WO1986001563A2 - Systeme d'entrainement du type a moteur a reaction pour centrales eoliennes - Google Patents

Systeme d'entrainement du type a moteur a reaction pour centrales eoliennes

Info

Publication number
WO1986001563A2
WO1986001563A2 PCT/DE1985/000287 DE8500287W WO8601563A2 WO 1986001563 A2 WO1986001563 A2 WO 1986001563A2 DE 8500287 W DE8500287 W DE 8500287W WO 8601563 A2 WO8601563 A2 WO 8601563A2
Authority
WO
WIPO (PCT)
Prior art keywords
wind
wind turbine
jet engine
propeller
drive
Prior art date
Application number
PCT/DE1985/000287
Other languages
German (de)
English (en)
Other versions
WO1986001563A3 (fr
Inventor
Ernst Jäckel
Original Assignee
Jaeckel Ernst
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 DE3430977A external-priority patent/DE3430977A1/de
Application filed by Jaeckel Ernst filed Critical Jaeckel Ernst
Publication of WO1986001563A2 publication Critical patent/WO1986001563A2/fr
Publication of WO1986001563A3 publication Critical patent/WO1986001563A3/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06—Rotors
    • F03D3/061—Rotors characterised by their aerodynamic shape, e.g. aerofoil profiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/21—Rotors for wind turbines
    • F05B2240/211—Rotors for wind turbines with vertical axis
    • F05B2240/215—Rotors for wind turbines with vertical axis of the panemone or "vehicle ventilator" type
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction

Definitions

  • the purpose of the invention is to make the experience more modern
  • Jet engines also benefit the wind power plants.
  • a jet engine intended for the acceleration of movable bodies generally works with an explosive maximum pressure in front of a punctiform nozzle with unlimited opportunity for expansion behind this compression.
  • a wind power plant aimed in this way only has a relative low pressure of the wind available. This must therefore be particularly compressed before a nozzle-like constriction.
  • the lack of maximum pressure in the wind power plant can also be compensated for by a large range of action of the jet engine, by not using one or more linear reflective masses, but area-like surfaces made of parallel lines that almost touch each other with compression before this narrowing and expansion opportunity behind this, a reflex drive acceleration of the wind turbine on the entire surface of the horizontal axis rotor or on the windward side of the vertical axis rotor also beyond the impact speed of the wind.
  • the surface jet engine for wind power plants therefore uses as a horizontal axis runner or as a vertical axis runner the entire wind attack surface with as many driving vanes as possible to interact with one another between wheel rims 7 by guiding the wind in such a way that all driving vanes 6 together with their own roll-shaped front beads 18 cause the wind to be compressed in front of nozzle-like constrictions between them, as they are formed by their overlap and linear approximation, flow through these nozzle-like constriction lines and behind them as reflective masses of a large, uniform jet engine acceleration of the wind turbine or the windward side of the wind cylinder on the whole Wind impact area of the wind power plant to expand.
  • the countless floating wings not only fill the entire one
  • Wind turbine surface or windward side wind cylinder surface they increase this attack surface of the wind again by about half by the fact that the propeller wing surfaces overlap one another by about half.
  • Horizontal axis rotor according to the invention corresponds to a wind wheel diameter of 16 meters, but the wind power on the entire rotor amounts to only a tenth of that on the entire horizontal axis rotor according to the invention, since the wind force is directly proportional to the pressure on the sum of the propeller wing areas and can never be stronger than that pressure - although the invention only makes better use of it.
  • the size of the constrictions between the propeller vanes is adapted to the respective wind speed, which is achieved by resilient mounting of the propeller vanes in the wind turbine, which corresponds to the wind cylinder in the vertical axis rotor.
  • the spokes 5 of the large wind wheel 3 are firmly connected between the inner carrier wheel 8 and the outer wheel rim 7 at a radius distance of approximately 2 meters with further wheel rims 7, which divide the spokes 5 into corresponding partial spokes, on which corresponding partial drive vanes correspond to the spoke distances accordingly, in a shape that widens from the inside to the outside on both sides, is rotatably supported in the wheel arches and each has a tension spring that counteracts the wind force, while the propulsion vanes of the vertical axis rotor are located vertically between two horizontal wheel arches, in which they rest on their top and bottom Axes 5 are rotatably mounted and each have a tension spring counteracting the wind power.
  • the retroreflective drive is secured against a sudden increase in the wind speed in such a way that sudden gusts of wind push the propeller vanes 6 against the tension of their tension springs 17 out of their normal position to the wind turbine surface in order to provide the wind with an increased outflow. until the wind acceleration of the wind wheel has brought about the same increased outflow and the tensioned tension springs pull the opened propulsion vanes back into the spring and propeller vane basic position of the retrospective constriction between the propelling vanes corresponding to the new wind speed as the wind acceleration changes to the increased wind speed.
  • the propulsion vanes 6, which use their tension springs 17 to determine the size of the reflector constrictions due to the strength and uniformity of their positions in relation to the wind turbine plane or for wind cylinder rounding within the wheel rims 7, are worked out at their ends to form bearing rollers 16 with which they can be rotated, but for all wind speeds are stably mounted and with which they give their tension springs a safe guidance between themselves and the wheel rims.
  • the type of feathering which allows the owl to fly silently, is also binding for the wing surfaces of the jet engine for wind turbines.
  • the wind presses the feathering towards the propeller blades as the least friction surface, as a stream of compressed air running in the direction of rotation or as a counter-current suction, on the other hand, it lifts the feathering from the surface and drives it behind grasping them, the propellers also in the direction of rotation.
  • the wind does not flow through the wind turbine, but instead gives its speed to the torque without gaps, so that it is then thrown sideways outwards by the centrifugal force of the wind turbine and forms an air screen in the extension of the wind turbine plane, which is why the wind vane 15 controlling the system in the wind must be attached high above the upper edge of the wind turbine behind the rotatable upper part of the wind power plant and why this rotatable upper part 2 of the system for collecting the high wind pressure can be rotated and deep in the bottom-fixed lower part 1 of the system a large massive axis of rotation must be stored, which extends deep down.
  • the jet engine does not work with isolated propeller blades or as a mere pressure control turbine, but as a unitary instrument of a spring-controlled intermeshing jet engine, which ultimately converts wind power into the torque that determines the output.
  • Such intensive work of the wind in the jet engine also requires its particularly stable construction.
  • Drawing 1 shows a front view of the surface jet engine wind power plant and drawing 2 shows a side view thereof.
  • the system consists of the lower part 1 firmly anchored in the ground and the rotatable upper part 2 with the wind turbine 3.
  • the tower of the lower part 1 has far reaching support feet, which are embedded deep in the ground or in the rocky ground. These feet carry a solid platform, in which a round rotatable plate for the upper part 2 of the system with the wind turbine 3 is embedded, and is secured in stable ball or plastic bearings by a massive, deeply extending axis of rotation against any tilting.
  • the platform of the lower part 1 of the system which is firmly anchored in the ground, is so high that it just protrudes above the treetops of the forest.
  • the tree tops with their inclination can deflect the wind upwards and let it hit the lower part of the wind turbine so that this lower part is not disadvantaged compared to the upper part of the wind turbine.
  • the forest should therefore remain under the platform of the lower part of the plant or be allowed to grow back.
  • a tour with a railing around the platform of the lower part serves as a lookout tower.
  • the tower of the upper part of the system which is constructed in a streamlined manner parallel to the axis of the wind turbine, rises above the rotatable base plate. In its massive uppermost part, the wind turbine axis is securely installed in ball or plastic bearings against any tilting.
  • the large high-performance dynamo machine 12 is firmly connected to the base plate of the upper part 2 of the system and counteracts top plasticity of the system at this point by being attached to the center of gravity of the entire system.
  • the magnet or armature windings of the dynamo are broken down so that individual parts of it automatically switch on or off with the increase or decrease in the number of revolutions corresponding to the strength of the wind and with such an automatic increase or decrease in the decrease in power to save the wind wheel from raging in the event of a storm or standing still during a lull.
  • the dynamo machine should therefore be designed so high in performance that it is not overloaded even with peak requirements of the highest wind speeds.
  • the wind turbine which is made as light as possible, compensates for the low pressure of the wind jet engine compared to an explosion pressure by making the wind area as large as possible by filling the entire wind turbine surface with as many propeller blades as possible, which are rotatably mounted on a corresponding number of spokes , the friction blades overlap each other by about half their width and circulate as much as possible due to the emission of as large an accelerated reflection mass.
  • the driving vanes which widen according to the spoke spacing towards the outer edge of the wind wheel, are mounted on the spokes with a thick, roller-like front bead 18, behind the front rounding of which the wind slides along into the nozzle-like narrowing of the surface between the driving vanes, in front of which it passes between this propeller wing surface and it increasingly constricting front curve of the next driving wing is compressed in order to radiate behind such narrowing accelerated against the direction of rotation.
  • the beads of the wind guide rollers 18 of the propeller blades are hollow and, with this hollow space, serve as a maintenance-free plastic bearing for the propeller blades on the spokes of the wind turbine as their axes.
  • the cavities are foamed and therefore noiseless.
  • the spokes of the large wind turbine are firmly connected between the inner support rim 8 and the outer wheel rim 7 at a radial distance of approximately 2 meters with further wheel rims 7, which divide the spokes into corresponding partial spokes on which corresponding partial propellers smooth-running are stored on both sides in the wheel rims 7.
  • Each of the wreaths is extended parallel to the wind turbine axis in the direction of the wind so that it prevents any alternative opportunity for the wind power which is intended to strike the wind turbine horizontally, so that it can be compressed in front of the nozzle-like constrictions between the propeller blades.
  • Drawing 3 shows, seen from the hub of the wind turbine, cross sections through the outer propeller vanes on the actual outer edge or through the inner propeller vanes on the actual inner edge in their main propeller and mainspring positions.
  • Drawing 4 shows a wind turbine section of two spokes with the inner support rim and three wheel rims, next to it six cutting patterns like drawing 3 between the inner support wheel and the outermost wheel rim in their various basic positions between them.
  • the drive effect of the wind speed in the adaptation to the circumferential travel speed of the center distances of the wind wheel grows rapidly from the pure thrust force on the innermost propeller part to the outward reflection, which accelerates the propeller wing to its fastest outer parts to an increasing extent.
  • Drawing 5 shows the drive vanes 6 mounted on both sides in the wheel rims 7 with bearing rollers 16, which give the tension springs 17 a guide.
  • a direct mechanical power take-off on the outer wheel rim of the wind turbine can be carried out in the simplest form into the working dimension of the force line cut in the dynamo machine and dissipate it as electrical power.
  • the outer wheel rim which is also intended to prevent the wind from flowing over the outer edge of the wind turbine, is wide and stable enough to directly drive the shaft of the generator, provided that the light metal construction of the wind turbine does not require the power take-off from the rear end of the wind turbine shaft by means of a gear 11.
  • the high force line cut of the high-performance dynamo machine 12 also ensures with its drive shaft when switched on with all windings that the wind turbine can be braked when there is no wind. This braking can be further increased in that on both sides of the dynamo drive shaft, a heavy brake block with a worm thread is raised from the platform of the lower part of the system and pressed against the outer wheel rim of the wind turbine.
  • the wind vane is equipped with a swivel joint that snaps in and out so that it can be brought down and secured to the platform of the lower part as a safeguard against sudden horizontal swiveling of the upper part of the system when the wind direction changes.
  • the high performance of the system is therefore characterized in that it covers the entire area through the design of the wind turbine surface It uses the wind that hits it, because the system does not let the wings circulate in braking vortices, but in air-diluted rooms without letting them run away from the wind. This is achieved in that, for example, compared to the Arthur wind turbine
  • the total wind turbine area according to the invention is compared in its power generation to be demanded by the generator with a Stephen wind power output table, which can be seen in the appendix on page 2 below.
  • the table contains the measured power in kilowatts for the wind speeds in m / s and the correspondingly observed revolutions of the wind turbine per minute.
  • the circumferential speed of the circumference of the wheel part that is used for the work of the wind power or for the electrical power is the corresponding wind speed itself.
  • the thrust of the wind is unable to overtake the orbital speed of the Arthur propeller.
  • the thrust of the wind on the Arthur wind turbine with a diameter of 12 m is only effective on an inner diameter of 2.73 m around the wheel axis.
  • 9.27 m of the outer part of the diameter cannot be overtaken by the thrust of the wind and therefore remains outside their working area.
  • the power of the jet engine calculated above is based solely on the full use of the area exposed to the wind. It is to be regarded as a minimum output, which must be taken into account when designing the dynamo. The factors of the circulation in the air-diluted space and the main drive at the cheapest lever arm have probably not been taken into account enough with the usage calculation of the entire wind turbine area alone.
  • the superiority of the reflex drive forces the gin calculation and recognition of a much higher performance, which outperforms all previous estimates.
  • the area jet engine for wind power plants provides the perfect opportunity to supply the entire Federal Republic with sufficient free electricity from the windy north of Germany and possibly also from Denmark.
  • the surface jet engine which provides an abundance of energy as a horizontal axis rotor, is also suitable for the vertical axis rotor which offers a smaller Y / attack surface. Only this can be said:
  • the effect of the wind is not always the same as that of the horizontal axis rotor, but changes intermittently during each revolution of the wind cylinder from a pressure that is followed by a reflective drive on the windward side to a suction that is followed by a thrust force on the leeward side.
  • the vertical axis rotor consists of a bottom-fixed lower part 1 with the generator 12 on its bottom and the rotatable upper part 2 with the wind cylinder 3 and a long axis 4, which extends deep down and drives the generator 12 via a gear 11.
  • Drawing 6 shows an elevation of the jet engine as a vertical axis rotor at the top and a section through the wind cylinder 3 below.
  • Drawing 7 shows the interaction of the drive blades for the retroreflective drives as they are adapted to the curvature of the wall of the wind cylinder 3.
  • Drawing 8 shows two propellers 6 as they are mounted above and below in the horizontal wheel rim 7 with bearing rollers 16, which give the tension springs 17 a guide.
  • the driving wings 6, which rotate easily on axes 5, are mounted between two horizontal wheel rims 7 with bearing rollers 16, which give the tension springs 17 a guide, and are adapted in their interaction to the reflective drives to the round wall of the wind cylinder 3, the Reflecting current is directed towards the interior.
  • the fact that the wind does not flow through the windward side of the wind cylinder, even in the case of the vertical axis rotor, but instead gives its speed completely to the torque, means that the leeward side of the wind cylinder remains without any counterforce.
  • the tension springs 17 are partially or entirely in their force directed inwards against the opening of the propulsion vanes by the centrifugal force directed from the inside outwards.
  • the wind pressure on the driving wings is strongest in the middle of the windward side. It builds up on the wing wall between its roller-like front beads 18 and slides sideways into the narrowing surface nozzles between the propeller vanes with a compression, which is increased by their counter-impact of the circulation with the circulation path speed, to act behind these surface nozzles as an accelerating return jet drive of the wind cylinder
  • the centrifugal force of the retroreflective flow from the circumferential surface nozzle and the lateral centrifugal force of the propellants themselves, in combination with the rectified force of the tension springs, are the equivalent counterweight to the pressure of the respective wind speed on the propellers to maintain the basic size of the nozzle-like constrictions between the propellers Correspondence with the wind speed and thus the strongest possible retro-beam.
  • the first wind action very quickly creates an opening pressure on the propulsion vanes and the nozzle-like constriction between them, until their normal position is supported by the expansion of the propulsion wing spring as a compression spring.
  • the opening of the nozzle-like constriction must now also be larger, so that the collision of the now highest congestion compression can flow away in front of it with its speed of circulation.
  • a tremendous backward blow pushes the previous counterflow of the backflow stream out of the propeller wing opening behind the wing nozzle and remains during the circulation of the wind cylinder on the windward side as a new jet drive with a new backflow stream on the inside of the propeller wing until it suddenly comes up again as it approaches the leeward side tears off.
  • the surface jet engine for Widkraftwerke as a vertical axis rotor by means of its design and Ferder control of the propulsion wing, intermittently supplements the restriction of the compression retroreflective drive on the windward side with a vacuum suction thrust relief in the same direction of rotation on the leeward side.
  • Steel eyes attached to the outer edge of the lower wheel rim can be used to attach air swings for the use of the vertical axis rotor as a children's carousel.
  • the jet engine for wind turbines enables the self-generation of the energy required worldwide and thus creates all the conditions for overcoming the nuclear energy that is harmful to life and ultimately eradicated.
  • the jet-engine type drive system for wind-mills solves the problem of the compression of the wind in front of a nozzle-type throat for a return action drive and also balances out the lack of a very high pressure by a large-surface operating ranks of as many drive fins as possible, which overlap one another and form, with their surfaces, linearly-shaped throats between one another for a broad-sur-faced nozzle-type reaction drive.
  • the reaction drive solves the technical problem of stability, the drop in eddying in the air, the deployment of force on the longest lever arm despite the wind-speed, better rotation speed and the coping with very high wind-speeds without any significant danger of breakage or frictional loss.
  • the pressure of a very high wind-speed is converted by adjustment into a multiplied flow with a higher rotation and is taken up by a flexible electrical force pick-up.
  • the calculation of the Performance of the installation consequently shows its great superiority and its ability to replace the present-day production of energy by har ful atomic power stations.
  • the same installation as a vertical-axis rotary system, completes the reaction drive of the wi side with a discharging counter-flow pushing-type drive on the sheltered side.
  • the area jet engine for wind power plants solves the problem of compressing the wind in front of a nozzle-like area constriction for a retro jet engine and additionally compensates for the lack of maximum pressure through a large-area effect width of as many wings as possible, which overlap and with their areas line-like constrictions between them for a wide-area nozzle-like reflex drive.
  • the retroreflective drive solves the technical problems of stability, the loss of vortex loss in the air, the power delivery on the longest lever arm despite the circulation speed superior to the wind speed and the interception of the highest wind speeds without any significant risk of breakage or friction losses.
  • the attack of the highest wind speeds is smoothly converted into an increased outflow with increased circulation and is absorbed by an elastic electrical power take-off.

Abstract

Le système d'entraînement du type à moteur à réaction pour des centrales éoliennes résout le problème de la compression du vent au devant d'un étranglement du type tuyère pour un entraînement à action de retour et compense l'absence d'une très haute pression par une plage de fonctionnement de grande surface par l'utilisation d'un nombre aussi grand que possible d'ailettes d'entraînement lesquelles, en se chevauchant, forment avec leur surface des étranglements ou gorges de forme linéaire pour un entraînement à réaction du type à tuyère de grande surface. En outre, le système d'entraînement à réaction résout le problème technique de stabilité, de chute due aux tourbillons d'air, du déploiement d'une force sur le bras de levier le plus long en dépit de la vitesse du vent, améliore la vitesse de rotation, et supporte des vents de vitesses élevées sans risque significatif de cassure ou de perte par frottement. La pression d'un vent de très haute vitesse est convertie par ajustement en un écoulement multiplié avec une rotation supérieure et est reprise par une prise de force électrique flexible. Le calcul du rendement de l'installation montre en conséquence sa grande supériorité et sa capacité à remplacer les systèmes actuels de production d'énergie utilisant des centrales d'énergie atomique de caractère dangereux et nuisible. La même installation qu'un système rotatif à axe vertical complète le système d'entraînement à réaction côté vent avec un entraînement du type de poussée d'un écoulement contraire de décharge côté abrité.
PCT/DE1985/000287 1984-08-23 1985-08-23 Systeme d'entrainement du type a moteur a reaction pour centrales eoliennes WO1986001563A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEP3430977.2 1984-08-23
DE3430977A DE3430977A1 (de) 1984-03-03 1984-08-23 Flaechen-strahltriebwerk fuer windkraftwerke

Publications (2)

Publication Number Publication Date
WO1986001563A2 true WO1986001563A2 (fr) 1986-03-13
WO1986001563A3 WO1986001563A3 (fr) 1986-05-22

Family

ID=6243688

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE1985/000287 WO1986001563A2 (fr) 1984-08-23 1985-08-23 Systeme d'entrainement du type a moteur a reaction pour centrales eoliennes

Country Status (2)

Country Link
EP (1) EP0191833A1 (fr)
WO (1) WO1986001563A2 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992003656A1 (fr) * 1990-08-16 1992-03-05 Lundquist, Mona Turbine hydraulique a elements flottants incorpores et a dispositifs d'intensification du sens du courant
WO2004076854A1 (fr) * 2003-02-26 2004-09-10 Francisco Javier Forte Ortega Aerogenerateur perfectionne pour applications de faible puissance
CN115202389A (zh) * 2022-06-27 2022-10-18 中国航天空气动力技术研究院 一种减弱大流量轨控喷流干扰力矩的控制方法
CN116183840A (zh) * 2023-05-04 2023-05-30 四川交通职业技术学院 一种智慧环保工程用环境监测系统

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE152387C (fr) *
FR1072478A (fr) * 1951-12-07 1954-09-13 Procédé et installation pour capter et emmagasiner de l'énergie à partir du vent
FR2298706A1 (fr) * 1975-01-22 1976-08-20 Sicard Charles Dispositif tournant actionne par un fluide en mouvement
DE2949057A1 (de) * 1979-12-06 1981-06-11 Heinz Dr.-Ing. 5207 Ruppichteroth Meyer zur Capellen Windrad fuer ein windkraftwerk, insbesondere ein kleinkraftwerk
DE3125372A1 (de) * 1980-10-23 1983-04-07 Peter 8360 Deggendorf Deckert Neuartige anlage mit spezial-stufen-elektro-generatoren fuer windkraftwerke

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE152387C (fr) *
FR1072478A (fr) * 1951-12-07 1954-09-13 Procédé et installation pour capter et emmagasiner de l'énergie à partir du vent
FR2298706A1 (fr) * 1975-01-22 1976-08-20 Sicard Charles Dispositif tournant actionne par un fluide en mouvement
DE2949057A1 (de) * 1979-12-06 1981-06-11 Heinz Dr.-Ing. 5207 Ruppichteroth Meyer zur Capellen Windrad fuer ein windkraftwerk, insbesondere ein kleinkraftwerk
DE3125372A1 (de) * 1980-10-23 1983-04-07 Peter 8360 Deggendorf Deckert Neuartige anlage mit spezial-stufen-elektro-generatoren fuer windkraftwerke

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992003656A1 (fr) * 1990-08-16 1992-03-05 Lundquist, Mona Turbine hydraulique a elements flottants incorpores et a dispositifs d'intensification du sens du courant
WO2004076854A1 (fr) * 2003-02-26 2004-09-10 Francisco Javier Forte Ortega Aerogenerateur perfectionne pour applications de faible puissance
CN115202389A (zh) * 2022-06-27 2022-10-18 中国航天空气动力技术研究院 一种减弱大流量轨控喷流干扰力矩的控制方法
CN116183840A (zh) * 2023-05-04 2023-05-30 四川交通职业技术学院 一种智慧环保工程用环境监测系统
CN116183840B (zh) * 2023-05-04 2023-06-30 四川交通职业技术学院 一种智慧环保工程用环境监测系统

Also Published As

Publication number Publication date
EP0191833A1 (fr) 1986-08-27
WO1986001563A3 (fr) 1986-05-22

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