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Title:
A NOZZLE FOR SUPERSONIC GAS FLOW AND AN INERTIA SEPARATOR
Document Type and Number:
WIPO Patent Application WO2000040338
Kind Code:
A8
Abstract:
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-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.

Inventors:
TJEENK WILLINK CORNELIS ANTONI (NL)
BETTING MARCO (NL)
VAN HOLTEN THEODOOR (NL)
VAN VEEN JOHANNES MIGUEL HENRI (NL)
Application Number:
PCT/EP1999/010496
Publication Date:
October 04, 2001
Filing Date:
December 29, 1999
Export Citation:
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Assignee:
SHELL INT RESEARCH (NL)
TJEENK WILLINK CORNELIS ANTONI (NL)
BETTING MARCO (NL)
HOLTEN THEODOOR VAN (NL)
VEEN JOHANNES MIGUEL HENRI MAR (NL)
International Classes:
B01D45/12; B01D45/16; B01D45/04; B01D49/00; B01D51/06; B01D51/08; B01D53/00; B04C3/06; B05B1/00; B05B1/02; C10L3/10; E21B43/38; F25J3/06; (IPC1-7): B05B1/02; B01D45/12
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