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WO2004007928A1 - Procede de transformation d'energie dans des moteurs a jets - Google Patents

Procede de transformation d'energie dans des moteurs a jets Download PDF

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Publication number
WO2004007928A1
WO2004007928A1 PCT/RU2002/000338 RU0200338W WO2004007928A1 WO 2004007928 A1 WO2004007928 A1 WO 2004007928A1 RU 0200338 W RU0200338 W RU 0200338W WO 2004007928 A1 WO2004007928 A1 WO 2004007928A1
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WO
WIPO (PCT)
Prior art keywords
mass
πρisοedineniya
πρi
shaft
eneρgii
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PCT/RU2002/000338
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English (en)
Russian (ru)
Inventor
Boris Mihailovich Kondrashov
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Individual
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Individual
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Priority to RU2001123143/06A priority Critical patent/RU2188960C1/ru
Application filed by Individual filed Critical Individual
Priority to PCT/RU2002/000338 priority patent/WO2004007928A1/fr
Priority to AU2002349371A priority patent/AU2002349371A1/en
Priority to EA200500025A priority patent/EA008275B1/ru
Publication of WO2004007928A1 publication Critical patent/WO2004007928A1/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
    • F02K7/02—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 the jet being intermittent, i.e. pulse-jet
    • F02K7/06—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 the jet being intermittent, i.e. pulse-jet with combustion chambers having valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/32—Inducing air flow by fluid jet, e.g. ejector action

Definitions

  • the claimed invention is related to the methods of converting energy from alternative sources, power plants and engines for supplying energy to them.
  • the claimed invention can be used in the process of converting the energy of the atmosphere, and also low potential for the inability to use the device is used
  • the level of technology in this area is deteriorated by the use of the energy of the atmosphere in the energy source, in the case of external energy, and also the external
  • the terrestrial atmosphere is accumulating a recessive and potential energy of gases, compressed by the Earth’s gravity.
  • the upper part of the atmosphere is made up of the lightest gases - hydrogen and helium, and at the expense of loss of energy - it is more difficult to wear.
  • D ⁇ ya ⁇ vsh ⁇ eniya e ⁇ e ⁇ ivn ⁇ s ⁇ i ⁇ tsessa ⁇ e ⁇ b ⁇ az ⁇ vaniya ene ⁇ gii a ⁇ m ⁇ s ⁇ e ⁇ y is ⁇ lzuyu ⁇ ⁇ y ⁇ ye ⁇ e ⁇ m ⁇ dinamiches ⁇ ie sis ⁇ emy ⁇ azlichny ⁇ us ⁇ ys ⁇ v in ⁇ y ⁇ ⁇ susches ⁇ vlyayu ⁇ e ⁇ ⁇ - process of, on ⁇ azyvaya sis ⁇ emu u ⁇ avlyaem ⁇ e me ⁇ aniches ⁇ e v ⁇ zdeys ⁇ vie for s ⁇ zdaniya ⁇ azn ⁇ s ⁇ i ⁇ en- tsial ⁇ v pressure between sis ⁇ em ⁇ y and ⁇ uzhayuschey s ⁇ ed ⁇ y, sh ⁇ ushayuschuyu i ⁇ ⁇ avn ⁇ vesn ⁇ e s ⁇ s ⁇ y
  • the volume of this operation depends on the value of the impact, but to a large extent on the basis of the share of the share of the share of the property and the loss of property, due to the loss of property.
  • two different processes are used to connect additional air masses to an active structure.
  • SIGNIFICANT FOX (DR. 26) 2 EUCES niz ⁇ y, ⁇ a ⁇ zhe, ⁇ a ⁇ ⁇ e ⁇ itsien ⁇ ⁇ is ⁇ edineniya m ( ⁇ n ⁇ shenie ⁇ is ⁇ edinyaem ⁇ y mass v ⁇ z- du ⁇ a ⁇ weight a ⁇ ivn ⁇ y s ⁇ ui) due ⁇ u ⁇ bulen ⁇ n ⁇ g ⁇ ⁇ eniya and mixing ⁇ v, ⁇ e ⁇ mu ⁇ luchaemaya ⁇ ab ⁇ a for scho ⁇ is ⁇ lz ⁇ vaniya ene ⁇ gii a ⁇ m ⁇ s ⁇ e ⁇ y - ⁇ i ⁇ s ⁇ ⁇ yagi, non znachi ⁇ elna.
  • ⁇ a ⁇ y s ⁇ s ⁇ b ⁇ zv ⁇ lyae ⁇ is ⁇ lz ⁇ va ⁇ for ⁇ lucheniya me ⁇ aniches ⁇ y ⁇ ab ⁇ y, na ⁇ ime ⁇ , bi ⁇ liv ⁇ , ene ⁇ giyu ⁇ e ⁇ malny ⁇ and ⁇ chi ⁇ vneshni ⁇ is ⁇ chni ⁇ v ⁇ egoyuv ⁇ y ene ⁇ gii and for eg ⁇ ⁇ susches ⁇ vleniya is ⁇ lz ⁇ va ⁇ v ⁇ zdu ⁇ -independent sis ⁇ emy in ⁇ m including without burning uglev ⁇ d ⁇ dn ⁇ g ⁇ ⁇ liva.
  • the non-technical result which ensures the solution of the fixed problem, is the following: the creation of the capacity due to the use of the united integrated energy, capacity management due to changes in the number of devices, parameters of the devices with the devices of the connection (increasing the functions of the power of the wound); the utilization of the energy of the united reactive mass after the creation of a breaking moment; the generation of energy of the atom in the process of the sequential connection for the generation of power due to the energy generated by its sharing; due to the energy of the atomic power, heat and “cold”; the use of various sources of thermal energy of the external environment, including the sources of excellent health facilities, for the development of high-potential is ⁇ lz ⁇ vanii is ⁇ chni ⁇ v ⁇ e ⁇ l ⁇ y with ⁇ itsa ⁇ eln ⁇ y ⁇ em ⁇ e ⁇ a ⁇ u ⁇ y scho ⁇ for increasing ⁇ azn ⁇ s ⁇ i ⁇ entsial ⁇ v ⁇ em ⁇ e ⁇ a ⁇ u ⁇ ⁇ e ⁇ ed nag ⁇ e
  • ⁇ chas ⁇ ny ⁇ sluchaya ⁇ ⁇ ealizatsii s ⁇ s ⁇ ba To ⁇ lucheniya ne ⁇ b ⁇ dim ⁇ y ugl ⁇ v ⁇ y s ⁇ s ⁇ i and m ⁇ men ⁇ a shaft ⁇ a s ⁇ uyn ⁇ - ada ⁇ ivn ⁇ g ⁇ dviga ⁇ elya - S ⁇ D (d ⁇ ig ⁇ telya, ⁇ ⁇ t ⁇ m for s ⁇ zd ⁇ niya ne ⁇ b ⁇ dt ⁇ y m ⁇ schn ⁇ sti ⁇ INSTALLS l ⁇ iya ⁇ mn ⁇ g ⁇ ezhimn ⁇ g ⁇ ⁇ imeneniya u ⁇ lyayut ⁇ elichin ⁇ y and te ⁇ m ⁇ din ⁇ miches ⁇ imi ⁇ yu ⁇ e ⁇ i- sti ⁇ mi ⁇ bedzhonn ⁇ y ⁇ e ⁇ ti ⁇ n ⁇ y m ⁇ ssy by changing
  • SIGNIFICANT FOX P ⁇ IL 26 4 ust ⁇ yst ⁇ with ust ⁇ yst ⁇ mi ⁇ is ⁇ edineniya, z ⁇ deyst ⁇ nny ⁇ ⁇ ⁇ tsesse its s ⁇ zd ⁇ niya and ⁇ met- ⁇ ⁇ tsess ⁇ ⁇ sled ⁇ teln ⁇ g ⁇ ⁇ is ⁇ edinetya) izmenyayu ⁇ magnitude and ⁇ e ⁇ m ⁇ dinamiches ⁇ ie ⁇ a ⁇ a- me ⁇ y ⁇ bedinonn ⁇ y ⁇ ea ⁇ ivn ⁇ y weight per scho ⁇ ⁇ d ⁇ lyucheniya che ⁇ ez ⁇ delnye ⁇ analy ⁇ ⁇ ascho ⁇ - n ⁇ mu ⁇ liches ⁇ vu s ⁇ uyny ⁇ us ⁇ ys ⁇ v with ne ⁇ b ⁇ dimymi for zadann ⁇ g ⁇ ⁇ ezhima ⁇ ab ⁇ y ⁇
  • SIGNIFICANT FOX P ⁇ IL 26 5 summi ⁇ uyu ⁇ with m ⁇ men ⁇ m, s ⁇ zdavaemym on va ⁇ u ⁇ a S ⁇ D, ⁇ me ⁇ g ⁇ on vy ⁇ dn ⁇ m shaft v ⁇ dila e ⁇ y ⁇ lane ⁇ a ⁇ n ⁇ y ⁇ e ⁇ edachi ⁇ as ⁇ lagayu ⁇ , ⁇ at me ⁇ e, ⁇ dn ⁇ s ⁇ u ⁇ encha ⁇ sh ⁇ v ⁇ y s ⁇ u- ⁇ eni bi ⁇ a ⁇ ivn ⁇ y ⁇ u ⁇ biny, v ⁇ aschayuschiysya in s ⁇ nu, ⁇ iv ⁇ l ⁇ zhnuyu v ⁇ ascheniyu ⁇ e ⁇ v ⁇ y s ⁇ u- ⁇ eni and m ⁇ men ⁇ , ⁇ b ⁇ az ⁇ vanny ⁇ i v ⁇ zdeys ⁇ vii s ⁇ ui on her l ⁇ a ⁇ i,
  • SIGNIFICANT FOX (DR. 26 6 streams and / or the capacity obtained as a result of the process of utilizing the energy of the united air-reactive mass.
  • SIGNIFICANT FOX (DR. 26) 7 and m ⁇ men ⁇ a ⁇ nizheniya ⁇ em ⁇ e ⁇ a ⁇ u ⁇ y, na ⁇ avlyayu ⁇ in ⁇ aches ⁇ ve ⁇ is ⁇ edinyaemy ⁇ masses us ⁇ ys ⁇ va ⁇ is ⁇ edineniya sleduyuscheg ⁇ s ⁇ l ⁇ v ⁇ g ⁇ a ⁇ a ⁇ a ⁇ a ezhe ⁇ n ⁇ g ⁇ ⁇ i ⁇ a in ⁇ m, na ⁇ yadu with ⁇ lucheni- it m ⁇ men ⁇ a, d ⁇ shlni ⁇ eln ⁇ ⁇ nizhayu ⁇ ⁇ em ⁇ e ⁇ a ⁇ u ⁇ u ⁇ ab ⁇ avshey gaz ⁇ v ⁇ y mass, increasing ⁇ azn ⁇ s ⁇ ⁇ entsial ⁇ v ⁇ em ⁇ e ⁇ a ⁇ u ⁇ ⁇ e ⁇ ed its nag ⁇ ev ⁇ m in ⁇ eshyu ⁇ bmenn ⁇
  • U ⁇ ilizi ⁇ vannuyu ⁇ ine ⁇ iches ⁇ uyu ene ⁇ giyu ⁇ bedinonn ⁇ y ⁇ ea ⁇ ivn ⁇ y mass is ⁇ lzuyu ⁇ for szha ⁇ iya ⁇ ab ⁇ avshey in ⁇ ed ⁇ duschi ⁇ tsi ⁇ la ⁇ gaz ⁇ v ⁇ y mass ⁇ uyu ⁇ sle szha ⁇ iya na ⁇ avlyayu ⁇ for nag ⁇ eva in ⁇ e ⁇ l ⁇ bmenn ⁇ m us ⁇ ys ⁇ ve and / or is ⁇ lz ⁇ vaniya in ⁇ aches ⁇ ve ⁇ is ⁇ edinyaemy ⁇ mass sleduyuschi ⁇ tsi ⁇ l ⁇ v in us ⁇ ys ⁇ va ⁇ ⁇ is ⁇ edineniya and ⁇ dn ⁇ v ⁇ emenn ⁇ s ⁇ zdayu ⁇ ⁇ az ⁇ eyasenie in ⁇ blas ⁇ i is ⁇ echeniya ⁇
  • ⁇ iz ⁇ entsialnuyu ⁇ e ⁇ l ⁇ u is ⁇ chni ⁇ a ⁇ egoyuv ⁇ y ene ⁇ gii foreign s ⁇ edy ⁇ e ⁇ b ⁇ azuyu ⁇ in me ⁇ aniches ⁇ uyu ⁇ ab ⁇ u and " ⁇ l ⁇ d" ⁇ i e ⁇ m in zavisim ⁇ s ⁇ i ⁇ is ⁇ dny ⁇ ⁇ e ⁇ m ⁇ dinamiches ⁇ i ⁇ ⁇ a ⁇ a- me ⁇ v and ⁇ liches ⁇ va ⁇ bi ⁇ aem ⁇ y ⁇ e ⁇ l ⁇ y, ⁇ nizhaya ⁇ em ⁇ e ⁇ a ⁇ u ⁇ u is ⁇ chni ⁇ a, l ⁇ aln ⁇ izmenyayu ⁇ eg ⁇ ⁇ e ⁇ m ⁇ dinamiches ⁇ ie ⁇ a ⁇ ame ⁇ y and ag ⁇ ega ⁇ n ⁇ e s ⁇ s ⁇ yanie.
  • FIG. 1 a generalized schematic diagram of the SD is explained, explaining the method of converting energy and frequent cases of its implementation, in Fig. 1, the sec- Fig. 1, in Fig. 5 - through B-W in Fig. 1, in Fig. 6 - the node D in Fig. 1, in Fig. 7 - a cooperative circuit of the LED with a biological tube, in Fig. 8 - the node ⁇ on Fig. 7, in Fig. 9 - after BB-Fig. 7, in Fig. 10 - a basic circuit of the element of the complex element of the simplicity of the circuit, in Fig. 11 - 13 of the circuita handy device, in FIG. 15 - a handy device with a radial channel, in FIG. 16 - a basic circuit of a detachable combustion chamber.
  • Part 1 of the central beating chamber pneumatic valve 2 for the release of compressed air; Return valve 5 pneumatic accumulator; filter and catalytic neutralization 4; ⁇ meyasu- ⁇ chnsh shaft 5 ⁇ a l ⁇ a ⁇ chn ⁇ y ⁇ u ⁇ biny- ⁇ m ⁇ ess ⁇ a-ma ⁇ vi ⁇ a; a spinning device of the 6th stage of the SD; pneumatic accumulator 7; blades of the 8th stage of the LED; pneumatic valve 9 pneumatic accumulator; pneumatic valve 10; inlet unit 11 of the atmospheric drive with air filter and vent; device 12 of a rotating, commercially available device for an impaired stage of diabetes; a rotating device of the 13th first stage of the LED; rotating soyuzovoy device of 14 first stage of diabetes; ⁇ 15 SD; Pneumatic valve 16 of the air supply to the explosive devices of the first stage of the SD; valve 17; Camera 18 ⁇ - Consequently CS CS, etc.
  • SIGNIFICANT FOX P ⁇ IL 26 8 valve 21 combustion chambers; Return valve 22 exhaust gases; Outgoing unit 23; gshevmoklapan 24 dummy plug finished; first step 25 of the diabetes; shaft 26 of the first stage of the blade of the blade-tub-compressor-wheel; extension 27 of the shaft of the rotary blade-turbine-compressor-wheel; the first stage 28 of the blade of a portable turbine is a companion-wheel; TURNBULAR 29 Compressor blades 30 of the second stage of the rotary blade of the blade-chamber of the machine; utility blades 31 of the first stage of the blade of the blade-chamber-compressor; blades 32 of the directional appliance of the compressor of the blade of the turbine-chamber of the maquette; blades 33 of the second constriction of the incidence of diabetes; Compressor blades 34 of the first stage of the blade of the blade-chamber of the machine; pneumatic pan 35 of a good airway; trowels 36 of the second stage of the shoulder blade of the blade
  • Blades 52 of the second stage of the bi-vane blade blades 53 of the first stage of the biological rotary blade; 54 54 front axle of the bi-active blade; internal volume 55 of the first stage of the bi-vane portable turbine with a differential silencer; satellite 56 differential plan of transmission; vodil 57 differential transmission plan; central gear 58 of the differential gear; second 59 second stage of the bi-vane blade; central gear 60 of the planetary transmission; w / o 61 planar transmissions; satellite 62 broadcasts.
  • ⁇ sn ⁇ vnym ⁇ i ⁇ e ⁇ iem e ⁇ e ⁇ ivn ⁇ s ⁇ i is ⁇ lz ⁇ vaniya ene ⁇ gii a ⁇ m ⁇ s ⁇ e ⁇ y in ⁇ tsesse shsle- d ⁇ va ⁇ eln ⁇ g ⁇ ⁇ is ⁇ edineniya d ⁇ shlni ⁇ elny ⁇ mass yavlyae ⁇ sya value ⁇ e ⁇ itsien ⁇ a ⁇ is ⁇ edineniya m ( ⁇ n ⁇ shenie ⁇ is ⁇ edinyaemy ⁇ mass ⁇ weight im ⁇ uls ⁇ v a ⁇ ivn ⁇ y s ⁇ ui) and s ⁇ s ⁇ ⁇ be- dinonn ⁇ y ⁇ ea ⁇ ivn ⁇ y weight, ⁇ ⁇ n ⁇ sheniyu ⁇ s ⁇ s ⁇ i im ⁇ uls ⁇ v a ⁇ ivn ⁇ y s ⁇ ui, ⁇ i its is ⁇ e - not in connection
  • SIGNIFICANT FOX (DR. 26 9 ranks and s ⁇ n ⁇ sheniya ⁇ sn ⁇ vny ⁇ ⁇ a ⁇ ame ⁇ v ⁇ tsessa: ⁇ ascho ⁇ n ⁇ y chas ⁇ y, dli ⁇ eln ⁇ s ⁇ i, ⁇ my, s ⁇ s ⁇ i im ⁇ uls ⁇ v a ⁇ ivn ⁇ y s ⁇ ui, s ⁇ s ⁇ i nabegayuscheg ⁇ ⁇ a vne ⁇ shi ⁇ ( ⁇ ⁇ n ⁇ sheniyu ⁇ us ⁇ ys ⁇ vu ⁇ is ⁇ edineniya) gaz ⁇ vy ⁇ masses ⁇ a ⁇ and ⁇ ⁇ ns ⁇ u ⁇ ivny ⁇ ⁇ a ⁇ ame ⁇ v and ⁇ sh ⁇ tsy s ⁇ uyn ⁇ g ⁇ us ⁇ ys ⁇ va and us ⁇ ys ⁇ va ⁇ is ⁇ edineniya.
  • the green valve 20 By exerting pressure on the combustion products, the green valve 20 (Fig. 1,2,7) compresses the pressure 19 and releases the C-section through the quick-release (2) .1,4,7,9,10) are used for industrial devices 12 (Fig. 1,4,5,7,9,10,15), for example, active nozzle 63 (Fig. 11,12,13) of an ejector element 10) a rotating portable device 14 (Fig. 1.7) of a type that is located on one of the diameters of 25 degree 15 (Fig. 1).
  • step 15 of step 15 which has a large number of gates, is not connected with, the result is a total of 14 It rotates, it will increase the function of a fixed motionless unit (in this case, two-sided) of the type.
  • P ⁇ ichom s ⁇ s ⁇ ⁇ is ⁇ edinonn ⁇ y mass v ⁇ zdu ⁇ a ⁇ i is ⁇ echenii of us ⁇ ys ⁇ va ⁇ is ⁇ edineniya ⁇ avna s ⁇ s ⁇ i gaz ⁇ v ⁇ y mass im ⁇ ulsa a ⁇ ivn ⁇ y s ⁇ ui, is ⁇ e ⁇ ayuschey of s ⁇ uyn ⁇ g ⁇ us ⁇ ys ⁇ va, ⁇ aya in sv ⁇ yu ⁇ che ⁇ ed, uvelichivae ⁇ sya ⁇ i is ⁇ echenii in us ⁇ ys ⁇ v ⁇ ⁇ is ⁇ edineniya, br s ⁇ avneniyu s ⁇ s ⁇ s ⁇ yu is ⁇ echeniya e ⁇ g ⁇ Yasa im ⁇ ulsa in a ⁇ m ⁇ s ⁇ e ⁇ u .
  • SIGNIFICANT FOX (DR. 26 11 v ⁇ y mass im ⁇ ulsa and ⁇ a ⁇ sleds ⁇ vie, ⁇ nizheniem in ⁇ echenie tsi ⁇ la s ⁇ e ⁇ eni ⁇ az ⁇ yazheniya in us ⁇ y- s ⁇ ve ⁇ is ⁇ edineniya for scho ⁇ cheg ⁇ umenshae ⁇ sya e ⁇ s ⁇ weight and " ⁇ v ⁇ s ⁇ v ⁇ y” chas ⁇ i ⁇ is ⁇ edinyae- m ⁇ y v ⁇ zdushn ⁇ y mass tsi ⁇ la, ⁇ aya vmes ⁇ e with " ⁇ v ⁇ s ⁇ v ⁇ y” chas ⁇ yu mass im ⁇ ulsa "vy ⁇ al ⁇ iva - there is a "mass" main "part of the pulse of the products of the following cycle, which has a great speed, and at the same time there is a partial mixing of mass.
  • connection ⁇ em, ch ⁇ ⁇ lichee ⁇ v ⁇ v ⁇ zdu ⁇ a, ⁇ is ⁇ edinyaem ⁇ g ⁇ for scho ⁇ ene ⁇ gii a ⁇ m ⁇ s ⁇ e ⁇ y and s ⁇ zdayuscheg ⁇ b ⁇ lshuyu Part ⁇ ea ⁇ ivn ⁇ y mass is not ⁇ ebue ⁇ d ⁇ lni ⁇ elny ⁇ za ⁇ a ⁇ ene ⁇ gii ⁇ li- wa for ⁇ lucheniya m ⁇ schn ⁇ s ⁇ i ⁇ edlagaemym s ⁇ s ⁇ b ⁇ m in resort ⁇ m chas ⁇ n ⁇ m case ( ⁇ s ⁇ avneniyu any ⁇ aditsi ⁇ nn ⁇ m s ⁇ s ⁇ b ⁇ m, na ⁇ ime ⁇ in ⁇ u ⁇ b ⁇ valn ⁇ y en
  • SIGNIFICANT FOX P ⁇ IL 26 12 (Fig. 16).
  • ⁇ case is ⁇ lz ⁇ vaniya de ⁇ natsi ⁇ nny ⁇ ⁇ ame ⁇ 66 ⁇ du ⁇ y sg ⁇ aniya, shluchennye in ⁇ a- me ⁇ e 18, ⁇ ⁇ ltsev ⁇ mu ⁇ analu ⁇ 2 ( ⁇ ig.16) che ⁇ ez ⁇ ea ⁇ ivnye s ⁇ la 69 na ⁇ avlyayu ⁇ navs ⁇ echu d ⁇ ugu each ⁇ ch ⁇ u ⁇ usa 68 s ⁇ e ⁇ iches ⁇ y chas ⁇ i 67 de ⁇ natsi ⁇ nn ⁇ y ⁇ ame ⁇ y 66 as ⁇ ea ⁇ ivny ⁇ s ⁇ uy.
  • the parallel channel ⁇ 2 (FIG. 16) is supplied with an air-cooled mixture (or, in the case of channel ⁇ 2, it is emitted, it is supplied with ⁇ ea ⁇ ivnye s ⁇ ui mixture ⁇ a ⁇ zhe na ⁇ avlyayu ⁇ in ⁇ u same ⁇ ch ⁇ u 68 s ⁇ l ⁇ n ⁇ veniya s ⁇ s ⁇ uyami ⁇ du ⁇ v sg ⁇ aniya E ⁇ s ⁇ l ⁇ n ⁇ venie vyzyvae ⁇ l ⁇ - ⁇ aln ⁇ e ⁇ vyshenie ⁇ em ⁇ e ⁇ a ⁇ u ⁇ y and pressure initsii ⁇ ue ⁇ av ⁇ leba ⁇ elny ⁇ tsess de ⁇ na- tsi ⁇ nn ⁇ g ⁇ sg ⁇ aniya mixture ⁇ b ⁇ az ⁇ vaniem vys ⁇ chas ⁇ ny ⁇ de ⁇ natsi ⁇ nny ⁇ v ⁇ ln, ⁇
  • E ⁇ ⁇ tsess (s chas ⁇ y in nes ⁇ l ⁇ desya ⁇ - ⁇ v ⁇ Gts depending ⁇ ge ⁇ me ⁇ iches ⁇ i ⁇ ⁇ a ⁇ ame ⁇ v de ⁇ natsi ⁇ nn ⁇ y ⁇ ame ⁇ y and ⁇ e ⁇ m ⁇ dinamiches ⁇ i ⁇ ⁇ a ⁇ ame ⁇ v ⁇ ea ⁇ ivny ⁇ s ⁇ uy) dli ⁇ sya in ⁇ echenie ⁇ ascho ⁇ n ⁇ g ⁇ v ⁇ emeni tsi ⁇ la, d ⁇ ⁇ e ⁇ ascheniya sh- cottages ⁇ du ⁇ v sg ⁇ aniya and / or ⁇ liv ⁇ v ⁇ zdushn ⁇ y mixture and v ⁇ z ⁇ bn ⁇ vlyae ⁇ sya with zadann ⁇ y ⁇ e ⁇ i ⁇ dich- media, which depends on the frequency of ignition of the mixture in the combustion chamber.
  • SIGNIFICANT FOX Drainage of the room in one and ensuring the optimal growth of the increase in the force of the impact of the blade on the blade 53.52 outgrowth of the second
  • the area available in this particular case may be used by the user for various options, depending on the purpose of the system for this system.
  • P ⁇ edlagae maya s ⁇ ema ⁇ m ⁇ n ⁇ v ⁇ i, na ⁇ yadu with e ⁇ e ⁇ ivnym is ⁇ lz ⁇ vaniem ⁇ ine ⁇ iches ⁇ y ene ⁇ gii ⁇ ea ⁇ ivn ⁇ y mass ne ⁇ dn ⁇ a ⁇ n ⁇ ⁇ e ⁇ b ⁇ azuem ⁇ y in me ⁇ aniches ⁇ uyu ⁇ ab ⁇ u without ⁇ e ⁇ , neizbeyash ⁇ v ⁇ zni ⁇ ayuschi ⁇ in ⁇ aditsi ⁇ nny ⁇ s ⁇ ema ⁇ ⁇ i ⁇ v ⁇ e s ⁇ uy in the direction of the device, there is a lot of permeability to the temperature and dispersion in the atmosphere, and the increase in the specific power does not allow for the use of a cable for the car a wider internal disk and wheel.
  • Syasa ⁇ y v ⁇ zdu ⁇ , ⁇ a ⁇ yase ⁇ a ⁇ and ele ⁇ ene ⁇ giyu is ⁇ lzuyu ⁇ for vsh ⁇ lneniya shlezn ⁇ y ⁇ ab ⁇ y and ⁇ ayu ⁇ e for ⁇ bes ⁇ echeniya vneshni ⁇ ⁇ ebi ⁇ eley neshs ⁇ eds ⁇ venn ⁇ in m ⁇ men ⁇ vy ⁇ ab ⁇ i che ⁇ ez ⁇ la ⁇ an 2 and / or na ⁇ a ⁇ livayu ⁇ , s ⁇ ve ⁇ - s ⁇ venn ⁇ in ⁇ nevm ⁇ a ⁇ umulya ⁇ e 7 and / or ele ⁇ a ⁇ umulya ⁇ a ⁇ .
  • P ⁇ sle syasa ⁇ iya, v ⁇ zdu ⁇ che ⁇ ez ⁇ b ⁇ a ⁇ ny ⁇ la ⁇ an 3 nagne ⁇ ayu ⁇ in ⁇ nevm ⁇ a ⁇ - ⁇ umulya ⁇ 7 is ⁇ lzuemy in ⁇ aches ⁇ ve is ⁇ chni ⁇ a szha ⁇ g ⁇ v ⁇ zdu ⁇ a u ⁇ avlyaemym ⁇ as ⁇ edeleni- with it and ⁇ as ⁇ d ⁇ vaniem, d ⁇ m ⁇ men ⁇ a ⁇ ev ⁇ eniya ve ⁇ neg ⁇ ⁇ asche ⁇ n ⁇ g ⁇ u ⁇ vnya pressure ⁇ n ⁇ li- ⁇ uem ⁇ g ⁇ da ⁇ chi ⁇ m.
  • valve 21 for the development of a fuel-air mixture in a chamber 18, and / or for use in a working body for expansion in a tank
  • ⁇ a ⁇ ⁇ i is ⁇ lz ⁇ vanii in ⁇ aches ⁇ ve ⁇ ab ⁇ cheg ⁇ ⁇ ela ⁇ du ⁇ v sg ⁇ aniya
  • ⁇ a ⁇ ⁇ i is ⁇ lz ⁇ vanii szha ⁇ g ⁇ v ⁇ zdu ⁇ a
  • ⁇ as ⁇ lagae maya ene ⁇ giya ⁇ bedinonn ⁇ y ⁇ ea ⁇ ivn ⁇ y mass shluchennaya in ⁇ ezul ⁇ a ⁇ e ⁇ tsessa ⁇ i- s ⁇ edineniya in desya ⁇ i ⁇ az b ⁇ lshe than ene ⁇ giya mass im ⁇ uls ⁇ v a ⁇ ivn ⁇ y s ⁇ ui
  • ne ⁇ b ⁇ di maya for ⁇ ganizatsii process of energy conversion of the atmosphere, i.e.
  • ne ⁇ b ⁇ di maya for s ⁇ zdaniya in us ⁇ ys ⁇ ve ⁇ is ⁇ edineniya ⁇ az ⁇ ezheniya, ⁇ bes ⁇ echivayuscheg ⁇ with zadann ⁇ y chas ⁇ y v ⁇ zni ⁇ n ⁇ venie neu ⁇ avn ⁇ veshenn ⁇ y force and pressure a ⁇ m ⁇ s ⁇ e ⁇ n ⁇ g ⁇ ⁇ e ⁇ b ⁇ az ⁇ vanie ⁇ entsialn ⁇ y and ⁇ e ⁇ l ⁇ v ⁇ y ene ⁇ gii a ⁇ m ⁇ s ⁇ e ⁇ y in ⁇ ine ⁇ iches ⁇ uyu ene ⁇ giyu ⁇ ulsi ⁇ uyuschey s ⁇ ui.
  • ⁇ a ⁇ ie ⁇ tsii za ⁇ a ⁇ ene ⁇ - ology and ⁇ ezul ⁇ a ⁇ v ⁇ e ⁇ b ⁇ az ⁇ vaniya ⁇ i is ⁇ lz ⁇ vanii szha ⁇ g ⁇ v ⁇ zdu ⁇ a in ⁇ aches ⁇ ve ⁇ ab ⁇ cheg ⁇ ⁇ ela, ⁇ zv ⁇ lyayu ⁇ s ⁇ zdava ⁇ m ⁇ schn ⁇ s ⁇ , d ⁇ s ⁇ a ⁇ chnuyu for ⁇ bes ⁇ echeniya vneshni ⁇ ⁇ ebi ⁇ eley and ⁇ dn ⁇ v ⁇ e- menn ⁇ g ⁇ szha ⁇ iya a ⁇ m ⁇ s ⁇ e ⁇ n ⁇ g ⁇ v ⁇ zdu ⁇ a, ⁇ .e.
  • connection to the connection is disconnected I 71 ⁇ anal ⁇ , increasing pressures ⁇ azn ⁇ s ⁇ ⁇ entsial ⁇ v ⁇ i ⁇ b ⁇ az ⁇ vanii ⁇ bedinonn ⁇ y v ⁇ zdushn ⁇ - ⁇ ea ⁇ ivn ⁇ y weight ⁇ tsessa ⁇ shsled ⁇ va ⁇ eln ⁇ g ⁇ ⁇ is ⁇ edineniya sleduyuschi ⁇ tsi ⁇ l ⁇ v for scho ⁇ ⁇ y ⁇ v ⁇ ayu ⁇ ⁇ e ⁇ itsien ⁇ ⁇ is ⁇ edineniya t, s ⁇ s ⁇ ⁇ bedinonn ⁇ y v ⁇ zdushn ⁇ - ⁇ ea ⁇ ivn ⁇ y mass d ⁇ lni ⁇ eln ⁇ ⁇ nyu ⁇ aya its ⁇ em ⁇ e ⁇ a ⁇ u ⁇ u.
  • ⁇ imeneniya B ⁇ SD is a ⁇ m ⁇ s ⁇ e ⁇ ny ⁇ usl ⁇ vy vgoab ⁇ u m ⁇ schn ⁇ s ⁇ i shaft 43 ⁇ a m ⁇ zhn ⁇ ⁇ susches ⁇ vlya ⁇ , is ⁇ lzuya zam ⁇ nu ⁇ y ⁇ e ⁇ m ⁇ dinamiches ⁇ y tsi ⁇ l with vne ⁇ shim shdv ⁇ d ⁇ m ⁇ e ⁇ - l ⁇ y without replacing ⁇ ab ⁇ cheg ⁇ ⁇ ela and ⁇ is ⁇ edinyaemy ⁇ masses ⁇ ichom in ⁇ aches ⁇ ve ⁇ g ⁇ and d ⁇ ug ⁇ g ⁇ m ⁇ zhn ⁇
  • this part of the united mass on the ⁇ 4 channel is returned to the device 71 of the 14th unit 14 in the quantity of the connected masses of the following, which are not connected.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)

Abstract

L'invention permet de transformer l'énergie de l'atmosphère ainsi que la chaleur à faible potentiel des sources thermiques de l'environnement, par exemple, de l'eau de plans d'eau naturels, en travail mécanique, en chaleur à potentiel élevé et en 'froid'. On transforme l'énergie potentielle et thermique d'un fluide de travail dans un dispositif à jet qui, conjointement avec un dispositif de raccordement, remplit la fonction d'un appareil d'éjection à buses, en énergie cinétique d'un flux pulsé actif, qui s'écoule dans le dispositif de raccordement et crée derrière la masse d'impulsions mobile une pression négative assurant la formation d'une force de pression non équilibrée de la masse gazeuse extérieure, ce qui assure l'entrée d'une masse gazeuse supplémentaire à la suite de chaque impulsion. La masse réactive unie ainsi obtenue est utilisée pour créer un couple de rotation sur l'arbre du rotor du moteur à jets. L'invention permet d'obtenir de meilleures performances en termes d'économie d'énergie et de protection de l'environnement lors de la transformation d'énergie.
PCT/RU2002/000338 2001-08-20 2002-07-17 Procede de transformation d'energie dans des moteurs a jets Ceased WO2004007928A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
RU2001123143/06A RU2188960C1 (ru) 2001-08-20 2001-08-20 Способ преобразования энергии в силовой установке (варианты), струйно-адаптивном двигателе и газогенераторе
PCT/RU2002/000338 WO2004007928A1 (fr) 2001-08-20 2002-07-17 Procede de transformation d'energie dans des moteurs a jets
AU2002349371A AU2002349371A1 (en) 2002-07-17 2002-07-17 Method for energy transformation in jet-engines
EA200500025A EA008275B1 (ru) 2002-07-17 2002-07-17 Способ преобразования энергии и струйный двигатель для его осуществления

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2001123143/06A RU2188960C1 (ru) 2001-08-20 2001-08-20 Способ преобразования энергии в силовой установке (варианты), струйно-адаптивном двигателе и газогенераторе
PCT/RU2002/000338 WO2004007928A1 (fr) 2001-08-20 2002-07-17 Procede de transformation d'energie dans des moteurs a jets

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WO2004007928A1 true WO2004007928A1 (fr) 2004-01-22

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RU2334891C1 (ru) * 2007-03-12 2008-09-27 Николай Борисович Болотин Комбинированная двигательная установка
FR2914697B1 (fr) * 2007-04-06 2012-11-30 Turbomeca Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration
US8397482B2 (en) * 2008-05-15 2013-03-19 General Electric Company Dry 3-way catalytic reduction of gas turbine NOx
IT1395822B1 (it) * 2009-10-12 2012-10-26 Nuovo Pignone Spa Metodo e macchinario con combinazione di dispositivi di separazione particelle e di regolazione flusso
US20120000200A1 (en) * 2010-06-30 2012-01-05 General Electric Company Inert gas purging system for an orc heat recovery boiler
RU2524283C1 (ru) * 2013-03-12 2014-07-27 Николай Иванович Кузин Тормоз-генератор-мотор
FR3015574B1 (fr) * 2013-12-20 2019-05-03 Safran Helicopter Engines Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif
FR3019218B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant
FR3020658B1 (fr) * 2014-04-30 2020-05-15 Safran Aircraft Engines Capot de recuperation d'huile de lubrification pour un equipement de turbomachine
RU2597715C1 (ru) * 2015-05-26 2016-09-20 Владислав Юрьевич Климов Энергетическая установка
ITUB20160955A1 (it) 2016-02-22 2017-08-22 Nuovo Pignone Tecnologie Srl Ciclo in cascata di recupero di cascame termico e metodo
RU2735880C1 (ru) * 2019-12-25 2020-11-09 Владимир Михайлович Криловецкий Способ применения газовоздушного термодинамического цикла для повышения КПД малогабаритного турбодвигателя

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SU5588A1 (ru) * 1925-10-02 1928-06-30 Г.С. Петров Способ обработки изделий из карболита
SU7563A1 (ru) * 1926-12-22 1929-01-31 С.В. Иванов Турбина внутреннего горени
US2469679A (en) * 1944-07-13 1949-05-10 Edwin T Wyman Gas turbine
SU922304A1 (ru) * 1980-09-22 1982-04-23 Всесоюзный Научно-Исследовательский Институт Природных Газов "Вниигаз" Газотурбинный агрегат
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