an outer cylinder and joining and integrating them,
A stamper and a stamp detector are installed at the start point and end point of 1 / N length obtained by dividing the final circumference when the core portion is wound into N,
When the plate is marked with the stamp, the stamp is detected by the stamp detector, the winding angle of the core at the time of detection is measured, and when the winding angle is less than 360 degrees / N A method for manufacturing a metal carrier, characterized in that the winding operation is terminated.
長尺状の平板と波板を重ねて巻芯に巻回することでハニカム構造のコア部を製造し、そのコア部を外筒に圧入して接合一体化してなるメタル担体の製造方法において、
前記平板を前記巻芯へと送り出す途中に、該平板の送り長さを測定する測長器を設け、
前記コア部を巻き終えたときの最終周長をN分割した1/N長さを、前記測長器で測長し、その測長時における前記巻芯の巻き上げ角度を測定し、その巻き上げ角度が360度/N未満となったときに巻き上げ動作を終了する
ことを特徴とするメタル担体の製造方法。
In the manufacturing method of a metal carrier formed by stacking a long flat plate and a corrugated sheet to be wound around a core to produce a core part of a honeycomb structure, and press-fitting the core part into an outer cylinder and joining and integrating them,
In the middle of feeding the flat plate to the core, a length measuring device for measuring the feed length of the flat plate is provided,
The 1 / N length obtained by dividing the final circumference when the core portion is finished into N is measured with the length measuring device, and the winding angle of the winding core at the time of the measurement is measured. The metal carrier manufacturing method is characterized in that the hoisting operation is terminated when the angle becomes less than 360 degrees / N.
請求項1または請求項2に記載のメタル担体の製造方法であって、
前記コア部の周長が、前記最終周長mの概ね95%程度まで高速で巻き上げ動作を行い、その後、前記刻印器で刻印する、または、前記測長器で測長する
ことを特徴とするメタル担体の製造方法。
It is a manufacturing method of the metal carrier according to claim 1 or 2,
The circumference of the core part is wound up at a high speed to approximately 95% of the final circumference m, and then engraved with the stamp or length measured with the length measuring device. A method for producing a metal carrier.
JP2005059240A 2005-03-03 2005-03-03 Method for manufacturing metallic carrier Withdrawn JP2006239580A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010090051A1 (en) 2009-02-03 2010-08-12 カルソニックカンセイ株式会社 Metallic catalyst support and process for producing same
EP2679320A1 (en) 2012-06-29 2014-01-01 Calsonic Kansei Corporation Method for producing metallic catalyst support

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010090051A1 (en) 2009-02-03 2010-08-12 カルソニックカンセイ株式会社 Metallic catalyst support and process for producing same
EP2679320A1 (en) 2012-06-29 2014-01-01 Calsonic Kansei Corporation Method for producing metallic catalyst support

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