CATALYTIC REFRACTORY HEATING APPLIANCE
20240376015 ยท 2024-11-14
Assignee
Inventors
Cpc classification
C04B41/52
CHEMISTRY; METALLURGY
F23C13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C04B2103/0021
CHEMISTRY; METALLURGY
C04B41/5027
CHEMISTRY; METALLURGY
C04B41/501
CHEMISTRY; METALLURGY
C04B41/52
CHEMISTRY; METALLURGY
C04B38/00
CHEMISTRY; METALLURGY
C04B41/89
CHEMISTRY; METALLURGY
B32B18/00
PERFORMING OPERATIONS; TRANSPORTING
C04B2111/00267
CHEMISTRY; METALLURGY
C04B38/00
CHEMISTRY; METALLURGY
C04B2103/0021
CHEMISTRY; METALLURGY
C04B41/501
CHEMISTRY; METALLURGY
International classification
Abstract
A catalytic refractory heating appliance includes a body formed from a silicon carbide refractory material having a porosity that permits ionic oxygen to pass through the refractory material. The body defines a gas flow channel. A catalyst coating is on a surface of the refractory material of the body, whereby the refractory material becomes an active component with catalytic capability. For example, when the catalytic refractory heating appliance is a fire tube carbon dioxide and sulfur compounds can be directly absorbed, or carbon monoxide is reduced to methane.
Claims
1. A catalytic refractory heating appliance, comprising: a body formed from a silicon carbide refractory material having a porosity that permits ionic oxygen to pass through the refractory material, the body defining a gas flow channel; and a catalyst coating a surface of the refractory material of the body, whereby the refractory material becomes an active component with catalytic capability.
2. The catalytic refractory heating appliance of claim 1, wherein the body is tubular.
3. The catalytic refractory heating appliance of claim 2, wherein the body is a fire tube.
4. The catalytic refractory heating appliance of claim 1, wherein the body is formed of conductive nitride-bonded silicon carbide refractory material.
5. The catalytic refractory heating appliance of claim 1, wherein the catalyst coating is a metal oxide framework catalyst.
6. The catalytic refractory heating appliance of claim 1, wherein the catalyst coating is a metal oxide framework of calcium and magnesium oxide layers interconnected with an iron oxidation pathway for oxygen.
7. The catalytic refractory heating appliance of claim 6, wherein the catalyst coating is a dolomitic limestone whitewash.
8. The catalytic refractory heating appliance of claim 1, wherein a metallic vapor coating is positioned on the silicon carbide refractory material.
9. The catalytic refractory heating appliance of claim 8, wherein the metal vapor coating is combined with the catalyst coating.
10. The catalytic refractory heating appliance of claim 9, wherein the metal vapor coating is comprised of a majority of lead sulfide with bismuth trioxide.
11. A catalytic refractory heating appliance, comprising: a body formed from a conductive nitride-bonded silicon carbide refractory material having a porosity that permits ionic oxygen to pass through the refractory material, the body being tubular and defining a gas flow channel; and a metal oxide framework catalyst coating a surface of the refractory material of the body, whereby the refractory material becomes an active component with catalytic capability.
12. The catalytic refractory heating appliance of claim 11, wherein the metal oxide framework catalyst coating is of calcium and magnesium oxide layers interconnected with an iron oxidation pathway for oxygen.
13. The catalytic refractory heating appliance of claim 11, wherein a metal vapor coating is combined with the metal oxide framework catalyst coating.
14. The catalytic refractory heating appliance of claim 13, wherein the metal vapor coating is comprised of a majority of lead sulfide with bismuth trioxide.
Description
DESCRIPTION OF THE DRAWINGS
[0017] Reference is now made to the accompanying drawings, in which:
[0018]
[0019]
[0020]
[0021]
DETAILED DESCRIPTION
[0022] Aspects of various embodiments are described in relation to the figures.
[0023] A catalytic refractory, generally identified by reference numeral 10, will now be described with reference to
Structure and Relationship of Parts
[0024] Nitride bonded silicon carbide material withstands extreme heat and does not disintegrate when exposed to oxygen. Due to the firing process the resulting silicon carbide material has a porosity that permits ionic oxygen to pass through the refractory materials. By modifying the porosity of the refractory and coating the surface of the refractory with a catalyst, the refractory becomes an active component with catalytic capability. For example, a fire tube can be coated with a metal oxide framework (MOF) catalyst whereby carbon dioxide and sulfur compounds can be directly absorbed, or carbon monoxide is reduced to methane.
[0025] Referring to
[0026] A variation in the dolomitic limestone containing calcium magnesium carbonate forms when iron carbonate is added prior to calcining to form a metal oxide framework of calcium and magnesium oxide layers interconnected with an iron oxidation pathway for oxygen. This catalyst has been demonstrated to reduce up to 80 percent of the carbon dioxide to carbon monoxide while the oxygen oxidizes the iron.
[0027] Referring to
[0028] Referring to
[0029] When heating appliance 50 is shut down, catalytic refractory 10 cools. As MOF catalyst 30 cools it continues to adsorb carbon dioxide from the atmosphere provided the humidity is above a minimum % relative humidity (RH). Regeneration of catalytic refractory 10 coated with MOF catalyst 30 occurs each cycle upon reheating the appliance. In order to increase the number of regeneration cycles and therefore the longevity of MOF catalyst 30, the electrons required to reduce the iron oxide are supplied by a metallic vapor coating 80, between the MOF and the conductive nitride bonded silicon carbide structure. This metal vapor coating consists of a base material consisting of a majority of lead sulfide and bismuth trioxide combined with the dolomitic limestone and iron carbonate prior to calcining the applied whitewash coating.
[0030] The embodiments described in this document provide non-limiting examples of possible implementations of the present technology. Upon review of the present disclosure, a person of ordinary skill in the art will recognize that changes may be made to the embodiments described herein without departing from the scope of the present technology. Practical implementation of the features may incorporate a combination of some or all of the aspects, and features described herein should not be taken as indications of future or existing product plans.