ES2456825A1 - Turbine comprising lenticular disks - Google Patents
Turbine comprising lenticular disks Download PDFInfo
- Publication number
- ES2456825A1 ES2456825A1 ES201200905A ES201200905A ES2456825A1 ES 2456825 A1 ES2456825 A1 ES 2456825A1 ES 201200905 A ES201200905 A ES 201200905A ES 201200905 A ES201200905 A ES 201200905A ES 2456825 A1 ES2456825 A1 ES 2456825A1
- Authority
- ES
- Spain
- Prior art keywords
- turbine
- shaft
- discs
- aerodynamic profiles
- disks
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
- 239000012530 fluid Substances 0.000 claims abstract description 9
- 230000008878 coupling Effects 0.000 claims abstract description 4
- 238000010168 coupling process Methods 0.000 claims abstract description 4
- 238000005859 coupling reaction Methods 0.000 claims abstract description 4
- 239000007788 liquid Substances 0.000 claims abstract description 4
- 238000006243 chemical reaction Methods 0.000 claims abstract 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 238000005086 pumping Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 claims 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 2
- 239000000463 material Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
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
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/12—Blades; Blade-carrying rotors
-
- 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
- F01D1/18—Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means
- F01D1/20—Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means traversed by the working-fluid substantially axially
-
- 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
- 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
- F03D3/064—Fixing wind engaging parts to rest of rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/24—Three-dimensional ellipsoidal
-
- 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
- Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Sustainable Energy (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Fluid Mechanics (AREA)
- Physics & Mathematics (AREA)
- Hydraulic Turbines (AREA)
- Tires In General (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
El rodete de la turbina, está equipado con los elementos siguientes: The impeller of the turbine is equipped with the following elements:
El eje (2). Trabaja normalmente en posición vertical; en la parte superior, se instala una brida (1) de acoplamiento y en la parte inferior un buje (5). The shaft (2). It works normally in an upright position; In the upper part, a coupling flange (1) is installed and in the lower part a bushing (5).
El disco (3).La sección del disco, es de lente plano convexa. En la parte superior, se tallan tres alabes (6), formando ángulos de 120°. Se acoplan al eje (2) con una chaveta, para evitar el deslizamiento. El número de discos, puede ser uno o varios, dependiendo de las condiciones de trabajo. The disc (3) .The section of the disc is convex flat lens. At the top, three blades (6) are carved, forming 120 ° angles. They are coupled to the shaft (2) with a key, to prevent slippage. The number of discs can be one or several, depending on the working conditions.
Perfiles aerodinámicas (4). Los discos van reforzados en la periferia con dos perfiles aerodinámico, separados por un ángulo de 180°' Aerodynamic profiles (4). The discs are reinforced on the periphery with two aerodynamic profiles, separated by an angle of 180 ° '
La turbina convierte la energía del fluido en movimiento, en energía mecánica o eléctrica. Si la conectamos a un generador eléctrico, tendremos energía eléctrica y si la conectamos a una bomba o cualquier otro dispositivo, tendremos energía mecánica. The turbine converts the energy of the moving fluid into mechanical or electrical energy. If we connect it to an electric generator, we will have electric power and if we connect it to a pump or any other device, we will have mechanical energy.
La fórmula para el cálculo de la potencia es la siguiente: The formula for calculating power is as follows:
P=FV dónde P = PV where
P = potencia P = power
F = fuerza de sustentación F = lift force
V = velocidad del fluido V = fluid velocity
La fuerza de sustentación se calcula por la fórmula siguiente: F = 112 p S V2 dónde The bearing force is calculated by the following formula: F = 112 p S V2 where
p = densidad del fluido S = área barrida V = velocidad del fluido sustituyendo tenemos p = fluid density S = swept area V = fluid speed replacing we have
P = 112 p S V3 la potencia real es: P = 112 p S V3 the real power is:
Prea1 = Cp 11112 p S V3 donde Cp = coeficiente de potencia 11 = rendimiento de la máquina Rendimiento total 11t = Cp 11 sustituyendo Prea1 = Cp 11112 p S V3 where Cp = power coefficient 11 = machine performance Total performance 11t = Cp 11 replacing
Preal = 1I211t p S V3 Si n = numero de discos Preal = 1I211t p S V3 If n = number of discs
Prea1 = 112 11t p n S V3 Prea1 = 112 11t p n S V3
Ventajas de la invencción: Reduce prácticamente a cero los problemas de cavitación. Puede funcionar con aire o agua indistintamente ó simultáneamente. Aumentando el número de discos, aumentamos el área de sustentación, sin variar la velocidad periférica. Advantages of the invention: Reduces virtually zero cavitation problems. It can work with air or water interchangeably or simultaneously. By increasing the number of discs, we increase the lift area, without varying the peripheral speed.
Aplicaciones industriales: En centrales de producción de energía eléctrica. Para el bombeo de fluidos líquidos ó gaseosos Industrial applications: In power plants. For pumping liquid or gaseous fluids
DIBUJO N° l(Alzado) DRAWING N ° l (Elevation)
(1) = Brida de acoplamiento; (2) = eje; (3) = Disco lenticular plano convexo; (4) = Perfiles aerodinámicos, instalados a 1800 (5) = Buje ó cojinete de apoyo (1) = Coupling flange; (2) = axis; (3) = Convex flat lenticular disc; (4) = Aerodynamic profiles, installed at 1800 (5) = Bushing or bearing support
DIBUJO N° 2 (Planta) DRAWING N ° 2 (Plant)
(6) = Álabes tallados en el disco, instalados a 1200 (6) = Blades carved on the disk, installed at 1200
Si hacemos pasar una corriente de aire por un conducto, de sección de entrada S1 y sección de salida S2 y S2 es menor que S], la velocidad de salida del aire V2 = V1S1/S2, de acuerdo con la ley de continuidad. Si variamos adecuadamente la relación S1/S2, podemos, teóricamente aumentar la velocidad de salida, en una cantidad ilimitada. En la práctica, por limitaciones en de fabricación y resistencia de materiales, existe una velocidad máxima. If we pass a stream of air through a duct, with inlet section S1 and outlet section S2 and S2 is less than S], the air outlet speed V2 = V1S1 / S2, in accordance with the law of continuity. If we properly vary the S1 / S2 ratio, we can theoretically increase the output speed by an unlimited amount. In practice, due to limitations in manufacturing and strength of materials, there is a maximum speed.
DIMENSIONADO DE UNA TURBINA DE 1500 KW.(CON AIRE) Aplicando la fórmula de potencia P = 1/2 11t Pn S V3 Si tenemos una velocidad del aire de 100 m/seg.-y queremos una turbina de 4 discos, necesitamos un área barrida de: S = P*2*100/11t P n V3 m2 dónde P = 1500 KW, P = 1,2, n = 4 V = 100 m/seg.-y 11t = 0,3 (para una relación de velocidades de 5) sustituyendo S = 1500*2* 100/0,3 * 1,2 * 1003 * 4 = 30000011440000 = 0,2 m2 luego D = (0,2*4/3,14)1/2 = 0,5 m de diámetro. Como la relación de velocidades 2JI W r/60V = 5 W = 5 * 60 *VI JID = 5*60*100/3.14*0,5 = 30000/1,57 = 19000rpm. DIMENSIONED OF A 1500 KW TURBINE. (WITH AIR) Applying the power formula P = 1/2 11t Pn S V3 If we have an air speed of 100 m / sec. - and we want a turbine of 4 discs, we need a swept area of: S = P * 2 * 100 / 11t P n V3 m2 where P = 1500 KW, P = 1.2, n = 4 V = 100 m / sec.-y 11t = 0.3 (for a speed ratio of 5) replacing S = 1500 * 2 * 100 / 0.3 * 1.2 * 1003 * 4 = 30000011440000 = 0.2 m2 then D = (0.2 * 4 / 3.14) 1/2 = 0.5 m in diameter. As the speed ratio 2JI W r / 60V = 5 W = 5 * 60 * VI JID = 5 * 60 * 100 / 3.14 * 0.5 = 30000 / 1.57 = 19000rpm
DIMENSIONADO DE UNA TURBINA DE 1500 KW (CON AGUA) Para una velocidad del agua de 10 m/seg. Diámetro del disco = 560mm (redondeando) DIMENSIONED OF A 1500 KW TURBINE (WITH WATER) For a water speed of 10 m / sec. Disc diameter = 560mm (rounding)
Revoluciones = 1750 rpm (redondeando) Revolutions = 1750 rpm (rounding)
Claims (1)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201200905A ES2456825B1 (en) | 2012-09-19 | 2012-09-19 | Lenticular Disc Turbine |
PCT/ES2013/000206 WO2014044878A1 (en) | 2012-09-19 | 2013-09-17 | Turbine comprising lenticular disks |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201200905A ES2456825B1 (en) | 2012-09-19 | 2012-09-19 | Lenticular Disc Turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2456825A1 true ES2456825A1 (en) | 2014-04-23 |
ES2456825B1 ES2456825B1 (en) | 2015-02-11 |
Family
ID=50340606
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201200905A Active ES2456825B1 (en) | 2012-09-19 | 2012-09-19 | Lenticular Disc Turbine |
Country Status (2)
Country | Link |
---|---|
ES (1) | ES2456825B1 (en) |
WO (1) | WO2014044878A1 (en) |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1741787A (en) * | 1922-04-15 | 1929-12-31 | Moody Lewis Ferry | Runner for turbines |
US7726934B2 (en) * | 2007-02-06 | 2010-06-01 | Preferred Energy, L.L.C. | Vertical axis wind turbine |
US7824060B2 (en) * | 2008-03-31 | 2010-11-02 | Syracuse University | Wind powered device |
WO2010075515A1 (en) * | 2008-12-24 | 2010-07-01 | Dominick Daniel Martino | Prime mover |
US8613586B2 (en) * | 2009-09-21 | 2013-12-24 | Qualitics, Inc. | Vortical wind energy apparatus |
US8487468B2 (en) * | 2010-11-12 | 2013-07-16 | Verterra Energy Inc. | Turbine system and method |
-
2012
- 2012-09-19 ES ES201200905A patent/ES2456825B1/en active Active
-
2013
- 2013-09-17 WO PCT/ES2013/000206 patent/WO2014044878A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2014044878A1 (en) | 2014-03-27 |
ES2456825B1 (en) | 2015-02-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SA519401300B1 (en) | Choke System for Wellhead Assembly Having A Turbine Generator | |
CN103195512B (en) | Radial air turbine powered by vacuum suction | |
CN101813006A (en) | Multi-stage jet-type reaction force disc generating system | |
TW201350674A (en) | Wind power installation | |
ES2456825A1 (en) | Turbine comprising lenticular disks | |
RU2014116100A (en) | SCREW FITTING ASSEMBLY TO TURBINE DRIVING WHEEL | |
RU2362904C1 (en) | Flow accelerator (versions) | |
WO2015031723A4 (en) | Axial fan inlet wind-turning vane assembly | |
CN201339532Y (en) | Small-sized francis turbine generator | |
RU101739U1 (en) | FLOW ENERGY CONVERTER | |
CN201209521Y (en) | Heating device by wind energy | |
CN203906177U (en) | Vertical axis wind turbine | |
US20150275913A1 (en) | Hydraulic Turbines with Exit Flow Direction Opposite to its Inlet Flow Direction | |
CN203656431U (en) | Pipe fitting | |
CN201771668U (en) | External snail-like vertical-horizontal water turbine | |
WO2011107799A3 (en) | Improved tidal stream turbine | |
US9546639B2 (en) | Hydraulic device of reversible type for the conversion of energy | |
CN204419694U (en) | Modified model fan impeller system | |
CN204267228U (en) | A kind of torque output device | |
KR100889043B1 (en) | Wind power system which has a air-compressor and a air-inducer turned according to the direction of the wind | |
CN112081750B (en) | Miniature doublestage vortex pump hydraulic pressure impeller | |
CN101806278A (en) | Vertical shaft wind wheel with multi-section combined vanes | |
RU2522271C2 (en) | Wind-driven plant | |
GB2506899A (en) | Hydrostatic pressure pumping wheel | |
RU93471U1 (en) | A HYDRAULIC WHEEL WITH A HORIZONTAL AXIS OF ROTATION |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 2456825 Country of ref document: ES Kind code of ref document: B1 Effective date: 20150211 |
|
GC2A | Exploitation certificate registered application with search report |
Effective date: 20180424 |