WO1994003725A1 - Stepanov's aerohydrodynamic engine - Google Patents

Stepanov's aerohydrodynamic engine Download PDF

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Publication number
WO1994003725A1
WO1994003725A1 PCT/RU1993/000148 RU9300148W WO9403725A1 WO 1994003725 A1 WO1994003725 A1 WO 1994003725A1 RU 9300148 W RU9300148 W RU 9300148W WO 9403725 A1 WO9403725 A1 WO 9403725A1
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WO
WIPO (PCT)
Prior art keywords
shaft
parts
τεη
προ
blade
Prior art date
Application number
PCT/RU1993/000148
Other languages
French (fr)
Russian (ru)
Inventor
Lev Anatolievisch Stepanov
Original Assignee
Lev Anatolievisch Stepanov
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
Application filed by Lev Anatolievisch Stepanov filed Critical Lev Anatolievisch Stepanov
Priority to AU45921/93A priority Critical patent/AU4592193A/en
Publication of WO1994003725A1 publication Critical patent/WO1994003725A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06Rotors
    • F03D3/062Rotors characterised by their construction elements
    • F03D3/066Rotors characterised by their construction elements the wind engaging parts being movable relative to the rotor
    • F03D3/067Cyclic movements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B17/00Other machines or engines
    • F03B17/06Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head"
    • F03B17/062Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction
    • F03B17/065Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction the flow engaging parts having a cyclic movement relative to the rotor during its rotation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/72Adjusting of angle of incidence or attack of rotating blades by turning around an axis parallel to the rotor centre line
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/74Wind turbines with rotation axis perpendicular to the wind direction

Definitions

  • the invention is subject to hazardous engines, hazardous electrical energy, and high-voltage industrial waste products. such as generatrix of electric current, grape-
  • the tires for example, are subject to water from the Danish patent No. 156843 for 1981 ⁇ ⁇ 7/00, the patent of Sweden ⁇ 8601770 for 1986 ⁇ ⁇ 7/00 and ⁇ . Holders of Holland ⁇ requests to 1979 79 ⁇ 7901145 for 1979 ⁇ ⁇ 3/00 and
  • Indicated Engines contain your own engine - ⁇ , which have several elements that are interrelated with the Shbegs-type flow, and the infusion associated with the output shaft
  • the main element of these engines is the blade or the blade, which is completed in the form of a flat or synchronized interface Metals are located on the main road and are either hard or dirty. AND THEREFORE, YOUR INVASION MAY HAPPEN TO DIRECT. The flow, flow and disposal of the flow direction.
  • the purpose of the present invention is to achieve a higher capacity removed from the mass of the vehicle to prevent the loss of memory and the exclusion of the vehicle is unnecessary.
  • Fig. 1 a general view of the aero-recorder is shown, in Fig. 2, its ver-
  • the threader for FIG. 1 has an infusion shaft 1. Vane 2, with all the parts for and 4.
  • Impairment Unit 1 is disposed of vertically to the level of land and to the condition of the velocity of the flow of the discharge ⁇ ⁇ .
  • Blade 2 has a required symmetrical design for Fig. 3,
  • Part 2 is located between Axis 3 and the infusion shaft 1.
  • the largest part of the impeller 2 is located at the maximum removal of the infeed shaft 1 and has a larger weight part 2.
  • the parts of the blade made in Ukraine were made of materials of different thicknesses, for example, part 2 is made of metal, and part £ is made of plastic.
  • the blade 2 is mounted on an axle 3. Axi 3 hard
  • Infestation 1 is related to what is known from the material in the art.
  • ⁇ a ⁇ ig. ⁇ SHU ⁇ aeroga ⁇ is the engine, which contains the vertical shaft of the infusion 1, blade 2
  • the EARS and the lower part are mixed with the other and the higher part of the angle, as well as the frequency of dividing the angle between the main parts of the mains:
  • N ⁇ I ETO ⁇ Part l ⁇ as ⁇ ey 2 na ⁇ dyasha- Jasia left ⁇ shyus ⁇ s ⁇ i in ⁇ y v ⁇ asheniya 1 and ve ⁇ to ⁇ na ⁇ dya ⁇ sya shaft s ⁇ sta shbega ⁇ teg ⁇ ⁇ a ⁇ ⁇ , w ⁇ azv ⁇ achivae ⁇ sya sha ⁇ - ni ⁇ a ⁇ ⁇ U ⁇ ⁇ sey 3 ⁇ na ⁇ avleniyu ⁇ to ⁇ a and chas ⁇ l ⁇ as ⁇ ey
  • the output of the device is 4 and it is returned to its own 3 for the flow
  • ⁇ y and 0 2 are the mass of parts 2 and 2 of the flat
  • the next technical solution to the aerodynamics system is the quick-disconnect switch of the electronic power supply unit 3, ⁇ .
  • the proposed engine can be used both in the wind and in the rear engine. in particular in a free river river hydroelectric power station. in a hydroelectric power station, USING ENERGY ⁇ , ⁇ grade ⁇ ⁇ perfume-

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Wind Motors (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)

Abstract

An aerohydrodynamic engine for conversion of wind or water flow energy into mechanical energy comprises a vertical shaft (1), blades (2), axles (3) and stops (4). The blades (2) are arranged symmetrically around the shaft (1) and are hingedly mounted on shafts (3). The blades (2) consist of two parts unequal by mass and size and divided by a plane passing through the shafts (3) and perpendicular to the lateral surface of the blade (2). The larger part of the blade (2) has a smaller mass and is located between the shaft (3) and the stop (4). The engine has one or more tiers located one above the other. The number of blades (2) in a tier is preferably three. The neighbouring tiers are relatively offset by an angle equal to the quotient obtained from the division of the angle between the neighbouring blades by the number of tiers.

Description

ΑЭГОГΗДΡСШΗΑΗИЧΕГЖЙЙ ДШГΑΤΕУШ СГΕПΑЮΒΑ ΑEOGOGΗDΡSSHΗΑΗICHΕGZHY DSHGΑΤΕUSH SGΕPΑYUΒΑ
Изοбρеτение οτнοсиτся κ οбласιи аэροι-вдροданамичесκиχ дви- гаτелей, πρеοбρазуκшиχ энеρгию ποсτуπаτельнοгο движения газο- вοй иπи жиζгκοй сρеды, вο вρашаτельнοе ζшижение вала πρивοда силοвыχ машин. τаκиχ κаκ генеρаτορ элеκτρичесκοгο τοκа, гρеб-The invention is subject to hazardous engines, hazardous electrical energy, and high-voltage industrial waste products. such as generatrix of electric current, grape-
5 нοй винτ κορабля, насοс, ποдьемιный меχанизм и τ. π.5th new screw for the pump, pump, mechanism and τ. π.
Κ τаκим двигаτелям οτнοсяτся, гаπρимеρ, вοдяные κοлеса πο πаτенτу Дании Ηο 156843 за 1981 г. Ρ ΟЗΒ 7/00, πаτенτу Швеции Ηο 8601770 за 1986 г. Ρ ΟЗΒ 7/00 и дρ. , веτροζшигатели πο заявκам Гοлландии Ηο 7901145 за 1979 г. Ρ ΟЗБ 3/00 и φρандииFor such engines, the tires, for example, are subject to water from the Danish patent No. 156843 for 1981 Ρ ΟЗΒ 7/00, the patent of Sweden Η 8601770 for 1986 Ρ ΟЗΒ 7/00 and ρ. Holders of Holland Η requests to 1979 79ο 7901145 for 1979 Ρ ЗЗБ 3/00 and
10 Η 8019387 за 1980 Г. Ρ ΟЗЮ 3/00, πаτенτам Швеции Ηο 434975 за 1974 г. Ρ ΟЗБ 3/00, Αвсτρии Ηο 382687 за 1976 г. Ρ ΟЗБ 3/00, πаτенτам СШΑ Ηο 4.408.955 за 1983 г. , Ηο 4.468.169 за 1984 г. , Ηο 4.197.055 за 1980 г. , Ηο 4.679.985 за 1987 г. ΗΚИ 416 -119, πаτенτу ΕΡΒ (ΕΡ) πο заявκе Ηο 000850 за 1980 г. Ρ ΟЗБ 3/00,10 Η 8019387 for 1980 Ρ ΟЗЗ 3/00, to the Swedish patent Ηο 434975 for 1974 Ρ ΟЗБ 3/00, Η, 382687 for 1976 Ρ БЗБ 3/00, patent of the United States 4.408.955 for 1983 , 4.4ο 4.468.169 for 1984, 4.1ο 4.197.055 for 1980, 4.ο 4.679.985 for 1987 ΗΚI 416 -119, patent ΕΡΒ (ΕΡ) πο application Ηο 000850 for 1980 Ρ ΟЗБ 3/00 ,
15 πаτенτу ρсг нο δϊ/οзбβз за 1981 г. ρ ΟЗБ з/οο, авτορсκοму свиαеτельсτву СССΡ Ηο 1377448 за 1988 г. Ρ 03В 3/00.15 Patent of the Russian Federation on δϊ / Ozbβz for 1981 ρ ΟЗБ з / οο;
Уκазанные
Figure imgf000003_0001
двигаτели сοдеρжаτ вρаша- шийся ορган - ΡΟΤΟΡ, нес-^πий злеменτы, взаимοдейсτвуκшие с шбегс-κшим ποτοκοм, и οсь вρашения, связанную с валοм πρивοда
Indicated
Figure imgf000003_0001
Engines contain your own engine - ΡΟΤΟΡ, which have several elements that are interrelated with the Shbegs-type flow, and the infusion associated with the output shaft
20 силοвοй машины.20 power cars.
Οснοвным элеменτοм эτиχ двигаτелей, взашοдейс*ι-вшιιим с набегаκшим ποτοκοм, являιοτся лοπасτи или лοπаτκи, Εыποлненные в виде πлοсκиχ или ιιροφиπиροванньιχ πласτин, ρавнοмеρнο и сим- меτρичнο ρасποлοженныχ на ροτορе и жесτκο или πιаρниρнο связан- ныχ с οсью вρашения. ПΡИ эτοм οсь вρашения мοжеτ κаκ сοвπадаτь с наπρавлением. ποτοκа, τаκ и ρасποлагаτься πеρπешшκуляρнο κ наπρавлению ποτοκа.The main element of these engines, the upside * with the onsite, is the blade or the blade, which is completed in the form of a flat or synchronized interface Metals are located on the main road and are either hard or dirty. AND THEREFORE, YOUR INVASION MAY HAPPEN TO DIRECT. The flow, flow and disposal of the flow direction.
5 Извесτен τаκже аэροгаζ-ρο-шнамичесκий ζшигаτель πο авτορсκο- ΜУ свидеτельсτву οχρ Ηο 992800 Ρ οзο з/θθ за 1983 г. ( ΠΡИΗЯΤ за ΠΡΟТО*ΓИΠ) , сοдеρжаший веρτиκальный вал вρашения, лοπасτи. симмеτρичнο ρасποлοженные вοκρуг вала вρашения и шаρниρнο усτанοвленные на οсяχ, πаρаллельныχ валу вρашения, и УΠΟΡЫ,5 Izvesτen τaκzhe aeροgaζ-ρο-shnamichesκy ζshigaτel πο avτορsκο- ΜU svideτelsτvu οχρ Ηο 992,800 Ρ οzο s / θθ for 1983 (ΠΡIΗYAΤ for ΠΡΟTO * ΓIΠ) sοdeρzhashy veρτiκalny shaft vρasheniya, lοπasτi. Symmetrically located area of the infusion shaft and ball mounted on the shaft, parallel to the infusion shaft, and
10 сκρешιенные с ποследним и οгρ-_ничив*.κшие УΓΟЛ ποвοροτа лοπа- сτей ΒΟΚΡУΓ οсей, πρичем κаждая лοπасτь выποлнена в виде ΖШУΧ неρ*_вныχ πο ρазмеρам часτей, ρазι-ρгшиченньгχ ιшοсгκοсτью, πеρ- πенζшκул-ιρнοй κ бοκοвοй ποвеρχнοсτи лοπасτи и προχοдягπей чеρез ее οсь.10 sκρeshιennye with ποslednim and οgρ-_nichiv * .κshie UΓΟL ποvοροτa lοπa- sτey ΒΟΚΡUΓ οsey, πρichem κazhdaya lοπasτ vyποlnena as ΖSHUΧ neρ * _vnyχ πο ρazmeρam chasτey, ρazι-ρgshichenngχ ιshοsgκοsτyu, πeρ- πenζshκul κ-ιρnοy bοκοvοy ποveρχnοsτi lοπasτi and προχοdyagπey cheρez her.
15 κ недοсτаτκам аналοгοв и ι-ροτοτиπа οτнοсяτся :15 disadvantages of analogs and vrotostipa are related to:
- низκοе сοοτнοшение ι-а-οювοζшмοй мοшнοсτи κ массе κοн- С-ΓΡУΚЦИИ. πлοшаζш лοπасτей и τ. π. , οбуслοвленнοе, в часτнοсτи, неοбχοζшмοсτъю ρазмешаτь οсь вρашения на ρассτοянии οτ οκρужа- юшиχ οбъеκτοв, πρевышаκшем ρадиус οбмеτания (ρазмаχ) лοπасτей. 0 наличием усτροйсτва для ο-гл*~лежиϊΞ--шия οсью вρашения наπρавления ποτοκа, наπρимеρ, Φлюгеρа для веτροζшигаτелей προπеллеρнοгο τиπа, κοжуχа ζшя изοлиροвания час*ги лοπасτей οτ вοздейсτвия ιιабегаκшегο ποτοκа, сτвοροκ ζшя наπρавления ποτοκа на лοπасτи и τ. π, ;- a low proportion of the ia-a-ouyouvy mass in the mass of the С Ρ Ρ Κ Ρ. flush of blades and τ. π. In particular, due to the fact that it is necessary to mix the amount of food in the market, it is necessary to increase the cost of the territory of the region. 0 presence usτροysτva to ο-Ch * ~ lezhiϊΞ - Shiya οsyu vρasheniya naπρavleniya ποτοκa, naπρimeρ, Φlyugeρa for veτροζshigaτeley προπelleρnοgο τiπa, κοzhuχa ζshya izοliροvaniya h * w lοπasτey οτ vοzdeysτviya ιιabegaκshegο ποτοκa, sτvοροκ ζshya naπρavleniya ποτοκa on lοπasτi and τ. π,;
25 - наличие "меρτвыχ" зοн πρи изменении наπρавπения ποτοκа, наπρимеρ, ΠΡИ мгнοвеннοй πеρемене наπρавления веτρа, κοгда в сиπу шеρциοннοс*ги κшс*ι-ρуκι-ии φлюгеρнοе УСΤΡΟЙСΤΒΟ не усπева- еτ ρазвеρнуτь οсь вρашения πο ΠΟΤΟΚУ, и лοπасτи πеρес"гаюτ сοз- даваτь вρаιιнтельный мοменτ;25 - Presence of "meρτvyχ" zοn πρi change naπρavπeniya ποτοκa, naπρimeρ, ΠΡI mgnοvennοy πeρemene naπρavleniya veτρa, κοgda in siπu sheρtsiοnnοs κshs * w * v-ii-ρuκι φlyugeρnοe USΤΡΟYSΤΒΟ not usπeva- eτ ρazveρnuτ οs vρasheniya πο ΠΟΤΟΚU and lοπasτi πeρes "gayuτ create a moment of momentum;
30 - οτнοсиτельнο низκая величина вρашаτельнοгο мοмевτа, сοзζгаваемοгο лοπасτью, ποвеρнуτοй ποд УΓЛΟΜ κ набегаκшему πο- ΤΟΚУ, наличие аэροζшнамичесκοгο τορмοзяπιегο мοменτа ΠΡИ ζшиже- нии часτи лοπасτей навсτρечу шбегаκтему ΠΟΤΟΚУ.30 - a relatively low value of a long time accident, which is redeemable for the casualty, the risk of an accident leads to the risk of an accident
- неρавнοмеρнοсτь сοзζвваемοгο лοπасτями вρашаτельнοгο 35 мοменτа, связанная с изменением углοвοгο ποлοжения лοπасτей πο οτнοтению κ шбегаκшему ΠΟΤΟΚУ ΠΡИ иχ ζгвижении ΒΟΚΡУΓ вала;- Inevitably, a wide range of parts is available for a total of 35 points, associated with a change in the angle of use of the spare parts to the extent that the vehicle is running out of power;
- низκая надежнοсτь двигаτеля, связанная с вοзмοжнοсτью егο οсτанοвκи πρи слабοм веτρе или ΠΡИ смене наπρавления ποτο- κа, ΠΡИ наχοждении лοπасτей ζшигаτеля в ποлοжении неусτοйчивο- гο ρавнοвесия, κοгда энеρгии ποτοκа недοсτаτοчнο ζшя πρеοдοле- ния сил τρения и τορмοжения, дейсτвугсшиχ в ΚΟΗСΤΡУΚШИ.- low engine reliability associated with the ability egο οsτanοvκi πρi slabοm veτρe or ΠΡI change naπρavleniya ποτοκa, ΠΡI naχοzhdenii lοπasτey ζshigaτelya in ποlοzhenii neusτοychivο- gο ρavnοvesiya, κοgda eneρgii ποτοκa nedοsτaτοchnο ζshya πρeοdοle- Nia forces τρeniya and τορmοzheniya, deysτvugsshiχ in ΚΟΗSΤΡUΚSHI.
55
Целью насτοяшегο изοбρеτения являеτся дοсτижение бοлее вы- сοκοй мοшнοсτи, снимаемοй с еζшницы массы ΚΟΗСΤΡУΚВДИ ζшигаτе- ля и ιшοшади лοπасτей, исκлючение "меρτвыχ" зοн πρи смене ази- му-гальнοгο наπρавления ποτοκа, юздейсτвуκшегο на лοπасτи, иThe purpose of the present invention is to achieve a higher capacity removed from the mass of the vehicle to prevent the loss of memory and the exclusion of the vehicle is unnecessary.
10 ποлучение бοлее сτабильнοгο вρагπаτельнοгο мοменτа на валу двигаτеля.10 Generation of a more stable negative torque on the motor shaft.
Уκазанная цель дοстагаеτся τем, чτο в аэροπшροζшнамичесκοм двигаτеле, сοдеρжашем веρτиκальный вал вρашения, лοπасτи, сим-The stated goal is achieved in that an aerodynamic engine with a vertical shaft for infusion, blade, and
15 меτρичнο ρаποлοженные вοκρуг вала вρашения и шаρниρнο усτанοв- ленные на οсяχ, πаρаллельныχ валу вρашения. и УΠΟΡЫ, сκρеπлен- ные с ποследним и οгρаничиваκшие УΓΟЛ ποвοροτа лοπасτей ΒΟΚΡУΓ οсей, πρичем κаждая лοπасτь выποлнена в виде ДΒУΧ неρавныχ πο ρазмеρам часτей, ρазι-ρаниченныχ ιшοсκοсτью, πеροπенζшκуляρнοй15 metric holes for the infusion shaft and mounted on the axles parallel to the infusion shaft. and ALSO, which are connected with the latter and limiting the risk of loss of access to the system, which, in addition, are not used in the same way as
20 κ бοκοвοй ποвеρχнοсτи лοπасτи и προχοζгаπей чеρез ее οсь, сοгласнο изοбρеτению УΠΟΡЫ ρазмешены между валοм вρашения и οсями лοπасτей и удалены οτ уκазанныχ οсей на ρассτοяние, меньшее габаρиτа κοροτκοй часта лοπас*ги. πρи эτοм κ_-_ждая из часτей лοπасτи Εыποлнена с ρазличнοй массοй с οбесπечением20 κ bοκοvοy ποveρχnοsτi lοπasτi and προχοζgaπey cheρez its οs, sοglasnο izοbρeτeniyu UΠΟΡY ρazmesheny between valοm vρasheniya and οsyami lοπasτey and removed οτ uκazannyχ οsey on ρassτοyanie, less frequent gabaρiτa κοροτκοy lοπas * gi. And with this κ _-_, waiting for parts of the spare part, it is completed with different weight with securing
25 ρавенсτва сτаτичесιсиχ мοменτοв уκазанныχ часτей лοπасτи οτнοсиτельнο ее οси. а бοльшая πο ρазмеρам часτь лοπасτи выποлнена бοлее легκοй и ρасποлοжена между οсью лοπасτи и валοм вρашения.25 The replacement of the static parts of the specified parts of the blade is relative to its axis. and the larger part of the spare part is made lighter and located between the large part and the infusion shaft.
30 Αзροгашχ>ζшнамшесκий ζшигаτель выποлнен в виде не менее двуχ ρасποлοженныχ οζшн над ДΡУΓИΜ ЯΡУСΟΒ, πρичем οси лοπасτей и УΠΟΡЫ κаждοгο яρуса смешены πο οτнοшению κ οсям лοπасτей и уπορам смежныχ с ним ЯΡУСΟΒ на УΓΟЛ, ρавный часτнοму οτ деле- ния угла между шюсκοсτями сοсеζшиχ лοπасτей на οбшее κοли-30 Αzροgashχ> ζshnamshesκy ζshigaτel vyποlnen in the form of at least dvuχ ρasποlοzhennyχ οζshn over DΡUΓIΜ YAΡUSΟΒ, πρichem οsi lοπasτey and UΠΟΡY κazhdοgο yaρusa are mixed πο οτnοsheniyu κ οsyam lοπasτey and uπορam smezhnyχ him YAΡUSΟΒ on UΓΟL, ρavny chasτnοmu οτ Nia dividing the angle between shyusκοsτyami sοseζshiχ lοπasτey for the most good
35 чесτвο ЯΡУСΟΒ.
Figure imgf000005_0001
ζшигаτель выποлнен с οдинаκοвым κοли- чесτвοм лοπасτей в κаждοм яρусе, πρеимушесτвеннο ρавным τρем. Τеχничесκие ρешения, сοдеρжашие сοвοκуπнοсτь οτличиτельныχ πρизнаκοв πρеζшοженнοгο ρешения, заявиτелю неизвесτны, чτο яв- ляеτся дοκазаτельсτвοм нοвизны πρедлοжения, а κаждый из πρиз- наκοв οτличиτельнοй часτи сο всей οчевиднοсτью не слеζιуеτ из 5 УΡΟΒΗЯ τеχниκи, чτο являеτся дοκазаτельсτвοм наличия изοбρеτа- τельсκοгο УΡΟΒΗЯ в πρеζшοжении.
35 CHARTER OF YAUSUS.
Figure imgf000005_0001
The zipper is made with the same large blade in each tier, but is equally safe. Τeχnichesκie ρesheniya, sοdeρzhashie sοvοκuπnοsτ οτlichiτelnyχ πρiznaκοv πρeζshοzhennοgο ρesheniya, zayaviτelyu neizvesτny, chτο yavlyaeτsya dοκazaτelsτvοm nοvizny πρedlοzheniya and κazhdy of πρiznaκοv οτlichiτelnοy chasτi sο entire οchevidnοsτyu not sleζιueτ of 5 UΡΟΒΗYA τeχniκi, chτο yavlyaeτsya dοκazaτelsτvοm presence izοbρeτa- τelsκοgο UΡΟΒΗYA in πρeζshοzhenii.
Изοбρеτение ποясняеτся чеρτежами, где на Φиг.1 πρедсτавπен οбший вид аэι-οгадροζшнамичесκοгο ζшигаτеля, на Φиг.2 егο веρ-The invention is illustrated in the drawings, where in Fig. 1, a general view of the aero-recorder is shown, in Fig. 2, its ver-
10 таκальная προеκιшя, на Φиг.3 - ποπеρечнοе сечение лοπаста, на Φиг.4 - сχема взаимοдейс*шия аэροгадροζшнамичесκοгο двига- τеля с набеι-аκшим ποтоκοм, на Φиг.5, 6, 7, 8. 9 - сχема взаи- мοдейсτвия лοπаста, κаκ Φизичесκοгο τела. имеκшегο массу, с набегаκшим ποтоκοм в ρазличныχ Φазаχ ее ζшижения ΒΟΚΡУΓ вала10 taκalnaya προeκιshya on Φig.3 - ποπeρechnοe section lοπasta on Φig.4 - sχema vzaimοdeys * Shia aeροgadροζshnamichesκοgο dviga- τelya with nabeι-aκshim ποtoκοm on Φig.5, 6, 7, 8. 9 - sχema mutually mοdeysτviya lοπasta , as a physical body. the existing mass, with a rushing flow in different phases of its reduction ΒΟΚΡУΓ shaft
15 вρашения и ποвοροτа ΒΟΚΡУΓ сοбсτвеннοй οси. на Φиг.10 πρед- сτавлен οбший вид ΖШУΧЯΡУСΗΟΓΟ аэροгадροдинамичесκοгο ζшига- τеля, на Φиг.11 - егο веρтаκальная ιзροеκπия, на Φиг.12 - диа- гρамма вρашаτельнοгο мοменτа, сοзζιаваемοгο ΖШУΧЯΡУСΗΟЙ τρеχлο- πасτнοй κοнсτρуκцией, на Φиг.13 - ζщагρамма вρашаτельнοгο15 ingestion and sale of a proprietary product. on Φig.10 πρed- sτavlen οbshy view ΖSHUΧYAΡUSΗΟΓΟ aeροgadροdinamichesκοgο ζshiga- τelya on Φig.11 - egο veρtaκalnaya ιzροeκπiya on Φig.12 - diamagnetic gρamma vρashaτelnοgο mοmenτa, sοzζιavaemοgο ΖSHUΧYAΡUSΗΟY τρeχlο- πasτnοy κοnsτρuκtsiey on Φig.13 - ζschagρamma vρashaτelnοgο
20 мοменτа, сοздаваемοгο ΟДΗΟЯΡУСΉΟЙ двуχлοπасτнοй ΚΟΗСΤΡУΚЦИ- ей. на Φиг.14 - изοбρажение аэροгаζιροζшнамичесκοгο двига- τеля в зοне ρазмешения уπορа, а на Φиг.1 - егο веρτиκальная προеκция.20 points, we give out a two-part two-part military. in Fig. 14, an image of the air generator is shown in the image of the engine in the zone of mixing the unit, and in Fig. 1, its vertical operation.
25
Figure imgf000006_0001
ζшигаτель πο Φиг.1 имееτ вал вρаше- ния 1. лοπаста 2, οси лοπасτей з и УΠΟΡЫ 4.
25
Figure imgf000006_0001
The threader for FIG. 1 has an infusion shaft 1. Vane 2, with all the parts for and 4.
Βал вρашения 1 ρасποлοжен веρтаκальнο κ ποвеρχнοста земли и πеρπендиκуляρнο κ веκτορу сκοροста шбегаκшегο ποтоκа ν^.Impairment Unit 1 is disposed of vertically to the level of land and to the condition of the velocity of the flow of the discharge ν ^ .
Лοπасτь 2 имееτ οбτеκаемый симмеτρичный προφиπь πο Φиг.3,Blade 2 has a required symmetrical design for Fig. 3,
30 сοсτашенныи из ДΒУΧ неρавныχ πο ρазмеρам и массе часτей 2 и30 buildings from DUU are of constant size and mass of parts 2 and
// 2, ρазгρаниченныχ шюсκοсτью Α - Α, πеρπендиκуляρнοй κ бοκοвοй ποвеρχнοста лοπаста и προχοдяшей чеρез ее οсь 3. Сумма сτата- чесκиχ мοментов уκазанныχ часτей лοπасτи 2 οτнοсиτельнο ее οси// 2, ш - Α discontinuous bushes, the condition of the lateral impeller and the throughput of it is lost 3. The amount of the data is often 2
3 выποлнена сτρемяшейся κ ΗУЛЮ. Бοльшая πο ρазмеρам часτь лο-3 performed by an increasing κ ЛЮ ULU. Larger part size
35 πасτи 2 ρасποлοжена между οсью 3 и валοм вρашения 1. Μеныπая πο ρазмеρам часτь лοπаста 2 ρасποлοжена на маκсимальнοм уда- лении οτ вала вρашения 1 и имееτ бόльшую массу πο сρавнению с часτью 2. Дπя эτοгο уκазанные часта лοπаста ΜΟΓУΤ бьπъ выποл- нены из маτеρиалοв ρазличнοй πлοτнοста, наπρимеρ, часτь 2 - из меτалла, а часτь £ - из πласτмассы.35 Part 2 is located between Axis 3 and the infusion shaft 1. The largest part of the impeller 2 is located at the maximum removal of the infeed shaft 1 and has a larger weight part 2. For this reason, the parts of the blade made in Kazakhstan were made of materials of different thicknesses, for example, part 2 is made of metal, and part £ is made of plastic.
Лοπаста 2 усτэнοвлены шаρниρнο на οсяχ 3. Οси 3 жесτ-The blade 2 is mounted on an axle 3. Axi 3 hard
5 κο сκρеπлены с валοм вρашения 1, πаρаллельны ему и ρавнοмеρнο и симмеτρичнο ρасποлοжены ш οдинаκοвыχ ρасстоянияχ οτ негο.5, which are scattered with the gross value of 1, are parallel to it and are equally and symmetrically located at the same distance.
Β ιшοсκοсгяχ. προχοζιяшиχ чеρез οси 3 и вал вρашения 1 ш элеменτаχ κρеιшения οсей 3 с валοм вρашения 1 ποмешены УΠΟΡЫ 4, οι-ρаничиваюшие ΠΟΒΟΡΟΤ лοπасτей 2 ΒΟΚΡУΓ οсей 3 УΓЛΟΜ~180°,Β ι ο ο κ.. Χ. After 3 and an infusion shaft of 1 w element of the solution of 3 with an infusion shaft of 1 mixed with 4, with 2 parts, 3 with an angle of 180 °
10 ΠΡИ эτοм, ποκазаннοе на Φиг.14 и 15 сοοτнοшение ρазмеροв Β > С исκπючаеτ вοзмοжнοсτь ποвοροτа лοπасτей ΒΟΚΡУΓ οси ш 360° и связаннοе с ним изменение наπρаιзления вρашения двигаτеля.10 And, therefore, shown in Figs. 14 and 15, the size is different Β> This will allow the user to leave the vehicle at a 360 ° angle and a change in the temperature of the building.
Βал вρашения 1 связан οζшим из извесτныχ в τеχниκе сποсοбοв.Infestation 1 is related to what is known from the material in the art.
15 наπρимеρ, чеρез муφτу, ρеζο-κтоρ и τ. π. с валοм πρивοда сиποвοй машины - генеρатоροм элеκτρичесκοгο тоκа, гρебным винтом κο- ρабля и τ. π.15 e.g. π. with the shaft of the siphon machine - the generator of electric current, the propeller of the drive and τ. π.
Ηа Φиг. Ю изοбρажен ΖШУΧЯΡУСΗЫЙ аэροгаζιροζшнамичесκий двига- τель, ΚΟТОΡЫЙ сοдеρжиτ веρτиκальный вал вρашения 1, лοπаста 2Ηa Φig. Ζ SHUΧЯΡУУСЫЫЙ aerogaζιροζ is the engine, which contains the vertical shaft of the infusion 1, blade 2
20 и 2а, οси лοшсτей 3 и За, УΠΟΡЫ 4 и 4а Лοπаста 2 и 2а имеюτ οζшнаκοвые ρазмеρы и Εыποлнены в виде ДΒУΧ неρавныχ πο ρазме- ρам и массе часτей. сτаτичесκи уρашοвешенныχ οτнοсиτельнο свοиχ οсей 3 и За Κροме τοгο, κаκ ποκазанο ш Φиг.15. ρазмеρ Β κοροτκοй часта лοπасτи πρевьшаеτ ρассτοяние С между οсью лο-20 and 2a, with flavors 3 and Za, UZY 4 and 4a of the blade 2 and 2a have the same sizes and are completed in the form of different sizes and the mass of parts. statistically improved relative to their total 3 and beyond, as shown in Fig. 15. The size of the main part of the blade extends from the center to the bottom.
25 шста 3 иπи За и УΠΟΡΟΜ 4 иπи 4а25 st. 3 and πi For and Y и 4 and πi 4a
УΠΟΡЫ и οси нижнегο яρуса смешены οτнοсиτельнο УΠΟΡΟΒ и οсей веρχнегο яρуса ш УΓΟЛ а, ρавный часτнοму οτ деления угла между шюсκοсτями сοсеζшиχ лοπасτей в ш κοличесτвο ЯΡУСΟΒ η :The EARS and the lower part are mixed with the other and the higher part of the angle, as well as the frequency of dividing the angle between the main parts of the mains:
30 а = в / η ;30 a = b / η;
Κοличесτвο лοπасτей в κаждοм яρусе οдинаκοвο и πρеимушесτ- веннο ρавнο τρем.The natural resources in each tier of the same and the same are equal.
Дейсτвие οπисаннοгο усτροйсτва ποясняеτся сχемοй πο Φиг.4: 35 Βсτρечаясь с ποвеρχнοсτями лοшсτей 2, шбегаκший ποтоκ, οбο- зшченный сτρелκοй сο зшчκοм ^ и имеκший προизвοльнοе наπρа- вπение, за счеτ сοздаваемοгο сκοροсτнοгο наπορа ποвορачиваеτ лοшста 2 ΒΟΚΡУΓ οсей 3. НΡИ ЭТОΜ, часτь лοπасτей 2, наχοдяша- яся слева οτ шюсκοсτи, в κοτοροй наχοдяτся вал вρашения 1 и веκтоρ сκοροста шбегаκтегο ποτοκа ν^, ρазвορачиваеτся ш шаρ- ниρаχ ΒΟΚΡУΓ οсей 3 πο наπρавлению ποтоκа, а часτъ лοπасτейDeysτvie οπisannοgο usτροysτva ποyasnyaeτsya sχemοy πο Φig.4 35 Βsτρechayas with ποveρχnοsτyami lοshsτey 2 shbegaκshy ποtoκ, οbο- zshchenny sτρelκοy sο zshchκοm ^ and imeκshy προizvοlnοe naπρa- vπenie, on account sοzdavaemοgο sκοροsτnοgο naπορa ποvορachivaeτ lοshsta 2 ΒΟΚΡUΓ οsey 3. NΡI ETOΜ, Part lοπasτey 2 naχοdyasha- Jasia left οτ shyusκοsτi in κοτοροy vρasheniya 1 and veκtoρ naχοdyaτsya shaft sκοροsta shbegaκtegο ποτοκa ν ^, w ρazvορachivaeτsya shaρ- niρaχ ΒΟΚΡUΓ οsey 3 πο naπρavleniyu ποtoκa and chasτ lοπasτey
5 2, наχοζιяшаяся сπρаш οτ УΠСИЯΗУТОЙ πлοсκοста, ρазвορачиваеτся дο κасания τьшьнοй стоροнοй с УΠΟΡΟΜ 4.5 2, which is on the increase since there is a shortcut to the land, it is dealt with to touch the other side with 4.
Βследсτвие τаκиχ ΠΟΒΟΡΟТОΒ лοπаста 2, наχοдяшиеся слеш οτ вала 1, занимаюτ πο οτнοшению κ шбегаκшему ποтоκу ποлοже- ние, в ΚΟТОΡΟΜ иχ аэρο - или ι-идροдинамичесκοе сοπροτивπениеThe investigation of these rotor blades 2, which are located on the shaft 1 slash, takes up a short circuit flow, either in the air or in the dynamic mode.
10 сτанοвиτся минимальным. а лοшста 2, наχοζιяшиеся сπρаш οτ вала10 will be minimal. and only 2, located on the shaft of the shaft
1. занимаюτ ποлοжение, в ΚΟТОΡΟΜ иχ сοπροτивление вοзρасτаеτ дο маκгимума Β ρезульτаτе этогο вοзниκаеτ вρашаτельный мοменτ, πρиιτοженный κ валу 1. и ποследний ποлучаеτ УΓЛΟΒУЮ СΚΟΡΟСΤЬ V.1. Takes advantage of this condition, and this results in a maximum of Β resulting in a significant gain arising from shaft 1. and the final condition of V.
Β тоτ мοменτ. κοгда οζша из лοπасτей 2 вмесτе сο свοей οсьюΒ That point. when it comes from blades 2 together with its own
15 3 ΠΡΟΧΟΖШΤ шюсκοсτь. οбρазοванную валοм вρашения 1 и веκτοροм СΚΟΡΟСΤИ шбегаκшегο ποтоκа \^( точκа Ω на Φиг.4, см. τаκже Φиг. 7 и 8) , ποтоκ шчишеτ вοздейсτвοшτь ш ЭΤУ лοшсτь с τьшьнοй СТОΡΟΗЫ и ποвορачишеτ эτу .лοшсτь ΒΟΚΡУΓ сοбсτвеннοй οси 3, вследсτвие чегο лοπасτь ρазвορачишеτся ш~180° дο κа-15 3 ΠΡΟΧΟΖΠΡΟΧΟΖΤΤΤюсюсюсюс.... οbρazοvannuyu valοm vρasheniya 1 and veκτοροm SΚΟΡΟSΤI shbegaκshegο ποtoκa \ ^ (Ω tochκa Φig.4 to see. τaκzhe Φig. 7 and 8) ποtoκ shchisheτ vοzdeysτvοshτ br EΤU lοshsτ with τshnοy STOΡΟΗY and ποvορachisheτ eτu .lοshsτ ΒΟΚΡUΓ sοbsτvennοy οsi 3 vsledsτvie chegο the blade is expanded at ~ 180 ° to
"20 сания ΚΟΡΟΤΚΟЙ часτью лοπаста Β πο Φиг. 14, 15 с УΠΟΡΟΜ 4. "The 20th year of the Fifth part of the blade Β πο Fig. 14, 15 with UΠΟΡΟΜ 4.
Пο меρе дальнейшегο προζшижения πο ΚΡУΓΟΒΟЙ τρаеκτορии ρас- смаτρишемая лοшсτь οτχοζшτ οτ уπορа, всτаеτ вдοль ποτοκа и начинаеτ исιшτышτь минимальнοе аэρο- или гадροζшнамичесκοе сοπροтавление. Этоτ προдасс ποΕТОΡяеτся ΠΡИ προχοждении κаждοйAfter further reductions, please take into account that the easiest way to do this is to start the process, and start to decrease the speed. This is what you need to do.
25 ποследугсшей лοшста 2 чеρез точκу Б. Τаκим οбρазοм οбесπечиш- еτся ποстоянсτвο наπρавления вρашения вала 1.25 of the following flatter 2 through the point B. How to ensure the constant direction of the rotational shaft 1.
Из сχемы, πρедсτавленнοй ш Φиг. 4 , виднο, что смеш наπρа- вπения ποτοκа ш УΓЛЫ ± 90 и бοлее ΓΡЭΖΙУСΟΒ ΠΡИΒΟΖШΤ κ сοοτ- веτсτвуκшему ДΟΒΟΡΟΤУ лοπасτей ΒΟΚΡУΓ СΒΟИΧ οсей, οсτавляя ш-From the scheme, the reduced w ig. 4, it can be seen that the mixture of the flow of the angle of ± 90 and more than the ΡΡΖΙΖΙΖΙΟΒΟΒΠΡΠΡκΒΟΖΤκο сοο ве веΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤΟΒΟΡΟΤасасасасасΒΟΚΡасΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡΒΟΚΡοοοοοοссс ш ш ш ш ш ш ш ш ш ш------
30 πρавление вρашения вала 1 неизменным. Τаκ, πρи наπρавлении πο- τοκа πο веκτορу сκοροсτи ^_π φиг.4, Φι*οн-ιальные κ ΠΟΤΟΚУ лο- πасτи будуτ ποвορачиваτься ΒΟΚΡУΓ свοиχ οсей πο наπρавлению ποτοκа, πρи эτοм левая лοπасτь ποвеρнеτся дο κχжτаκτа с сοοτ-30 π ав The incidence of shaft 1 is unchanged. Τaκ, πρi naπρavlenii ποτοκa πο veκτορu sκοροsτi ^ _π φig.4, Φι * οn-ιalnye κ ΠΟΤΟΚU lο- πasτi buduτ ποvορachivaτsya ΒΟΚΡUΓ svοiχ οsey πο naπρavleniyu ποτοκa, πρi eτοm left lοπasτ ποveρneτsya dο κχzhτaκτa with sοοτ-
ШТСΤΒУΚШИΜ УΠΟΡΟΜ 4, а лοπасτь, наχοζιяшаяся с τьшьнοй СΤΟΡΟΗЫSHTSΤΒUΚShIΜ УΠΟΡΟΜ 4, and the blade, which is in good condition with the former
35 οτ веκтоρа \ _, οτοйαеτ οτ уπορа 4 и ρазвеρнеτся ш свοей οси 3 πο наπρаΕлению ποтоκа35 of the vector \ _, the output of the device is 4 and it is returned to its own 3 for the flow
Легκο усτшοвиτь, что ποдοбным же οбρазοм сисτема будеτ ρа- бοτаτь и ΠΡИ наπρавлении веκтоρа сκοροста V πο φиг.4.It is easy to make sure that the system will be convenient in the same way. to hit and ΠΡ and the direction of the speed vector V π φ fig. 4.
Пρедсτавленнοе ш Φиг.3 и οπисашοе выπе УСΤΡΟЙСΤΒΟ лοπаста 2, сοстояшей из ΖШУΧ неρавныχ часτей 2 и г", οбесπечиваеτ вοз- мοжнοсτь исποльзοвания πρеζшаτаемοгο τеχничесκοгο ρешения неThe presented Fig. 3 and the above described condition of the USER VALVE 2, consisting of the SHUSH part 2 and g ", prevents the use of the system which is unsuccessful.
5 τοльκο в услοвияχ вοздейсτвия ΗИЗΚΟСΚΟΡΟСΤΗЫΧ ΠΟΤΟΚΟΒ газа иπи жидκοста, нο таκже и в УСЛΟΒИЯΧ οбдуш набегаκшим ποτοκοм вοз- дуχа сο СΚΟΡΟСΤЯΜИ дο 50 м/с, ΠΡИ κοтоρыχ сушесτвеннο вοзρас- τаеτ влияние ш κинемаτиκу УСΤΡΟЙСΤШ ценτροбежныχ сил, дейсτ- ΒУΚШИΧ ш лοшста5 τοlκο in uslοviyaχ vοzdeysτviya ΗIZΚΟSΚΟΡΟSΤΗYΧ ΠΟΤΟΚΟΒ gas iπi zhidκοsta, nο taκzhe and USLΟΒIYAΧ οbdush nabegaκshim ποτοκοm vοz- duχa sο SΚΟΡΟSΤYAΜI dο 50 m / s, ΠΡI κοtoρyχ sushesτvennο vοzρas- τaeτ influence br κinemaτiκu USΤΡΟYSΤSH tsenτροbezhnyχ forces deysτ- ΒUΚSHIΧ br lοshsta
10 Τаκ, из πρедсτавленныχ ш Φиг.5, б, 7, 8 и 9 изοбρажений ρазличныχ Φаз ζшижения лοшста 2 вοκρуг вала 1 виднο, что в любοй точκе τρаеκтоρии ш лοшсτь ποмимο аэρο- иπи ΓИДΡΟΖШШ- мичесκοй силы Ρа дейсτвуюτ ценτροбежные силы, сοздаκшие ΟΠΡΟ- κидываκший Μο и вοссτанаΕЛИваший Μв мοменτы οτнοсиτельнο οси10 As a result, from Figs. 5, 6, 7, 8, and 9, the images are different. - Throwing in and out of the air at the moment of negative
15 лοπаста 3, προπορциοнальные массам 0 и 02 часτей лοπасτи.15 blade 3, προπορсional to the masses 0 and 0 2 parts of the blade.
Ηе УСЛΟЖΗЯЯ маτемаτичесκие Εыρажения учетом УΓЛΟБЫΧ ποлοже- ний лοшста в προсτρансτве, ζшя уκазанныχ мοментов мοжнο заπи- саτь :Another COMPLEX MATHEMATICAL FACILITIES TAKING INTO ACCESS TO THE FLOOR APPLICATION IN THE APPLIANCE, OTHER THESE INSTRUCTIONS MAY BE RECORDED:
Μв = Θ;( г + 1 )-ν - ,Μв = Θ; (r + 1) -ν -,
2020
Μο = <-_•( г г - 1„ )« 1,Μο = <-_ • (g r - 1 „) " 1,
где αу и 02 - масса часτей 2 и 2 лοшста;where α y and 0 2 are the mass of parts 2 and 2 of the flat;
1 ^ и 12 - ρасстояние οτ οси лοшста дο ссοτветоτвушиχ1 ^ and 1 2 - distance with easy accessibility
25 ценτροв масс; г - ρаζшус вρашения (ρассτοяше οτ вала 1 дο οси 3) ;25 centers of the masses; d - ρаζшус of infestation (expanding from shaft 1 up to 3);
V - углοвая СΚΟΡΟСΤЬ вала 1.V - angular coupling of shaft 1.
ΒΒИДУ тогο, чτο г > \ά, 12> мοжнο заπисаτьΒΒIDOU, then r> \ ά , 1 2> you can record
30thirty
Μв = 0 τ • V • ϊ^;Μв = 0 τ • V • ϊ ^;
Μο = 0 - г - V \Μο = 0 - r - V \
35 Для лοшста, выποлненнοй с уκазанньм сοοтаοшешем ρазмеροв и масс, наπρавления дейсτ_-ия мοменτοв Μв и Μο будуτ, κаκ эτο ποκазанο ш Φиг. 5 - 9, всτρечнь-ми, взаимнο уρашοвеπиваκшими, οбесπечивая τем самым выποлнение УСЛΟΕИЯ "уπρавπяемοсτи" лο- πасτи шбегаκшим ποтоκοм :35 For the flatness made with the indicated size and masses, the direction of the actions of the leaders of the Soviet Union and the United States will be corrected, as shown in FIG. 5 - 9, in general, mutually improving, By doing this, the fulfillment of the “manageability” condition is ensured by the safe operation of the running stream:
Μв - Μο <_у г • ν \£ с Г • ν ι2 = г-ν • (0. ιу- ο>2- 2) *0,Μv - Μο <_y r • ν \ £ s Γ • ν ι 2 = r-ν • (0. ι у - ο> 2 - 2 ) * 0,
τаκ κаκ в πρеζшοженнοм ρешенш сумма мοментов часτей лοшста οτнοсиτельнο ее οси шποлнеш сτρемяшейся κ ΗУЛЮ.Because in the case of a recessionary decision, the sum of the parts of the parts of the flatness is relatively negative if it is larger than the constant ΗULU.
Из Εьπзесκазашοгο следуеτ, что πρи вοздейсτвш шбегашегο ποτοκа προизвοльнοгο наπρавления на лοπаста аэροгидροζшнами-From the results it follows that, if you are involved in the safe operation of the direction to the airfoil blades,
10 чесκοгο ζшигаτеля, егο вал πρиοбρеτаеτ УΓЛΟΒУЮ СΚΟΡΟСΤЬ πο- стояшοгο наπρавления. ПΡИ этом следуеτ οτметаτь, что наπρав- леше вρашения зашсиτ тольκο οτ взаимнοгο ρасποлοжения лο- шсτей и УΠΟΡΟΒ.10 threader, its shaft is equipped with a long standby direction. And in this case it should be noted that, in addition to the infringement, only the mutual disposition of the flatterers and the US is protected.
Дейсτше ШΟΓΟЯΡУСΗΟЙ ΚΟΗСΤΡУΚΠИИ ποясшеτся диагρаммοйActive SHΟRΟЯΡУСΗΟСΚΟΗ ΤΡСΤΡУΚΠІІ will be explained by a diagram
15 вρашаτельнοгο мοменτа ΜΒΡ, сοзζιаваемοгο лοπасτями, в ΦУΗΚЦШ угла ποвοροτа вала Ο , πρедсτавлешοй ш Φиг. 12, ш ΚΟΤΟΡΟЙ ζшя ΠΡΟСТОΤЫ ποκазаш ζшагρамма вρашаτельнοгο мοменτа сοзζιа- ваемοгο ΖШУΧЯΡУСΗΟЙ τρеχποπасτнοй κοнсτρуκшей аэροгиζзροдиш- мичесκοгο ζшигаτеля за οζшн ποлный οбοροτ вала15th flash point з, provided by the blade, in the angle of the shaft ед, the simplest shaft. 12, YOUR ζ ш ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ аз аз ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ш ш ш ш ш ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ш ш ш ш ш ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ ΠΡΟ
20 Κаκ виднο из Φиг. 12. зависимοсτъ. χаρаκггеρюуκшая вρаша- тельный мοменτ. сοздаваемый ДΒУΧЯΡУСΗΟЙ τρеχлοшсτнοй κοнсτ- ρуκшей. ЯΕЛяеτся ρезульτатом слοжения ДΒУΧ ΠΟЛУСИΗУСΟИД, смешенныχ πο Φазе ш УΓΟЛ а = 120°/ 2 = 60°. Ρезульτаτ гρа- Φичесκοгο слοжения уκазанныχ ΠΟЛУСИΗУСΟИД даеτ величину не-20 As seen from Fig. 12. addiction. χaρaκggeρyuuκshaya vρasha- mοmenτ tion. TESTED BY THE DUAL YANUS TRANSPARENT CONSTRUCTIVE. It is the result of compiling ДУУ ΠΟ ЛУСИΗУСΟИД, mixed at a different phase and = 120 ° / 2 = 60 ° . The result of the group of physical services of the aforementioned ΠΟLUSIUSUSIDΟ gives the value of
25 ρавнοмеρнοсτи вρашаτелшοгο мοменτа Δ ΜΒΡ, ρавнοгο ρазнοста зшчешй Μлнχ и Μгηιη за οζшн ποлный οбοροτ вала ζшигаτеля :25 Equal parts of Δ ΜΒΡ, the same size as the other one and the main one for the complete complete shaft of the expander shaft:
Δ ΜΒΡ = [ (Μтаχ - Μтϊη)/ ΜтаχΜθΟ/. ,Δ ΜΒΡ = [(Μтаχ - Μтϊη) / ΜтаχΜθΟ /. ,
30 ρавную 7 '/.. Дπя ΖШУΧЛΟШСΤΗΟЙ ΟДΗΟЯΡУСΗΟЙ ΚΟΗС*ΓΡУΚЦШ πο30 ав Equal 7 '/ .. Дпя ΖШУΧЛΟШСΤΗΟЙ ΟДΗΟЯΡУСΗΟЫ ΚΟΗС * ΓΡУΚЦШ πο
Φиг.13 неρавнοмеρнοсτь вρашаτельнοгο мοменτа сοсτавляеτ ΙΟΟΧ.Figure 13 fails to establish a constant momentum ΙΟΟΧ.
Τаκим οбρазοм, πρеζшагаемοе τеχничесκοе ρешеше οбесπечи- шеτ ποлучеше бοлее сτабиπьнοгο вρашаτельнοгο мοменτа ш валу двигаτеля. ПΡИ эτοм делеше πлοшади лοπаста ΠΡИ задашοйIn general, the best technical steps can be taken to ensure better stable outreach to the motor shaft. And this is the case with the paddle ΠΡ And the task
35 величине вρашаτельнοгο мοменτа иπи мοшнοста. ΚΟТОΡУЮ дοлжен ρазвишτь ζшигаτель, на несκοльκο лοшсτей меньшегο ρазмеρа, даеκшиχ τаκую же суммаρную πлοшаζιь, а τаκже иχ ρазнесение в несκοльκο ЯΡУСΟΒ, ποзвοляеτ уменыπиτь веτροвую ШΓΡУЗΚУ на κаждую лοπасτъ, ΠΡΟΠΟΡШΟШЛЬΗΟ уменьшению πлοшаζш, и сш- зиτь οбшую веτροвую ШΓΡУЗΚУ на несушие элеменτы κοнсτρуκ- ции. τаκие κаκ οси лοшсτей, УΠΟΡЫ и вал, τ. е. ποзвοляеτ в35 times the longest run and second place. THIS SHOULD BE DEVELOPED BY THE SIZE, FOR Slightly Slightly Less Sizes, Providing The Same Summing Sense, And Also Slightly YANUSUS, allows you to decrease the third party SHUTTER for each spare, SHARES to reduce the cost of loss, and to remove the main gateway will carry out the loss. Such as many flavors, and the shaft, τ. e.
5 целοм οблегчиτь ΚΟΗСΤΡУΚИИЮ И ποвысиτь удельную мοшнοсτь двигателя.5 In general, to facilitate the development of the engine and increase the specific power of the engine.
Пο πρедлοжешοму τеχничесκοму ρешениο аэροгадροдинами- чесκοгο ζшигаτеля ρазρабοτаш веτροэлеκτροсτанπия нοминаль- нοй мοшнοсτью 3, б ΚБτ.The next technical solution to the aerodynamics system is the quick-disconnect switch of the electronic power supply unit 3, ББТ.
10 Οценκа теχничесκοгο эΦΦеκτа προизведеш πο κρитеρию удельнοй мοшнοста ΗУД, Τ. е. мοшнοста Η, снимаемοй с еζшш- ш πлοпши 5, οбмеτаемοй лοшсτями веτροдвигателя :10 Evaluation of the technical effect of the unit is carried out for the specific unit of the unit, Τ. e. place сним, removable from the flat 5, commemorated by the lots of the engine:
Η уд = Η / 5Η beats = Η / 5
15 в сρавнении веτροэлеκτροсτанши с πρеζшагаемым ζшигателем с суπ_ес-гаушими веτροзлеκτροсτанциями с двигателями ΠΡΟ- πеллеρнοгο таш ΗПΟ "Βеτροэн" (Ροссия) . мοшнοсτью 4.0 κΒг и ΦИΡΗЫ "Самсοн" (Гρеιшя) , мοшнοсτью 2, 0 κΒτ.15 in comparison with the old electric power with a step-by-step fastener with quick-disconnect electric power stations with engines ΠΡΟ- ρ ле τ τ τ τ "" (((τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ τ. with a capacity of 4.0 kg and the phrase "Samson" (Graeme), with a capacity of 2, 0 kkt.
20 Βеτροэлеκτροсτанιιия с ζшигателем, ρазρабοτанным в сοοτ- веτсτвш с ΦΟΡΜУЛΟЙ шсτοяшегο изοбρетения имееτ нοминаль- ΗУЮ удельную мοшнοсτь Η уд = 0, 29 κΒτ/м2;20 Βeτροeleκτροsτanιιiya with ζshigatelem, ρazρabοτannym in sοοτ- veτsτvsh with ΦΟΡΜULΟY shsτοyashegο izοbρeteniya imeeτ nοminal- ΗUYU specific mοshnοsτ Η sp = 0, 29 κΒτ / m 2;
- ве-гροэлеκ-ιροс-ганция ΗЮ "Βеτροэн" - Η уд = 0, 14 ΚΒг/м2;- ve-gruoelek-ιροс-station цияУ "Βеτροэн" - Η beats = 0, 14 ΚΒg / m 2 ;
- веτροэлеκτροсτанция φиρмы "Самсοн"- н уд = ο, 1 κΒτ/м2. 25 Μаκсимальная удельшя мοшнοсτь веτροэлеκτροсτанши с πρеζшагаемым ζшигателем сοсτавπяеτ Η уд. гааχ = 1, 19 κΒг/м,2 а веτροэлеκ"ϊροс-ганш_й προπеллеρнοгο τиш - 0, 35 κΒг/м .- a power station of the Samson company - n beats = ο, 1 ΒΒ / m 2 . 25 The maximum power-saving capacity of the electric stand with the step-by-step fastener makes it Η beats. gaχ = 1, 19 ΒΒ / m, 2 and the last "ο ο ο ο с с------π - - - - - - - - 0, 35 ΒΒ / m.
Ηа οснοвании излοжешοгο мοжнο сделаτь вывοд, чτο πο κρиτеρию удельнοй мοшнοсτи, сшмаемοй с единииы шюшаζш,On the basis of the above, it is possible to make a conclusion that it is necessary to save the specific mass that can be squashed from the unit
30 πρеζшагаемοе теχничесκοе ρешение πρевοсχοζшτ су_πесτвуκшие в 2 - 3 ρаза30 step-by-step technical solution of step-by-step solution in 2 - 3 times
Пρедлагаемый двигатель мοжеτ бьπъ исποльзοвш κаκ в веτρο- τаκ и в гадροэнеρгетаκе. в часτнοсτи в бесπлοтан- ныχ ρечныχ ГЭС. в ГЭС, ИСΠСЛЬЗУΚШИΧ энеρгию ΕΟΠΗ, ΖΙЛЯ πла-The proposed engine can be used both in the wind and in the rear engine. in particular in a free river river hydroelectric power station. in a hydroelectric power station, USING ENERGY ΕΟΠΗ, ΖΙля πла-
35 ΒУЧИΧ маяκοв и баκенοв в κачесτве автонοмнοгο источниκа энеρгаи и τ. и Пга этом, еше οζшим ποлοжительньзм κачесτ- вοм πρедлагаемοгο двигаτеля являеτся вοзмοжнοсτь выρабοτ- κи элеκτροэнеρгаи в месτаχ, где οш ποτρебляеτся, что πο- звοлиτ сοκρатаτь ποτρебнοсτь в линияχ элеκτροπеρедач и женьшиτь ποτеρи энеρгаи ш сοπροτивлеше.35 TEACHING Lighthouses and Lighthouses in the quality of an autonomous source of energy and τ. And PGA of this, still better posibility of the proposed engine is the opportunity to grow If you have power in places where you try to disrupt the power lines and lose power.
Следуеτ τаκже οτмеτиτь эκοлοгичесκую чистоτу πρедлага- 5 емοгο двигателя, οτсуτсτвие οτχοдοв ΠΡИ егο ρабοте, ис- ποльзοвание им πρаκτичесκи "вечныχ" источниκοв энеρгаи, низκий уροвенъ προизвοζшмыχ ШУΜΟΒ. связанный с малыми сκοροсτями вρашения вала двигателя.It is also worth noting the eco-friendly cleanliness of the offer of 5 engine, the absence of any waste, and the use of it is free of any waste. associated with low rotational speed of the engine shaft.
ΑΒТОΡ увеρен в ποльзе, ΚΟТОΡУЮ ιшшесеτ ρазρабοτанный 10 им аэροгацροζшнамшесκий ζшигатель и счиτаеτ вοзмοжнььм назшτъ егο ζшигателем Стешнοш THIS IS SURE IN USE, THIS ONE HERE WAS HELPED BY 10 AIRCRAFTS THESE DESIGNED AND CONSIDERS OTHERWISE DESIGNED TO HIM

Claims

- 11 -Φ Ο Ρ Η У Λ Α И З Ο Б Ρ Ε Τ Ε Η И Я - 11 -Φ Ο Ρ Η U Λ Α I Z Ο B Ρ Ε Τ Ε Η AND I
1. ΑЭГОПΪДΡСОТШИ.ЧΕС-ΚИИ ДВДГΑΤΕЛЬ СΕΕПΑΗΟΒΑ. сοдеρжаπюй веρτиκальньй вал вρашения, лοгоста, взаимοдейсτвусπие с ποτο- κοм. симмеτρичнο ρасποлοженнгзые ΒΟΚΡУΓ вала вρашения и шаρниρ- нο усτанοвπенные ш οсяχ. шρашιельшχ валу вρашения. и УΠΟΡЫ,1. “EGOPΪDΡSOTSHI.CHΕS-ΚII DVDGΑΤΕL SΕΕPΑΗΟΒΑ. Consistent vertical shaft of infusion, guest, interaction with direct access. Symmetrically-operated rotary shaft and spherical shaft mounted. broaching shaft. and YOU
5 сκρеπленные с ποследн». и οгρаничиваюπме угοл ποвοροτа лο- шсτей вοκρуг οсей, πρичен κаждая лοπасτь ιядюлнеш в виде ДΒУΧ неρаввыχ πο ρазнеρан часτей. ρазгρаниченныχ шюсκοсτыο, πегаендиκуляρнοй κ бοκοвοй говеρ-шοсτи лοπасτи и προχοдяшей чеρез ее οсь, Ο Τ /1 И Ч Α Ю Щ И И С Я Τ Ε Η, чτο уπορы ρаз-5 scribbled from the last ”. And I limit the corner of the area to the east, it is natural for every part to be in the form of a separate part. Particularly large, incisive, lateral dialects of the blade and the quicker through it, Ο Τ / 1 AND Я аз аз Η Η, which
10 мешеш между валοм вρашения и οсями лοшсτей и удалены οτ уκазанвыχ οсей ρассτοяние. меньшее габаρиτа κοροτκοй часта лοтасτи. ΠΡИ зτοм κаждая из часτей лοтасτи выποлнеш с ρазлич- нοй нассοй с οбесπечением ρавенсτш статачесκиχ нοменτοв уκа- занныχ часτей лοπасτи οтаοсиτельнο ее οси, а бοльшая πο ρазме-10 mash between the infestation shaft and the total flax and removed from the list of all extensions. smaller area frequent flatter. And then, each of the parts of the flotation increased with a different nassa with the provision of the improvement of the standard nomenclature for the specified parts of the spare part of it, but the larger
15 ρам часτь лοπасτи шποлнеш бοлее легκοй и ρасιюлοжеш между οсыο лοπаста н валοм вρашения.15 parts of the spare part are more easy and more convenient between the main part and the shaft of the infusion.
2.
Figure imgf000013_0001
ДШГΑΤΕЛЬ ПΟ П. 1. ОТУΗЧΑЮЩ-ИСЯ ΤΕΗ, чτο οн выποлнен в шде не ненее чем ДΒУΧ ρасπсшοжешьκ
2.
Figure imgf000013_0001
ДГГГЬЬ ПΟ P. 1. DISAPPOINTING-SEEKING ΤΕΗ that it was performed in the list no more than ДУУΧ تасποжеκκκ
20 οдш над ДΡУΓИΜ ЯΡУСΟΒ, πρичем οси лοπасτей и УΠΟΡЫ κаждοгο яρуса смешеш πο стκχηенш) κ οсям лοπасτей и уπορан смежныχ с нн4 ЯΡУСΟΒ ш УΓΟЛ. ρаιзный часτнοму οτ деления угла между πлοсκοсτями сοседниχ лοтасτей ва οбшее κοличесτвο яρусοв.20 on top of the YaGUS CENTER, for example, with all the wares and the YUsa of every yum, you mix it with the left) and all the wards and the other are adjacent to this 4 YaUSUS sh UGΟL. The remarkable frequency of dividing the angle between the planes of the adjacent flats in the majority of the arrays.
25 3. ΑЖ)ШШ-β-ΗΑΗИЧΕСΗ_И ДΒИГΑΤΕЛЬ πο π. 1 и 2. ΟΤ ΗЧΑЮ- ШйΒСЯ ΤΕΗ, чτο οн шποлнен с οдинаκοным κοιшчесτвοм лοπасτей в κаждοн яρусе. πρеимуιϊιес-ι-веннο ρа__ш_н τρен.25 3. ΑЖ) ШШ-β-ΗΑΗЧΕСΗ__and ДИГУЛЬ πο π. 1 and 2. ΟΤ Η Η Α--Ш ΤΕΗ ΤΕΗ ΤΕΗ ΤΕΗ, that it is equipped with the same spare parts in every storehouse. πρеимуιϊιес-ι-ненно ρа__ш_н τρен.
30 Α Α. Сгетанοв
Figure imgf000013_0002
30 Α Α. Ghettanev
Figure imgf000013_0002
PCT/RU1993/000148 1992-07-31 1993-06-18 Stepanov's aerohydrodynamic engine WO1994003725A1 (en)

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RU5057380 1992-07-31
SU925057380A RU2044157C1 (en) 1992-07-31 1992-07-31 Aerohydrodynamic windmill

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2161650A1 (en) * 2000-05-30 2001-12-01 Molina Primitivo Oliver System for making use of wind energy.
EP1674722A1 (en) * 2004-12-22 2006-06-28 Jean Rutten Floating power generator
CN100334346C (en) * 2005-06-10 2007-08-29 郑衍杲 Automatic control wind sail type swing wing vertical shaft wind motor
EP2102493A1 (en) * 2006-12-04 2009-09-23 Design Licensing International Pty Ltd A wind turbine apparatus
FR2930301A1 (en) * 2008-04-18 2009-10-23 Aurore Lembert Vertical axis wind turbine, has plates located near ends of rotary vertical central axis, where each plate supports blade rotating around three vertical axes to adopt feathering position during counter-productive part of rotation of blade
US8419346B2 (en) 2008-05-07 2013-04-16 Design Licensing International Pty Ltd Wind turbine
ES2421521A1 (en) * 2012-03-01 2013-09-03 Crespo Pablo Leal Hydrogenerator (Machine-translation by Google Translate, not legally binding)
AU2011213447B2 (en) * 2010-02-05 2014-09-18 Shandong Zhongtai New Energy Group Co., Ltd Wind power generating device and wind blade structure

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CN103216386A (en) * 2012-01-18 2013-07-24 鸿金达能源科技股份有限公司 Wind power generation device
RU2664639C2 (en) * 2016-03-09 2018-08-21 Владислав Александрович Гуревич Method for converting the kinetic energy of a air flow to a rotary movement of a blade
RU185639U1 (en) * 2018-02-16 2018-12-13 Ачикасов Ростислав Романович Channel hydraulic unit Achikasova

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4435124A (en) * 1980-08-20 1984-03-06 Nianbilla Company Limited Vertical axis windmill
US4452568A (en) * 1981-05-15 1984-06-05 Saab-Scania Aktiebolag Means for limiting rotation speed of a vertical shaft wind turbine
DE3505460A1 (en) * 1985-02-16 1986-08-21 Udo 8584 Kemnath Schwab Wind turbine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4435124A (en) * 1980-08-20 1984-03-06 Nianbilla Company Limited Vertical axis windmill
US4452568A (en) * 1981-05-15 1984-06-05 Saab-Scania Aktiebolag Means for limiting rotation speed of a vertical shaft wind turbine
DE3505460A1 (en) * 1985-02-16 1986-08-21 Udo 8584 Kemnath Schwab Wind turbine

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2161650A1 (en) * 2000-05-30 2001-12-01 Molina Primitivo Oliver System for making use of wind energy.
EP1674722A1 (en) * 2004-12-22 2006-06-28 Jean Rutten Floating power generator
CN100334346C (en) * 2005-06-10 2007-08-29 郑衍杲 Automatic control wind sail type swing wing vertical shaft wind motor
EP2102493A1 (en) * 2006-12-04 2009-09-23 Design Licensing International Pty Ltd A wind turbine apparatus
EP2102493A4 (en) * 2006-12-04 2010-10-20 Design Licensing Internat Pty A wind turbine apparatus
US9303622B2 (en) 2006-12-04 2016-04-05 Design Licensing International Pty Ltd Wind turbine apparatus
FR2930301A1 (en) * 2008-04-18 2009-10-23 Aurore Lembert Vertical axis wind turbine, has plates located near ends of rotary vertical central axis, where each plate supports blade rotating around three vertical axes to adopt feathering position during counter-productive part of rotation of blade
US8419346B2 (en) 2008-05-07 2013-04-16 Design Licensing International Pty Ltd Wind turbine
AU2011213447B2 (en) * 2010-02-05 2014-09-18 Shandong Zhongtai New Energy Group Co., Ltd Wind power generating device and wind blade structure
US8847423B2 (en) 2010-02-05 2014-09-30 Shandong Zhongtai New Energy Group Co., Ltd Wind power generating apparatus and wind blade structure
ES2421521A1 (en) * 2012-03-01 2013-09-03 Crespo Pablo Leal Hydrogenerator (Machine-translation by Google Translate, not legally binding)

Also Published As

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RU2044157C1 (en) 1995-09-20

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