JPH0394834A - Carrier for catalyst - Google Patents
Carrier for catalystInfo
- Publication number
- JPH0394834A JPH0394834A JP1230065A JP23006589A JPH0394834A JP H0394834 A JPH0394834 A JP H0394834A JP 1230065 A JP1230065 A JP 1230065A JP 23006589 A JP23006589 A JP 23006589A JP H0394834 A JPH0394834 A JP H0394834A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- catalyst carrier
- niobium
- based superalloy
- superalloy
- 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 31
- 229910000601 superalloy Inorganic materials 0.000 claims abstract description 22
- 239000000835 fiber Substances 0.000 claims abstract description 15
- 239000002131 composite material Substances 0.000 claims abstract description 13
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 11
- 239000000758 substrate Substances 0.000 claims abstract description 7
- 229910001257 Nb alloy Inorganic materials 0.000 claims abstract description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 16
- 239000010955 niobium Substances 0.000 claims description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 11
- 239000003870 refractory metal Substances 0.000 claims description 9
- 229910052759 nickel Inorganic materials 0.000 claims description 8
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 8
- 229910017052 cobalt Inorganic materials 0.000 claims description 7
- 239000010941 cobalt Substances 0.000 claims description 7
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 7
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 150000002821 niobium Chemical class 0.000 claims 2
- 230000035939 shock Effects 0.000 abstract description 11
- 229910052751 metal Inorganic materials 0.000 abstract description 5
- 239000002184 metal Substances 0.000 abstract description 5
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 abstract description 2
- 229910052721 tungsten Inorganic materials 0.000 abstract description 2
- 239000010937 tungsten Substances 0.000 abstract description 2
- MWUXSHHQAYIFBG-UHFFFAOYSA-N Nitric oxide Chemical compound O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 9
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 239000000446 fuel Substances 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 229910052727 yttrium Inorganic materials 0.000 description 4
- 239000000919 ceramic Substances 0.000 description 3
- 229910052878 cordierite Inorganic materials 0.000 description 3
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 229910052700 potassium Inorganic materials 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 description 3
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- 229910001080 W alloy Inorganic materials 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000000969 carrier Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 2
- 229910052737 gold Inorganic materials 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000007750 plasma spraying Methods 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 238000001953 recrystallisation Methods 0.000 description 2
- 229910003452 thorium oxide Inorganic materials 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 238000007084 catalytic combustion reaction Methods 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000009841 combustion method Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910001120 nichrome Inorganic materials 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Exhaust Gas Treatment By Means Of Catalyst (AREA)
- Catalysts (AREA)
- Gas Burners (AREA)
Abstract
Description
【発明の詳細な説明】
[発明の目的]
(産業七の利用分野)
本発明は触媒用担体に係わり、特に、熱衝撃に強ク、.
高温で高強度を有する耐熱複合体から或る触媒用担体に
関する。[Detailed Description of the Invention] [Object of the Invention] (Field of Application in Industry 7) The present invention relates to a carrier for a catalyst, and particularly to a carrier for a catalyst that is resistant to thermal shock, .
The present invention relates to a catalyst carrier made of a heat-resistant composite material having high strength at high temperatures.
(従来の技術)
最近、省エネルギー、省資源の観点から、ガスタービン
等を駆動するためのガス燃焼器内において、できるだけ
高温で燃料を燃焼させるこ色が望まれている。(Prior Art) Recently, from the viewpoint of energy saving and resource saving, it has been desired to burn fuel at as high a temperature as possible in a gas combustor for driving a gas turbine or the like.
この要望に答えるため、従来は燃料と空気との混合物を
スパークプラグ等の着火手段を用いて、着火燃焼させる
方法が採用きれてきた。しかし,、この場合、燃焼器内
において、2000℃を超える部分が局部的に発生し、
この部分から室素酸化物(NOx)が多量に生成きれる
ために環境汚染の原因となる等の問題があった。In order to meet this demand, conventional methods have been adopted in which a mixture of fuel and air is ignited and combusted using an ignition means such as a spark plug. However, in this case, the temperature exceeds 2000°C locally in the combustor,
There was a problem that a large amount of nitrogen oxide (NOx) could be generated from this part, causing environmental pollution.
この様な問題を解消するために、触媒を用いて燃料と空
気との混合物を燃焼させる触媒方式が提案きれている。In order to solve these problems, a catalytic method has been proposed in which a mixture of fuel and air is combusted using a catalyst.
この燃焼方式は希薄燃料の均一燃焼が可能となり、しか
も、NOxが生成されない上限温度である1500℃程
度まで燃焼温度を高めることができるために、ガス燃焼
器等への応用が有望視されている。This combustion method enables uniform combustion of lean fuel and can raise the combustion temperature to around 1,500 degrees Celsius, which is the upper limit temperature at which no NOx is generated, so it is seen as promising for application in gas combustors, etc. .
この触媒燃焼方式に使用される触媒用担体としては、一
定の機械的強度を有し、しかも、耐熱性を有するコーデ
ィライトセラミックス(2MgO・2’ AI2 0
3 ・5Si02)が良く知られている。しかし、この
コーディライトセラミックスは熱衝撃に弱く、数回の熱
サイクルを受けるとクラックが発生して破横するという
問題かある。The catalyst carrier used in this catalytic combustion method is cordierite ceramics (2MgO・2' AI2 0
3.5Si02) is well known. However, this cordierite ceramic is susceptible to thermal shock and has the problem of cracking and fracture after being subjected to several thermal cycles.
最近、この観点から、自動車の排気ガス浄化用触媒用担
体として、熱衝撃に強く、耐酸化性に優れたフエクラp
イ(FeCrAjl合金)が用いられている。しかしな
がら、このフエクラロイの耐熱温度は900℃程度であ
り、これ以上の温度領域では高温強度が低く、触媒用担
体として使用することができないという問題がある。Recently, from this point of view, Feclap, which is resistant to thermal shock and has excellent oxidation resistance, has been used as a catalyst carrier for purifying automobile exhaust gas.
(FeCrAjl alloy) is used. However, the heat resistance temperature of this Feclaroy is about 900° C., and there is a problem that the high temperature strength is low in a temperature range higher than this, and it cannot be used as a catalyst carrier.
(発明が解決しようとする課題)
前述した様に、従来のコーデイライトセラミックスの触
媒用担体は熱衝撃に弱く、耐久性が充分テはなく、また
、フエクラロイの触媒用担体は耐熱温度が900℃程度
であり、これ以.1二の温度では高温強度が不十分で使
用できないという問題点があった。(Problems to be Solved by the Invention) As mentioned above, conventional cordierite ceramic catalyst carriers are susceptible to thermal shock and do not have sufficient durability, and Feclaroy catalyst carriers have a heat resistance temperature of 900°C. That's about it, and beyond that. At a temperature of 12, there was a problem that the high temperature strength was insufficient and it could not be used.
本発明の目的は、熱衝撃に強く、耐久性に優れており、
高温で高強度を有する触媒用担体を提供することにある
。The purpose of the present invention is to have high resistance to thermal shock and excellent durability.
The object of the present invention is to provide a catalyst carrier that has high strength at high temperatures.
[発明の構成1
(課題を解決するための手段および作用)本発明は、ニ
ッケル基またはコバルト基の超合金基体中に、外周をニ
オブもしくはニオブ合金からなるニオブ層並びにこのニ
オブ層を覆う鉄基超合金からなる超合金層の2重層で覆
われた耐火金属繊維を配設した耐熱複合体からなること
を特徴とする触媒用担体である。また、本発明の触媒用
担体は、この耐熱複合体からなる耐熱複合線で構成され
た網シートを複数積層した構造、例えば、ハニカム構造
を有する。[Structure 1 of the invention (Means and effects for solving the problems) The present invention provides a niobium layer made of niobium or a niobium alloy on the outer periphery and an iron base covering the niobium layer in a nickel-based or cobalt-based superalloy base. This is a catalyst carrier characterized in that it is made of a heat-resistant composite body in which refractory metal fibers covered with a double layer of a superalloy layer made of a superalloy are arranged. Further, the catalyst carrier of the present invention has a structure, for example, a honeycomb structure, in which a plurality of mesh sheets made of heat-resistant composite wires made of this heat-resistant composite are laminated.
本発明の触媒用担体は、高温強度に優れている耐火金属
繊維を高温酸化から保護するために、耐高温酸化に優れ
ているニッケル基またはコバルh基の超合金基体中に配
設した構造の耐熱複合体から成る。The catalyst carrier of the present invention has a structure in which it is disposed in a nickel-based or cobal-h-based superalloy substrate that has excellent high-temperature oxidation resistance in order to protect refractory metal fibers that have excellent high-temperature strength from high-temperature oxidation. Consists of heat-resistant composite.
本発明の触媒用担体としては、タングステン、モリブデ
ン、タンタルもしくはその合金から或る耐火金属繊維を
用いることができるが、実用上は、タングステン合金を
用いることが好ましい。また、W線の高温強度特性を向
上するためにレニウム(Re)を3〜30vt%含有さ
せるのは、この含有量が3vt%を下回ると効果が期待
できず、30vt%を超えるとW線の強度が低下する。As the catalyst carrier of the present invention, a certain refractory metal fiber made of tungsten, molybdenum, tantalum, or an alloy thereof can be used, but it is practically preferable to use a tungsten alloy. In addition, adding rhenium (Re) from 3 to 30vt% to improve the high-temperature strength characteristics of the W wire cannot be expected to be effective if the content is less than 3vt%, and if it exceeds 30vt%, the Strength decreases.
また、W線に酸化トリウム(ThO2)、カリウム、シ
リコン、アルミニウムのいずれかをドープ等により含冑
キせることにより、同様にW線の強度をきらに増すこと
ができる。この含有量はTh02の場合、0.5vt%
〜8vz%の範囲である。また、K,SiもしくはAj
l!を単体もしくは複合で用いる場合の含有量は、50
ppm〜3θOppmの範囲である。ThO2の添加は
分散強化を期待しており、その添加量が0.5wt%未
満ではその効果が期待できず、また、8.vt%を超え
るとむしろ欠陥となる。K,Si,1?については、粒
界への析出を生じ、再結晶に対する抵抗を持たせるので
、50〜300ppmの範囲外では期待できない。この
タングステン合金は1000℃以上の高温での強度劣化
の要因となる再結晶を起こし難いために好適である。Furthermore, the strength of the W wire can be similarly greatly increased by impregnating the W wire with thorium oxide (ThO2), potassium, silicon, or aluminum by doping or the like. In the case of Th02, this content is 0.5vt%
It is in the range of ~8vz%. Also, K, Si or Aj
l! When used alone or in combination, the content is 50
It ranges from ppm to 3θOppm. Addition of ThO2 is expected to strengthen dispersion, but if the amount added is less than 0.5 wt%, this effect cannot be expected. If it exceeds vt%, it will actually become a defect. K, Si, 1? However, it cannot be expected to be outside the range of 50 to 300 ppm because it causes precipitation at grain boundaries and provides resistance to recrystallization. This tungsten alloy is suitable because it hardly causes recrystallization, which causes strength deterioration, at high temperatures of 1000° C. or higher.
また、このWからなる耐火金属繊維の周囲をNb層と超
合金層との2重層で覆うことにより、マトリックスであ
るニッケル基またはコバルト基の超合金ε耐大金属繊維
との高温での反応を防止して、耐火金篇繊維の強度劣化
を防止することができる。このNb層は耐火金属繊維の
熱膨張率とニッケル基またはコバルト基の超合金の熱膨
張率とのψ間の熱膨張率を有するために、熱膨張率差に
よる熱疲労を防止して耐熱衝撃特性を向上きせる。In addition, by covering the periphery of this refractory metal fiber made of W with a double layer of an Nb layer and a superalloy layer, it is possible to prevent the reaction at high temperatures with the nickel-based or cobalt-based superalloy ε-resistant metal fiber that is the matrix. This can prevent deterioration in the strength of the refractory metal fiber. This Nb layer has a coefficient of thermal expansion between ψ between the coefficient of thermal expansion of the refractory metal fiber and the coefficient of thermal expansion of the nickel-based or cobalt-based superalloy, so it prevents thermal fatigue due to the difference in thermal expansion coefficient and resists thermal shock. Improve characteristics.
本発明におけるニッケル基の超合金基体としては、例え
ば、10〜40vt%のC r s 5 〜20vt%
のAN 、0.3 〜!..5wt%のYおよび残部N
iから或るNiCr/JY合金またはto〜40wt%
のCr,5 〜20vt%のAII, 0.3 〜l.
5wt%のY, 5 〜30wt%のCO、O 〜30
wt%のFeおよび残部Niから威るNiCoCrA,
RY合金が用(.1られる。また、コバルト基の超合金
基体とし,では、5〜35vt%のC r , 5 −
20vt%のAJ 、0.3 〜I..5wi%のY,
0〜20wt%のNjおよび残部C0から成るコバルL
基超含企を用いるここができる。The nickel-based superalloy substrate in the present invention includes, for example, 10 to 40 vt% C r s 5 to 20 vt%.
AN, 0.3~! .. .. 5wt% Y and balance N
i to some NiCr/JY alloy or to ~40wt%
of Cr, 5 to 20 vt% AII, 0.3 to l.
5wt% Y, 5~30wt% CO, O~30
NiCoCrA from wt% Fe and balance Ni,
RY alloy is used (.1).Also, a cobalt-based superalloy substrate is used, and 5 to 35 vt% of Cr, 5-
20vt% AJ, 0.3~I. .. 5wi% Y,
Kobal L consisting of 0-20wt% Nj and the balance C0
This is where you can use basic supercompany.
きらに、削大金属繊維の被覆層εし1ての鉄基超合金と
してほ、重量比で20%以下のアルミニウムを含む鉄基
超合金であれば良い。例えば、lO〜30wt%のC
v , 5 〜20vt%のAd! , 0.3 〜1
.5vl%のYおよび残部鉄から或るFeCrAfJY
合金を用いることができる。Furthermore, the iron-based superalloy for the coated layer ε of the reduced metal fibers may be any iron-based superalloy containing 20% or less of aluminum by weight. For example, lO ~ 30 wt% C
v, 5-20vt% Ad! , 0.3 ~1
.. Some FeCrAfJY from 5vl% Y and balance iron
Alloys can be used.
本発明の触媒用担体はニオブ層および超含金膚で彼覆さ
れた耐火金属繊維で超合金の高温強度を高めた耐熱複合
体で構成ずることにより、1000℃以−1二の高温に
おいても充分な高温強度を存(7、しかも、金@蟻の耐
熱諏含休であるために、常温と烏温εの繰返しの熱負葡
を4えた時の耐熱衝撃特性にも優れている。The catalyst carrier of the present invention is composed of a heat-resistant composite made of refractory metal fibers covered with a niobium layer and a supermetallic layer, which increases the high-temperature strength of a superalloy, so that it can withstand temperatures of -12 to 1000°C. It has sufficient high-temperature strength (7).Moreover, it has excellent thermal shock resistance when subjected to repeated heat loads at room temperature and temperature ε, since it contains the heat resistance of gold.
(実施例)
以−F,本発明の実施例について図而を参照して説明す
る。(Embodiments) Hereinafter, embodiments of the present invention will be described with reference to the drawings.
まず、1 . 7vl%のThO2を含有する1a径0
.3 mmのW線を金騰砕に固定し、、回転させながら
、W線の表面に低圧雰囲気プラズマ溶射によってNbを
O..03m+*の厚さに被覆した。続いて、同様な低
圧雰囲気プラズマ溶射によってNb層の上にFeCrA
fiY合金を0.03mmの厚さに被覆し、さらに、低
圧雰囲気プラズマ溶射によってNiCoCrAjlY合
金をO.l+e+mの厚さに被覆して、W/Nb/Fe
C rAj7 Y/N i CoC rAll Yなる
構造を有する複合材料線を作製し,た。First, 1. 1a diameter 0 containing 7vl% ThO2
.. A 3 mm W wire was fixed on a gold plate, and while rotating, Nb was applied to the surface of the W wire by plasma spraying in a low-pressure atmosphere. .. The coating was applied to a thickness of 0.3m+*. Subsequently, FeCrA was deposited on the Nb layer by plasma spraying in a similar low-pressure atmosphere.
The fiY alloy was coated to a thickness of 0.03 mm, and the NiCoCrAjlY alloy was coated with an O. Coated with a thickness of l+e+m, W/Nb/Fe
A composite material wire having the structure C rAj7 Y/N i CoC rAll Y was fabricated.
第1図に平面図、第2詞に側面図を示す様に、この複合
材料線0)を編んで網状シ一ト(2)を作製し,、この
シート20枚をそれらの間にNi基ろう材を挟み込んで
積層し,、この積層体を真空中で1100℃、10分間
の加熱処理を施すことにより、ハニカム構造を有する触
媒用担体(3)を作製した。As shown in the plan view in Fig. 1 and the side view in Fig. 2, this composite material wire 0) was knitted to produce a net-like sheet (2), and 20 sheets of this sheet were placed between them. A catalyst carrier (3) having a honeycomb structure was produced by stacking the layers with a brazing filler metal sandwiched therebetween, and heat-treating the stacked body in a vacuum at 1100° C. for 10 minutes.
この触媒用担体は人気中で、1200℃で200時間の
加熱後、1100℃の高温引張り強さを測定したところ
、60kg『/關2の強度を有しでいた。この測定結果
から、この触媒用担体は高温で長時間加熱を行っても、
充分な高温強度をHし、でいるこεが分った。また、こ
の触媒用担体は、大気中で1200℃、500時間の加
熱処理を行っても酸化されず、耐酸化待性にも優れてい
ることが分った。This catalyst carrier is popular, and when its high-temperature tensile strength at 1100°C was measured after heating at 1200°C for 200 hours, it had a strength of 60 kg/2. From this measurement result, this catalyst carrier shows that even when heated at high temperature for a long time,
After obtaining sufficient high-temperature strength, the strength ε was found. Further, it was found that this catalyst carrier was not oxidized even when subjected to heat treatment at 1200° C. for 500 hours in the air, and had excellent oxidation resistance.
さらに、室温と1200℃との開を急加熱、急冷却を1
00同以」二繰返す熱負荷を勾えても、変形やクラック
の発生はなく、耐熱衝撃特性に優れていることが分った
。Furthermore, the gap between room temperature and 1200℃ was rapidly heated and rapidly cooled for 1 time.
It was found that even when subjected to repeated thermal loads of 0.00 or higher, no deformation or cracks occurred, indicating that the material had excellent thermal shock resistance.
この触媒用担体にニッケル、コバルト等の酸化物や白金
、パラジウム等の触媒をI11持させるこεにより、触
媒とすることができる。A catalyst can be obtained by carrying an oxide such as nickel or cobalt, or a catalyst such as platinum or palladium on this catalyst carrier.
F発明の効果]
Vl上の様に、本発明によれば、熱衝撃に強《、耐久性
に優t1でおり、高温で高強度を角゛する触媒用{U体
を提供することができる。Effects of the Invention] As mentioned above, according to the present invention, it is possible to provide a U-body for catalysts that is resistant to thermal shock, has excellent durability, and exhibits high strength at high temperatures. .
第1図は本発明の実施例に基づく触媒用担体の平面図、
第2図は第1図の触媒用担体の側面図である。
1・・・複合材料線、
3・・・触媒用担体。
2・・・網状シート、FIG. 1 is a plan view of a catalyst carrier according to an embodiment of the present invention;
FIG. 2 is a side view of the catalyst carrier of FIG. 1. 1... Composite material wire, 3... Catalyst carrier. 2... Reticulated sheet,
Claims (2)
外周をニオブもしくはニオブ合金からなるニオブ層並び
にこのニオブ層を覆う鉄基超合金からなる超合金層の2
重層で覆われた耐火金属繊維を配設した耐熱複合体から
なることを特徴とする触媒用担体。(1) In a nickel-based or cobalt-based superalloy substrate,
A niobium layer consisting of niobium or a niobium alloy on the outer periphery, and a superalloy layer consisting of an iron-based superalloy covering this niobium layer.
A catalyst carrier characterized by being made of a heat-resistant composite material in which refractory metal fibers covered with multiple layers are arranged.
外周をニオブもしくはニオブ合金からなるニオブ層並び
にこのニオブ層を覆う鉄基超合金からなる超合金層の2
重層で覆われた耐火金属繊維を配設した耐熱複合体から
なる耐熱複合線で構成された網シートを複数積層した構
造を有することを特徴とする触媒用担体。(2) in a nickel-based or cobalt-based superalloy substrate;
A niobium layer consisting of niobium or a niobium alloy on the outer periphery, and a superalloy layer consisting of an iron-based superalloy covering this niobium layer.
A catalyst carrier characterized in that it has a structure in which a plurality of mesh sheets made of a heat-resistant composite wire made of a heat-resistant composite wire covered with multilayered refractory metal fibers are laminated.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1230065A JPH0394834A (en) | 1989-09-05 | 1989-09-05 | Carrier for catalyst |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1230065A JPH0394834A (en) | 1989-09-05 | 1989-09-05 | Carrier for catalyst |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0394834A true JPH0394834A (en) | 1991-04-19 |
Family
ID=16901995
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1230065A Pending JPH0394834A (en) | 1989-09-05 | 1989-09-05 | Carrier for catalyst |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0394834A (en) |
-
1989
- 1989-09-05 JP JP1230065A patent/JPH0394834A/en active Pending
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