Nozzle for supersonic gas flow and an inertia separator
A nozzle of converging-diverging shape for creating mist flow at supersonic velocity comprising: a throat having a characteristic diameter D*; an inlet having a characteristic diameter D1, positioned a distance L1 upstream of the nozzle throat; and an outlet having a characteristic diameter D2, positioned a distance L2 downstream of the nozzle throat, wherein the ratio of L2/(D2&#8722;D*) is larger than 4, but smaller than 250; an inertia separator based thereon, and a method for supersonic separation of one or more components of a predominantly gaseous stream.
Shell Oil Company
B B B B Y B B E
B04C B01D B05B B01D Y10S B01D B01D E21B
inventional inventional inventional additional additional inventional inventional inventional
Theodoor Cornelis Antonie Johannes Miguel Henri Maria Marco
Van Holten Tjeenk Willink Van Veen Betting