JPH04334547A - Ozone decomposing catalyst - Google Patents
Ozone decomposing catalystInfo
- Publication number
- JPH04334547A JPH04334547A JP3198971A JP19897191A JPH04334547A JP H04334547 A JPH04334547 A JP H04334547A JP 3198971 A JP3198971 A JP 3198971A JP 19897191 A JP19897191 A JP 19897191A JP H04334547 A JPH04334547 A JP H04334547A
- Authority
- JP
- Japan
- Prior art keywords
- catalyst
- mno2
- ozone
- ozone decomposing
- thickness
- 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.)
- Pending
Links
- 239000003054 catalyst Substances 0.000 title claims abstract description 38
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 title claims abstract description 33
- NUJOXMJBOLGQSY-UHFFFAOYSA-N manganese dioxide Chemical compound O=[Mn]=O NUJOXMJBOLGQSY-UHFFFAOYSA-N 0.000 claims abstract description 33
- 239000013543 active substance Substances 0.000 claims abstract 2
- 238000000354 decomposition reaction Methods 0.000 claims description 17
- 230000000694 effects Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 12
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N titanium dioxide Inorganic materials O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 10
- 238000006243 chemical reaction Methods 0.000 description 9
- 229910000108 silver(I,III) oxide Inorganic materials 0.000 description 8
- 239000004927 clay Substances 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 241000264877 Hippospongia communis Species 0.000 description 4
- 239000011230 binding agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 239000002002 slurry Substances 0.000 description 4
- 230000003197 catalytic effect Effects 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 3
- 238000002156 mixing Methods 0.000 description 3
- 238000001179 sorption measurement Methods 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 239000000969 carrier Substances 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910044991 metal oxide Inorganic materials 0.000 description 2
- 150000004706 metal oxides Chemical class 0.000 description 2
- 229920000609 methyl cellulose Polymers 0.000 description 2
- 239000001923 methylcellulose Substances 0.000 description 2
- 235000010981 methylcellulose Nutrition 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 1
- QPLDLSVMHZLSFG-UHFFFAOYSA-N CuO Inorganic materials [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 description 1
- XOLBLPGZBRYERU-UHFFFAOYSA-N SnO2 Inorganic materials O=[Sn]=O XOLBLPGZBRYERU-UHFFFAOYSA-N 0.000 description 1
- 229910003082 TiO2-SiO2 Inorganic materials 0.000 description 1
- 229910021536 Zeolite Inorganic materials 0.000 description 1
- 230000002378 acidificating effect Effects 0.000 description 1
- 239000003463 adsorbent Substances 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000007865 diluting Methods 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- HNPSIPDUKPIQMN-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Al]O[Al]=O HNPSIPDUKPIQMN-UHFFFAOYSA-N 0.000 description 1
- 238000004453 electron probe microanalysis Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012784 inorganic fiber Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004898 kneading Methods 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- JKQOBWVOAYFWKG-UHFFFAOYSA-N molybdenum trioxide Inorganic materials O=[Mo](=O)=O JKQOBWVOAYFWKG-UHFFFAOYSA-N 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000006386 neutralization reaction Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- GNRSAWUEBMWBQH-UHFFFAOYSA-N nickel(II) oxide Inorganic materials [Ni]=O GNRSAWUEBMWBQH-UHFFFAOYSA-N 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000006864 oxidative decomposition reaction Methods 0.000 description 1
- 238000005949 ozonolysis reaction Methods 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000012495 reaction gas Substances 0.000 description 1
- 230000008929 regeneration Effects 0.000 description 1
- 238000011069 regeneration method Methods 0.000 description 1
- 239000012744 reinforcing agent Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 235000012239 silicon dioxide Nutrition 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 150000003467 sulfuric acid derivatives Chemical class 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- XJDNKRIXUMDJCW-UHFFFAOYSA-J titanium tetrachloride Chemical compound Cl[Ti](Cl)(Cl)Cl XJDNKRIXUMDJCW-UHFFFAOYSA-J 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- 239000010457 zeolite Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A50/00—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE in human health protection, e.g. against extreme weather
- Y02A50/20—Air quality improvement or preservation, e.g. vehicle emission control or emission reduction by using catalytic converters
Landscapes
- Exhaust Gas Treatment By Means Of Catalyst (AREA)
- Catalysts (AREA)
Abstract
Description
【産業上の利用分野】本発明は、気体等の中に含まれる
、オゾンを分解除去するための触媒に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a catalyst for decomposing and removing ozone contained in gases.
【従来の技術】従来、気体中に含まれる有害成分である
オゾンを除去する方法として、活性炭、ゼオライト等の
多孔質物質を用いる吸着法、あるいは、MnO2などの
触媒を用いることによる酸化分解法等の方法が行われて
きた。[Prior Art] Conventionally, methods for removing ozone, a harmful component contained in gases, include adsorption methods using porous materials such as activated carbon and zeolite, and oxidative decomposition methods using catalysts such as MnO2. method has been used.
【発明が解決しようとする問題点】しかしながら、上記
従来のオゾンの除去方法はいずれも、充分に満足のいく
方法であるとは言い難い。すなわち、吸着法には、吸着
剤が吸着能力を発揮する期間が有限であるため、再生等
することを要し、除去装置のメンテナンスに多大の労力
及び費用が必要となるという問題がある。又、触媒を用
いるオゾンの酸化分解法には、上記のような問題は無い
ものの、現状では触媒性能上充分に満足のいくものであ
るとは言い難く、また初期性能は良くても、反応中に経
時的に劣化するという問題があった。本発明は、従来の
オゾン除去方法が有していたこれらの問題を解決するた
めになされたものであって、その目的とするところは、
従来方法に比べてオゾンの除去能力に優れると同時に、
長期間の使用が可能な耐久性に優れたオゾン分解触媒を
提供することにある。また、本発明は既に本発明者らが
出願している特願平2−24843にかかる発明を改良
したものである。すなわち本発明にかかる反応は反応律
速が固体内拡散であるため反応が触媒表面部においての
み進行するため触媒構造として触媒成分を触媒表面近傍
にのみ担持するコート型が最も好ましいことを本発明者
らが既に提案している。しかしながらこれらの方法も例
えばハニカム構造体のセル数/inch2が大きくなる
にしたがってその製造方法が難しくなるという問題点を
有していた。本発明は、これらの問題点をも解決するこ
とを可能にしたもので、すなわちコート厚みを低減する
ことが可能となったため成形触媒とりわけ低ピッチハニ
カムの生産性に優れると同時にオゾン分解能力、及び、
長期耐久性に優れたオゾン分解触媒を提供することにあ
る。[Problems to be Solved by the Invention] However, none of the above conventional ozone removal methods can be said to be fully satisfactory. That is, the adsorption method has a problem in that since the period during which the adsorbent exhibits its adsorption ability is limited, it requires regeneration, etc., and a great deal of labor and cost is required for maintenance of the removal device. In addition, although the ozone oxidation decomposition method using a catalyst does not have the above-mentioned problems, it is difficult to say that the catalyst performance is fully satisfactory at present, and even if the initial performance is good, there are problems during the reaction. There was a problem that it deteriorated over time. The present invention was made to solve these problems that conventional ozone removal methods had, and its purpose is to:
At the same time, it has superior ozone removal ability compared to conventional methods.
The purpose of the present invention is to provide an ozone decomposition catalyst that can be used for a long period of time and has excellent durability. Furthermore, the present invention is an improvement on the invention disclosed in Japanese Patent Application No. 2-24843 filed by the present inventors. In other words, in the reaction according to the present invention, the reaction rate is determined by diffusion within the solid, and the reaction proceeds only on the surface of the catalyst. has already been proposed. However, these methods also have the problem that, for example, as the number of cells/inch2 of the honeycomb structure increases, the manufacturing method thereof becomes more difficult. The present invention has made it possible to solve these problems. In other words, since it has become possible to reduce the coating thickness, it has excellent productivity of shaped catalysts, especially low pitch honeycombs, and at the same time has improved ozone decomposition ability and ,
The objective is to provide an ozone decomposition catalyst with excellent long-term durability.
【問題を解決するための手段】上記目的を達成するため
の本発明にかかるオゾン分解用触媒は、MnO2を含有
する担体をBaseとして、オゾン分解能を有する活性
種を担持させてなることを特徴としている。オゾン分解
能を有する触媒活性種として既に本発明者らが提案して
いるようなTi、Cu、Mn、Ni、Fe、Ag、Au
、Mo、Zr、Sn、Nb、Wなどの種々の金属、及び
金属酸化物もしくは硫酸塩の少なくとも1種以上からな
るもの、あるいはこれらに活性炭、酸性粘土を含有させ
たものなどを挙げることができる。こうした触媒として
は、例えば担持されるべき金属酸化物を用いて表せば、
MnO2、NiO、CuO、Fe2O3、を主成分とす
るもの及びMnO2−TiO2、MnO2−CuO、M
nO2−Fe2O3、MnO2−Ag2O、NiO−C
o3O4、NiO−TiO2、NiO−MnO2、Ni
O−Ag2O、NiO−MoO3、NiO−WO3、N
iO−SnO2等を主成分とするもの及び、MnO2−
Ag2O−TiO2、MnO2−CuO−Ag2O、N
iO−MnO2−Ag2O、NiO−MnO2−TiO
2等を主成分とするものが例示される。本発明方法にお
いて用いられる触媒の形状は特に限定されず、例えばハ
ニカム状、ペレット状、円柱状、板状、パイプ状等、種
々の形状のものを用いることができる。このうちMnO
2を含有する担体は、主に、混練法によって製造するこ
とができる。担体の製造においては、賦形性を与えるた
めに成形助剤を添加したり、機械強度等を向上させるた
めに無機繊維等の補強剤、有機バインダー等を適宜添加
したりしてもよい。これらの担体中に含まれるMnO2
は、10wt%以上が好ましく、20wt%以上がより
好ましい。10wt%以下とすると担体のオゾン分解能
が著しく低下するため、高分解能を得るためにはコート
厚みを厚くする必要がある。これらの担体の上に担持さ
れる触媒活性種は、主にウォシュコート法などによって
製造することが出来る。これらのコート厚みは、5〜1
00μが好ましく、10〜50μがより好ましい。又、
5μ以下とすると分解活性が低下し100μ以上とする
と分解活性の向上がなく圧損のみが上昇する。オゾン分
解の際の反応温度は、0〜40℃が好ましく、10〜3
0℃がより好ましい。0℃未満の場合、反応速度が遅く
なるからであり、40℃を越えた場合、新たに昇温のた
めの熱エネルギーを必要とし不経済であるからである。
又、触媒と反応ガスとの接触は、5〜70の面積速度(
AV;area velocity)で行うことが好
ましい。これは、面積速度が5未満であると触媒が多く
必要になるからであり、面積速度が50を超えると効率
が低く所定の分解率が得られないからである。ここで、
面積速度とは、空間速度(1/Hr)を単位容積当たり
のガス接触面積(m2/m3)で除去した値である。[Means for Solving the Problems] The ozone decomposition catalyst according to the present invention for achieving the above object is characterized in that an active species having an ozone decomposition ability is supported on a carrier containing MnO2 as a base. There is. Ti, Cu, Mn, Ni, Fe, Ag, Au, which the present inventors have already proposed as catalytic active species having ozone decomposition ability.
, various metals such as Mo, Zr, Sn, Nb, and W, and at least one of metal oxides or sulfates, or those containing activated carbon or acidic clay. . As such a catalyst, for example, if it is expressed using a metal oxide to be supported,
Those whose main components are MnO2, NiO, CuO, Fe2O3, and MnO2-TiO2, MnO2-CuO, M
nO2-Fe2O3, MnO2-Ag2O, NiO-C
o3O4, NiO-TiO2, NiO-MnO2, Ni
O-Ag2O, NiO-MoO3, NiO-WO3, N
Those whose main component is iO-SnO2 etc., and MnO2-
Ag2O-TiO2, MnO2-CuO-Ag2O, N
iO-MnO2-Ag2O, NiO-MnO2-TiO
An example is one in which the main component is 2 or the like. The shape of the catalyst used in the method of the present invention is not particularly limited, and various shapes can be used, such as a honeycomb shape, a pellet shape, a columnar shape, a plate shape, a pipe shape, and the like. Of these, MnO
A carrier containing 2 can be mainly produced by a kneading method. In producing the carrier, a molding aid may be added to impart shapeability, and reinforcing agents such as inorganic fibers, organic binders, etc. may be appropriately added to improve mechanical strength. MnO2 contained in these carriers
is preferably 10 wt% or more, more preferably 20 wt% or more. If it is less than 10 wt%, the ozone decomposition ability of the carrier will be significantly reduced, so in order to obtain high resolution, it is necessary to increase the coating thickness. The catalytically active species supported on these carriers can be produced mainly by a wash coating method or the like. The thickness of these coats is 5 to 1
00μ is preferable, and 10-50μ is more preferable. or,
When it is less than 5μ, the decomposition activity decreases, and when it is more than 100μ, there is no improvement in the decomposition activity and only the pressure drop increases. The reaction temperature during ozonolysis is preferably 0 to 40°C, and 10 to 3°C.
0°C is more preferred. This is because if the temperature is less than 0°C, the reaction rate will be slow, and if it exceeds 40°C, additional thermal energy will be required to raise the temperature, which is uneconomical. In addition, the contact between the catalyst and the reaction gas is carried out at an areal velocity of 5 to 70 (
It is preferable to carry out at AV (area velocity). This is because if the areal velocity is less than 5, a large amount of catalyst is required, and if the areal velocity is more than 50, the efficiency is low and a predetermined decomposition rate cannot be obtained. here,
The area velocity is the value obtained by removing the space velocity (1/Hr) by the gas contact area per unit volume (m2/m3).
【実施例】以下、本発明を実施例に基づいて詳細に説明
する。但し本発明は、下記の実施例に限定されるもので
はない。
A.触媒の調整
実施例1
木節粘土を100℃にて18時間乾燥後、スクリーンが
0.5mmφであるサンプルミルにて粉砕した。これら
の粉砕物を8kg、比表面積が67m2/gであるMn
O2を2kg、メチルセルロース系バインダー(ユケン
工業 YB−32)0.8kgと水を加え、混合後ニ
ーダーで充分に混練を行った。これらの坏土を、ハニカ
ム押出用ダイスを装着したオーガスクリュー式押出機に
投入し、ハニカム状物を常温にて通風乾燥乾燥後、N2
気流中で5℃/時間の昇温速度で500℃まで昇温し、
昇温後3時間キープした後、10℃/時間の降温速度で
冷却し、開口率64%、ピッチ1.0mmのハニカム状
担体を得た。次に比表面積が67m2/gであるMnO
2、1kgに500mlの水と少量のバインダーを加え
、更にガラスビーズ250gを加えて、30分間攪拌混
合した後、ビーズを分離し、スラリーを得た。このスラ
リーに水300mlを加えて希釈した後、上述したハニ
カム状担体を適切な大きさに切り出したものを浸漬し、
過剰のスラリーを除去して乾燥し、MnO2を平均厚み
38μ担持した触媒を得た。なお厚みの算定はEPMA
による線分折によりn数を10としてその平均値を求め
ることにより行った。以下同様の方法により厚を求めた
。
実施例2
実施例1において、MnO2、1kgのうち200gを
TiO2にかえ、さらに希釈水を500mlとすること
以外は実施例1と同様にして、MnO2−TiO2(重
量比80:20)をこの時コート回数を調節し、担持し
た触媒を得た。コート厚みを6μ、10μ、15μ、3
0μ、42μに変えた5種類の触媒を得た。
実施例3
実施例1において、MnO2、1kgのうち100gを
Ag2Oにかえる以外は実施例1と同様にして、MnO
2−Ag2O(重量比90:10)を平均厚み47μで
担持した触媒を得た。
実施例4
実施例1の方法において、木節粘土粉砕物を5kg、M
nO2を5kg、メチルセルロース系バインダー(ユケ
ン工業 YB−32)を1kgとすること以外実施例
1にしたがいハニカム状担体を得た。この担体を実施例
2で用いたものと同様のスラリーで処理しコート回数を
調節しコート厚みが5μ、11μ、20μ、33μ、4
5μの5種類の触媒を得た。
実施例5
実施例1において、MnO2、1kgのうち400gを
比表面積が38m2/gであるFe2O3、100gを
Ag2Oにかえる以外は実施例1と同様にして、MnO
2−Fe2O3−Ag2O(重量比50:40:10)
を平均厚み51μで担持した触媒を得た。
実施例6
実施例1において、MnO2、1kgのうち200gを
活性炭(武田薬品製白鷺A)100gをTiO2にかえ
る以外は実施例1と同様にして、MnO2−活性炭−T
iO2(重量比70:20:10)を平均厚み38μで
担持した触媒を得た。
実施例7
実施例1において、MnO2にかえて比表面積が55m
2/g、CuOを用いること以外は実施例1と同様にし
て、CuOを平均厚み45μで担持した触媒を得た。
比較例1
実施例1において、担体を押出し成形する際に、木節粘
土を20kgとし、活性炭を加えないこと以外は実施例
1と同様にしてMnO2を平均厚み50μ担持した触媒
を得た。
実施例8
実施例4において、担体を押出し成形する際に、木節粘
土を18kgとし、活性炭を2kgとすること以外は実
施例4と同様にしてMnO2を平均厚み57μ担持した
触媒を得た。
参考例
比表面積48m2/gのMnO230gと、四塩化チタ
ンとシリンゾルとの混合物(TiO2:SiO2が1:
1)70gとを攪拌混合しつつ、アンモニアガスを吹き
込んで中和反応を行い、スラリー状の沈澱物を生成させ
た。得られた沈澱物を充分に水洗した後、温度500℃
で3時間焼成、粉砕して比表面積162m2/gの三元
触媒MnO2−TiO2−SiO2(重量比35:30
:35)パウダーを得た。以下、実施例1と同様にして
SiO2−MnO2−TiO2(重量比35:30:3
5)を担持率99%で担持した三元触媒を得た。
B.触媒活性試験
上記実施例1〜8及び比較例1、及び参考例で得た触媒
について、第1図にそのフローシートを示すような試験
装置を用いて、下記反応条件で触媒活性試験を行い、初
期、10時間経過後、及び100時間経過後のオゾン分
解率を求めた。図において、(1)はオゾン発生器であ
り、これに導入されたエアーより適切な濃度のオゾンを
発生させ、このオゾン含有エアーを触媒層(2)に導く
。オゾン分解率(%)は、(3)のオゾン分析計にて測
定される触媒層の入口及び出口の値により次式で求めら
れる。
(反応条件)
空間速度:20,000/Hr
入口オゾン濃度:10ppm
反応温度:20℃
上記試験結果を表1に示す。
上記表より明らかなように、実施例1〜8で得たいずれ
の触媒も、比較例1及び参考例で得た触媒に比べて高い
オゾン分解率(%)を有していると同時に長時間にわた
って殆ど性能の劣化を示さず、優れた耐久性を有してい
る。EXAMPLES The present invention will be explained in detail below based on examples. However, the present invention is not limited to the following examples. A. Catalyst Preparation Example 1 Kibushi clay was dried at 100° C. for 18 hours and then ground in a sample mill with a screen of 0.5 mmφ. 8 kg of these pulverized materials, Mn with a specific surface area of 67 m2/g
2 kg of O2, 0.8 kg of methyl cellulose binder (Yuken Kogyo YB-32) and water were added, and after mixing, the mixture was thoroughly kneaded using a kneader. These clays were put into an auger screw extruder equipped with a die for honeycomb extrusion, and the honeycomb-like material was dried with ventilation at room temperature, and then heated with N2
Raise the temperature to 500°C at a heating rate of 5°C/hour in an air flow,
After the temperature was raised and maintained for 3 hours, it was cooled at a cooling rate of 10° C./hour to obtain a honeycomb-shaped carrier with an aperture ratio of 64% and a pitch of 1.0 mm. Next, MnO with a specific surface area of 67 m2/g
2. 500 ml of water and a small amount of binder were added to 1 kg, and 250 g of glass beads were added, and after stirring and mixing for 30 minutes, the beads were separated to obtain a slurry. After diluting this slurry by adding 300 ml of water, the above-mentioned honeycomb-shaped carrier cut into an appropriate size was immersed.
Excess slurry was removed and dried to obtain a catalyst supporting MnO2 with an average thickness of 38μ. The thickness is calculated using EPMA.
The average value was determined by line analysis with n number of 10. The thickness was determined using the same method below. Example 2 In the same manner as in Example 1, except that 200 g of 1 kg of MnO2 was changed to TiO2 and the dilution water was further changed to 500 ml, MnO2-TiO2 (weight ratio 80:20) was used. A supported catalyst was obtained by adjusting the number of coats. Coat thickness: 6μ, 10μ, 15μ, 3
Five types of catalysts were obtained with different sizes of 0μ and 42μ. Example 3 In the same manner as in Example 1 except that 100 g of 1 kg of MnO2 was changed to Ag2O, MnO
A catalyst was obtained in which 2-Ag2O (weight ratio 90:10) was supported with an average thickness of 47μ. Example 4 In the method of Example 1, 5 kg of pulverized Kibushi clay, M
A honeycomb-shaped carrier was obtained in accordance with Example 1 except that nO2 was 5 kg and methyl cellulose binder (Yuken Kogyo YB-32) was 1 kg. This carrier was treated with the same slurry as that used in Example 2, and the number of coats was adjusted to give a coating thickness of 5μ, 11μ, 20μ, 33μ, and 4μ.
Five types of catalysts of 5μ were obtained. Example 5 In the same manner as in Example 1, except that 400 g of 1 kg of MnO2 was changed to Fe2O3 with a specific surface area of 38 m2/g, and 100 g was changed to Ag2O, MnO
2-Fe2O3-Ag2O (weight ratio 50:40:10)
A catalyst having an average thickness of 51 μm was obtained. Example 6 In Example 1, MnO2-activated carbon-T was prepared in the same manner as in Example 1 except that 200g of 1kg of MnO2 and 100g of activated carbon (Shirasagi A manufactured by Takeda Pharmaceutical Co., Ltd.) was replaced with TiO2.
A catalyst was obtained in which iO2 (weight ratio 70:20:10) was supported with an average thickness of 38μ. Example 7 In Example 1, instead of MnO2, the specific surface area was 55 m
A catalyst supporting CuO with an average thickness of 45 μm was obtained in the same manner as in Example 1 except that CuO was used. Comparative Example 1 A catalyst in which MnO2 was supported with an average thickness of 50 μm was obtained in the same manner as in Example 1 except that 20 kg of Kibushi clay was used and activated carbon was not added when extruding the carrier. Example 8 A catalyst in which MnO2 was supported to an average thickness of 57 μm was obtained in the same manner as in Example 4, except that when extruding the carrier, Kibushi clay was used in an amount of 18 kg, and activated carbon was added in an amount of 2 kg. Reference example: A mixture of 30 g of MnO2 with a specific surface area of 48 m2/g, titanium tetrachloride, and syrinsol (TiO2:SiO2: 1:
1) While stirring and mixing 70 g, ammonia gas was blown in to perform a neutralization reaction, and a slurry-like precipitate was generated. After thoroughly washing the obtained precipitate with water, the temperature was 500°C.
The three-way catalyst MnO2-TiO2-SiO2 (weight ratio 35:30
:35) Powder was obtained. Hereinafter, in the same manner as in Example 1, SiO2-MnO2-TiO2 (weight ratio 35:30:3
A three-way catalyst was obtained in which 5) was supported at a loading rate of 99%. B. Catalytic activity test The catalysts obtained in Examples 1 to 8, Comparative Example 1, and Reference Example were subjected to a catalytic activity test under the following reaction conditions using a testing apparatus whose flow sheet is shown in Figure 1. The ozone decomposition rate at the initial stage, after 10 hours, and after 100 hours was determined. In the figure, (1) is an ozone generator, which generates ozone at an appropriate concentration from the air introduced into it, and guides this ozone-containing air to the catalyst layer (2). The ozone decomposition rate (%) is determined by the following formula from the values at the inlet and outlet of the catalyst layer measured by the ozone analyzer in (3). (Reaction conditions) Space velocity: 20,000/Hr Inlet ozone concentration: 10 ppm Reaction temperature: 20° C. The above test results are shown in Table 1. As is clear from the above table, all the catalysts obtained in Examples 1 to 8 have a higher ozone decomposition rate (%) than the catalysts obtained in Comparative Example 1 and Reference Example, and at the same time It shows almost no deterioration in performance over time and has excellent durability.
【発明の効果】本発明に係るオゾン分解触媒は、オゾン
を効率良く除去し、かつ長時間にわたってその性能の劣
化を示さない。Effects of the Invention The ozone decomposition catalyst according to the present invention efficiently removes ozone and does not show any deterioration in its performance over a long period of time.
第1図は触媒活性試験のフローシートである。 (1)・・オゾン発生器 (2)・・触媒層 (3)・・オゾン分析計 FIG. 1 is a flow sheet of the catalyst activity test. (1)...Ozone generator (2)...Catalyst layer (3)...Ozone analyzer
Claims (1)
質が5〜100μの厚みで担持されていることを特徴と
するオゾン分解用触媒。An ozone decomposition catalyst characterized in that an active substance having ozone decomposition ability is supported on a carrier containing MnO2 to a thickness of 5 to 100 μm.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3198971A JPH04334547A (en) | 1991-05-07 | 1991-05-07 | Ozone decomposing catalyst |
| US07/747,062 US5212140A (en) | 1991-02-28 | 1991-08-19 | Catalyst for decomposing ozone |
| EP91113995A EP0501003B1 (en) | 1991-02-28 | 1991-08-21 | Catalyst and method for decomposing ozone by the use thereof |
| DE69118161T DE69118161T2 (en) | 1991-02-28 | 1991-08-21 | Catalyst and method for decomposing ozone through its use |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3198971A JPH04334547A (en) | 1991-05-07 | 1991-05-07 | Ozone decomposing catalyst |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04334547A true JPH04334547A (en) | 1992-11-20 |
Family
ID=16399975
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3198971A Pending JPH04334547A (en) | 1991-02-28 | 1991-05-07 | Ozone decomposing catalyst |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04334547A (en) |
-
1991
- 1991-05-07 JP JP3198971A patent/JPH04334547A/en active Pending
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