ES3063767A1 - Pala estriada - Google Patents
Pala estriadaInfo
- Publication number
- ES3063767A1 ES3063767A1 ES202430726A ES202430726A ES3063767A1 ES 3063767 A1 ES3063767 A1 ES 3063767A1 ES 202430726 A ES202430726 A ES 202430726A ES 202430726 A ES202430726 A ES 202430726A ES 3063767 A1 ES3063767 A1 ES 3063767A1
- Authority
- ES
- Spain
- Prior art keywords
- striations
- hub
- approach
- leading edge
- area closer
- 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.)
- Pending
Links
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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/18—Aerodynamic features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/467—Aerodynamic features
-
- 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
- F03D1/0649—Rotors characterised by their aerodynamic shape of the blades of the blade surfaces, e.g. roughened
-
- 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
- F03D1/06495—Aerodynamic elements attached to or formed with the blade, e.g. flaps, vortex generators or noise reducers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/002—Influencing flow of fluids by influencing the boundary layer
- F15D1/0025—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply
- F15D1/003—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising surface features, e.g. indentations or protrusions
- F15D1/0035—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising surface features, e.g. indentations or protrusions in the form of riblets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/002—Influencing flow of fluids by influencing the boundary layer
- F15D1/0025—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply
- F15D1/003—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising surface features, e.g. indentations or protrusions
- F15D1/0035—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising surface features, e.g. indentations or protrusions in the form of riblets
- F15D1/004—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising surface features, e.g. indentations or protrusions in the form of riblets oriented essentially parallel to the direction of flow
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Abstract
Pala de hélice o turbina en cuyo extradós 7 se conforman un conjunto de acanaladuras, rebajes o estrías 9 cuyas trayectorias son aproximadamente o totalmente paralelas entre ellas y transcurren desde una zona más cercana al borde de ataque 4 hasta una zona más cercana al borde de salida 5. Dichas trayectorias se van alejando del eje de giro o buje 3 a medida que se aproximan el borde de ataque 4 y, análogamente, a medida que se aproximan al borde de salida 5, su distancia respecto del buje 3 se va reduciendo. La introducción de estas estrías 9 mejora el rendimiento de la pala al incrementar el ratio resultante de dividir el coeficiente de sustentación entre el coeficiente de arrastre además de mitigar la entrada en pérdida al retrasar el desprendimiento de la capa límite.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES202430726A ES3063767A1 (es) | 2024-09-13 | 2024-09-13 | Pala estriada |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES202430726A ES3063767A1 (es) | 2024-09-13 | 2024-09-13 | Pala estriada |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES3063767A1 true ES3063767A1 (es) | 2026-04-20 |
Family
ID=99477224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES202430726A Pending ES3063767A1 (es) | 2024-09-13 | 2024-09-13 | Pala estriada |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES3063767A1 (es) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8460779B2 (en) * | 2011-03-30 | 2013-06-11 | General Electric Company | Microstructures for reducing noise of a fluid dynamic structure |
| US9945352B2 (en) * | 2012-07-25 | 2018-04-17 | Lm Wp Patent Holding A/S | Wind turbine blade having a shaped stall fence or flow diverter |
| US20190202547A1 (en) * | 2016-06-20 | 2019-07-04 | 3M Innovative Properties Company | Aerodynamic articles and methods thereof |
| US10422363B2 (en) * | 2013-08-22 | 2019-09-24 | Airbus Defence and Space GmbH | Structural component with a riblet surface |
| US20240102389A1 (en) * | 2021-02-05 | 2024-03-28 | Nikon Corporation | Blade member and structural member |
-
2024
- 2024-09-13 ES ES202430726A patent/ES3063767A1/es active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8460779B2 (en) * | 2011-03-30 | 2013-06-11 | General Electric Company | Microstructures for reducing noise of a fluid dynamic structure |
| US9945352B2 (en) * | 2012-07-25 | 2018-04-17 | Lm Wp Patent Holding A/S | Wind turbine blade having a shaped stall fence or flow diverter |
| US10422363B2 (en) * | 2013-08-22 | 2019-09-24 | Airbus Defence and Space GmbH | Structural component with a riblet surface |
| US20190202547A1 (en) * | 2016-06-20 | 2019-07-04 | 3M Innovative Properties Company | Aerodynamic articles and methods thereof |
| US20240102389A1 (en) * | 2021-02-05 | 2024-03-28 | Nikon Corporation | Blade member and structural member |
Non-Patent Citations (1)
| Title |
|---|
| García Mayoral, Ricardo (2011). The interaction of riblets with wall-bounded turbulence = La interacción de los microsurcos con la turbulencia de pared. Tesis (Doctoral). todo el documento. * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE602006011640D1 (de) | Blatt für einen windturbinenrotor | |
| ES2679368T3 (es) | Pala de turbina eólica que tiene una placa de sustentación o desviador de flujo conformado | |
| BR102013025213A2 (pt) | Pá de rotor de turbina eólica, turbina eólica com inúmeras pás de rotor e disposição de correção de fluxo de ar | |
| CN108980101B (zh) | 一种基于鲨鱼表面减阻技术的仿生叶片 | |
| BR112013013569B8 (pt) | pá de turbomáquina, compressor de turbomáquina, turbina de turbomáquina e turbomáquina | |
| NO20053757D0 (no) | Kjolevifte med forsterket blad | |
| ES413589A1 (es) | Perfeccionamientos introducidos en aeronaves. | |
| BRPI0515409A (pt) | dispositivo de ponta, superfìce de sustentação aerodinámica, aeronave, e, helicóptero | |
| SE447469B (sv) | Beryteblad | |
| WO2014044414A1 (en) | A wind turbine blade | |
| DK2877737T3 (en) | Wind turbine blade with a shaped stall fence or flow diverter | |
| EP2910772B1 (en) | Wind turbine blade, wind turbine rotor and wind turbine generator system | |
| CN109915407A (zh) | 一种非光滑表面的离心泵叶轮及其效率和噪声协同提升设计方法 | |
| EP2562427A3 (en) | A rotor for a compressor of a gas turbine | |
| CN104816827A (zh) | 一种翼尖后掠下反的低诱导阻力直升机旋翼 | |
| CN104819106A (zh) | 一种风力机叶片翼型族 | |
| CN110155318A (zh) | 确定桨叶的翼型的初始前缘圆的方法和改进桨叶以增大其负失速迎角的方法 | |
| CN206155775U (zh) | 螺旋桨、动力组件及飞行器 | |
| BR112018002793B1 (pt) | Pá de rotor de turbomáquina, disco de pá de peça única, rotor, e, turbomáquina | |
| CN104097770B (zh) | 一种直升机主转翼用翼片 | |
| DK2912307T3 (en) | WIND Turbine rotor blades | |
| CN105065302B (zh) | 一种高效前掠型地铁隧道轴流风机 | |
| JPH01141199A (ja) | プロペラ羽根 | |
| FR3115012B1 (fr) | Méthode d’amélioration du comportement aérodynamique de pales d’un giravion en vol stationnaire par un déplacement du bord d’attaque des profils aérodynamiques de ces pales | |
| CA2350161A1 (en) | Airfoil suitable for forward and reverse flow |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| BA2A | Patent application published |
Ref document number: 3063767 Country of ref document: ES Kind code of ref document: A1 Effective date: 20260420 |