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WO2003025379A1 - Procede et dispositif de chesterenko d'acceleration de gaz par ejection avec generation d'energie a partir du vide - Google Patents

Procede et dispositif de chesterenko d'acceleration de gaz par ejection avec generation d'energie a partir du vide Download PDF

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Publication number
WO2003025379A1
WO2003025379A1 PCT/RU2002/000391 RU0200391W WO03025379A1 WO 2003025379 A1 WO2003025379 A1 WO 2003025379A1 RU 0200391 W RU0200391 W RU 0200391W WO 03025379 A1 WO03025379 A1 WO 03025379A1
Authority
WO
WIPO (PCT)
Prior art keywords
gas
section
ποlοsτi
usτροysτvο
laval
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/RU2002/000391
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English (en)
Russian (ru)
Inventor
Nikolai Alekseevich Chesterenko
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from RU2001125157A external-priority patent/RU2206409C2/ru
Priority claimed from RU2001125176A external-priority patent/RU2206410C2/ru
Priority claimed from RU2001125177A external-priority patent/RU2212282C2/ru
Priority claimed from RU2001125756/06A external-priority patent/RU2001125756A/ru
Priority claimed from RU2001134699/06A external-priority patent/RU2001134699A/ru
Priority to EA200400300A priority Critical patent/EA200400300A1/ru
Application filed by Individual filed Critical Individual
Publication of WO2003025379A1 publication Critical patent/WO2003025379A1/fr
Priority to RU2003121606/12A priority patent/RU2003121606A/ru
Priority to AU2003264567A priority patent/AU2003264567A1/en
Priority to PCT/RU2003/000351 priority patent/WO2004016338A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/12—Injection-induction jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D21/00—Pump involving supersonic speed of pumped fluids

Definitions

  • the method of concentrating the aerosol particles in the main part of the exhaust gas stream is known, when the exhaust gas is exhausted
  • Tax 1 The method of concentrating aerosol particles in the main part of the exhaust gas is known to be off when the gas is absorptive
  • a technical task is to reduce energy in the startup mode and in the operating mode, as well as to expand the area of the application of energy generation from a vacuum.
  • the technical task is performed by the following:
  • the critical cross-section of each supernumerary supernatus is not less than the critical cross-section of the supernumerary supernatant gas.
  • FIG. 1 The devices for performing the above method are shown in FIG. 1,
  • the tapering seropl 1 has an external cross-section 14, and the Laval supersonic one is 5.
  • the tapering assembly 26 has an inward section 30. Between the nozzles there are areas, respectively 22, 31, 32 and 33. Sealing in the construction
  • ⁇ a ⁇ ig. 5 A variant is shown when a tapering unit after 1 is fitted with an integrated (flat) 45 with a cross section of 46 in the form of an outlet.
  • Fig. 7 one more variant of installation is shown on the tapering nozzle after 1 critical section 46 (answer). There is an area of 47 between them.
  • 49 cylinder has a critical cross section over its entire length 50.
  • 48 cylinder has 49 cross section 51. . Sealing is carried out on the basis of the use of blades (not shown in FIG.) And rubber products 54 and 55.
  • Figure 8 also shows a variation, when between the Laval supersonic airships.
  • expanding nozzles 56, 57, and 58 are installed, which are between 59, 60, 61, and 62 sections.
  • the expanding nozzles 56, 57, and 58 have 64 outgoing sections.
  • FIG. 9 a variant is shown, when in the Laval 3 sound unit, apart from 66 and 67, areas 68 and 69, as well as a flexible element
  • Forced vacuum source 91 has an electric motor 98.
  • Fig. 10 between the Laval sve ⁇ zvu ⁇ vymi s ⁇ lami 3 and 86 imee ⁇ sya ⁇ l ⁇ s ⁇ 99.
  • FIG. 11 a variant is shown, when at least 1 hard disk is installed, and if you install 101, we install the device that we consider, but with a smaller size, it means that
  • ⁇ a ⁇ ig. 12 is an alternative, when the 90 is supplied with an additional one, which we consider in FIG. 10 devices, but devices with a "b" designation and a smaller size.
  • ⁇ a ⁇ ig. 13 variant is available, when the volume 13 is communicated with a source of pumping (vacuum pump) 91, the device 112 having a device of 113.
  • ⁇ a ⁇ ig. 14 is a variant, when the Laval saple 5 is fitted with a Laval 114 hematically mounted system, the quick section 115 and the end section 116. Sig.
  • the 14th Laval 3 unit has an inlet section 117.
  • the " ⁇ " unit of the Laval 3 unit complies with the calculated mode of operation in the case of acceleration of gas flow at a time.
  • Uchas ⁇ "B" s ⁇ la Laval 3 s ⁇ ve ⁇ s ⁇ vue ⁇ ⁇ i ⁇ scheniyu ene ⁇ gii on account of the increase in ⁇ azg ⁇ na va ⁇ uumi ⁇ uem ⁇ y chas ⁇ i s ⁇ la Laval 3.
  • ⁇ u ⁇ b ⁇ ea ⁇ ivny dviga ⁇ el ⁇ a ⁇ zhe s ⁇ s ⁇ i ⁇ of ⁇ u ⁇ biny ⁇ ea ⁇ ivn ⁇ g ⁇ s ⁇ la 120 and 121.
  • YAYU IY LIS ⁇ P ⁇ IL ⁇ 26 Referring to Fig. 16, an electric 127 is also shown, going from an electric generator.
  • Lines 128 and 1286 are damaged by the mechanism of picking up and tearing off shafts 96 and 966.
  • the house 123 is connected to the 124th vehicle or 144
  • FIG. 19 an alternative is shown when the 90 trunk is equipped with no less than one additional connecting device 145, connected (communicated)
  • (room) 152 which has an electric power 153.
  • Unit 150 and
  • ⁇ a ⁇ ig. 20 A variant is also shown, when on a slotted or ring ring
  • Laval 158 is hermetically sealed and has the option of walls 163, 164, 165 and flexible elements
  • the blinds 185 are also provided with taps 189 and 190. All gearboxes with blinds are connected through the taps.
  • the Laval family of 158 has a critical section of 194.
  • the tapering nozzles made from the blinds 167 and 176 have a critical section 195 and 196, respectively.
  • the blinds 167, 176 and 185 also have flexible elements connecting them along the entire length with end walls (which are not shown in the figure). In this case, all the walls are sealed with end walls and the Laval 158 serpent also has an end wall (in Fig. Not shown). ⁇ With this option, end walls
  • Historical cross-section 2 is the smallest in the device and the flow rate of gas in this section is the lowest at the start-up mode.
  • ⁇ a ⁇ ⁇ a ⁇ ⁇ i ⁇ iches ⁇ ie sections 4 and 6 are not menyle (preferably chu ⁇ b ⁇ lshe) ⁇ i ⁇ iches ⁇ go section 2 then za ⁇ i ⁇ aniya s ⁇ ui in us ⁇ ys ⁇ ve not ⁇ is ⁇ di ⁇ and ⁇ az ⁇ gnannaya s ⁇ uya ⁇ i ⁇ iches ⁇ m in section 2 of ⁇ ine ⁇ tsii vy ⁇ di ⁇ ⁇ i ⁇ iches ⁇ g ⁇ section 6.
  • Increase in s ⁇ s ⁇ i is ⁇ echeniya ⁇ to ⁇ a sectional ⁇ i ⁇ iches ⁇ m 2
  • Formula 13 are not menyle (preferably chu ⁇ b ⁇ lshe) ⁇ i ⁇ iches ⁇ go section 2 then za ⁇ i ⁇ aniya s ⁇ ui in us ⁇ ys ⁇ ve not ⁇ is ⁇ di ⁇ and ⁇ az ⁇ gnannaya s ⁇ uya ⁇ i ⁇ iches ⁇ m in section 2
  • ⁇ zaimn ⁇ e increase va ⁇ uumi ⁇ vaniya ⁇ l ⁇ s ⁇ i 13 and s ⁇ s ⁇ i ⁇ i ⁇ iches ⁇ m in section 2 ⁇ d ⁇ lzhae ⁇ sya d ⁇ ⁇ e ⁇ ⁇ , ⁇ a ⁇ i ⁇ iches ⁇ m in section 2 is not v ⁇ zni ⁇ ne ⁇ s ⁇ s ⁇ ⁇ avnaya zvu ⁇ u, which increase ⁇ sle ⁇ as ⁇ da gas and increase ⁇ a ⁇ of s ⁇ s ⁇ i che ⁇ ez ⁇ i ⁇ iches ⁇ e ⁇ e ⁇ a ⁇ i ⁇ sya section 2, and the increase va ⁇ uumi ⁇ vaniya ⁇ l ⁇ s ⁇ i 13 ⁇ ivede ⁇ ⁇ ⁇ e ⁇ e ⁇ asshi ⁇ eniyu s ⁇ ui gas for ⁇ i ⁇ iches ⁇ im section 2.
  • the flow does not exceed 60 °, which excludes the transfer of supersonic speed to the sound in the Laval complex 5.
  • a critical cross-section of 4 may be less than, equal to or greater than a critical cross-section of 6.
  • ⁇ sli us ⁇ ys ⁇ v ⁇ is ⁇ lzue ⁇ sya in ⁇ aches ⁇ ve ae ⁇ z ⁇ le ⁇ ntsen ⁇ i ⁇ uyuscheg ⁇ us ⁇ ys ⁇ va then ⁇ db ⁇ s ⁇ n ⁇ sheny e ⁇ i ⁇ sections zavisi ⁇ ⁇ available ⁇ e ⁇ v ⁇ nachaln ⁇ g ⁇ ⁇ e ⁇ e ⁇ ada pressure us ⁇ ys ⁇ ve, s ⁇ e ⁇ eni za ⁇ ylenn ⁇ s ⁇ i ⁇ a ae ⁇ z ⁇ lya, ⁇ iziches ⁇ i ⁇ sv ⁇ ys ⁇ v gas and ⁇ azme ⁇ a chas ⁇ its ae ⁇ z ⁇ lya, ⁇ ye ne ⁇ b ⁇ dim ⁇ s ⁇ ntsen ⁇ i ⁇ va ⁇ in tsen ⁇ e ⁇ azgonyaem ⁇ g ⁇ ⁇ to ⁇ a.
  • a variant was installed when it was installed in the form of a large section with a critical cross-section 2. This part is installed on the other hand, where there is a loss of ⁇ sli s ⁇ s ⁇ b and us ⁇ ys ⁇ v ⁇ vy ⁇ lnyayu ⁇ ⁇ l gaz ⁇ v ⁇ go ⁇ yam ⁇ chn ⁇ go dviga ⁇ elya, ⁇ us ⁇ ys ⁇ v ⁇ us ⁇ anavlivae ⁇ sya on ⁇ be ⁇ (sam ⁇ le ⁇ , ⁇ a ⁇ e ⁇ u) ⁇ to ⁇ ye dvigayu ⁇ sya with b ⁇ lsh ⁇ y s ⁇ s ⁇ yu, ⁇ to ⁇ aya ⁇ bes ⁇ echivae ⁇ us ⁇ ys ⁇ vu ne ⁇ b ⁇ dimy ⁇ e ⁇ v ⁇ nachalny pressure ⁇ e ⁇ e ⁇ ad in s ⁇ le 1.
  • ⁇ a ⁇ ig. 4, 5, 6, 7, and 8 are alternative options for consumables, when self-evacuating rooms in an e-mail mode, you must disconnect them from the phone.
  • ⁇ a ⁇ ig. 9 ⁇ ass ⁇ yaniya change between sections 80 and ⁇ i ⁇ iches ⁇ imi 4 dae ⁇ v ⁇ zm ⁇ zhn ⁇ s ⁇ ma ⁇ simaln ⁇ i ⁇ ⁇ iblizi ⁇ , ⁇ bes ⁇ echivaya ⁇ i minimaln ⁇ m pressure ⁇ e ⁇ e ⁇ ade e ⁇ e ⁇ ezhe ⁇ tsii this ⁇ s ⁇ ans ⁇ ve and ⁇ sle increase s ⁇ s ⁇ i and ⁇ as ⁇ da dae ⁇ v ⁇ zm ⁇ zhn ⁇ s ⁇ increasing e ⁇ ⁇ asstoyanie, ⁇ luchi ⁇ best e ⁇ e ⁇ ezhe ⁇ tsii already ⁇ i b ⁇ ly ⁇ i ⁇ s ⁇ s ⁇ ya ⁇ .
  • ⁇ i ⁇ iches ⁇ e section 94 yavlyae ⁇ sya ⁇ a ⁇ zhe zvu ⁇ vym ba ⁇ e ⁇ m for vse ⁇ v ⁇ zmuscheny, iduschi ⁇ s ⁇ sto ⁇ ny vy ⁇ dn ⁇ g ⁇ section 95, che ⁇ ez ⁇ to ⁇ e v ⁇ lny pressure ⁇ uzhayuschey s ⁇ edy not s ⁇ stoyanii ⁇ ni ⁇ nu ⁇ , ⁇ a ⁇ ⁇ a ⁇ ⁇ ⁇ az ⁇ gnan d ⁇ gi ⁇ e ⁇ zvu ⁇ vy ⁇ s ⁇ s ⁇ ey in section 44 and ene ⁇ giya to ⁇ m ⁇ zheniya ⁇ a (eg ⁇ pressure) v ⁇ mn ⁇ go ⁇ a ⁇ above the atmospheric and penetrating through the hypersonic or super-sonic section in the critical section 94 is not possible.
  • a compressed air is delivered to the Laval supersonic system 102. Due to the placement of a connection connected to a short-circuited connection to an arrester The air, mixed with the superfluous flow, will pass through the critical section 2a and 4a, so far, the device will be completely destroyed.
  • the installation is started.
  • ⁇ a ⁇ ig. 14 on account ⁇ inudi ⁇ eln ⁇ go ⁇ e ⁇ e ⁇ ada pressure (istochni ⁇ ⁇ e ⁇ e ⁇ ada pressure ⁇ ig. ⁇ azan not) s ⁇ zdae ⁇ sya sve ⁇ zvu ⁇ v ⁇ y ⁇ in s ⁇ le Laval 3 extending s ⁇ sto ⁇ ny v ⁇ dn ⁇ go section 117 to section 116.
  • sto ⁇ nu vy ⁇ dn ⁇ go Sve ⁇ zvu ⁇ vym ⁇ m first va ⁇ uumi ⁇ ue ⁇ sya ⁇ l ⁇ s ⁇ ⁇ i ⁇ iches ⁇ imi between sections 4 and 6 and za ⁇ em The area between the critical sections 6 and 115. After that, as the stable mode was established, the source of the intuitive air (gas) discharge is removed from the process. Due to the displacement due to a cross section of 4 of all elemental
  • ⁇ ⁇ m ⁇ ess ⁇ e 119 ( ⁇ u ⁇ b ⁇ m ⁇ ess ⁇ e) ⁇ is ⁇ di ⁇ further szha ⁇ ie v ⁇ zduha.
  • the compressed air is emitted from the generator for vacuum energy, which is a quick source of 86 Laval sorbent, and 99 E ⁇ ⁇ va ⁇ uumi ⁇ ue ⁇ ⁇ l ⁇ s ⁇ between 99 and ⁇ s ⁇ ans ⁇ v ⁇ ⁇ i ⁇ iches ⁇ imi s ⁇ el Laval sections 86 and 3.
  • the proposed device for all options may be made slotted or ring.
  • 122 It may be filled with inert gas, or may collect harmful gases.
  • the gas pressure can be significantly higher than the atomic pressure, which improves the temperature of the vacuum cooking. Ele ⁇ gene ⁇ ato ⁇ 124 ⁇ ⁇ v ⁇ du 127 ⁇ dae ⁇ ele ⁇ ene ⁇ giyu ⁇ ebi ⁇ elyu, Part ⁇ to ⁇ y m ⁇ zhe ⁇ ⁇ s ⁇ u ⁇ a ⁇ in a ⁇ umulya ⁇ and che ⁇ ez it v ⁇ zv ⁇ ascha ⁇ sya on istochni ⁇ ⁇ inudi ⁇ eln ⁇ y ⁇ e ⁇ e ⁇ ach ⁇ i gas (or ⁇ m ⁇ ess ⁇ va ⁇ uumny nas ⁇ s) ⁇ to ⁇ ye v ⁇ lyuchayu ⁇ sya ⁇ i ⁇ vto ⁇ ny ⁇ za ⁇ us ⁇ a ⁇ us ⁇ ys ⁇ va or ⁇ dde ⁇ zhaniya ⁇ ans ⁇ i ⁇ uyuscheg ⁇ ⁇ e ⁇ e ⁇ ada pressure zam
  • the option to start the device is discharged (Fig. 19) if you need to save the device 152.
  • 113 and 92 are forgotten.
  • Squeegee 96 Disconnecting device 145 is forgotten.
  • Disconnect device 150 out.
  • the electric device 153 is switched off.
  • the compressor generates the necessary pressure and discharge, so that in the case of Laval 86, an overturned sound is generated. After that, it is evacuated due to the ejection of the areas 99 and 100.
  • the operating device is installed in the device 151. It is observed that, each device 150 and 151 is omitted and is not used in any way.
  • the startup mode has already been accessed. Initially vacuuming the operating mode results in a 146 capacity; If in this case, the incapacitating devices 150, 92, 113, 155, 157 and 96 are forgotten, 151 are lost. After that, a transfer device of 145 receivers 146 is turned off, and a second is vacuumed. After being installed in areas 99 and 100, the bulldozer (transient device) is 96 turned off.
  • receiver capacity of 146 may be small.
  • the battery capacity of 146 may also be used a little for startup, and if necessary, then the time of installation is necessary.
  • the angle changes, which changes at the rate of increase of all cross-sections, in order to exclude the hardening of the hygroscopic vent and the interruption of the blinds 167, 176 and 185.
  • Za ⁇ em ⁇ i s ⁇ anenii us ⁇ ychiv ⁇ g ⁇ va ⁇ uuma in ⁇ l ⁇ s ⁇ ya ⁇ 191, 192 and 193 of louvers 167, 176 and 185 che ⁇ vyachnymi ⁇ e ⁇ edachami uvelichivayu ⁇ ⁇ ass ⁇ yanie therebetween and us ⁇ anavlivae ⁇ sya ⁇ imalny ug ⁇ l ⁇ i ⁇ ab ⁇ e in gi ⁇ e ⁇ zvu ⁇ v ⁇ m ⁇ ezhime, n ⁇ already ⁇ i b ⁇ ly ⁇ em ⁇ as ⁇ de gas (v ⁇ zdu ⁇ a) che ⁇ ez ⁇ i ⁇ iches ⁇ e section 194.
  • the variant is discontinued, when at the same time with an increase in the critical section 194, the mode of acceleration of the hypersonic flow increases and the greater section increases 195, and the increase is 195 In this case, an option is available when all the blinds 167, 176 and 185 are connected to the same directing Laval unit and these are connected to the room.
  • start-up modes may take place in various operating systems. For options 9, 10, and 20, and if you run these modes, you should install the settings that are optimal for the interruptions.
  • the first flow of gas is due to a critical cross-section of 198;
  • the first vapor is a phase separator, primarily purifying gas.
  • aerosol particles (not shown in FIG.).
  • ⁇ ncha ⁇ eln ⁇ ⁇ chischenny gas ⁇ chas ⁇ its ⁇ s ⁇ u ⁇ ae ⁇ next ⁇ a ⁇ u ⁇ ltsevy ⁇ s ⁇ el Laval 203 and 204 ⁇ sle ⁇ to ⁇ y m ⁇ zhe ⁇ by ⁇ us ⁇ an ⁇ vlena gaz ⁇ vaya ⁇ u ⁇ bina, ⁇ iv ⁇ dyaschaya lyub ⁇ y me ⁇ anizm in motion or pressure ene ⁇ giya ⁇ to ⁇ a m ⁇ zhe ⁇ by ⁇ is ⁇ lz ⁇ vana ⁇ usm ⁇ eniyu ⁇ ebi ⁇ elya.
  • ⁇ ⁇ ezul ⁇ a ⁇ e ⁇ edl ⁇ zhennye s ⁇ s ⁇ b and us ⁇ ys ⁇ v ⁇ m ⁇ gu ⁇ ⁇ bes ⁇ echi ⁇ s ⁇ l ug ⁇ dn ⁇ d ⁇ lguyu ⁇ ab ⁇ u in ⁇ aches ⁇ ve is ⁇ chni ⁇ a ene ⁇ gii for ⁇ ab ⁇ y or gaz ⁇ v ⁇ g ⁇ ⁇ yam ⁇ chn ⁇ g ⁇ dviga ⁇ elya or v ⁇ ascheniya l ⁇ a ⁇ ⁇ u ⁇ biny ele ⁇ gene ⁇ a ⁇ a, or ⁇ ab ⁇ y in ⁇ aches ⁇ ve ae ⁇ z ⁇ le ⁇ ntsen ⁇ i ⁇ uyuscheg ⁇ nasad ⁇ a in sis ⁇ eme ⁇ chis ⁇ i v ⁇ zdu ⁇ a ⁇ v ⁇ edny ⁇ chas ⁇ its ae ⁇ z ⁇ lya ⁇ a ⁇ and more ...
  • Vacuum energy is ecologically pure, inexhaustible and infinitely cheap.
  • ⁇ e ⁇ niches ⁇ y e ⁇ e ⁇ ⁇ a ⁇ zhe za ⁇ lyuchae ⁇ sya that ⁇ i is ⁇ lz ⁇ vanii in ⁇ aches ⁇ ve is ⁇ chni ⁇ a va ⁇ uuma em ⁇ s ⁇ i, ⁇ to ⁇ ye ⁇ edva ⁇ i ⁇ eln ⁇ va ⁇ uumi ⁇ uyu ⁇ sya any s ⁇ s ⁇ b ⁇ m, ⁇ zv ⁇ lyayu ⁇ mn ⁇ g ⁇ a ⁇ n ⁇ ⁇ s ⁇ anavliva ⁇ and za ⁇ us ⁇ a ⁇ us ⁇ an ⁇ v ⁇ u without d ⁇ lni ⁇ eln ⁇ go istochni ⁇ a ⁇ inudi ⁇ eln ⁇ go gas ⁇ achivaniya, ch ⁇ ⁇ asshi ⁇ yae ⁇ ⁇ imenenie ⁇ edlagaemy ⁇ s ⁇ s ⁇ ba and us ⁇ ys ⁇ va.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Recrystallisation Techniques (AREA)

Abstract

L'invention appartient au domaine des installations de génération d'énergie et des dispositifs d'accélération ou de transport de gaz; elle peut aussi s'utiliser comme un statoréacteur pour aéronefs ou un moteur pour véhicule terrestre, un dispositif à buse dans des turbines à gaz et dans plusieurs autres domaines de la technique dans lesquelles on cherche à produire de l'énergie à partir du vide, à des fins de réchauffement et d'accélération des gaz; elle peut aussi s'utiliser en tant que dispositif de concentration d'aérosols. L'invention permet de réduire les dépenses en énergie au stade de lancement et à élargir le domaine d'utilisation du dispositif. Selon l'invention, dans le procédé et le dispositif d'accélération de gaz par éjection avec génération d'énergie, le procédé consiste à utiliser une source de pompage forcé dans un mode ultrasonique à éjection on crée au moyen d'un flux de gaz un vide dans une cavité dans laquelle on utilise une chute de pression créée sous l'effet de l'éjection de la cavité dans la partie d'accélération de l'éjecteur; le flux de gaz est accéléré jusqu'à des vitesses élevées, ce qui permet d'augmenter l'effet d'éjection et de création de vide dans la cavité; on continue à augmenter le vide dans la cavité et en même temps on accélère le flux de gaz jusqu'à une vitesse maximale possible. L'énergie cinétique complémentaire obtenue par l'accélération du flux de gaz est évacuée de la cavité par la partie d'évacuation de l'éjecteur.
PCT/RU2002/000391 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 Ceased WO2003025379A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EA200400300A EA200400300A1 (ru) 2001-09-14 2002-08-19 Способ и устройство (насадок) шестеренко эжекторного разгона газа
RU2003121606/12A RU2003121606A (ru) 2002-08-19 2003-07-16 Способ и устройство шестеренко эжекторного разгона газа или "насадок шестеренко"
PCT/RU2003/000351 WO2004016338A1 (fr) 2002-08-19 2003-08-07 Procede et dispositif de chesterenko d'acceleration de gaz par ejection ou « ajutage de chesterenko »
AU2003264567A AU2003264567A1 (en) 2002-08-19 2003-08-07 Shesterenko method and device for jet acceleration of gas or shesterenko attachment

Applications Claiming Priority (16)

Application Number Priority Date Filing Date Title
RU2001125157A RU2206409C2 (ru) 2001-09-14 2001-09-14 Насадок шестеренко
RU2001125157 2001-09-14
RU2001125176 2001-09-17
RU2001125177A RU2212282C2 (ru) 2001-09-17 2001-09-17 Насадок шестеренко
RU2001125176A RU2206410C2 (ru) 2001-09-17 2001-09-17 Насадок шестеренко
RU2001125177 2001-09-17
RU2001125756/06A RU2001125756A (ru) 2001-09-24 Способ шестеренко получения энергии из вакуума
RU2001125756 2001-09-24
RU2001126361/12A RU2001126361A (ru) 2001-10-01 Способ и устройство шестеренко разгона газа
RU2001126361 2001-10-01
RU2001134699 2001-12-24
RU2001134699/06A RU2001134699A (ru) 2001-12-24 2001-12-24 Способ и устройство шестеренко разгона потоков газа
RU2002102471/06A RU2002102471A (ru) 2002-02-01 Способ и устройство Шестеренко разгона газа
RU2002102471 2002-02-01
RU2002108065/06A RU2002108065A (ru) 2002-04-02 Способ и устройство шестеренко эжекторного разгона газа с получением энергии из вакуума
RU2002108065 2002-04-02

Publications (1)

Publication Number Publication Date
WO2003025379A1 true WO2003025379A1 (fr) 2003-03-27

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PCT/RU2002/000391 Ceased 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

Country Status (2)

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EA (1) EA200400300A1 (fr)
WO (1) WO2003025379A1 (fr)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004112968A1 (fr) * 2003-06-25 2004-12-29 Lobashinskaya, Alla Vladimirovna Ajutage de chesterenko
RU2267360C2 (ru) * 2003-07-28 2006-01-10 Лобашинская Алла Владимировна Насадок шестеренко
RU2272678C2 (ru) * 2003-06-25 2006-03-27 Лобашинская Алла Владимировна Насадок шестеренко
RU2277441C2 (ru) * 2004-09-01 2006-06-10 Николай Алексеевич Шестеренко Насадок шестеренко
RU2282047C1 (ru) * 2004-12-22 2006-08-20 Государственное образовательное учреждение высшего профессионального образования Военно-морская академия имени Адмирала Флота Советского Союза Н.Г. КУЗНЕЦОВА Воздушная реактивная двигательная установка
RU2313403C2 (ru) * 2006-03-03 2007-12-27 Лобашинская Алла Владимировна Теплонасадок шестеренко
RU2325954C2 (ru) * 2005-03-28 2008-06-10 Лобашинская Алла Владимировна Зеркальный насадок шестеренко
RU2346753C2 (ru) * 2004-09-01 2009-02-20 Николай Алексеевич Шестеренко Насадок шестеренко
RU2354459C2 (ru) * 2005-09-14 2009-05-10 Лобашинская Алла Владимировна Насадок шестеренко
RU2356637C2 (ru) * 2006-11-28 2009-05-27 Лобашинская Алла Владимировна Насадок шестеренко (варианты)
RU2361679C2 (ru) * 2004-12-16 2009-07-20 Лобашинская Алла Владимировна Супернасадок шестеренко (варианты)
RU2361680C2 (ru) * 2005-01-31 2009-07-20 Лобашинская Алла Владимировна Сверхнасадок шестеренко (варианты)
RU2377059C2 (ru) * 2007-07-04 2009-12-27 Лобашинская Алла Владимировна Устройство шестеренко диспергирования газожидкостной смеси
RU2551289C2 (ru) * 2011-03-11 2015-05-20 Николай Алексеевич Шестеренко Насадок
RU2618183C2 (ru) * 2012-01-23 2017-05-02 Сергей Николаевич Шестеренко Способ нагрева теплообменника отопительной системы обогрева домов и других объектов и устройство для осуществления способа

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RU2272678C2 (ru) * 2003-06-25 2006-03-27 Лобашинская Алла Владимировна Насадок шестеренко
WO2004112968A1 (fr) * 2003-06-25 2004-12-29 Lobashinskaya, Alla Vladimirovna Ajutage de chesterenko
EA008458B1 (ru) * 2003-06-25 2007-06-29 Лобашинская, Алла Владимировна Насадок шестеренко
RU2267360C2 (ru) * 2003-07-28 2006-01-10 Лобашинская Алла Владимировна Насадок шестеренко
RU2346753C2 (ru) * 2004-09-01 2009-02-20 Николай Алексеевич Шестеренко Насадок шестеренко
RU2277441C2 (ru) * 2004-09-01 2006-06-10 Николай Алексеевич Шестеренко Насадок шестеренко
RU2361679C2 (ru) * 2004-12-16 2009-07-20 Лобашинская Алла Владимировна Супернасадок шестеренко (варианты)
RU2282047C1 (ru) * 2004-12-22 2006-08-20 Государственное образовательное учреждение высшего профессионального образования Военно-морская академия имени Адмирала Флота Советского Союза Н.Г. КУЗНЕЦОВА Воздушная реактивная двигательная установка
RU2361680C2 (ru) * 2005-01-31 2009-07-20 Лобашинская Алла Владимировна Сверхнасадок шестеренко (варианты)
RU2325954C2 (ru) * 2005-03-28 2008-06-10 Лобашинская Алла Владимировна Зеркальный насадок шестеренко
RU2354459C2 (ru) * 2005-09-14 2009-05-10 Лобашинская Алла Владимировна Насадок шестеренко
RU2313403C2 (ru) * 2006-03-03 2007-12-27 Лобашинская Алла Владимировна Теплонасадок шестеренко
RU2356637C2 (ru) * 2006-11-28 2009-05-27 Лобашинская Алла Владимировна Насадок шестеренко (варианты)
RU2377059C2 (ru) * 2007-07-04 2009-12-27 Лобашинская Алла Владимировна Устройство шестеренко диспергирования газожидкостной смеси
RU2551289C2 (ru) * 2011-03-11 2015-05-20 Николай Алексеевич Шестеренко Насадок
RU2618183C2 (ru) * 2012-01-23 2017-05-02 Сергей Николаевич Шестеренко Способ нагрева теплообменника отопительной системы обогрева домов и других объектов и устройство для осуществления способа

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