WO2013009646A3 - Vortex generators - Google Patents
Vortex generators Download PDFInfo
- Publication number
- WO2013009646A3 WO2013009646A3 PCT/US2012/045828 US2012045828W WO2013009646A3 WO 2013009646 A3 WO2013009646 A3 WO 2013009646A3 US 2012045828 W US2012045828 W US 2012045828W WO 2013009646 A3 WO2013009646 A3 WO 2013009646A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- base
- fluid
- vortex generators
- vortex
- height
- Prior art date
Links
- 239000012530 fluid Substances 0.000 abstract 3
- 238000000926 separation method Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D21/00—Pump involving supersonic speed of pumped fluids
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/545—Ducts
- F04D29/547—Ducts having a special shape in order to influence fluid flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
- F04D29/682—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid extraction
-
- 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
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
-
- 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
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/306—Surface measures
- F05B2240/3062—Vortex generators
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/127—Vortex generators, turbulators, or the like, for mixing
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/85938—Non-valved flow dividers
Abstract
A vortex generator (100), or an array of vortex generators, for attenuating flow separation during flow of fluid over a surface (201). Vortex generators include a base (200) with a forward end (202) and a leading edge (204) extending outward and rearward from the forward end to an outward end (206). The leading edge includes a first angular discontinuity (210) at a height Hi above the base, and a second angular discontinuity (212) at a height H2 above the base. The vortex generator(s) are configured for generating, adjacent a surface, at least two vortices V1 and V2 in a fluid, and turning the outermost generated vortice toward the surface over which the fluid is passing.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012103194688A CN102865274A (en) | 2011-07-09 | 2012-07-06 | Vortex generators |
US13/542,673 US20130037657A1 (en) | 2011-07-09 | 2012-07-06 | Vortex generators |
CN2012204422441U CN202937553U (en) | 2011-07-09 | 2012-07-06 | Vortex generator and airplane, device, land vehicle, wind turbine and vortex generator array using same |
PCT/US2012/045828 WO2013009646A2 (en) | 2011-07-09 | 2012-07-06 | Vortex generators |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161506055P | 2011-07-09 | 2011-07-09 | |
US61/506,055 | 2011-07-09 | ||
PCT/US2012/045828 WO2013009646A2 (en) | 2011-07-09 | 2012-07-06 | Vortex generators |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2013009646A2 WO2013009646A2 (en) | 2013-01-17 |
WO2013009646A3 true WO2013009646A3 (en) | 2013-05-02 |
Family
ID=62904783
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2012/045828 WO2013009646A2 (en) | 2011-07-09 | 2012-07-06 | Vortex generators |
Country Status (3)
Country | Link |
---|---|
US (1) | US20130037657A1 (en) |
CN (2) | CN102865274A (en) |
WO (1) | WO2013009646A2 (en) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9884688B2 (en) * | 2013-02-14 | 2018-02-06 | Gulfstream Aerospace Corporation | Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system |
CN103303469B (en) * | 2013-07-05 | 2015-05-27 | 上海交通大学 | Device for controlling flow separation caused by interference between high-Mach-number shock waves and boundary layers |
US9777418B2 (en) * | 2013-08-05 | 2017-10-03 | Whirlpool Corporation | Laundry treating appliance laundry mover with liquid diverter |
US9909597B2 (en) | 2013-10-15 | 2018-03-06 | Dresser-Rand Company | Supersonic compressor with separator |
US9752559B2 (en) | 2014-01-17 | 2017-09-05 | General Electric Company | Rotatable aerodynamic surface features for wind turbine rotor blades |
CN105314097A (en) * | 2014-08-01 | 2016-02-10 | 郭宏斌 | Anti-dragging device with vortex forming anti-dragging shell pieces |
DK3037656T3 (en) * | 2014-12-22 | 2017-03-13 | Siemens Ag | Rotor blade with vortex generators |
GB2536214B (en) * | 2015-03-05 | 2020-05-27 | Elogab O | Engine system and method of generating electricity from an internal combustion engine |
JP6569303B2 (en) * | 2015-05-28 | 2019-09-04 | 三菱航空機株式会社 | Flaps and aircraft |
JP6486201B2 (en) * | 2015-05-28 | 2019-03-20 | 国立研究開発法人宇宙航空研究開発機構 | Wings, flaps and aircraft |
FR3041596B1 (en) * | 2015-09-30 | 2017-12-08 | Plastic Omnium Cie | AERODYNAMIC SYSTEM WITH VORTEX GENERATOR SUPPLIED BY EXHAUST GASES |
US11085471B2 (en) | 2016-06-22 | 2021-08-10 | Quest Integrated, Llc | Active control of vortices for skin friction reduction |
EP3284667B1 (en) * | 2016-08-16 | 2019-03-06 | Airbus Operations GmbH | Wing-tip arrangement having vortilons attached to a lower surface, an aircraft having such a wing-tip arrangement and the use of vortilons on a wing-tip arrangement |
US10364021B2 (en) * | 2016-09-26 | 2019-07-30 | General Electric Company | Aircraft having an aft engine and stabilizer root fillet |
US10920742B2 (en) * | 2018-07-26 | 2021-02-16 | Institute of Nuclear Energy Research, Atomic Energy Council, Executive Yuan, R.O.C. | Noise-reduction device for wind turbine and the wind turbine applied thereof |
CN109190256B (en) * | 2018-09-06 | 2022-05-17 | 吉林大学 | Vortex generator simulating bird wing feather covering and optimization method thereof |
GB2578447A (en) * | 2018-10-26 | 2020-05-13 | Airbus Operations Ltd | Aircraft assembly with a hot-air exhaust outlet |
CN112173082B (en) * | 2020-08-25 | 2021-11-16 | 中国航天空气动力技术研究院 | Micro-vortex generating device with auxiliary control of airflow |
CN112092927A (en) * | 2020-10-22 | 2020-12-18 | 河北工业大学 | Vortex generator based on FSAE racing car |
CN116534246B (en) * | 2023-07-05 | 2023-09-12 | 中国空气动力研究与发展中心计算空气动力研究所 | Flow direction vortex modulation device |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050163963A1 (en) * | 2004-01-12 | 2005-07-28 | Munro Alexander S. | Method and apparatus for reducing drag and noise for a vehicle |
DE102008022504A1 (en) * | 2008-05-07 | 2009-11-19 | Eads Deutschland Gmbh | Switchable vortex generator e.g. turbulator, for aircraft, has vortex generating element movable back and forth between two different positions, where vortex generating element is designed as profile element with profile structure |
US20110262705A1 (en) * | 2011-03-30 | 2011-10-27 | General Electric Company Global Research | Microstructures for reducing noise of a fluid dynamic structure |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2800291A (en) * | 1950-10-24 | 1957-07-23 | Stephens Arthur Veryan | Solid boundary surface for contact with a relatively moving fluid medium |
US3578264A (en) * | 1968-07-09 | 1971-05-11 | Battelle Development Corp | Boundary layer control of flow separation and heat exchange |
US4354648A (en) * | 1980-02-06 | 1982-10-19 | Gates Learjet Corporation | Airstream modification device for airfoils |
DE3023466C2 (en) * | 1980-06-24 | 1982-11-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Device for reducing secondary flow losses in a bladed flow channel |
US4718620A (en) * | 1984-10-15 | 1988-01-12 | Braden John A | Terraced channels for reducing afterbody drag |
DE3521329A1 (en) * | 1985-06-14 | 1986-12-18 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Vortex generator and boundary layer deflector arrangement |
US5058837A (en) * | 1989-04-07 | 1991-10-22 | Wheeler Gary O | Low drag vortex generators |
FI115764B (en) * | 2003-11-03 | 2005-07-15 | Patria Finavicomp Oy | Arrangement for forming vortexes |
DE502004002003D1 (en) * | 2004-03-25 | 2006-12-28 | Rolls Royce Deutschland | Compressor for an aircraft engine |
US20070018055A1 (en) * | 2005-07-11 | 2007-01-25 | Schmidt Eric T | Aerodynamically efficient surface |
GB0514338D0 (en) * | 2005-07-13 | 2005-08-17 | Univ City | Control of fluid flow separation |
US8528601B2 (en) * | 2009-03-30 | 2013-09-10 | The Regents Of The University Of Michigan | Passive boundary layer control elements |
-
2012
- 2012-07-06 US US13/542,673 patent/US20130037657A1/en not_active Abandoned
- 2012-07-06 CN CN2012103194688A patent/CN102865274A/en active Pending
- 2012-07-06 CN CN2012204422441U patent/CN202937553U/en not_active Expired - Fee Related
- 2012-07-06 WO PCT/US2012/045828 patent/WO2013009646A2/en active Application Filing
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050163963A1 (en) * | 2004-01-12 | 2005-07-28 | Munro Alexander S. | Method and apparatus for reducing drag and noise for a vehicle |
DE102008022504A1 (en) * | 2008-05-07 | 2009-11-19 | Eads Deutschland Gmbh | Switchable vortex generator e.g. turbulator, for aircraft, has vortex generating element movable back and forth between two different positions, where vortex generating element is designed as profile element with profile structure |
US20110262705A1 (en) * | 2011-03-30 | 2011-10-27 | General Electric Company Global Research | Microstructures for reducing noise of a fluid dynamic structure |
Also Published As
Publication number | Publication date |
---|---|
CN102865274A (en) | 2013-01-09 |
CN202937553U (en) | 2013-05-15 |
US20130037657A1 (en) | 2013-02-14 |
WO2013009646A2 (en) | 2013-01-17 |
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