US 7,762,807 B2Granted

Gas-fired radiant tube with internal recuperator

AssigneeGas Technology Institute

InventorsMartin Brendan Linck, Harry S. Kurek, Mark J. Khinkis, Aleksandr P. Kozlov

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Abstract

A single-ended, internally recuperated, radiant tube annulus system in which at least part of the heat recovery takes place within the furnace to which the system is attached and in which the oxidant and/or fuel are preheated not only by heat transfer from the exhaust gases, but also directly from the combustion process. The system includes a plurality of concentric radiant tubular members arranged in a manner providing an outer annular region in which the combustion process is carried out, an inner tubular member through which exhaust gases are exhausted from the system, and intermediate annular regions between the inner tubular member and the outer annular region through which preheated oxidant is provided to the outer annular region for the combustion process. In accordance with one embodiment of this invention, the internal recuperator is used as a fuel reformer.

Claims16

Dependent claims

A radiant tube system comprising:

an inner tubular member having an exhaust gas inlet end forming an exhaust gas inlet opening and having an exhaust gas outlet end forming an exhaust gas outlet opening;
an outwardly extending circumferential flange connected with said exhaust gas inlet end of said inner tubular member;
an inner intermediate tubular member concentrically disposed around said inner tubular member having a preheated first gaseous fluid outlet end forming a preheated first gaseous fluid outlet opening proximate said outwardly extending circumferential flange, a first gaseous fluid inlet end proximate said exhaust gas outlet end of said inner tubular member, and forming an inner annular region between said inner tubular member and said inner intermediate tubular member;
an outer intermediate tubular member concentrically disposed around said inner intermediate tubular member forming an outer intermediate annular region between said outer intermediate tubular member and said inner intermediate tubular member and having a first end connected with said outwardly extending circumferential flange and having an opposite second end proximate said first gaseous fluid inlet end of said inner intermediate tubular member;
an outer tubular member concentrically disposed around said outer intermediate tubular member having a closed-offend proximate said exhaust gas inlet end of said inner tubular member, an opposite end proximate said exhaust gas outlet end of said inner tubular member forming an opening through which each of said inner tubular member, inner intermediate tubular member and outer intermediate tubular member extends, and forming an outer annular region between said outer tubular member and said outer intermediate tubular member;
fluid communication means for providing fluid communication between said outer intermediate annular region and said outer annular region;
seal means for sealing between said outer tubular member and said outer intermediate tubular member proximate said exhaust gas outlet end of said inner tubular member proximate said exhaust gas outlet end of said inner tubular member, between said outer intermediate tubular member and said inner intermediate tubular member proximate said exhaust gas outlet end of said inner tubular member, and between said inner intermediate tubular member and said inner tubular member proximate said exhaust gas outlet end of said inner tubular member;
a first gaseous fluid conduit connected with said opposite end of said outer tubular member proximate said exhaust gas outlet end of said inner tubular member and in fluid communication with said outer annular region;
and
a second gaseous conduit connected with said inner intermediate tubular member proximate said first gaseous fluid inlet end and in fluid communication with said inner annular region.

7 more elements

A method for combustion of a fuel and oxidant comprising the steps of:

introducing a first gaseous fluid into an inner annular region formed by an inner tubular member having an exhaust gas inlet end forming an exhaust gas inlet opening and having an exhaust gas outlet end forming an exhaust gas outlet opening and an inner intermediate tubular member concentrically disposed around said inner tubular member having a preheated first gaseous fluid outlet end forming a preheated first gaseous fluid outlet opening proximate said exhaust gas inlet end of said inner tubular member and a first gaseous fluid inlet end proximate said exhaust gas outlet end of said inner tubular member, whereby said first gaseous fluid flows in a direction of said exhaust gas inlet end of said inner tubular member, producing a preheated first gaseous fluid;
passing said preheated first gaseous fluid through an outer intermediate annular region formed between said inner intermediate tubular member and an outer intermediate tubular member concentrically disposed around said inner intermediate tubular member whereby said preheated first gaseous fluid flows in a direction of said exhaust gas outlet end of said inner tubular member;
introducing a second gaseous fluid into an outer annular region formed between said outer intermediate tubular member and an outer tubular member concentrically disposed around said outer intermediate tubular member and introducing said preheated first gaseous fluid into said outer annular region, resulting in mixing of said preheated first gaseous fluid and said second gaseous fluid;
igniting said mixture in said outer annular region, forming a flame and producing exhaust gas;
introducing said exhaust gas through said exhaust gas inlet opening into said inner tubular member;
and
exhausting said exhaust gas through said exhaust gas outlet opening of said inner tubular member.

4 more elements

Dependencies are inferred from the claim text.

Facts

Application: 12/108,986Filed 24 Apr 2008
Published: US 2009/0269710 A129 Oct 2009
Granted: 27 Jul 2010
Term ends: Not estimatedThe source records don’t support an estimate.

Classification14 codes

F23L 15/04
Heating of air supplied for combustion: arrangements of recuperators
F23C 3/002
Combustion apparatus characterised by the shape of the combustion chamber: the chamber having an elongated tubular form, e.g. for a radiant tube
F23D 14/126
Radiant burners: cooperating with refractory wall surfaces
F23C 2900/03002
Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor:…