WO2019185470A1 - Méthode pour la conception et la fabrication de turbines à cuillères à jet calibré - Google Patents
Méthode pour la conception et la fabrication de turbines à cuillères à jet calibré Download PDFInfo
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- WO2019185470A1 WO2019185470A1 PCT/EP2019/057216 EP2019057216W WO2019185470A1 WO 2019185470 A1 WO2019185470 A1 WO 2019185470A1 EP 2019057216 W EP2019057216 W EP 2019057216W WO 2019185470 A1 WO2019185470 A1 WO 2019185470A1
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- WIPO (PCT)
- Prior art keywords
- zone
- fluid
- turbine
- turbines
- tubes
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 22
- 239000012530 fluid Substances 0.000 claims abstract description 53
- 238000004519 manufacturing process Methods 0.000 claims abstract description 31
- 238000013461 design Methods 0.000 claims abstract description 20
- 239000000463 material Substances 0.000 claims abstract description 8
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- 230000005611 electricity Effects 0.000 claims description 4
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- 238000009987 spinning Methods 0.000 claims description 3
- 230000003042 antagnostic effect Effects 0.000 claims 1
- 238000010276 construction Methods 0.000 abstract description 3
- 230000007480 spreading Effects 0.000 abstract description 3
- 238000003892 spreading Methods 0.000 abstract description 3
- 239000000411 inducer Substances 0.000 abstract 1
- 239000000654 additive Substances 0.000 description 3
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- 101100233916 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) KAR5 gene Proteins 0.000 description 2
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- 241000283690 Bos taurus Species 0.000 description 1
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 210000003323 beak Anatomy 0.000 description 1
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- 125000006850 spacer group Chemical group 0.000 description 1
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Classifications
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- 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
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- 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
-
- 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
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
- F03D1/0641—Rotors characterised by their aerodynamic shape of the blades of the section profile of the blades, i.e. aerofoil profile
-
- 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
- F03D3/062—Rotors characterised by their construction elements
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
-
- 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
- F05B2220/00—Application
- F05B2220/30—Application in turbines
-
- 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
- F05B2230/00—Manufacture
- F05B2230/30—Manufacture with deposition of material
-
- 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
- F05B2240/24—Rotors for turbines
-
- 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
- F05B2240/24—Rotors for turbines
- F05B2240/241—Rotors for turbines of impulse type
- F05B2240/2411—Pelton type
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2113/00—Details relating to the application field
- G06F2113/06—Wind turbines or wind farms
-
- 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 present invention relates to a method for designing and manufacturing on demand calibrated jet spoon turbines.
- Turbines used to generate fluid-provided energy are essentially constructed from the kinetic energy provided by the impact of fluids on the surface of propeller blades of all sizes
- propellers have been used for a very long time to capture the energy of fluids, for example wind turbines are used with reasonable dimensions in desert countries to extract water from wells and in Europe to give water to drinkers. cows in the meadows or windmills to make flour.
- CARPYZ says the five parameters (publication WO2008 / 012425, patent application PCT / FR2007 / 001 1267), a new research has been pursued until now, during over 10 years, by CARPYZ SAS Engineering created in 2017.
- the so-called five parameters principle makes it possible to manufacture a double-sided blade in using simultaneously only five numerical values to choose from, namely numerical values respectively for 1) the leading edge, 2) the trailing edge, 3) the body, 4) the length, and 5) the camber.
- WO2014067823 (A1) describes a known method of this type using the arithmetic principle CARPYZ said parameters, applied to a turbine comprising at least two hollow 3D wheels nested one inside the other in which, d ' on the one hand, a fixed hollow wheel is open at the front at the inlet of the fluid at its largest diameter and consists of successive circular curved washers which each have their inner diameter which decreases going from the front towards the center and have their inner edge oriented forward and are intersected by preferably spirally wound blades which go from the front to the center and form with the washers channels oriented tangentially towards the periphery of the wheel and, on the other hand at least one rotating wheel which surrounds the fixed wheel consists of blades preferably spirally wound which go from the large diameter towards the center and are curved in of hollow buckets, one of whose beaks is oriented tangentially inside this wheel and these bucket blades are intersected with circular washers which go from the inside to the outside and divide the
- the industrial computer tool says the five parameters can easily generate on demand and at infinity, helical blades of very complex shapes and provides the computer files to build them. Those skilled in the art must provide all the numerical values necessary for the so-called "five parameters" principle for each element described independently. The skilled person has the skill to associate the elements with each other as described.
- An object of the invention is to provide a method for designing, constructing and manufacturing turbines with the CARPYZ calibrated jet spoon wheels, all of whose elements are fully digitized, and which are on demand adapted to all fluids, for all uses, and of all sizes.
- the method for the design and on-demand manufacture of calibrated jet spoon turbines of the invention is characterized by the fact that the skeletons of the turbines presented on the screen make it possible to design them and then to manufacture them in all dimensions, in all materials and in all quantities, and they are constructed using blades designed with the arithmetic principle called the five parameters.
- the skeleton of the turbine is represented on the screen by means of "virtual neutral fibers" which are thereafter covered with material, the turbines being contained over their entire length in a circular envelope which is in principle slightly curved, the diameter of which on the The length of this monoblock envelope is shown on drawing and divided into four zones cut by ephemeral virtual disks which each separate the zones according to the functions performed at these locations, the front edge of this envelope being very small. tapered or on-demand provided with a Br flange to allow connection to facilities.These four areas include:
- a first zone (1) of introduction of the fluid empty space or occupied by sills or inductors, of the corkscrew type, which possibly generate a pre-rotation of the fluid which enters a second zone (2), a pointed shield spreading the fluid stream from the center at the inlet, and the ruler spreading it away to the second zone (2), the second zone (2) where fluid is rotated, in channels which spiral out and which open at the rear of the second zone (2) by rotating the fluid ,
- a third zone (3) where is located the rotating wheel provided with calibrated jet spoons that capture the energy provided by the fluid jets exiting the second zone (2)
- a fourth zone (4) where is located a a casing fixed to the fixed casing of the turbine, placed after the rotating wheel, which contains channels which direct the fluid towards the outlet at the rear of the turbine, and
- the fluid is led as soon as it arrives in the second zone (2) by channels, contained in tubes which are put in continuity face to face, along the entire length of the turbine.
- the CARPYZ industrial computer tool makes it easy to generate on demand and infinitely, helical blades of very complex shapes and provides the computer files to build them.
- the "five-parameter arithmetic principle” is used. This feature refers to G industrial computer design and manufacturing computer tool, which was developed by the applicant of this application. However, this precise principle is universally accepted and defines a standard principle or procedure that is accepted internationally as a particular sequence of standard operations.
- This new invention shows how CARPYZ spinner turbines are constructed using known geometric and mathematical principles and laws, but which are associated and employed simultaneously or independently of complementary ways. Each principle, if it is perhaps already known individually, can not be considered as a sufficient opposition having left the global context, the elements of the monoblock wheel being all dependent on each other.
- CARPYZ says 5 parameters, that it is possible to design, build and manufacture turbines with calibrated jet wheels, all elements of which are fully digitized, and which are on demand adapted to all fluids, for all uses
- the device is remarkable in that the skeletons of the turbines presented on the screen make it possible to design them and then to manufacture them in all dimensions, in all materials and in all quantities, and they are built to the using blades designed with the CARPYZ arithmetic principle of parameters (see publication WO2008 / 012425, PCT / FR2007 / 0011267).
- the edges of the tubes at the inlet of the second zone (2) and at the outlet of the tubes of the fourth zone (4) are very slender, and in that the edges of the spoons of the third zone (3) are very slender, the edges of the tubes of the spoon wheel and those of the tubes which surround it, having the same diameter, being flat and rotating opposite each other.
- the channels are constructed in fixed circular tubes of different diameter, which are contained in each other, and which start from the front of the second zone (2) with tapered edges (3, FIG 4) and whose diameters are evolutive, these tubes being pursued face to face in concordance with identical tubes contained in a rotary box which contains the spoons, these rotary tubes being again pursued face to face in concordance with the fixed tubes contained in the box fixed to the fixed sleeve of the turbine in the fourth zone (4).
- the wheel of the third zone (3) which rotates is constructed with spoons which are placed in the wheel between its tubes, the spoons being portions of open circles mouth open, oriented for their feeding according to the direction of rotation decided by the designer, the spoons being modifiable by changing the values of the width of the wheel, their inclination and their depth, the results obtained changing with the diameter of the wheel and with the number of spoons which are determined by the designer.
- a virtual straight line is drawn between the two edges of the spoon and on this line is pointed in the middle a center, and in that, referring to this center are placed with a differential X, X, a , according to the will of the designer, the centers of portions of circle which position the opposing bosses which will strangle the inner jet of the spoon.
- a hole is drilled over the entire height of the box.
- the rotary box of the spoon wheel is mechanically connected to the shaft of the turbine.
- an electric generator whose stator is fixed with the inside of all the channels for rotating the fluid, the rotor of this electric generator being fixed to the shaft of the turbine and being mechanically connected to the stator by a bearing / stop, smooth or ball, the other end of the shaft coming out the other side after the wheel and allowing to use the mechanical energy produced with pulleys or electric generators held by supports connected to the casing of the turbine.
- the production of electricity is made by devices based on the principle of Brushless motors, fixing magnets all around the periphery of the spinning spoon wheel, and fixing the coils, which receive the magnetic fields of the magnets , which are placed at the periphery on the turbine casing using magnetic and non-magnetic elements with low remanence.
- Figure 1 shows as an example the spoons that can be modified by changing the values of the width of the wheel, their inclination and their depth;
- Figure 2 shows, starting from the edges of the bump are drawn by the designer, curved lines that will join at their tangent the back of each spoon which precedes them;
- Figure 3 shows in section a half-turbine cut at the axis of the shaft, divided into four zones
- Figure 4 shows the so-called principle of the parameters applied to the spoons
- Figure 5 shows the generation on demand of the bosses by displacing the position of the centers with X, X, a, to be able to modify at will the channel of the spoon which conditions the jet of the fluid.
- FIG. 4 recalls the CARPYZ arithmetic principle of the parameters and shows that the edges (3) of a spoon can be very sharp because the diameters used with the computer and obtained with the 3D additive machines can be extremely thin and practically invisible and sharp. This same drawing also shows that the edge of the ends of the tubes can be flat.
- FIG 1 It is shown FIG 1 that it is possible to modify at will the hollow depth of the spoon and its angulation.
- FIG 5 shows in section a half-turbine cut to the axis of the tree.
- the fluid inlet is arrowed to the left of the drawing and the circular envelope in bold whose edge can be tapered in the case of ambient fluid intake, or provided with a flange (Br) for its connection to an installation.
- It shows the channels consisting of concentric tubes and the radial blades. It also shows the rotary box whose circular tubes contain the spoons, which correspond with the tubes of the channels which bring the fluid.
- Figure 1 shows that using the 5 parameters it is possible to orient the spoons and change their dimensions.
- Figure 5 shows that a boss is placed inside the spoon and that the center of this boss is shifted on demand relative to the center of the axis drawn between the edges of the spoon and allows to modify the importance of the channel that exists between the boss and the bottom of the spoon.
- Figure 2 shows the portions of curves that connect the front edge of the boss to the tangent of the spoon that precedes it. It also shows an oblong central hole that runs through the box.
- Figure 4 recalls the so-called principle of the 5 parameters.
- the skeleton of the turbine is represented on the screen with the help of "virtual neutral fibers" which are afterwards covered with material.
- the turbines are contained over their entire length in a circular envelope. a slightly convex principle whose diameter over the length evolves according to its content
- the length of this one-piece envelope is shown in the drawing divided into four zones cut by ephemeral virtual disks which each separate the zones according to the functions performed at these locations.
- This envelope is very thin or on request provided with a Br flange to allow connection to facilities.
- a ZONE 1 for introducing the fluid, an empty space or occupied by louvers or inductors, like a corkscrew, which possibly generates a pre-rotation of the fluid that enters zone 2.
- FIG 3. A shield The pointed vein separates the fluid vein from the center at the end, and directs it towards the zone 2.
- a ZONE 2 where the fluid is created, in channels that spiral and open at back of zone 2 by rotating the fluid.
- a ZONE 3 where is the rotating wheel provided with calibrated jet spoons that capture the energy provided by the fluid jets exiting the zone 2
- a ZONE 4 where is located a casing fixed to the fixed sleeve of the turbine , placed after the rotating wheel, which contains channels that direct the fluid to the outlet at the back of the turbine.
- the fluid is led from its arrival zone 2 by channels, contained in tubes which are placed in continuity face to face over the entire length of the turbine. Unless they are provided with flanges, the edges of the tubes at the entrance to zone 2 and at the outlet of the tubes of zone 4 are very thin. The edges of the spoons of zone 3 are very tapered.
- the edges of the tubes of the spoon wheel and those of the tubes which surround it, have the same diameter, are flat (FIG 4) and rotate opposite each other.
- the channels are built in fixed circular tubes of different diameters, which are contained in each other, and which start from the front of zone 2 with tapered edges (3 of FIG 4) and whose diameters are evolving. These tubes are pursued face to face in concordance with identical tubes contained in a rotary box which contains the spoons. These rotary tubes are again pursued face to face in accordance with the fixed tubes contained in the casing fixed to the fixed jacket of the turbine (zone 4).
- Figure 3 shows, starting from the front face of zone 2, straight or inclined radial blades whose edges are tapered in the direction chosen by the designer, spiraling backwards in the tubes, forming channels that turn the fluid, and project it out at their tapered edges into the spoons.
- the rotating zone wheel 3 is constructed with spoons which are placed in the wheel between its tubes.
- the spoons are portions of open circles mouth open, oriented for their feeding in the direction of rotation decided by the designer.
- the spoons are modified by changing the values of the width of the wheel, their inclination and their depth.
- the results obtained vary with the diameter of the wheel and with the number of spoons that are determined by the designer. It is drawn a virtual straight line between the two edges of the spoon and on this line is pointed in the middle a center.
- Figure 2 shows that, starting from the edges of the bump are drawn by the designer, curved lines that will join at their tangent the back of each spoon which precedes them.
- an electric generator whose stator is fixed with the inside of all the channels for rotating the fluid.
- the rotor of this electric generator is attached to the shaft of the turbine and is mechanically connected to the stator by a bearing / abutment, smooth or ball.
- the other end of the shaft exits the other side after the wheel and allows to use the mechanical energy produced with pulleys or electric generators held by supports connected to the casing of the turbine (FIG3).
- the production of electricity is made by devices based on the principle of Brushless motors, by fixing magnets all around at the periphery of the spinning spoon wheel, and by fixing the coils, which receive the magnetic fields of the magnets, which are peripherally aligned on the turbine casing using magnetic and non-magnetic low-remanence elements.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
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- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Theoretical Computer Science (AREA)
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- Life Sciences & Earth Sciences (AREA)
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- Mathematical Optimization (AREA)
- Pure & Applied Mathematics (AREA)
- Computer Hardware Design (AREA)
- Evolutionary Computation (AREA)
- Fluid Mechanics (AREA)
- Hydraulic Turbines (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Wind Motors (AREA)
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Abstract
Description
Claims
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2019245914A AU2019245914A1 (en) | 2018-03-28 | 2019-03-22 | Method for designing and producing turbines having buckets with calibrated jets |
RU2020135210A RU2020135210A (ru) | 2018-03-28 | 2019-03-22 | Способ проектирования и изготовления по заказу турбин, имеющих ковши с калиброванными струями |
CN201980022887.5A CN111919024A (zh) | 2018-03-28 | 2019-03-22 | 用于设计和制造具有带校准射流的戽的涡轮机的方法 |
EP19715014.7A EP3775529A1 (fr) | 2018-03-28 | 2019-03-22 | Méthode pour la conception et la fabrication de turbines à cuillères à jet calibré |
US17/042,346 US20210017947A1 (en) | 2018-03-28 | 2019-03-22 | Method for designing and producing turbines having buckets with calibrated jets |
CA3094024A CA3094024A1 (fr) | 2018-03-28 | 2019-03-22 | Methode pour la conception et la fabrication de turbines a cuilleres a jet calibre |
SG11202008704PA SG11202008704PA (en) | 2018-03-28 | 2019-03-22 | Method for designing and fabricating on demand turbines having buckets with calibrated jets |
BR112020019860-9A BR112020019860A2 (pt) | 2018-03-28 | 2019-03-22 | Método para projetar e fabricar turbinas sob demanda tendo recipientes com jatos calibrados |
JP2020552715A JP2021519881A (ja) | 2018-03-28 | 2019-03-22 | 噴射を較正する動翼を備えるタービンの設計及び製造方法 |
IL277558A IL277558A (en) | 2018-03-28 | 2020-09-23 | A method for the design and manufacture on demand of cupped turbines with calibrated jets |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LU100749A LU100749B1 (fr) | 2018-03-28 | 2018-03-28 | Méthode pour la conception et la fabrication à la demande de turbines à cuillères à jet calibré |
LULU100749 | 2018-03-28 |
Publications (2)
Publication Number | Publication Date |
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WO2019185470A1 true WO2019185470A1 (fr) | 2019-10-03 |
WO2019185470A4 WO2019185470A4 (fr) | 2019-11-21 |
Family
ID=62025911
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2019/057216 WO2019185470A1 (fr) | 2018-03-28 | 2019-03-22 | Méthode pour la conception et la fabrication de turbines à cuillères à jet calibré |
Country Status (12)
Country | Link |
---|---|
US (1) | US20210017947A1 (fr) |
EP (1) | EP3775529A1 (fr) |
JP (1) | JP2021519881A (fr) |
CN (1) | CN111919024A (fr) |
AU (1) | AU2019245914A1 (fr) |
BR (1) | BR112020019860A2 (fr) |
CA (1) | CA3094024A1 (fr) |
IL (1) | IL277558A (fr) |
LU (1) | LU100749B1 (fr) |
RU (1) | RU2020135210A (fr) |
SG (1) | SG11202008704PA (fr) |
WO (1) | WO2019185470A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN113868796B (zh) * | 2021-09-28 | 2024-04-09 | 哈尔滨电机厂有限责任公司 | 一种冲击式水轮机水斗根部过渡自适应方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0334737A1 (fr) * | 1988-03-24 | 1989-09-27 | Pierre Carrouset | Machine rotative à déplacement non positif, utilisable comme pompe, compresseur,propulseur, générateur ou turbine motrice |
WO2005111413A1 (fr) * | 2004-05-19 | 2005-11-24 | Envision Corportion | Projection pour rotor d'eolienne |
WO2007011267A1 (fr) | 2005-07-20 | 2007-01-25 | Obschestvo S Ogranichennoy Otvetstvennostyu 'dipo Lnye Struktury' | Procede de stimulation de reactions biochimiques dans l'organisme humain, dispositif de traitement et de regeneration des tissus par ce procede et diode lumineuse destinee a ce dispositif |
WO2008012425A2 (fr) | 2006-07-24 | 2008-01-31 | Pierre Carrouset | Procede de configuration, de roues helices creuses et de leurs cages |
FR2963842A1 (fr) * | 2010-08-13 | 2012-02-17 | Pierre Carrouset | Procede de configuration pour la creation et la fabrication de propulseurs |
FR2997460A1 (fr) | 2012-10-29 | 2014-05-02 | Carpyz | Turbine comportant au moins 2 roues 3d creuse emboitees l'une dans l'autre |
Family Cites Families (5)
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EP1256715A1 (fr) * | 2001-05-11 | 2002-11-13 | VA TECH HYDRO GmbH & Co. | Auget pour turbine Pelton |
CN1930394A (zh) * | 2004-03-18 | 2007-03-14 | 弗兰克·丹尼尔·洛特里翁特 | 涡轮和用于其的转子 |
CN102865177B (zh) * | 2012-09-13 | 2015-08-26 | 沈阳市盛华特种铸造有限公司 | 一种组合式的冲击式水轮发电机转轮的结构及制造方法 |
US20140341709A1 (en) * | 2012-11-19 | 2014-11-20 | Innocent Hervé Yamodo | Double impulse turbine system |
CN109563800A (zh) * | 2016-07-26 | 2019-04-02 | 纳特尔能源公司 | 线性水斗式水轮机 |
-
2018
- 2018-03-28 LU LU100749A patent/LU100749B1/fr active IP Right Grant
-
2019
- 2019-03-22 CA CA3094024A patent/CA3094024A1/fr not_active Abandoned
- 2019-03-22 SG SG11202008704PA patent/SG11202008704PA/en unknown
- 2019-03-22 EP EP19715014.7A patent/EP3775529A1/fr not_active Withdrawn
- 2019-03-22 BR BR112020019860-9A patent/BR112020019860A2/pt not_active Application Discontinuation
- 2019-03-22 CN CN201980022887.5A patent/CN111919024A/zh active Pending
- 2019-03-22 US US17/042,346 patent/US20210017947A1/en not_active Abandoned
- 2019-03-22 JP JP2020552715A patent/JP2021519881A/ja active Pending
- 2019-03-22 RU RU2020135210A patent/RU2020135210A/ru unknown
- 2019-03-22 WO PCT/EP2019/057216 patent/WO2019185470A1/fr active Search and Examination
- 2019-03-22 AU AU2019245914A patent/AU2019245914A1/en not_active Abandoned
-
2020
- 2020-09-23 IL IL277558A patent/IL277558A/en unknown
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0334737A1 (fr) * | 1988-03-24 | 1989-09-27 | Pierre Carrouset | Machine rotative à déplacement non positif, utilisable comme pompe, compresseur,propulseur, générateur ou turbine motrice |
WO2005111413A1 (fr) * | 2004-05-19 | 2005-11-24 | Envision Corportion | Projection pour rotor d'eolienne |
WO2007011267A1 (fr) | 2005-07-20 | 2007-01-25 | Obschestvo S Ogranichennoy Otvetstvennostyu 'dipo Lnye Struktury' | Procede de stimulation de reactions biochimiques dans l'organisme humain, dispositif de traitement et de regeneration des tissus par ce procede et diode lumineuse destinee a ce dispositif |
WO2008012425A2 (fr) | 2006-07-24 | 2008-01-31 | Pierre Carrouset | Procede de configuration, de roues helices creuses et de leurs cages |
FR2963842A1 (fr) * | 2010-08-13 | 2012-02-17 | Pierre Carrouset | Procede de configuration pour la creation et la fabrication de propulseurs |
FR2997460A1 (fr) | 2012-10-29 | 2014-05-02 | Carpyz | Turbine comportant au moins 2 roues 3d creuse emboitees l'une dans l'autre |
WO2014067823A1 (fr) | 2012-10-29 | 2014-05-08 | Carpyz Sas | Turbine comportant au moins deux roues 3d creuses emboîtées l'une dans l'autre |
Also Published As
Publication number | Publication date |
---|---|
BR112020019860A2 (pt) | 2021-01-05 |
US20210017947A1 (en) | 2021-01-21 |
AU2019245914A1 (en) | 2020-10-01 |
CN111919024A (zh) | 2020-11-10 |
SG11202008704PA (en) | 2020-10-29 |
IL277558A (en) | 2020-11-30 |
WO2019185470A4 (fr) | 2019-11-21 |
LU100749B1 (fr) | 2019-10-01 |
RU2020135210A (ru) | 2022-04-28 |
JP2021519881A (ja) | 2021-08-12 |
CA3094024A1 (fr) | 2019-10-03 |
EP3775529A1 (fr) | 2021-02-17 |
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