JPH0324967Y2 - - Google Patents
Info
- Publication number
- JPH0324967Y2 JPH0324967Y2 JP662885U JP662885U JPH0324967Y2 JP H0324967 Y2 JPH0324967 Y2 JP H0324967Y2 JP 662885 U JP662885 U JP 662885U JP 662885 U JP662885 U JP 662885U JP H0324967 Y2 JPH0324967 Y2 JP H0324967Y2
- Authority
- JP
- Japan
- Prior art keywords
- support
- heat
- combustion
- combustion catalyst
- particle layer
- 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.)
- Expired
Links
- 239000003054 catalyst Substances 0.000 claims description 33
- 238000002485 combustion reaction Methods 0.000 claims description 31
- 239000007789 gas Substances 0.000 claims description 28
- 239000002245 particle Substances 0.000 claims description 22
- 230000003197 catalytic effect Effects 0.000 claims description 12
- 239000000446 fuel Substances 0.000 claims description 9
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 2
- 238000007084 catalytic combustion reaction Methods 0.000 claims description 2
- 239000001301 oxygen Substances 0.000 claims description 2
- 229910052760 oxygen Inorganic materials 0.000 claims description 2
- 238000006243 chemical reaction Methods 0.000 description 11
- 238000002407 reforming Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 5
- 230000001737 promoting effect Effects 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 239000002737 fuel gas Substances 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 1
- 229910052878 cordierite Inorganic materials 0.000 description 1
- 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 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Description
【考案の詳細な説明】
(産業上の利用分野)
本考案は触媒燃焼器に係り、特に粒状の燃焼触
媒のサポートの熱による変形、破損を防止するに
好適な触媒燃焼器に関する。[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to a catalytic combustor, and more particularly to a catalytic combustor suitable for preventing deformation and damage of supports for granular combustion catalysts due to heat.
(従来の技術)
従来の触媒燃焼器は、例えば燃料電池用改質炉
(水素ガス発生装置)を例にとれば、第4図に示
すように、水素発生装置の反応管3を加熱するた
め、反応管3の間に充填した燃焼触媒層4内で燃
料ガスと空気の予混合ガスを燃焼させるようにし
たもので、筒状の装置本体1の底部に設けられた
板状多孔体またはハニカム状体からなるサポート
5と、該サポート5の下部に設けられたウインド
ボツクス9と、該サポート5上に充填、支持され
た燃焼触媒層4およびその上部に設けられた伝熱
促進粒子層6と、該燃焼触媒層4内に挿入された
反応管3と、該反応管3内に充填された改質触媒
2と、該反応管の改質触媒2中に挿入された、底
部が開放された改質ガス管3内と、前記ウインド
ボツクス9に設けられた予混合ガスノズル8と、
前記改質触媒2を通してガスを供給するための原
料ガスノズル11と、前記改質ガス管3Aの上部
の改質ガス室12Aに設けられた改質ガス排出ノ
ズル12とから構成される。このような装置にお
いて、燃料を含む予混合ガスは約300℃に予熱さ
れてノズル8からウインドボツクス9内に供給さ
れ、ハニカム状または多孔板状のサポート5を通
過して燃焼触媒層4内で約1000〜1200℃で燃焼
し、反応管3を加熱した後、燃焼排ガスは排ガス
出口10から排出される。(Prior Art) Taking a fuel cell reformer (hydrogen gas generator) as an example, a conventional catalytic combustor is used to heat the reaction tube 3 of the hydrogen generator, as shown in FIG. , a premixed gas of fuel gas and air is combusted in a combustion catalyst layer 4 filled between reaction tubes 3, and a plate-shaped porous body or honeycomb provided at the bottom of the cylindrical device body 1. A support 5 consisting of a shaped body, a wind box 9 provided at the bottom of the support 5, a combustion catalyst layer 4 filled and supported on the support 5, and a heat transfer promoting particle layer 6 provided above the support 5. , a reaction tube 3 inserted into the combustion catalyst layer 4, a reforming catalyst 2 filled in the reaction tube 3, and a bottom part of the reaction tube inserted into the reforming catalyst 2. A premixed gas nozzle 8 provided in the reformed gas pipe 3 and the wind box 9,
It is composed of a source gas nozzle 11 for supplying gas through the reforming catalyst 2, and a reformed gas discharge nozzle 12 provided in the reformed gas chamber 12A above the reformed gas pipe 3A. In such a device, a premixed gas containing fuel is preheated to approximately 300°C and is supplied from a nozzle 8 into a wind box 9, passes through a honeycomb-shaped or perforated plate-shaped support 5, and enters the combustion catalyst layer 4. After burning at about 1000-1200°C and heating the reaction tube 3, the combustion exhaust gas is discharged from the exhaust gas outlet 10.
(考案が解決しようとする問題点)
しかしながら、このような触媒燃焼器において
は下記のような欠点がある。(Problems to be solved by the invention) However, such a catalytic combustor has the following drawbacks.
(1) サポート5が燃焼触媒層4と直接接触するた
め、サポート5の厚さ方向の温度差が大きく、
サポートが熱変形または破損する。第5図は、
触媒層付近の燃焼装置の詳細図、第6図は、ウ
インドボツクスから触媒層までの温度分布を示
す図であるがサポートの厚さ方向の温度差が大
きいことがわかる。(1) Since the support 5 is in direct contact with the combustion catalyst layer 4, the temperature difference in the thickness direction of the support 5 is large.
Supports become thermally deformed or damaged. Figure 5 shows
FIG. 6, a detailed view of the combustion device near the catalyst layer, shows the temperature distribution from the wind box to the catalyst layer, and it can be seen that there is a large temperature difference in the thickness direction of the support.
(2) サポート5の材料として、耐熱性に優れたム
ライト(使用限界温度1650℃)等を使用して
も、熱衝撃性が劣るため破損することがある。(2) Even if mullite, which has excellent heat resistance (maximum operating temperature 1650°C), is used as the material for the support 5, it may be damaged due to its poor thermal shock resistance.
(3) サポート5の材料として熱衝撃性の比較的優
れたコーデイエライト等を使用した場合、使用
限界温度が約1200℃であり、特にサポート表面
で熱による変形、破損を生じ易い。(3) When cordierite or the like, which has relatively excellent thermal shock resistance, is used as the material for the support 5, the operating temperature limit is approximately 1200°C, and the support surface is particularly susceptible to deformation and breakage due to heat.
本考案の目的は、上記した従来技術の欠点をな
くし、燃焼触媒層との直接接触によるサポートの
熱変形、破損を防止した触媒燃焼器を提供するこ
とにある。 It is an object of the present invention to provide a catalytic combustor that eliminates the drawbacks of the prior art described above and prevents thermal deformation and damage of the support due to direct contact with the combustion catalyst layer.
(問題点を解決するための手段)
要するに本考案は、粒子状の燃焼触媒層とサポ
ート間に耐熱性粒子層を設け、燃焼部の熱が直接
サポートに伝わらないようにしたものである。す
なわち、本考案は、燃料と酸素を含むガスを燃焼
させるための粒状の燃焼触媒と該燃焼触媒を支持
するためのサポートを有する触媒燃焼器におい
て、燃焼触媒粒子層とサポートとの間に耐熱性粒
子層を配置し、高温の触媒燃焼部との直接接触に
よるサポートの熱変形および破損を防止したこと
を特徴とする。(Means for Solving the Problems) In short, the present invention provides a heat-resistant particle layer between the particulate combustion catalyst layer and the support so that the heat of the combustion part is not directly transmitted to the support. That is, the present invention provides a catalytic combustor having a granular combustion catalyst for combusting gas containing fuel and oxygen and a support for supporting the combustion catalyst. A particle layer is arranged to prevent the support from being thermally deformed and damaged due to direct contact with the high-temperature catalytic combustion section.
本考案において、耐熱粒子層としては、アルミ
ナ粒子層など、一般に燃焼温度(例えば1200℃)
以上の耐熱性を有する粒子層が用いられる。 In this invention, the heat-resistant particle layer is generally made of alumina particle layer, etc., which has a combustion temperature (for example, 1200℃).
A particle layer having the above heat resistance is used.
(実施例)
第1図は、本考案の触媒燃焼器を燃料電池用改
質炉に適用した場合の実施例を示す。本改質炉
は、サポート5と燃焼触媒層4の間に耐熱性粒子
層7を設ける以外は第4図の装置と同じ構成を有
する。すなわち、本装置は、改質装置本体1と、
改質触媒2を充填した反応管3と、予混合ガスを
燃焼させるための粒状の燃焼触媒層4と、そのサ
ポート5と、伝熱促進粒子層6と、本考案による
耐熱性粒子層7等から構成される。(Example) FIG. 1 shows an example in which the catalytic combustor of the present invention is applied to a reforming furnace for fuel cells. This reformer has the same configuration as the apparatus shown in FIG. 4 except that a heat-resistant particle layer 7 is provided between the support 5 and the combustion catalyst layer 4. That is, this device includes a reformer main body 1,
A reaction tube 3 filled with a reforming catalyst 2, a granular combustion catalyst layer 4 for burning premixed gas, its support 5, a heat transfer promoting particle layer 6, a heat-resistant particle layer 7 according to the present invention, etc. It consists of
上記構成の装置において、予混合ガスノズル8
からウインドボツクス9内に供給された燃料ガス
と空気の予混合ガスは、約300℃に予熱されてお
り、ハニカム状のサポート5および耐熱性粒子層
7を通つて燃焼触媒粗4内で約1200℃で燃焼す
る。反応管3の先端部より上方は断熱促進粒子6
が充填されており、燃焼ガスは該伝熱促進粒子層
を通過しながら反応管3を加熱し、約550℃で排
ガスノズル10から排出される。 In the apparatus having the above configuration, the premixed gas nozzle 8
The premixed gas of fuel gas and air supplied into the wind box 9 from Burns at ℃. Above the tip of the reaction tube 3 are heat insulation promoting particles 6.
The combustion gas heats the reaction tube 3 while passing through the heat transfer promoting particle layer, and is discharged from the exhaust gas nozzle 10 at about 550°C.
一方都市ガスとスチームの混合ガスは原料ガス
ノズル11から反応管3内に入り、改質触媒層2
内で管外からの伝熱により約800℃まで加熱され
て水素リツチな改質ガスとなり、改質ガスノズル
12から排出され、燃料電池用の燃料として使用
される。 On the other hand, the mixed gas of city gas and steam enters the reaction tube 3 from the raw material gas nozzle 11, and enters the reforming catalyst layer 2.
Inside the tube, it is heated to about 800° C. by heat transfer from outside the tube, becoming hydrogen-rich reformed gas, which is discharged from the reformed gas nozzle 12 and used as fuel for the fuel cell.
前述の如く、燃料ガスと空気の予混合ガスは、
燃焼触媒層4内で約1200℃で燃焼するが、該燃焼
触媒層とハニカム状のサポート5の間には第2図
に示すように本考案になる耐熱温度1500℃のアル
ミナ製耐熱粒子層7が設けられているため、サポ
ート5は高温の燃焼触媒層7と直接接触せず、熱
的に保護される。 As mentioned above, the premixed gas of fuel gas and air is
Combustion occurs at approximately 1200°C within the combustion catalyst layer 4, and between the combustion catalyst layer and the honeycomb-shaped support 5 is a heat-resistant particle layer 7 made of alumina with a heat-resistant temperature of 1500°C according to the present invention, as shown in FIG. , the support 5 does not come into direct contact with the high-temperature combustion catalyst layer 7 and is thermally protected.
改質装置の燃焼部付近の軸方向の温度分布を第
3図に示す。サポート5内の厚さ方向の温度分布
は均一化されているが、これは以下の理由によ
る。すなわち、耐熱性粒子層7により燃焼触媒層
4からの熱輻射が防止されること、耐熱性粒子と
サポートとの接触面積が少なく、伝導伝熱はほと
んど無いこと、および下方からの予混合ガスによ
りサポートは常に冷却されていることなどのため
である。以上に述べた理由により、サポート5の
厚さ方向の温度分布はほとんど無く、均一で、か
つ温度も例えば約300℃と一定である。 Figure 3 shows the temperature distribution in the axial direction near the combustion section of the reformer. The temperature distribution in the thickness direction within the support 5 is made uniform for the following reason. That is, heat radiation from the combustion catalyst layer 4 is prevented by the heat-resistant particle layer 7, the contact area between the heat-resistant particles and the support is small, and there is almost no conductive heat transfer, and the premixed gas from below This is because the support is always cooled. For the reasons stated above, the temperature distribution in the thickness direction of the support 5 is almost non-uniform, and the temperature is constant, for example, about 300°C.
なお、耐熱性粒子層7内には、第3図に示すよ
うに急勾配の温度分布を生じるが、粒子状である
ため、温度分布を生じるが、粒子状であるため、
温度分布に基づく熱応力による変形、破損を生じ
ることはない。また燃料電池用改質装置では、高
速起動、停止を頻繁に生じ、従つてサポートに耐
熱衝撃性が要求されるが、約300℃程度の低温で
使用されるため、耐熱衝撃性に優れたSUS材等
の使用も可能である。 In addition, as shown in FIG. 3, a temperature distribution with a steep gradient occurs within the heat-resistant particle layer 7, but since it is in the form of particles, a temperature distribution occurs; however, since it is in the form of particles,
No deformation or damage occurs due to thermal stress based on temperature distribution. In addition, fuel cell reformers frequently start up and stop at high speeds, so the support must have thermal shock resistance.Since it is used at a low temperature of approximately 300°C, SUS, which has excellent thermal shock resistance, is used. It is also possible to use materials such as wood.
本考案の触媒燃焼器は、燃料電池用の改質反応
装置のみならず、触媒粒子のサポートが高温にさ
れる他の燃焼装置にも広く適用することができ
る。 The catalytic combustor of the present invention can be widely applied not only to reforming reactors for fuel cells but also to other combustion devices in which catalyst particle supports are heated to high temperatures.
(考案の効果)
本考案によれば、燃焼触媒層を指示するサポー
トの上部に耐熱性粒子層を設けることにより、該
サポートの熱による変形、破損が防止することが
でき、従つてサポート材として耐熱温度の低い材
料も使用可能になる。(Effects of the invention) According to the invention, by providing a heat-resistant particle layer on the top of the support that directs the combustion catalyst layer, it is possible to prevent the support from deformation and damage due to heat, and therefore it can be used as a support material. Materials with low heat resistance can also be used.
第1図は、本考案による触媒燃焼器を改質装置
に適用した場合の断面図、第2図は、第1図の燃
焼触媒支持の詳細図、第3図は、第2図に示す部
分の軸方向の温度分布を示す図、第4図は、従来
技術による燃焼触媒燃焼器の断面図、第5図は、
第4図の燃焼触媒支持部の詳細図、第6図は、第
5図に示す部分の軸方向の温度分布を示す図であ
る。
1……触媒燃焼器(改質装置)本体、2……改
質触媒、3……反応管、4……燃焼触媒層、5…
…サポート、6……伝熱促進粒子、8……予混合
ガスノズル、9……ウインドボツクス、10……
排ガスノズル、11……原料ガスノズル、12…
…改質ガスノズル。
Figure 1 is a cross-sectional view of the catalytic combustor according to the present invention applied to a reformer, Figure 2 is a detailed view of the combustion catalyst support in Figure 1, and Figure 3 is the part shown in Figure 2. FIG. 4 is a cross-sectional view of a combustion catalyst combustor according to the prior art, and FIG. 5 is a diagram showing the temperature distribution in the axial direction of
FIG. 4 is a detailed view of the combustion catalyst support portion, and FIG. 6 is a diagram showing the temperature distribution in the axial direction of the portion shown in FIG. 5. 1... Catalytic combustor (reformer) main body, 2... Reforming catalyst, 3... Reaction tube, 4... Combustion catalyst layer, 5...
... Support, 6 ... Heat transfer accelerator particles, 8 ... Premixed gas nozzle, 9 ... Wind box, 10 ...
Exhaust gas nozzle, 11... Raw material gas nozzle, 12...
...Reformed gas nozzle.
Claims (1)
の燃焼触媒と該燃焼触媒を支持するためのサポー
トを有する触媒燃焼器において、燃焼触媒粒子層
とサポートとの間に耐熱性粒子層を配置し、高温
の触媒燃焼部との直接接触によるサポートの熱変
形および破損を防止したことを特徴とする触媒燃
焼器。 In a catalytic combustor having a granular combustion catalyst for burning a gas containing fuel and oxygen and a support for supporting the combustion catalyst, a heat-resistant particle layer is arranged between the combustion catalyst particle layer and the support, A catalytic combustor characterized by preventing thermal deformation and damage of a support due to direct contact with a high-temperature catalytic combustion part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP662885U JPH0324967Y2 (en) | 1985-01-21 | 1985-01-21 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP662885U JPH0324967Y2 (en) | 1985-01-21 | 1985-01-21 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61128512U JPS61128512U (en) | 1986-08-12 |
| JPH0324967Y2 true JPH0324967Y2 (en) | 1991-05-30 |
Family
ID=30484245
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP662885U Expired JPH0324967Y2 (en) | 1985-01-21 | 1985-01-21 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0324967Y2 (en) |
-
1985
- 1985-01-21 JP JP662885U patent/JPH0324967Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS61128512U (en) | 1986-08-12 |
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