WO2006068529A1 - Rotor relativiste de grande capacite - Google Patents

Rotor relativiste de grande capacite Download PDF

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Publication number
WO2006068529A1
WO2006068529A1 PCT/RO2005/000017 RO2005000017W WO2006068529A1 WO 2006068529 A1 WO2006068529 A1 WO 2006068529A1 RO 2005000017 W RO2005000017 W RO 2005000017W WO 2006068529 A1 WO2006068529 A1 WO 2006068529A1
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WO
WIPO (PCT)
Prior art keywords
rotor
alveoli
spherical
radius
walls
Prior art date
Application number
PCT/RO2005/000017
Other languages
English (en)
Inventor
Dumitru Panu-Misailescu
Original Assignee
Dumitru Panu-Misailescu
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 Dumitru Panu-Misailescu filed Critical Dumitru Panu-Misailescu
Priority to AT0953705A priority Critical patent/AT505467A2/de
Priority to DE112005003702T priority patent/DE112005003702T5/de
Priority to AU2005319820A priority patent/AU2005319820A1/en
Publication of WO2006068529A1 publication Critical patent/WO2006068529A1/fr
Priority to IL191708A priority patent/IL191708A0/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • 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
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B1/00—Engines of impulse type, i.e. turbines with jets of high-velocity liquid impinging on blades or like rotors, e.g. Pelton wheels; Parts or details peculiar thereto
    • F03B1/02—Buckets; Bucket-carrying rotors
    • 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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D1/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D1/02—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/18—Rotors
    • 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
    • F05B2250/00—Geometry
    • F05B2250/20—Geometry three-dimensional
    • F05B2250/24—Geometry three-dimensional ellipsoidal
    • F05B2250/241—Geometry three-dimensional ellipsoidal spherical
    • 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
    • Y02E10/20—Hydro energy
    • 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
    • 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
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50—Manufacturing or production processes characterised by the final manufactured product

Definitions

  • the invention refers to a new type of high capacity relativist rotor (H.C.R.R.) characterized by a successive asymmetrical positioning of closed or opened alveoli which make up the pallets assembly.
  • H.C.R.R. high capacity relativist rotor
  • the alveoli make up the rotor pallets assembly with closed outline while when opened they make up the rotor pallets assembly with open outline.
  • Each closed alveolus is made up of three spherical surface walls while the opened alveoli are made up each of two spherical walls.
  • the consecutive alveoli are asymmetrically disposed one relative to the other, the former leftwards while the latter rightwards by such a manner that all pairs of adjacent alveoli present one common wall, so that between the consecutive alveoli no empty room is provided.
  • the high capacity relativist rotor eliminates the disadvantages known in the present by that that it presents a simple, perfectly balanced construction which provides for uniform charging on both sides of median rotor plane which is simultaneously distributed on all spherical alveoli of pallets assembly.
  • the axial stresses compensate one another by the symmetrical left-right alveoli alternation and the radial- axial disposition of the alveoli common walls, while the compensation of radial stress is accomplished by the uniformly distributed rotational field during one complete rotation, such field being instantaneously created by the working fluid which come out from special injectors in order to hit the alveoli walls which make up the rotor pallets assembly whose outline can be open or closed.
  • the open outline rotor pallets assembly can be obtained from the closed outline rotor pallets assembly by removing its side spherical walls, thus resulting a rotor of continuous pallets assembly which is radial-axial oriented and only made up of the common spherical walls of the closed outline rotor pallets assembly.
  • Each alveolus in the closed or open outline rotor pallets assembly presents one common wall with the adjacent alveolus, thus making up together a configuration successively disposed around an axis that covers the angle of 360°.
  • the common wall of the alveoli plays also the function of synchronous divider-distributor, thus providing for the simultaneous feeding with working fluid of two adjacent alveoli, although asymmetrically positioned one relative to the other.
  • the honeycomb represents a natural model of filling a planar space at its maximum capacity, and is characterized by the edge of a hexagon inscribable in a circle.
  • the rotor pallets assembly of H.C.R.R. represents the ideal model of filling at maximum capacity of a curved space uniformly distributed around a rotational axis and characterized by the spherical radius of the curved space.
  • H.C.R.R. can also be used in energetic domain. It can be used as active driving part for generators or motors, no matter what working fluid is used, and can work free or in a case.
  • the shape of stator surface is the conjugate of that of the rotor, the latter conditioning the former.
  • H.C.R.R. device can work by itself or when driven.
  • Another special version of implementation of a H.C.R.R. is that one used in recovery of eolian energy. I herein insist upon three examples of implementation of H.C.R.R. devices which, according to their final form, can be perfectly inscribed in a sphere of radius R and wherein all the spherical surface walls which make up the alveoli present the same spherical radius of curvature R which is equal to the radius R of the sphere where the closed or open outline rotor pallets assembly can be inscribed in.
  • the edges of the alveoli spherical walls that make up the open or closed rotor pallets assembly are situated on the sphere of radius R.
  • An example of implementation describes a six-alveolus H. CR. R., another example an eight-alveolus H.C.R.R. and the third one a six, respectively eight-alveolus H.C.R.R. driven by micro- rotors.
  • four groups can be made out: I) Open or closed rotor with symmetrical alveoli made up of spherical walls of different spherical radii II) Open or closed rotor with symmetrical alveoli made up of spherical walls of different spherical radii III) Open or closed rotor with asymmetrical alveoli made up of spherical walls of the same radius IV) Open or closed rotor with asymmetrical alveoli made up of spherical walls with different spherical radii.
  • the optimal thickness of a special injector slit equals the thickness of the common wall, while the maximal width of a special injector slit equals the height of the equilateral triangle obtained when connecting the vertices whereat the spherical walls of radius R belonging to a symmetrical alveolus meet together.
  • each alveolus of the H.C.R.R. rotor pallets assembly (that one made up of six consecutive alveoli) is continuously and simultaneously attacked, thus providing for a high capacity of transportation, recovery, transfer and transforming of working fluid energy directly into mechanical energy of rotation.
  • the rotor permanently works at maximal parameters with instantaneous turning on and off, no matter what its relative position is.
  • a H.C.R.R. is noise-free during its work, as it works symmetrically and provides for a constant, perfectly balanced couple, the asymmetric alternation of pallets assembly alveoli contributing decisively to the attainment of such performances.
  • H.C.R.R. can also be driven to work by the liquids that flow under gravitation, not only by fluids under pressure. It works at superior output as compared to the present known rotors that work under the action of the same types of fluids.
  • H.C.R.R. using liquids that flow under gravitation works like a very precise volume counter that can be easily filled-up and emptied.
  • Fig.1 Natural isometric view of a H.C.R.R. wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius.
  • FIG.2 Front view of a H.C.R.R. wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius.
  • Fig.3 Axial section view of a H.C.R.R. wherein the pallets assembly is made up of six alveoli.
  • FIG.4 Side view of a H.C.R.R. wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius.
  • FIG.5 Cross section view of a H.C.R.R. wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius.
  • FIG.7 Assembly natural isometric view of a H.C.R.R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius, driven by two micro-rotors.
  • Fig.8) Exploded assembly natural isometric view of a H. CR. R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius, driven by two micro-rotors.
  • FIG.9 Exploded assembly isometric view of a H.C.R.R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius, driven by two micro-rotors.
  • Fig.10 Singular front view of a driven H.C.R.R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • Fig.11 Axial section view of a driven H.C.R.R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • FIG.12 Side view of a driven H.C.R.R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • FIG.13 Cross section view of a driven H.C.R.R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • FIG.14 Front view of a micro-rotor that can drive a H.C.R.R. wherein the pallets assembly is made up of spherical walls of same radius.
  • Fig.15 Front view of a micro-rotor that can drive a H.C.R.R. wherein the pallets assembly is made up of spherical walls of same radius.
  • Fig.16 Isometric view of a micro-rotor that can drive a H.C.R.R. wherein the pallets assembly is made up of spherical walls of same radius.
  • Fig.17 Side view of a micro-rotor that can drive a H.C.R.R. wherein the pallets assembly is made up of spherical walls of same radius.
  • Fig.18 Rear view of a micro-rotor that can drive a H.C.R.R. wherein the pallets assembly is made up of spherical surfaces of same radius.
  • Fig.19 Assembly natural isometric view of a H.C.R.R driven by two micro-rotors, wherein the pallets assembly is made up of six symmetrical alveoli made up of spherical walls of same spherical radius.
  • Fig.20 Assembly isometric view of a cased H.C.R.R. wherein the pallets assembly is made up of six asymmetrical alveoli made up of spherical walls of same spherical radius.
  • Fig.21 Assembly isometric view of a half-cased H.C.R.R. wherein the pallets assembly is made up of six asymmetrical alveoli made up of spherical walls of same spherical radius.
  • Fig.22 Assembly natural isometric view of a half-case that houses a H. C. R. R.
  • Fig.23 Assembly natural isometric view of a half-cased H. C. R. R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • Fig.24 Assembly natural isometric view of a H. C. R. R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • Fig.25 Assembly natural isometric view of a driven half-cased H. C. R. R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • Fig.26 Assembly natural isometric view of a driven not-cased H.C.R.R. wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • Fig.28 Assembly natural isometric view of a driven H.C.R.R. which can work as hydraulic turbine, wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • Fig.29 Natural top view of an assembly of a driven H.C.R.R. which can work as hydraulic turbine, wherein the pallets assembly is made up of eight asymmetrical alveoli made up of walls of same spherical radius.
  • Fig.30 Transparent natural isometric view of a ultra-light, dismountable H.C.R.R., wherein the pallets assembly is made up of six asymmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.31 Natural isometric view of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.32 Bottom view of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.33 Front view of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.34 Top view of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.35 Cross section view of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.36 Side view of a ultra-light dismountable H. CR. R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.37 Isometric view of resistance structure of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.38 Bottom view of resistance structure of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.39 Front view of resistance structure of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.40 Top view of resistance structure of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • FIG.41 Cross section view of resistance structure of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.42 Side view of resistance structure of a ultra-light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.43 Natural isometric view of a light dismountable H.C.R.R., wherein the pallets assembly is made up of six symmetrical alveoli made up of walls of same spherical radius, devised for recovery of eolian energy.
  • Fig.44 Natural isometric view of a light dismountable H.C.R.R., wherein the pallets assembly is made up of six alveoli, devised for recovery of eolian energy, and which is perfectly inscribable into an overall structure of regular octahedron in order to ease its component parts assembling.
  • FIG.45 Front view of a H.C.R.R. with an open outline rotor pallets assembly, which is made up of six symmetrical alveoli made up of walls of same spherical radius.
  • FIG.46 Side view of a H.C.R.R. with an open outline rotor pallets assembly, which is made up of six symmetrical alveoli made up of walls of same spherical radius.
  • FIG.47 Front view of a H.C.R.R. with an open outline rotor pallets assembly, which is made up of six asymmetrical alveoli made up of spherical walls of same spherical radius.
  • FIG.48 Side view of a H.C.R.R. with an open outline rotor pallets assembly, which is made up of six asymmetrical alveoli made up of spherical walls of same spherical radius.
  • Figs 1 to 48 by numbers and letters there have been denoted the following: 1 -rotor with six alveoli and closed outline (made up of symmetrical alveoli of same radius); 1 ' - rotor with open outline and convex core (made up of six symmetrical alveoli of same radius); 1 " - rotor with open outline and concave core (made up of six asymmetrical alveoli of same radius); 2 - rotor with eight alveoli with closed outline at pallets assembly; 3 - micro-rotor with pallets made up of spherical surfaces of same radius; 4 - simple half-case; 5 - special injector; 6- elastic sleeve; 7 - servomotor; 8 - simple window; 9 - main channel; 14 - elastic element; 15 -joint hobnail; 16 - centring part; 17 - ultra-light thin cover; 18 - central elastic balloon; 19 - grate; 20 - lamellar spherical profile
  • High capacity relativist rotor (H.C.R.R.) according to the invention, as there results from the text and the drawings shown in Figs.1 to 48, namely: a rotor 1 (with six alveoli and closed outline made up of symmetrical alveoli of same radius); a rotor 1 ' (rotor with open outline and convex core, made up of six symmetrical alveoli of same radius) or a rotor 2 (with eight asymmetrical alveoli of same radius, with closed outline at pallets assembly).
  • the pallets assembly of rotor 1 is made up of six symmetrical alveoli, each thereof being made up of spherical walls of same radius R, two successive alveoli presenting a common wall.
  • the open outline rotor pallets assembly 1 ' is obtained out of the closed outline rotor pallets assembly 1 by removing the side spherical walls thereof, thus resulting a radial-axial continuous pallets assembly which is only made up of common spherical walls of the closed outline rotor pallets assembly which meet together at the central area on a convex core of radius R.
  • the pallets assembly of rotor 1 " is obtained out of a closed outline rotor whose pallets assembly is made up of asymmetrical alveoli of spherical walls of same radius, by removing the side spherical walls thereof, thus resulting a radial-axial oriented continuous pallets assembly rotor which is only made up of the common walls of the closed outline rotor pallets assembly which meet together on the central area on a concave core of radius R. All the alveoli that make up the pallets assembly of rotors 1 , 1 ' , 1 " and 2 present a common wall to the adjacent alveolus and make up together a configuration disposed successively around one axis and covering 360°.
  • the spherical walls of alveoli making up the pallets assembly of rotor 1 and 1 ' meet together at the central area to make up a regular body, namely a cube with convex outer faces curved by a radius R whose diagonal axis is coincident to the axis of rotation of rotor 1 or 1 ' .
  • the spherical walls of alveoli which make up the pallets assembly of rotor 1 " meet together at the central area to make up a regular body, namely a cube with concave outer faces curved by a radius R and whose diagonal axis is coincident to the axis of rotation of rotor 1".
  • the rotor 2 presents a pallets assembly made up of eight asymmetrical alveoli, each thereof being composed of spherical walls of same spherical radius R.
  • the successive alveoli also present one common wall.
  • the radius of curvature R of the spherical walls is in both cases coincident to the radius R of the spherical space described by the spherical wall edges of the alveoli when in rotational movement.
  • Rotors 1 and 2 can also be driven by two micro-rotors 3 (with pallets assembly made up of spherical surfaces of same radius), a micro-rotor thereof being the mirrored replicate of the other.
  • the functional assembly described herein being a dismountable assembly which can be also executed as non-dismountable; the micro-rotors 3 playing also the role of start and uniform the repartition of a force field that appears in the curved space W 2
  • a micro-rotor 3 being actually made up of three alveoli with spherical walls of same radius R a wall thereof being common to all the three alveoli and being situated on rotor 1 or 2, so that it is identifiable by the concave surface whereat the micro-rotor 3 lays on rotor 1 or 2.
  • Rotors 1, 1 ' , 1 " and 2 can also work as cased, housed into the simple half-cases 4, a simple case 4 being the mirrored replicate of the other, wherein by means of special injectors 5 (equidistantly positioned on the transversal plane passing through the rotor centre) the working fluid is brought towards the alveoli of rotor 1 , 1 ' , 1 " or 2. Between the simple half-case 4 and the special injectors 5 there is placed an elastic sleeve 6 provided for seal. The change of position of special injectors 5 relative to pallets assembly of rotors 1, 1 ' , 1 " and 2 is achieved by servomotors 7.
  • the working fluid after it finished its work in the alveoli, can be evacuated through the simple windows 8, the energy thereof being taken up from the axis of rotors 1, 1 ' , 1 " and 2.
  • the simple half- case 4 is provided at the interior with three main equidistant channels 9 which are to prevent permanent contact between a point belonging to the edges of alveoli walls and the interior spherical surface of the simple half-case 4 during one complete rotation, thus preventing the seizing and performing the de-straining of rotors 1, 1 ' , 1 " and 2.
  • the rotors 1 and 2 can work closed into double half-cases 10 wherein the working fluid is brought through pilot injectors 11 towards micro-rotors 3, and after it worked into the alveoli of micro-rotors 3 and rotors 1 and 2 it is evacuated through the double windows 12.
  • the special injectors 5 and the pilot injectors 11 create a uniform rotational field perfectly distributed along one complete rotation, thus ensuring for rotor 1 the highest grade of filling.
  • the optimal thickness for the slit of a special injector 5 equals the thickness of the common wall between two consecutive alveoli, and the maximal width of a slit of a special injector equals the height of the equilateral triangle described by the vertices wherein the spherical walls of radius R of a symmetrical alveolus meet together.
  • three special injectors 5 we can simultaneously attack all the six symmetrical alveoli of a rotor 1, 1 ' and 1 " .
  • the maximal filling degree is similar to that of the honeycomb, with the difference that the alveoli of rotor 1, 1 ' and 1 " are not hexagonal and not situated in the same plane one adjacent to the other, but in a radial left-right alternant disposition one adjacent to the other in reference to the axis of rotation and the transversal plane passing through the rotor centre.
  • All the alveoli that make up the pallets assembly of rotors 1, 1 ' and 1 " being defined by one common constant parameter, namely the spherical radius R and each thereof also presenting one common wall; H.C.R.R. being cased with simple half-cases 4 and double half-cases 10 when the rotors 1, 1 ' , 1 " and 2 are driven by auxiliary motors, and the special injector 5 and the sleeve 6 are replaced by several coupling pipes; the rotor works as a high capacity pump whose input-output parameters can be controlled by means of servomotors 7, when these drive a known system for opening and closing the working fluid circulation through coupling pipes.
  • the double half-case 10 present two separated areas, one thereof being a spherical area of radius R which houses half of the rotor 1 or 2, while the other area is different to the first by its ovoid shape devised to house the micro-rotor 3.
  • This area that houses the micro-rotor 3 is provided with three secondary channels 13 which play the same role as the main channels 9 with the difference that the former serve for the micro-rotor 3.
  • the rotors 1, 1 ' and 1 " can also be executed as dismountable, that version of implementation being used in case of high overall dimension; for example, when used for obtaining high power from recovery and transforming of eolian, hydro or thermo energy.
  • a rotor 1 or 1 ' devised for eolian energy recovery is made up of elastic elements 14 assembled together and dismountable by means of six joint hobnails 15 and two centring parts 16.
  • the elastic elements 14 also constitute the resistance structure for a thin cover 17 and are spatially oriented by means of the six joint hobnails so that, once the thin cover 17 is mounted upon the elastic elements 14, an equilibrated rotor 1 or 1 ' is achieved that instantaneously starts its rotational movement in presence of wind.
  • the joint hobnails 15 and centring parts 16 are provided with known systems of preventing against accidental freed of elastic elements 14 from the joint hobnails 15.
  • Each joint hobnail 15 is positioned in a joint knot coincident to the intersection points of alveoli of rotor 1 and marked with: A, B, C, A ' , B ' , C which, when connected with straight lines, describe a regular octahedron of vertices ABCA ⁇ ' C * .
  • an elastic central balloon 18 (of convex central core) is situated which, when filled up with air, fills the space wherein it is placed and takes the shape of a cube with convex faces of radius R whereupon the six alveoli making up rotor 1 or 1 'meet together at its interior.
  • This elastic central balloon 18 when filled up with air becomes the foreshadowing embryo of the spherical walls of radius R.
  • the sleeve When the wind blows upon the unfolded sleeve 14 which is supported by the elastic elements 14, the sleeve regains its original shape, namely that of rotor 1 or 1 ' .
  • a dismountable rotor 1 or 1 ' can be equipped with a known system in order to provide for the automatic adjustment of input and output load parameters. The adjustment is achieved by automatic control of filling or evacuating of air volume in the elastic central balloon 18, resulting in an increase or decrease of its volume that acts upon the total or partial obturation of grates 19.
  • the grates 19 are symmetrically disposed and present a spherical curvature of radius R, being positioned on the same position with the faces of the elastic central balloon 18.
  • the pressure differences between the alveoli increase and the rotor 1 or 1 ' starts its rotational movement, the maximal power of rotor 1 or 1 ' being obtained when the elastic central balloon 18 is filled up with air, and at that very moment it completely obturates the grate 19 and the wind cannot freely pass through the rotor.
  • the elastic central balloon 18 works as a rapid pneumatically driven valve that connects simultaneously all the six symmetrical alveoli of rotor 1 or 1 ' .
  • the elastic central balloon 18 works as a rapid pneumatically driven valve that connects simultaneously all the six symmetrical alveoli of rotor 1 or 1 ' .
  • the spherical pre-formation of other areas belonging to the thin sleeve 17 is achieved, different to the central areas that are preformed by the elastic central balloon 18.
  • a octahedral frame 21 that, after the correct assembling in functional position of rotor parts is achieved, can also be easily dismounted.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Hydraulic Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pallets (AREA)
  • Wind Motors (AREA)
  • Feeding Of Workpieces (AREA)

Abstract

La présente invention concerne un nouveau type de rotor (2), caractérisé par un positionnement successif asymétrique de plusieurs alvéoles fermées ou ouvertes qui composent un ensemble de clapets avec une apparence fermée ou ouverte, chacun desdits clapets ayant une paroi commune avec l’alvéole adjacente, remplissant ainsi sa fonction de diviseur synchrone qui prévoit une alimentation simultanée de fluide de travail à travers des injecteurs spéciaux de deux alvéoles consécutives, bien qu’ils soient positionnés de manière asymétrique, c’est-à-dire l’un sur la gauche et l’autre sur le côté droit du plan transversal passant à travers le centre du rotor, produisant ainsi une grande capacité de transport, de récupération, de transfert et de transformation directe de l’énergie du fluide de travail en énergie mécanique de rotation, le rotor étant utilisé dans le domaine énergétique en tant que principale pièce mobile active de générateurs de moteurs, peu importe le fluide de travail utilisé.
PCT/RO2005/000017 2004-12-22 2005-11-25 Rotor relativiste de grande capacite WO2006068529A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AT0953705A AT505467A2 (de) 2004-12-22 2005-11-25 Hochkapazitätsrelativistrotor
DE112005003702T DE112005003702T5 (de) 2004-12-22 2005-11-25 Hochkapazitätsrelativistrotor
AU2005319820A AU2005319820A1 (en) 2004-12-22 2005-11-25 High capacity relativist rotor
IL191708A IL191708A0 (en) 2004-12-22 2008-05-26 High capacity relativist rotor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ROA200401143A RO122501B1 (ro) 2004-12-22 2004-12-22 Rotor cu configuraţie optimă
ROA200401143 2004-12-22

Publications (1)

Publication Number Publication Date
WO2006068529A1 true WO2006068529A1 (fr) 2006-06-29

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RO2005/000017 WO2006068529A1 (fr) 2004-12-22 2005-11-25 Rotor relativiste de grande capacite

Country Status (7)

Country Link
AT (1) AT505467A2 (fr)
AU (1) AU2005319820A1 (fr)
DE (1) DE112005003702T5 (fr)
DK (1) DK200800417A (fr)
IL (1) IL191708A0 (fr)
RO (1) RO122501B1 (fr)
WO (1) WO2006068529A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007113399A2 (fr) * 2006-04-05 2007-10-11 Pierre Moreau Eolienne spherique a canaux dotee d'un deflecteur central mobile
WO2009150039A2 (fr) * 2008-05-27 2009-12-17 Syneola Sa Eolienne multipale sensiblement sphérique
WO2013158501A1 (fr) 2012-04-18 2013-10-24 4Sphere Llc Ensemble turbine
WO2014124717A1 (fr) * 2013-02-18 2014-08-21 Wwt Rotorenbau Gmbh Rotor d'éolienne
CN105298850A (zh) * 2015-10-10 2016-02-03 黄敬易 向心轴流管

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1039946C2 (nl) * 2012-05-11 2013-11-20 Briemen Diverse aandrijvingen en uitvoeringen van de hexa-tetrahedron propeller.

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB216428A (en) * 1923-10-02 1924-05-29 Alois Heibl Improvements in rotary motors
GB856281A (en) * 1957-06-11 1960-12-14 Technica Ets Bucket wheel for inward flow turbines or for centrifugal pumps
FR1522468A (fr) * 1967-03-15 1968-04-26 Turbine à gaz à jet tangentiel
US3592558A (en) * 1969-12-10 1971-07-13 Robert G Bandy Pressure fluid operated motor
DE29712301U1 (de) * 1997-07-14 1997-09-04 Hielscher, Lutz, 42279 Wuppertal Turbine, insbesondere für Fahrzeugmodelle
EP0965753A1 (fr) * 1998-06-15 1999-12-22 Dinesh Patel Rotor entraíné par un fluide avec des pales sphériques
WO2000011322A1 (fr) * 1998-08-21 2000-03-02 OMASI, Anstalt Helice polyvalente a impulsions orientables
EP1201922A2 (fr) * 2000-10-31 2002-05-02 Behn, Hans-Joachim Turbine hydraulique
WO2002081906A2 (fr) * 2001-04-03 2002-10-17 Ernst Thannesberger Element profile pour parties constitutives aero- ou hydrodynamiques
WO2004070202A1 (fr) * 2003-02-07 2004-08-19 Dumitru Panu Misailescu Transformateur d'energie sphero-torique

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB216428A (en) * 1923-10-02 1924-05-29 Alois Heibl Improvements in rotary motors
GB856281A (en) * 1957-06-11 1960-12-14 Technica Ets Bucket wheel for inward flow turbines or for centrifugal pumps
FR1522468A (fr) * 1967-03-15 1968-04-26 Turbine à gaz à jet tangentiel
US3592558A (en) * 1969-12-10 1971-07-13 Robert G Bandy Pressure fluid operated motor
DE29712301U1 (de) * 1997-07-14 1997-09-04 Hielscher, Lutz, 42279 Wuppertal Turbine, insbesondere für Fahrzeugmodelle
EP0965753A1 (fr) * 1998-06-15 1999-12-22 Dinesh Patel Rotor entraíné par un fluide avec des pales sphériques
WO2000011322A1 (fr) * 1998-08-21 2000-03-02 OMASI, Anstalt Helice polyvalente a impulsions orientables
EP1201922A2 (fr) * 2000-10-31 2002-05-02 Behn, Hans-Joachim Turbine hydraulique
WO2002081906A2 (fr) * 2001-04-03 2002-10-17 Ernst Thannesberger Element profile pour parties constitutives aero- ou hydrodynamiques
WO2004070202A1 (fr) * 2003-02-07 2004-08-19 Dumitru Panu Misailescu Transformateur d'energie sphero-torique

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007113399A2 (fr) * 2006-04-05 2007-10-11 Pierre Moreau Eolienne spherique a canaux dotee d'un deflecteur central mobile
FR2899652A1 (fr) * 2006-04-05 2007-10-12 Pierre Moreau Eolienne spherique a canaux, inedite, grace a une ossature spherique et geodesique.
WO2007113399A3 (fr) * 2006-04-05 2008-03-06 Pierre Moreau Eolienne spherique a canaux dotee d'un deflecteur central mobile
WO2009150039A2 (fr) * 2008-05-27 2009-12-17 Syneola Sa Eolienne multipale sensiblement sphérique
WO2009150039A3 (fr) * 2008-05-27 2010-05-14 Syneola Sa Eolienne multipale sensiblement sphérique
WO2013158501A1 (fr) 2012-04-18 2013-10-24 4Sphere Llc Ensemble turbine
EP2839148A4 (fr) * 2012-04-18 2015-12-09 4Sphere Llc Ensemble turbine
WO2014124717A1 (fr) * 2013-02-18 2014-08-21 Wwt Rotorenbau Gmbh Rotor d'éolienne
CN105298850A (zh) * 2015-10-10 2016-02-03 黄敬易 向心轴流管

Also Published As

Publication number Publication date
DK200800417A (da) 2008-03-18
DE112005003702T5 (de) 2009-06-04
AU2005319820A1 (en) 2006-06-29
IL191708A0 (en) 2009-02-11
AT505467A2 (de) 2009-01-15
RO122501B1 (ro) 2009-07-30

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