ES2456825A1 - Turbine comprising lenticular disks - Google Patents

Turbine comprising lenticular disks Download PDF

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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
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ES
Spain
Prior art keywords
turbine
shaft
discs
aerodynamic profiles
disks
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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
Application number
ES201200905A
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Spanish (es)
Other versions
ES2456825B1 (en
Inventor
Domingo González Martín
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Individual
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Individual
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Publication date
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Priority to ES201200905A priority Critical patent/ES2456825B1/en
Priority to PCT/ES2013/000206 priority patent/WO2014044878A1/en
Publication of ES2456825A1 publication Critical patent/ES2456825A1/en
Application granted granted Critical
Publication of ES2456825B1 publication Critical patent/ES2456825B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/12Blades; Blade-carrying rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/18Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means
    • F01D1/20Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means traversed by the working-fluid substantially axially
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06Rotors
    • F03D3/061Rotors characterised by their aerodynamic shape, e.g. aerofoil profiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06Rotors
    • F03D3/062Rotors characterised by their construction elements
    • F03D3/064Fixing wind engaging parts to rest of rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/24Three-dimensional ellipsoidal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/74Wind turbines with rotation axis perpendicular to the wind direction

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

The invention relates to a turbine such as a reaction turbine that can operate with a liquid or gas fluid. The runner of the turbine is provided with the following elements: the shaft (2), which operates normally in a vertical position, a coupling flange (1) being installed in the upper part and a hub (5) or supporting hub flange being installed in the lower part at least one disk (3), which has a convex-planar-lens-type cross-section, and has three blades (6) in the upper part thereof that form angles of 120 DEG and are coupled to the shaft (2) by means of a cotter and aerodynamic profiles (4), the disks being reinforced on the periphery thereof by two aerodynamic profiles, separated by an angle of 180 DEG . The calculation formula: Preal = 1/2 [eta]t [rho] n S V3 Preal = useful power [eta]t = total yield n = number of disks S = swept area V = speed of the fluid.

Description

Descripción detallada de la invención Detailed description of the invention

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

Exposición detallada de un modo de realización de la invención Detailed statement of an embodiment of the invention

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)

REIVINDICACIONES l. Turbina de reacción de discos lenticulares, para funcionamiento continuo, que transforma la energía cinética de un fluido líquido (agua) ó la energía cinética de un fluido gaseoso (aire), en energía mecánica. l. Reaction turbine of lenticular discs, for continuous operation, which transforms the kinetic energy of a liquid fluid (water) or the kinetic energy of a gaseous fluid (air) into mechanical energy. 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) ó cojinete de apoyo. 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) or bearing support. El disco (3).La sección del disco, es de lente plano convexa. En la parte superior, se tallan tres álabes (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. 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. Perfiles aerodinámicas (4). Los discos van reforzados en la periferia con dos perfiles aerodinámico, separados por un ángulo de 180°· Una turbina caracterizada porque puede funcionar con fluido líquido Aerodynamic profiles (4). The discs are reinforced at the periphery with two aerodynamic profiles, separated by a 180 ° angle. o gaseoso, indistintamente o simultáneamente. Con aplicación en la producción de energía eléctrica y bombeo de gases y líquidos. or gas, interchangeably or simultaneously. With application in the production of electrical energy and pumping of gases and liquids.
ES201200905A 2012-09-19 2012-09-19 Lenticular Disc Turbine Active ES2456825B1 (en)

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

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Family Applications (1)

Application Number Title Priority Date Filing Date
ES201200905A Active ES2456825B1 (en) 2012-09-19 2012-09-19 Lenticular Disc Turbine

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ES (1) ES2456825B1 (en)
WO (1) WO2014044878A1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
WO2014044878A1 (en) 2014-03-27
ES2456825B1 (en) 2015-02-11

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