JP2019163760A5 - - Google Patents

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JP2019163760A5
JP2019163760A5 JP2019005518A JP2019005518A JP2019163760A5 JP 2019163760 A5 JP2019163760 A5 JP 2019163760A5 JP 2019005518 A JP2019005518 A JP 2019005518A JP 2019005518 A JP2019005518 A JP 2019005518A JP 2019163760 A5 JP2019163760 A5 JP 2019163760A5
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honeycomb structure
outer peripheral
honeycomb
heating
porosity
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JP2019005518A
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JP7146657B2 (en
JP2019163760A (en
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Priority to US16/296,734 priority Critical patent/US11310873B2/en
Priority to CN201910187017.5A priority patent/CN110307648A/en
Priority to DE102019203792.5A priority patent/DE102019203792A1/en
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ここで、図2は流体加熱部品1を上方から視た平面図である。更に、外周面3に被設される導電性皮膜層4は、ハニカム構造体2の外周面3の全体に亘って必ずしも被設される必要はなく、外周面3の少なくとも一部においてリング状(環状)を呈して電気的に接続された状態であればよい(詳細は後述する)。 Here, FIG. 2 is a plan view of the fluid heating component 1 as viewed from above. Further, the conductive film layer 4 overlaid on the outer peripheral surface 3 does not necessarily have to be applied over the entire outer peripheral surface 3 of the honeycomb structure 2, and is ring-shaped (at least a part of the outer peripheral surface 3). It suffices as long as it exhibits an annular shape and is electrically connected (details will be described later).

ハニカム構造体40を自動車用の触媒担体や排ガス浄化フィルタとして用いる場合は、所定のセラミックスを主成分とし、気孔率を30〜60%としてもかまわない。30%未満の気孔率であると、触媒を効率的に担持できなくなり、また、フィルタとしての機能を低下させるため、好ましくない。また、60%の気孔率であると、強度が十分でなく、耐久性が低下するため好ましくない。 When the honeycomb structure 40 is used as a catalyst carrier for automobiles or an exhaust gas purification filter, a predetermined ceramic may be used as a main component and the porosity may be 30 to 60%. If the porosity is less than 30%, the catalyst cannot be supported efficiently and the function as a filter is deteriorated, which is not preferable. Further, if it is the porosity of more than 60%, the strength is not sufficient, unfavorably the durability is lowered.

2.流体加熱部品複合体
上記のように構成された本発明の流加熱部品を複数組み合わせることで一体的に構築された流体加熱部品複合体30a,30bを形成することができる。ここで、図7は流体加熱部品複合体30aの構築前の状態を示す分解斜視図であり、図8は流体加熱部品複合体30aの構築後の概略構成を示す斜視図であり、図9は別例構成の流体加熱部品複合体30bの構築前の状態を示す分解斜視図であり、図10は図9の流体加熱部品複合体30bの構築後の概略構成を示す斜視図である。
2. Integrally constructed fluid heating component composite body 30a by combining a plurality of flow bodies heating element of the present invention configured as a fluid heating element complexes above, it is possible to form a 30b. Here, FIG. 7 is an exploded perspective view showing a state before construction of the fluid heating component composite 30a, FIG. 8 is a perspective view showing a schematic configuration after construction of the fluid heating component composite 30a, and FIG. 9 is a perspective view showing a schematic configuration after construction. FIG. 10 is an exploded perspective view showing a state before construction of the fluid heating component composite 30b having another example configuration, and FIG. 10 is a perspective view showing a schematic configuration after construction of the fluid heating component composite 30b of FIG.

(1)ハニカム構造体
SiCを主成分とするハニカム構造体の製造を行った。始めに、所定の粒度、調合量に調整したSiC粉末、バインダー、水又は有機溶剤などを混練した成形用原料を、所望の形状に押出成形し、乾燥させてハニカム成形体を得た後、適宜加工を加えて、高温でSi含浸焼成を行い、ハニカム構造体を得た。ここで、ハニカム構造体は、ハニカム径が43mm、軸方向のハニカム長さが23mmのサイズのものを用いた。ここで、Si含浸焼成の含浸比率等を変更することにより、実施例1ではハニカム構造体の気孔率が10%以下になるように調整した。同様に、実施例2〜6、及び比較例1,2では、ハニカム構造体の気孔率が5%以下、実施例12ではハニカム構造体の気孔率が10%以上となるように調整を行った。実施例7〜12については、実施例1〜6のハニカム構造体と同様の条件で焼成したものを準備し、ハニカム径が40mmになるように外周壁を研削加工し、実施例1〜6と比べて外周壁の薄いハニカム構造体を準備した。外周壁厚さは、測定顕微鏡を用いて計16か所の測定を行い、平均した値を外周壁厚さとした。すなわち、実施例12を除き、流体加熱部品のベースとなるハニカム構造体(柱状部材)は、緻密質のものである。
(1) Honeycomb structure A honeycomb structure containing SiC as a main component was manufactured. First, a molding raw material obtained by kneading SiC powder, a binder, water, an organic solvent, etc. adjusted to a predetermined particle size and blending amount is extruded into a desired shape and dried to obtain a honeycomb molded product, and then appropriately. After processing, Si impregnation firing was performed at a high temperature to obtain a honeycomb structure. Here, as the honeycomb structure, a honeycomb structure having a honeycomb diameter of 43 mm and a honeycomb length in the axial direction of 23 mm was used. Here, by changing the impregnation ratio of the Si impregnation firing, the porosity of the honeycomb structure was adjusted to 10% or less in Example 1. Similarly, in Examples 2 to 6 and Comparative Examples 1 and 2, the porosity of the honeycomb structure was adjusted to 5% or less, and in Example 12, the porosity of the honeycomb structure was 10% or more. .. For Examples 7 to 12 , fired ones were prepared under the same conditions as the honeycomb structures of Examples 1 to 6, and the outer peripheral wall was ground so that the honeycomb diameter was 40 mm. A honeycomb structure with a thinner outer wall was prepared. The outer peripheral wall thickness was measured at a total of 16 points using a measuring microscope, and the average value was taken as the outer peripheral wall thickness. That is, except for Example 12, the honeycomb structure (columnar member) that is the base of the fluid heating component is dense.

なお、実施例1〜6の流加熱部品においては、ハニカム構造体の外周面に形成される導電性皮膜層の金属種類及び形成方法については、特に大きな有意性は認められず、本願発明の規定した範囲であれば良好な結果を得ることが確認された。また、外周壁の薄い実施例7〜12の流加熱部品においても良好な結果が得られることを確認し、実施例1〜6と比べて、より大きな加熱速度においても割れを生じずに加熱が可能であることが確認された。 In the flow body heating components of Examples 1 to 6, for the metal type and method for forming a conductive film layer formed on the outer peripheral surface of the honeycomb structure, it is not observed particularly great significance, the present invention It was confirmed that good results were obtained within the specified range. Further, it was confirmed that good results are obtained in the flow body heating elements of thin Example 7-12 of the outer peripheral wall, as compared with Example 1-6, heated without causing cracks even in a larger heating rate Was confirmed to be possible.

一方、導電性皮膜層を有しない流加熱部品(比較例1)、及び、流体の流通方向に直交するハニカム構造体の切断面において、電気的に接続した状態でハニカム構造体の切断面全周を被設していない流加熱部品(比較例2)は、いずれも加熱速度が遅く、誘導加熱試験による加熱開始から300℃に到達するまでの経過時間が100s必要であったり(比較例1)、または115sを経過して、ようやく100℃に到達するもの(比較例2)であり、速やかな加熱や昇温ができないことが示された。そのため、燃費改善のための加熱システムに採用することが困難であることが確認された。 On the other hand, no Fluid heating element a conductive coating layer (Comparative Example 1), and, at the cut face of the honeycomb structure perpendicular to the flow direction of the fluid, the cutting face of the honeycomb structure in a state of electrically connected all flow body heating elements have not be set in the circumferential (Comparative example 2) are both slow heating rate, elapsed time is 100s or is required (Comparative examples to reach 300 ° C. from the start of heating by induction heating test It was shown that 1) or 115 s passed and finally reached 100 ° C. (Comparative Example 2), and rapid heating and temperature rise were not possible. Therefore, it was confirmed that it is difficult to adopt it in a heating system for improving fuel efficiency.

JP2019005518A 2018-03-20 2019-01-16 Fluid heating component and fluid heating component composite Active JP7146657B2 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US16/296,734 US11310873B2 (en) 2018-03-20 2019-03-08 Fluid heating component, and fluid heating component complex
CN201910187017.5A CN110307648A (en) 2018-03-20 2019-03-13 Fluid heating element and fluid heating element complex
DE102019203792.5A DE102019203792A1 (en) 2018-03-20 2019-03-20 Fluid heating component and fluid heating component complex

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JPWO2021079556A1 (en) * 2019-10-25 2021-04-29
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CN1034462A (en) * 1988-01-20 1989-08-02 侯梦斌 Titanium nitride electrothermal film type heater and technology
JP3899404B2 (en) * 2002-12-26 2007-03-28 国立大学法人東京海洋大学 Equipment for removing particulate matter in exhaust gas
CN101042950B (en) * 2003-12-12 2010-07-28 日本曹达株式会社 Method for manufacturing transparent conductive film cling matrix
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