BURNER AND METHOD FOR COMBUSTING FUELS

51 BURNER AND METHOD FOR COMBU6TING FUELS ABSTRACT OF THE DISCLOSURE A BURNER INCLUDES SEPARATE FUEL AND OXIDANT CONDUITS. THE FUEL CONDUIT HAS INLET, TRANSITIONAL, AND OUTLET SECTIONS, AND THE OXIDANT CONDUIT HAS INLET AND OUTLET SECTIONS. THE 5 CROSS SECTIONAL FLOW AREA OF THE FUEL TRANSITIONAL SE...

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1. Verfasser:	MARK DANIEL D' AGOSTINI
Format:	Patent
Sprache:	eng
Schlagworte:	AIR BLASTING BURNERS CHEMISTRY COMBUSTION APPARATUS COMBUSTION PROCESSES GLASS HEATING LIGHTING MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES MECHANICAL ENGINEERING METALLURGY METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN MINERAL OR SLAG WOOL WEAPONS
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Zusammenfassung:	51 BURNER AND METHOD FOR COMBU6TING FUELS ABSTRACT OF THE DISCLOSURE A BURNER INCLUDES SEPARATE FUEL AND OXIDANT CONDUITS. THE FUEL CONDUIT HAS INLET, TRANSITIONAL, AND OUTLET SECTIONS, AND THE OXIDANT CONDUIT HAS INLET AND OUTLET SECTIONS. THE 5 CROSS SECTIONAL FLOW AREA OF THE FUEL TRANSITIONAL SECTION VARIES FROM AN INITIAL CROSS SECTIONAL FLOW AREA AT THE FUEL INTAKE TO A DIFFERENT CROSS SECTIONAL FLOW AREA AT THE FUEL OUTTAKE, AND THE CROSS SECTIONAL FLOW AREA OF THE FUEL OUTLET SECTION IS SUBSTANTIALLY UNIFORM. AT LEAST SOME OF THE OXIDANT INLET SECTION IS SPACED AROUND SUBSTANTIALLY ALL OF AT LEAST A PORTION OF AT LEAST ONE OF THE FUEL INLET, TRANSITIONAL, AND OUTLET SECTIONS. THE CROSS SECTIONAL FLOW AREA OF THE OXIDANT 'JO OUTLET SECTION IS LESS THAN OR EQUAL TO THE CROSS SECTIONAL FLOW AREA OFTHE OXIDANT INLET SECTION AND IS SUBSTANTIALLY UNIFORM, AND AT LEAST SOME OF IT IS SPACED AROUND SUBSTANTIALLY ALL OF AT LEAST A PORTION OF THE FUEL OUTLET SECTION. S7