FIELD: power engineering industry. SUBSTANCE: side surface of power separation chamber (at distance within one-fourth and three-fourth of its length) is provided with through holes 8. Sound gas-dynamics resonator 3 is connected to pipe connection for incoming compressed flow and communicated with nozzle head 4 through cavity 2 enveloping power separation chamber; resonator itself is located in this chamber. Besides, if more than one resonating cavity is available, cavities are furnished with pistons, limiting length of at least one of cavities within 2-4 its diameters and of at least another one within 5-8 its diameters. At same time, holes 8 in side surface of power separation chamber, arranged closer to nozzle head 4, have diameters within 0.01-0.03 of chamber diameter but not in excess of 0.5 mm, and holes 8 located closer to throttle valve 7 have diameters 1.5-2.0 times greater, with total area of all holes 8 amounting to 0.05-0.1 of minimum passage area of nozzle head 4. EFFECT: enhanced reliability of operation. 2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
VORTEX TUBE | 0 |
|
SU1048264A1 |
VORTEX TUBE | 1992 |
|
RU2043584C1 |
METHOD OF AND DEVICE FOR VORTEX ENERGY SEPARATION OF FLOW | 2002 |
|
RU2227878C1 |
METHOD AND DEVICE FOR VORTEX ENERGY DIVISION OF WORKING FLUID FLOW | 2008 |
|
RU2371642C1 |
VORTEX PIPE | 1992 |
|
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METHOD FOR VORTEX ENERGY SEPARATION OF GAS FLOW AND APPARATUS FOR PERFORMING THE SAME | 2002 |
|
RU2213914C1 |
VORTEX TUBE | 0 |
|
SU1728597A1 |
VORTEX TUBE | 1996 |
|
RU2114358C1 |
VORTEX TUBE | 2013 |
|
RU2533590C2 |
VORTEX TUBE | 0 |
|
SU1099193A1 |
Authors
Dates
1994-09-15—Published
1992-09-07—Filed