Injection of solids into liquids by means of a shrouded supersonic gas jet
View Patent ↗A method of introducing a solid particulate reagent into a bath of metallurgical liquid comprises a step of introducing a solid particulate reagent into a main supersonic gas jet. The main supersonic gas jet is directed at the surface of the bath and is surrounded with a jet of shrouding gas, preferably of a burning hydrocarbon fluid fuel, provided at a supersonic velocity. The main supersonic gas jet is formed at a velocity which is in the range of minus 10% to plus 10% of the velocity at which the jet of shrouding gas is formed, preferably in the range of Mach 2 to 3.
1. A method of introducing a solid particulate reagent into a bath of metallurgical liquid, comprising: introducing a solid particulate reagent into a main supersonic gas jet, directing the main supersonic gas jet at a surface of the bath, and surrounding the main supersonic gas jet with a jet of shrouding gas, characterized in that the shrouding gas jet is ejected from a converging-diverging nozzle at supersonic velocity, the main supersonic gas jet is at a first velocity and the shrouding gas jet at a second velocity, the second velocity being equal to or greater than the first velocity, and the shrouding gas jet comprises a burning hydrocarbon fluid fuel.
2. The method according to claim 1 , wherein a flame created by the burning hydrocarbon fluid fuel terminates at the surface of the bath.
3. The method according to claim 1 , wherein the main supersonic gas jet issues from a converging-diverging nozzle.
4. The method according to claim 1 , wherein the main supersonic gas jet and the shrouding gas jet are provided at a velocity in the range of Mach 1.5 to 4.
5. The method according to claim 4 , wherein the velocity is in the range of Mach 2 to 3.
6. The method according to claim 1 , wherein the main supersonic gas jet includes a gas comprising at least 70% by volume of a gas selected from the group consisting of free oxygen, air, argon and nitrogen.
7. The method according to claim 3 , wherein the jet of shrouding gas is ejected from another converging-diverging nozzle.