WO2004016338A1 - Procede et dispositif de chesterenko d'acceleration de gaz par ejection ou « ajutage de chesterenko » - Google Patents

Procede et dispositif de chesterenko d'acceleration de gaz par ejection ou « ajutage de chesterenko » Download PDF

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Publication number
WO2004016338A1
WO2004016338A1 PCT/RU2003/000351 RU0300351W WO2004016338A1 WO 2004016338 A1 WO2004016338 A1 WO 2004016338A1 RU 0300351 W RU0300351 W RU 0300351W WO 2004016338 A1 WO2004016338 A1 WO 2004016338A1
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WIPO (PCT)
Prior art keywords
gas
section
chτο
nozzle
ποτοκa
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Ceased
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PCT/RU2003/000351
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English (en)
Russian (ru)
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WO2004016338A8 (fr
Inventor
Nikolai Alekseyevich Shesterenko
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Priority claimed from PCT/RU2002/000391 external-priority patent/WO2003025379A1/fr
Priority claimed from RU2003121606/12A external-priority patent/RU2003121606A/ru
Priority claimed from RU2003123127/12A external-priority patent/RU2267360C2/ru
Application filed by Individual filed Critical Individual
Priority to AU2003264567A priority Critical patent/AU2003264567A1/en
Publication of WO2004016338A1 publication Critical patent/WO2004016338A1/fr
Publication of WO2004016338A8 publication Critical patent/WO2004016338A8/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
    • B01D45/12—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces
    • B01D45/16—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces generated by the winding course of the gas stream, the centrifugal forces being generated solely or partly by mechanical means, e.g. fixed swirl vanes

Definitions

  • the invention is obtained by the technique of collecting and drying the gas, and may also be used as a result of increased gas consumption.
  • ⁇ ed ⁇ s ⁇ a ⁇ m ⁇ i ⁇ a yavlyaegsya not is ⁇ lz ⁇ vanie eg ⁇ in ⁇ am ⁇ a ⁇ ⁇ muly iz ⁇ b ⁇ e ⁇ eniya in ⁇ aches ⁇ ve gaz ⁇ v ⁇ g ⁇ ⁇ azdeli ⁇ elya ⁇ e ⁇ ⁇ az and ⁇ azdeli ⁇ elya ⁇ ⁇ a ⁇ tsiyam mn ⁇ g ⁇ m ⁇ nen ⁇ n ⁇ g ⁇ gas and ⁇ ayu ⁇ e ⁇ su ⁇ s ⁇ vie ⁇ muly iz ⁇ b ⁇ e ⁇ eniya on va ⁇ ian ⁇ , iz ⁇ b ⁇ azhenny on ⁇ ig. 21. - 4 - Tax 1
  • Tax 3 Failure of Tax 3 is the same as for analogs 1 and 2. - 5 -
  • Tax 4 The Asset of the Sixth Edition of the Patent of the Russian Federation is known. ⁇ 2206410 (C2)
  • s ⁇ de ⁇ z haschy s ⁇ sn ⁇ us ⁇ an ⁇ vlennye with ge ⁇ me ⁇ ichnym s ⁇ edineniem between s ⁇ b ⁇ y s ⁇ la, ⁇ i ⁇ iches ⁇ e section ⁇ azhd ⁇ g ⁇ ⁇ y ⁇ of not less ⁇ i ⁇ iches ⁇ g ⁇ sectional ⁇ e ⁇ v ⁇ g ⁇ ⁇ ⁇ du movement s ⁇ la gas ⁇ lichayuschiysya ⁇ em, ch ⁇ least dvu ⁇ s ⁇ el ⁇ e ⁇ vy ⁇ ⁇ du gas motion vy ⁇ lneny tapered.
  • Tax 4 Failure of Tax 4 is the same as for analogs 1, 2, and 3.
  • the inadequacy of analogue 5 is the inability to use it for the separation of phases and the non-disengagement of pressure
  • ⁇ ed ⁇ s ⁇ a ⁇ m anal ⁇ ga 6 yavlyae ⁇ sya nev ⁇ zm ⁇ zhn ⁇ s ⁇ is ⁇ lz ⁇ va ⁇ it in ⁇ aches ⁇ ve ⁇ az ⁇ v ⁇ g ⁇ ⁇ azdeli ⁇ elya on ⁇ i ⁇ azy (gas ⁇ ve ⁇ dye chas ⁇ itsy, zhid ⁇ s ⁇ ) and ⁇ a ⁇ zhe ne ⁇ b ⁇ dim ⁇ s ⁇ s ⁇ zdaniya sve ⁇ zvu ⁇ v ⁇ g ⁇ ⁇ e ⁇ e ⁇ ada pressure and ⁇ a ⁇ zhe nev ⁇ zm ⁇ zhn ⁇ s ⁇ is ⁇ lz ⁇ va ⁇ eg ⁇ for ⁇ azdeleniya gas to ⁇ a ⁇ tsii.
  • Tax 7 A phased isolator of the Sixth Automated Certificate of the CCC ° 845065 is known.
  • the separator item 2 characterized in that the support is in the form of a vessel with a liquid for discharging a dispersed phase.
  • analogue 7 The disadvantage of analogue 7 is the inability to use it as a separator for phases and for various fractions, and it is also indispensable - 7 - there is a compressor at the input that ensures an ultrasonic pressure drop, and at the outlet there is a vacuum pump with a large output.
  • Tax ⁇ A phased isolator is known for autocertificate CCC ⁇ ° 920468.
  • Phase Separator for Auto St. ⁇ 845,065, ⁇ lichayuschiysya ⁇ em, ch ⁇ the purpose ⁇ vysheniya e ⁇ e ⁇ ivn ⁇ s ⁇ i ⁇ azdeleniya ⁇ az dis ⁇ e ⁇ sn ⁇ g ⁇ ⁇ a, sve ⁇ zvu ⁇ v ⁇ y di ⁇ uz ⁇ vy ⁇ lnen mn ⁇ g ⁇ s ⁇ ach ⁇ vym with external szha ⁇ iem, ⁇ ichem ⁇ ve ⁇ n ⁇ s ⁇ , ⁇ b ⁇ azuyuschaya s ⁇ ach ⁇ i, ⁇ b ⁇ aschena in sto ⁇ nu ⁇ dl ⁇ zh ⁇ i.
  • the separator is ⁇ .1, distinguished by the fact that, for the purpose of applying the aerosol to the rotational enclosure, it is complete and multi-diffuser made by the koltsy.
  • analogue 8 Failure of analogue 8 is the same as for analogue 7, i.e. It is not possible to use it to separate the dispersed flow into phases, and the gas into various fractions and the need to have a vacuum and vacuum.
  • the purpose of the proposed invention is the separation of the dispersed flow into phases and phases, as well as the separation of the flow of gases into the fraction and expansion of the use of the device. The above goal is achieved by the following: - 8 -
  • s ⁇ de ⁇ z haschy us ⁇ an ⁇ vlennye ge ⁇ me ⁇ ichn ⁇ between s ⁇ b ⁇ yu s ⁇ la, ⁇ i ⁇ iches ⁇ ie sectional ⁇ to ⁇ y ⁇ not less ⁇ e ⁇ v ⁇ go ⁇ ⁇ du dis ⁇ e ⁇ sn ⁇ g ⁇ ⁇ a (gas) s ⁇ la, ⁇ lichayuschiysya ⁇ em, ch ⁇ ⁇ s nasad ⁇ a is ⁇ ivlena, ⁇ i e ⁇ m not mnee than ⁇ dn ⁇ not ⁇ slednee s ⁇ l ⁇ ⁇ ⁇ du movement dis ⁇ e ⁇ sn ⁇ g ⁇ ⁇ a ( gas) or as a vy ⁇ lnen ⁇ sve ⁇ zvu ⁇ v ⁇ g ⁇ s ⁇ la She ⁇ ge ⁇ en ⁇ , imeyuscheg ⁇ d ⁇ zvu ⁇ v ⁇ y ⁇ n ⁇ uz ⁇ and simme ⁇ ichn
  • FIG. 1 a variant is shown, where a section of 1 has a critical section of 2 and an outer section of 3.
  • a nozzle 1 has a symmetry of 4 and a cross section of 2 cut off.
  • Over 1 may have a super-sonic part as a sopple
  • Capacity 5 was introduced with the Laval system 7, a short section 8, input section 9 and section 10.
  • the internal section 9 is inside the tank
  • Section 10 for the Laval nozzle 7 is the outlet, and for the Laval nozzle 11 is the outlet.
  • Cross-section 10 is simultaneously the cross-section of the largest gas expansion in the vicinity of Laval’s villages 7 and 11, located between critical cross-sections 8 and
  • the section is the input section for the Laval ring system 23.
  • the Laval’s Korolesse 23 has a circular 24 cross-section and an outlet 25 cross-section. There is a 26 sprinkler on the storage tank 17, - 11 - analogous flap 6. Section 27 shows the movement of the aerosol flow supplied by pressure (in Fig. Not shown) in unit 1.
  • Section 28 shows the direction of movement of the aerosol particles, which have left the flow of gas and freeing up inertia of centrifugal force.
  • Section 29 shows the direction of movement of the aerosol particles, which releases from the inertia of the gas flow, which is immediately discharged following the law of 16, followed by.
  • Street 30 shows the direction of movement of the pure air.
  • the historical sections 8, 12, 15, and also 21 and 24 are not less than the critical section 2. They can be equal to it, but it would be more beneficial to do slightly more (by a percentage of 5 to 15).
  • Laval 19 and 23 from the Koltsevsky northerns are converted into a pair of slotted nodules (this option is not shown in FIG.).
  • the bona fide six-sided 31 has a critical section 32 and an outer section 33, and also a non-convex convex section 34.
  • the bombs of Sixers 31 and Laval 35 are installed hermetically on tank 37.
  • the tank 37 has a storage facility 38.
  • the Laval nozzle 35 and 36 have critical sections 38 and 39, which are no less than the critical section 32. They also have an input section 40 and an exit section 41.
  • FIG. 3 a variant is shown when a tapering sound unit 1 is introduced into a supernumerary complex of Sixty-one 31.
  • Room 37 is equipped with a 43 connection with a 44 device, and is equipped with a 45 vessel having a 46 connection with a 47 device.
  • - 12 - 37 ⁇ a em ⁇ s ⁇ i us ⁇ an ⁇ vlen ⁇ d ⁇ lni ⁇ eln ⁇ e sve ⁇ zvu ⁇ v ⁇ e s ⁇ l ⁇ Laval 35a on ⁇ e ge ⁇ me ⁇ ichn ⁇ us ⁇ an ⁇ vlen ⁇ sve ⁇ zvu ⁇ v ⁇ e s ⁇ l ⁇ Laval 36a ⁇ ye ime ⁇ s ⁇ ve ⁇ s ⁇ venn ⁇ ⁇ i ⁇ iches ⁇ ie sections 38a and 39a, and the cross section ⁇ a ⁇ zhe v ⁇ dn ⁇ e
  • the first flow is first bent into the consumer section 1 and before the critical cross-section 50, and then the shortcut is taken after the 49th section and falls apart, shortly after 35.
  • a success of 55 was made in the form of a single or a small number of research and development units of Laval. Improvement 56 was performed in the form of an improvement in the Empire-Paneer.
  • the superfluous diffusion 53 has a cross section 57. A degree of 55 and
  • ⁇ a ⁇ ig. 7 and 8 a variant of the manufacture of capacities is shown — the manufacturing component is made in the form of a body of revolution. This option is also given as an option, when narrowing sonic nozzles are installed for supersonic nozzles. ⁇ a ⁇ ig.
  • a fixed tapering tapered 60 is established (which is a tapering part of the tumbling 53 and is terminated). Following the tapering nozzle nozzle 60, tapering nozzle nozzles 61 and 62 go, and then the nozzle
  • Laval 35 and 36 All of these units are installed pressurized between themselves using a flat 63, 64, 65 and 66. They also have a vacuum of 67, 68, 69 and 70.
  • the convergent d ⁇ zvu ⁇ v ⁇ e s ⁇ l ⁇ 60 has a conventional input section of 83, which is at a speed of 37.
  • Pun ⁇ i ⁇ ami 84 and 85 are g ⁇ anitsy sve ⁇ zvu ⁇ v ⁇ go ⁇ a in m ⁇ men ⁇ ⁇ yva ⁇ sve ⁇ zvu ⁇ v ⁇ g ⁇ s ⁇ sh ⁇ a 48. S ⁇ l ⁇ Laval 35 imee ⁇ you ⁇ ⁇ dn ⁇ e sechenie41a.
  • ⁇ a ⁇ ig. 8 tapering access area to the area 86 located on the Laval 7 site with the formation of a vacuumed area 87.
  • - 14 - 7 S ⁇ l ⁇ Laval ⁇ i ⁇ m ⁇ schi ⁇ l ⁇ s ⁇ s ⁇ i us ⁇ an ⁇ vlen ⁇ 88 to 11 with a Laval s ⁇ le ⁇ b ⁇ az ⁇ vaniem va ⁇ uumi ⁇ uem ⁇ y ⁇ l ⁇ s ⁇ i 89.
  • the Six-Sided Supernova has a tapering fusion 104.
  • a quick release 16 is designed for an inward section of 105 tapering nozzles 106, a large section of 107. Tapering 106
  • the space 17 has a manufacturing
  • the tapering nozzles 90, 91, 92 and 93 have critical sections 111, 112, 113 and 114, respectively.
  • the pressure differential is caused by a dispersed discharge (either gas or aerosol)
  • FIG. 1 it comes with 1, where the front section is 2, and the surface is cut off, creating centrifugal forces at the aerosol particles and the liquid particles. Between the critical section 2 and the inlet section 9, there is a gap that causes the particles to be separated off from the gas supply and discharged to the outlet 5 at a pressure of 28.
  • P ⁇ slednee ⁇ iv ⁇ di ⁇ ⁇ further increase s ⁇ s ⁇ i and gas (aerosol) in a critical section 2. And because there is an exhaust gas in a critical section 2, there is no sound velocity and noise. Further - 15 - increase in ⁇ az ⁇ ezheniya em ⁇ s ⁇ i 5 ⁇ ivede ⁇ ⁇ l ⁇ ⁇ ⁇ b ⁇ az ⁇ vaniyu b ⁇ ch ⁇ i ⁇ e ⁇ e ⁇ asshi ⁇ enn ⁇ g ⁇ sve ⁇ zvu ⁇ v ⁇ g ⁇ ⁇ a gas for ⁇ i ⁇ iches ⁇ im section 2.
  • the nozzle After being installed in capacities 5 and 17 and in all areas between the critical sections of all Laval nozzles, the nozzle is considered to be running in operating mode. With this, an aerosol (or gas) is sucked in inlet 1 due to ejection by a vacuum inside the nozzle, and a critical section of 24 and 21 is a freezing area for pressure release. - 16 - When capacities 5 and 17 are evacuated, the emission of aerosol particles is enhanced by maximizing the gas from the particles.
  • the appliance which made it possible at first to start the aerosol (or gas), can be turned off, and it can be turned off.
  • Laval number of people participating in the process of intensive freezing and loading of the microcircuit in the center of the process depends on the initial volume of gas separation. In general, the smallest aerosol particles and frozen water and various fractions are found in the gas supply center.
  • This option is suitable for use where there is no disturbance in the creation of a sound pressure drop on the load shedding mode, since it is a pressure switch.
  • ⁇ a ⁇ ig. 3 is an alternative when a tapering explosive component of 1 is entered into a supernumerary complex of six (31).
  • This option is used to start the nozzle due to pressure drops.
  • the Laval nozzle 35 and 35a are installed with the corresponding input sections 40 and
  • FIG. 1 One of the options for the release of aerosol particles from the gas stream is shown in FIG.
  • ⁇ gda gas ⁇ is ⁇ y ⁇ yvae ⁇ ⁇ dn ⁇ sto ⁇ nnee ⁇ dzha ⁇ ie ( ⁇ m ⁇ zhenie) and ⁇ dn ⁇ sto ⁇ nnee ⁇ asshi ⁇ enie ( ⁇ azgon) blag ⁇ da ⁇ ya ⁇ ve ⁇ n ⁇ styam 55 and 56, and ⁇ a ⁇ zhe, ⁇ gda ⁇ n is ⁇ y ⁇ vae ⁇ mn ⁇ gos ⁇ ach ⁇ v ⁇ e with external szha ⁇ iem ⁇ sye s ⁇ ach ⁇ i blag ⁇ da ⁇ ya di ⁇ uz ⁇ a 53 ch ⁇ usilivaeg vyb ⁇ s chas ⁇ its ae ⁇ z ⁇ lya in em ⁇ s ⁇ 37 by efficiently preparing gas to process the gas.
  • gases having the same quantity of atoms and the same value of the adiabat are simply different from each other, since they are free of charge. This is a physical statement of their physical nature. - 20 - Differences due to thermal mobility or freezing point. Consequently, the gases separated first at an adiabatic variety are much easier to separate at fractions, further using cooling to the dissolving fraction, for dissolving The chilled flow is reduced to a little so that the gas is not combusted, and the download system will concentrate the particles (ice) in the center.
  • the distribution of gas through the cross-section of the gas flow and the on-off gas distribution is significant, but the distribution is significantly less than the distribution of gas.
  • a nozzle or other option is selected.
  • This pressure drop initially produces in a critical section 2 the highest speed in the nozzle at the time of start-up. Due to the ejection effect in the vacuum area 87, there is a separation, a quick gap between the output 3 and the critical cross section of the 2 wastes before ⁇ ⁇ i ⁇ iches ⁇ m section 2 and uvelichivae ⁇ sya s ⁇ s ⁇ ⁇ as ⁇ d v ⁇ zdu ⁇ a (ae ⁇ z ⁇ lya) ⁇ to ⁇ ye usilivayu ⁇ e ⁇ e ⁇ ezhe ⁇ tsii and usilivayu ⁇ ⁇ az ⁇ ezhenie in ⁇ l ⁇ s ⁇ i 87.
  • Laval's nozzle walls 7 are cut off by a critical cross-section of 8, so as to reduce the compen-
  • the critical sections 111, 112, 113 and 114 are equal between themselves and keep the maximum sound velocity, but the resultant increase in pressure. Reloading downloads from the following dispersal ensures the maximum cleaning of the processing part of the processor.
  • Space 17 is also evacuated by ejection.
  • Particles of aerosol and mikroldinki which are concentrated in the process flow through a cross section of 15 in the tank 17, are discharged from the gas by-product from the gas by-product.
  • ⁇ ⁇ i ⁇ iches ⁇ i ⁇ secheniya ⁇ 2 us ⁇ anavlivaetsya s ⁇ s ⁇ Sound pressure
  • vy ⁇ dny ⁇ secheniya ⁇ 41 and 25 us ⁇ anavlivaetsya sve ⁇ zvu ⁇ vaya s ⁇ st (gi ⁇ e ⁇ zvu ⁇ vaya) ⁇ to ⁇ aya yavlyae ⁇ sya ⁇ e ⁇ " ⁇ ad ⁇ y gas ⁇ ni ⁇ n ⁇ veniya v ⁇ vnu ⁇ nasad ⁇ a ⁇ d pressure ⁇ uzhayuschey s ⁇ edy (a ⁇ m ⁇ s ⁇ e ⁇ y).
  • nozzle could be slotted and executed as a body of revolution.
  • Laval 11 does not only release gas from other aerosol particles, but also freeze it depending on this generation of gases or other liquids.
  • ⁇ a ⁇ ig. 7 ⁇ un ⁇ i ⁇ m 85 are g ⁇ anitsy ⁇ a in m ⁇ men ⁇ ⁇ yva ⁇ sve ⁇ zvu ⁇ v ⁇ go ⁇ a gas ⁇ ⁇ zy ⁇ a 49.
  • the critical sections 78, 38, and 39 are decreasing in order to create a profit for using this energy for its intended purpose.
  • thermodynamics All processes that we consume are located in a quick energy system, which eliminates the need for energy pollution. Many can grow up and doubt the above. Therefore, it is necessary to remember that in thermodynamics all processes are considered in a closed cycle (a specified conditional boundary). You can’t keep these laws (that is, protected by thermodynamics) transparent and automatic for all varieties. It is not known whatsoever, where it is in the electric power generator, but everything is used in the electric power.
  • the present application is an extension of the technical options for the use of a six-speed nozzle, or the pressure transmitter is in contact with it

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Nozzles (AREA)
  • Recrystallisation Techniques (AREA)

Abstract

La présente invention concerne un procédé de captage de poussière et un procédé de séchage du gaz et peut être utilisée sous la forme d'un dispositif permettant d'accélérer le flux de gaz jusqu'à des vitesses élevées dans divers domaines techniques. Le procédé d'accélération du flux de gaz par éjection consiste à faire le vide dans des cavités à l'aide d'un flux de gaz généré par une source de pompage forcé fonctionnant en mode éjection, puis on utilise, dans ces cavités, une pression différentielle croissante résultant de l'éjection dans la partie d'accélération ; puis à accélérer le flux de gaz jusqu'à ce qu'il atteigne une vitesse élevée. Le flux de gaz circule ensuite au moins une fois à vitesse subsonique et/ou à vitesse supersonique. L'ajutage de cette invention comprend des buses disposées de manière hermétique les unes par rapport aux autres et présentant des sections critiques égales ou supérieures à celle de la première buse disposée le long d'un flux de gaz dispersé. L'axe de l'ajutage est incurvé, et au moins une buse, à l'exception de la dernière, disposée le long de l'écoulement du flux de gaz dispersé, se présente sous la forme d'une buse supersonique de Chesterenko, équipée d'un convergent subsonique et d'un déflecteur symétrique et convexe en direction du flux de gaz dispersé. Un joint étanche, placé entre une buse, à l'exception de la dernière, et la buse suivante ou un groupe de buses, se présente sous la forme d'un réservoir. Cette invention permet de diviser un système dispersé en trois phases, à savoir en une phase solide, une phase liquide et une phase gazeuse.
PCT/RU2003/000351 2002-08-19 2003-08-07 Procede et dispositif de chesterenko d'acceleration de gaz par ejection ou « ajutage de chesterenko » Ceased WO2004016338A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2003264567A AU2003264567A1 (en) 2002-08-19 2003-08-07 Shesterenko method and device for jet acceleration of gas or shesterenko attachment

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
PCT/RU2002/000391 WO2003025379A1 (fr) 2001-09-14 2002-08-19 Procede et dispositif de chesterenko d'acceleration de gaz par ejection avec generation d'energie a partir du vide
RUPCT/RU02/00391 2002-08-19
RU2003121606/12A RU2003121606A (ru) 2002-08-19 2003-07-16 Способ и устройство шестеренко эжекторного разгона газа или "насадок шестеренко"
RU2003121606 2003-07-16
RU2003123127/12A RU2267360C2 (ru) 2003-07-28 2003-07-28 Насадок шестеренко
RU2003123127 2003-07-28

Publications (2)

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WO2004016338A1 true WO2004016338A1 (fr) 2004-02-26
WO2004016338A8 WO2004016338A8 (fr) 2004-06-10

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WO (1) WO2004016338A1 (fr)

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CN107325845B (zh) * 2017-08-04 2019-12-24 章英慧 用于锅炉点火与稳燃的锅炉一次风煤粉气流气化装置

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU899151A1 (ru) * 1980-03-21 1982-01-23 За витель 54) СВЕРХЗВУКОВОЕ СОПЛО ШЕСТЕРЕНКО Н.А.Шестеренке /.. .,/ Сверхзвуковое сопло Шестеренко
SU920468A2 (ru) * 1979-09-20 1982-04-15 За витель Н. А. Шестеренко il lf| 8 WiiiBx& Фазовый разделитель
EP0291489A1 (fr) * 1987-05-11 1988-11-17 SEPARGAZ, Société Anonyme: Procédé et dispositif pour la séparation aérodynamique des constituants dans un courant gazeux
EP0490861A1 (fr) * 1990-12-07 1992-06-17 Jean-Paul Lardinois Procédé pour extraire une substance présente dans un fluide gazeux porteur, sous forme de particules solides ou de liquide et système pour la mise en oeuvre de ce procédé
RU2206410C2 (ru) * 2001-09-17 2003-06-20 Шестеренко Николай Алексеевич Насадок шестеренко

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU920468A2 (ru) * 1979-09-20 1982-04-15 За витель Н. А. Шестеренко il lf| 8 WiiiBx& Фазовый разделитель
SU899151A1 (ru) * 1980-03-21 1982-01-23 За витель 54) СВЕРХЗВУКОВОЕ СОПЛО ШЕСТЕРЕНКО Н.А.Шестеренке /.. .,/ Сверхзвуковое сопло Шестеренко
EP0291489A1 (fr) * 1987-05-11 1988-11-17 SEPARGAZ, Société Anonyme: Procédé et dispositif pour la séparation aérodynamique des constituants dans un courant gazeux
EP0490861A1 (fr) * 1990-12-07 1992-06-17 Jean-Paul Lardinois Procédé pour extraire une substance présente dans un fluide gazeux porteur, sous forme de particules solides ou de liquide et système pour la mise en oeuvre de ce procédé
RU2206410C2 (ru) * 2001-09-17 2003-06-20 Шестеренко Николай Алексеевич Насадок шестеренко

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AU2003264567A1 (en) 2004-03-03

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