CL2019001216A1 - Álabe y aparato de turbina. - Google Patents

Álabe y aparato de turbina.

Info

Publication number
CL2019001216A1
CL2019001216A1 CL2019001216A CL2019001216A CL2019001216A1 CL 2019001216 A1 CL2019001216 A1 CL 2019001216A1 CL 2019001216 A CL2019001216 A CL 2019001216A CL 2019001216 A CL2019001216 A CL 2019001216A CL 2019001216 A1 CL2019001216 A1 CL 2019001216A1
Authority
CL
Chile
Prior art keywords
blade
mountain
formation
fluid
pressure
Prior art date
Application number
CL2019001216A
Other languages
English (en)
Inventor
Colm Joseph Caren
Original Assignee
Caren Meicnic Teoranta
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 Caren Meicnic Teoranta filed Critical Caren Meicnic Teoranta
Publication of CL2019001216A1 publication Critical patent/CL2019001216A1/es

Links

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
    • F03DWIND MOTORS
    • F03D5/00Other wind motors
    • 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
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • F03D1/0608Rotors characterised by their aerodynamic shape
    • F03D1/0633Rotors characterised by their aerodynamic shape of the blades
    • 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
    • F03D80/00Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/301Cross-section characteristics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/20Heat transfer, e.g. cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/20Heat transfer, e.g. cooling
    • F05B2260/211Heat transfer, e.g. cooling by intercooling, e.g. during a compression cycle
    • F05B2260/212Heat transfer, e.g. cooling by intercooling, e.g. during a compression cycle by water injection
    • 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
    • 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
    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)

Abstract

LA PRESENTE INVENCIÓN PROPORCIONA UN ÁLABE DE TURBINA PARA EL MOVIMIENTO RELATIVO EN UN FLUIDO DE AMBIENTE Y UN APARATO DE TURBINA QUE COMPRENDE AL MENOS UN ÁLABE. EL ÁLABE COMPRENDE UN LARGUERO PRINCIPAL QUE TIENE DOS FORMACIONES DE MONTÍCULO Y MEDIOS DE DESCARGA OPERABLES PARA DESCARGAR FLUIDOS EVAPORATIVO Y DE CONDENSACIÓN HACIA AFUERA EN EL FLUIDO DE AMBIENTE QUE FLUYE SOBRE EL LARGUERO PRINCIPAL. LA PRIMERA DE ESTAS FORMACIONES DE MONTÍCULO ACELERA EL FLUJO DEL FLUIDO DE AMBIENTE HASTA QUE ALCANZA LA VELOCIDAD DEL SONIDO. LUEGO DE LA PRIMERA FORMACIÓN DE MONTÍCULO, EL NÚMERO DE MACH CONTINÚA AUMENTANDO Y SE DESCARGA EL FLUIDO EVAPORATIVO EN EL AMBIENTE, LO QUE GENERA QUE EL AIRE SE ENFRÍE, LO CUAL ACELERA EL FLUJO DE AMBIENTE ADICIONALMENTE Y DISMINUYE LA PRESIÓN. EN LA SEGUNDA FORMACIÓN DE MONTÍCULO, LA PRESIÓN MENOR GENERA UN IMPULSO. A MEDIDA QUE SE MUEVE EL FLUJO RESPECTO A LA SEGUNDA FORMACIÓN DE MONTÍCULO, DISMINUYE EL NÚMERO DE MACH Y LUEGO AUMENTA A MEDIDA QUE BAJA POR LA SEGUNDA REGIÓN. SE DESCARGA UN FLUIDO DE CONDENSACIÓN, LO QUE GENERA QUE EL CONTENIDO DE AGUA DEL AIRE SE CONDENSE, LIBERANDO CALOR, QUE PRODUCE UNA DISMINUCIÓN EN EL NÚMERO DE MACH Y UN AUMENTO EN LA PRESIÓN. EL AUMENTO DE PRESIÓN EN LA SEGUNDA FORMACIÓN DE MONTÍCULO PRODUCIRÁ UN IMPULSO QUE SE PUEDE UTILIZAR PARA GIRAR UN ROTOR. LA PRESENTE INVENCIÓN PROPORCIONA UN ÁLABE PARA PRODUCIR TRABAJO Y ENERGÍA DIRECTAMENTE DE LA HUMEDAD EN EL AIRE. NO DEPENDE DE LA VELOCIDAD DEL VIENTO Y SU FUENTE ENERGÉTICA DERIVA DIRECTAMENTE DE LA ATMÓSFERA DEL AMBIENTE QUE SIEMPRE SE ENCUENTRA DISPONIBLE.
CL2019001216A 2016-11-02 2019-05-02 Álabe y aparato de turbina. CL2019001216A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP16196917.5A EP3318750B1 (en) 2016-11-02 2016-11-02 An airfoil and a turbine apparatus

Publications (1)

Publication Number Publication Date
CL2019001216A1 true CL2019001216A1 (es) 2019-09-13

Family

ID=57226835

Family Applications (1)

Application Number Title Priority Date Filing Date
CL2019001216A CL2019001216A1 (es) 2016-11-02 2019-05-02 Álabe y aparato de turbina.

Country Status (19)

Country Link
US (1) US10968886B2 (es)
EP (1) EP3318750B1 (es)
JP (2) JP2019537682A (es)
KR (1) KR102412684B1 (es)
CN (1) CN109891090B (es)
AR (1) AR110025A1 (es)
AU (1) AU2017353216B2 (es)
BR (1) BR112019008860A2 (es)
CA (1) CA3042299A1 (es)
CL (1) CL2019001216A1 (es)
DK (1) DK3318750T3 (es)
ES (1) ES2751752T3 (es)
IL (1) IL266081B (es)
MX (1) MX2019005129A (es)
PH (1) PH12019500752A1 (es)
PL (1) PL3318750T3 (es)
RU (1) RU2747533C2 (es)
WO (1) WO2018082983A1 (es)
ZA (1) ZA201903331B (es)

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4134062C2 (de) * 1991-10-15 1997-07-24 Dieter Schulz Luftschraube mit Tandemprofil und Abströmkanal
US5395071A (en) * 1993-09-09 1995-03-07 Felix; Frederick L. Airfoil with bicambered surface
AU3541797A (en) 1996-07-09 1998-02-02 Private Universitat Witten/Herdecke Gmbh Rotor for a wind power station
RU2178830C2 (ru) * 1999-09-09 2002-01-27 Николай Алексеевич Лаврентьев Способ управления отбором мощности ветрового потока и ветроэнергетическое устройство
EP1757806A1 (en) * 2004-05-27 2007-02-28 Intellectual Property Bank Corp. Blade for vertical shaft wind wheel and vertical shaft wind wheel
US20090211371A1 (en) * 2006-04-26 2009-08-27 Mergenet Medical, Inc. Flow measuring device
SG154344A1 (en) * 2008-01-09 2009-08-28 United Technologies Corp Airfoil mask, airfoil and mask system, and masking method for edge profile finishing
CN101598105B (zh) * 2008-06-06 2011-09-07 中国科学院工程热物理研究所 控制叶片表面流动流体分离的装置
US8128037B2 (en) * 2009-01-19 2012-03-06 The Boeing Company Apparatus and method for passive purging of micro-perforated aerodynamic surfaces
WO2011101847A2 (en) * 2010-02-16 2011-08-25 Technion Research And Development Foundation Ltd. Flow control on a vertical axis wind turbine (vawt)
US8523524B2 (en) * 2010-03-25 2013-09-03 General Electric Company Airfoil cooling hole flag region
CH705323A1 (de) * 2011-07-25 2013-01-31 Alstom Technology Ltd Verfahren zum Einspritzen von Wasser in einen mehrstufigen Axialverdichter einer Gasturbine.
US9249666B2 (en) * 2011-12-22 2016-02-02 General Electric Company Airfoils for wake desensitization and method for fabricating same
ITMI20120010A1 (it) * 2012-01-05 2013-07-06 Gen Electric Profilo aerodinamico di turbina a fessura
US9175569B2 (en) * 2012-03-30 2015-11-03 General Electric Company Turbine airfoil trailing edge cooling slots
WO2014158245A1 (en) * 2013-03-14 2014-10-02 Hodgson Benedict N Airfoil with leading edge reinforcement

Also Published As

Publication number Publication date
KR102412684B1 (ko) 2022-06-23
RU2747533C2 (ru) 2021-05-06
JP2019537682A (ja) 2019-12-26
RU2019116510A3 (es) 2021-02-24
JP2024084793A (ja) 2024-06-25
PH12019500752A1 (en) 2019-08-05
EP3318750A1 (en) 2018-05-09
MX2019005129A (es) 2019-06-20
WO2018082983A1 (en) 2018-05-11
IL266081B (en) 2020-11-30
KR20190079649A (ko) 2019-07-05
BR112019008860A2 (pt) 2019-07-09
US10968886B2 (en) 2021-04-06
CN109891090B (zh) 2020-10-30
EP3318750B1 (en) 2019-09-11
CN109891090A (zh) 2019-06-14
AR110025A1 (es) 2019-02-13
IL266081A (en) 2019-06-30
DK3318750T3 (da) 2019-11-18
AU2017353216B2 (en) 2023-07-27
CA3042299A1 (en) 2018-05-11
AU2017353216A1 (en) 2019-05-30
RU2019116510A (ru) 2020-12-03
PL3318750T3 (pl) 2020-03-31
US20190257288A1 (en) 2019-08-22
ES2751752T3 (es) 2020-04-01
ZA201903331B (en) 2020-02-26

Similar Documents

Publication Publication Date Title
CO6360216A1 (es) Sistema de resistencia variable al flujo para su uso en un pozo subterráneo
CL2015000314A1 (es) Sistema de enfriamiento integrado de una turbina eolica que incluye un generador que tiene un estator, y al menos un rectificador, donde dicho sistema comprende una bomba, un intercambiador de calor, y un primer subsistema de enfriamiento; intercambiador de calor; turbina eolica.
CO6360214A1 (es) Sistema de resistencia de flujo variable con estructura que induce la circulación en la misma para resistir variablemente el flujo en un pozo subterráneo
WO2015175073A3 (en) Gas turbine engine airfoil
EP2762724A3 (en) Ultrasonic sound emitting devices for wind turbines
AR093096A1 (es) Sistema de alabes de turbina
BR112012028640A2 (pt) geradores de vórtice para geração de vórtices a montante de uma cascata de lâminas de compressor
RU2012151011A (ru) Полая внутренняя направляющая для турбинных лопаток
BR102016010007A2 (pt) sistema, método e sistema de turbina a gás
BR112018001163A2 (pt) carcaça de escape para um motor de turbina de aeronave, motor de turbina e aeronave
CL2015002883A1 (es) Una instalacion de turbina hidraulica generadora de energia
ES2570568T3 (es) Turbina eólica con sistema de climatización de torre que usa aire exterior
EP3034785A3 (en) A gas turbine fan blade with varying fracture resistance
RU2015107543A (ru) Конструкция лопаток турбины
CL2014002974A1 (es) Aparato para la generacion de energia porque inlcuye una carcasa, un pasaje que se extiende a traves de la carcasa que tiene un primer extremo y un segundo extremo y que forma un camino para el flujo de fluido entre el primer extremo y el segundo extremo y una turbina que esta montada en una ubicacion dentro del pasaje para su rotacion alrededor de un eje.
PH12020550268A1 (en) Flow energy installation, in particular encased wind turbine
WO2015160955A3 (en) Fluid turbine with turbine shroud and ejector shroud coupled with high thrust-coefficient rotor
WO2015130380A3 (en) Blade outer air seal cooling passage
CL2019001216A1 (es) Álabe y aparato de turbina.
RU2015112104A (ru) Трубка принудительного охлаждения для лопатки газовой турбины, имеющая разделительную стенку
RU2016123061A (ru) Впускающий вихри корпус для компрессора осевой турбомашины
BR112012024519A2 (pt) compressor de motor, em particualr de turborreator de aeronave, dotado de um sistema de extração de ar
WO2017191075A3 (en) A turbomachine blade or vane having a vortex generating element
PE20211222A1 (es) Motor de uso general
RU2010150179A (ru) Способ борьбы с атмосферной жарой и стужей и устройство для его осуществления