Furnace for the production of russian gas and a method for its operation

摘要

PICT:0673155/III/1 PICT:0673155/III/2 PICT:0673155/III/3 A furnace for the production of carbon black wherein a hydrocarbon injector tube is centrally situated in the inlet end wall and is surrounded by a plurality of burners parallel thereto positioned near the side walls, comprises a combustion chamber in which the distance between opposing flat inlet and exit end walls is 0.25 to 2 times the distance between the side walls, an outlet orifice in the centre of the exit wall having an area of 5-25 per cent of the cross-sectional area of the combustion chamber and a reaction chamber communicating with the combustion chamber through the orifice having a volume equal to at least 45 per cent of the volume of the combustion chamber and a cross-sectional area at least equal to that of the orifice. The cross-section of orifice, combustion and reaction chambers is preferably cylindrical. In Fig. 1 the hydrocarbon inlet pipe 38 passes through an opening of larger diameter in the inlet wall 22 of the combustion chamber 18 so as to provide an annular passage 36 for cooling air from a plenum chamber 26. A plurality of burners 44 supplied with fuel from jets 48 and air from the plenum chamber are arranged perpendicular to the end wall 16 of the combustion chamber. The orifice 54 lets into a section chamber 20 which may, as shown in Fig. 4, be larger than the orifice. The inlet end wall of the combustion chamber may be formed by a loose fitting adjustable block 78, Fig. 5, leaving an annular passage 80 between it and the chamber wall. A circular burner pipe 92 injects fuel into the passage through a plurality of orifices preferably at 45 degrees to the side walls. In operation a combustible mixture of fuel and an oxygen containing gas in a proportion of 90-125 per cent of that required for complete combustion of the fuel, is injected at such a rate that the combustion gases pass through the combustion chamber at 150-600 c.f.m., perpendicularly on to the exit end wall to form violent turbulence. A gaseous hydrocarbon is injected axially into the combustion chamber as an expanding cone. Specification 672,074 is referred to.