NZ710406A - Energy efficiency improvements for turbomachinery - Google Patents

Energy efficiency improvements for turbomachinery

Info

Publication number
NZ710406A
NZ710406A NZ710406A NZ71040613A NZ710406A NZ 710406 A NZ710406 A NZ 710406A NZ 710406 A NZ710406 A NZ 710406A NZ 71040613 A NZ71040613 A NZ 71040613A NZ 710406 A NZ710406 A NZ 710406A
Authority
NZ
New Zealand
Prior art keywords
flow
vortex
fluid
streaming
rearward
Prior art date
Application number
NZ710406A
Inventor
Peter Ireland
Anthony Ireland
Original Assignee
Peter Ireland
Anthony Ireland
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 Peter Ireland, Anthony Ireland filed Critical Peter Ireland
Publication of NZ710406A publication Critical patent/NZ710406A/en

Links

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
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F04D29/684—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid injection
    • 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38—Blades
    • 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
    • F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
    • 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
    • F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
    • 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
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
    • 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
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/183—Two-dimensional patterned zigzag
    • 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
    • F15D1/02—Influencing flow of fluids in pipes or conduits
    • F15D1/06—Influencing flow of fluids in pipes or conduits by influencing the boundary layer
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)

Abstract

System and method for controlling flow in turbo machinery. The method provides an input source of fluid-flow; and a fluid-flow modifying surface that has at least one conformal vortex generator. A portion of the fluid-flow is conveyed to the fluid-flow modifying surface. The conformal vortex generator then provides a flow-angled step-down that rolls up a portion of the bottom-most boundary layer of the incoming fluid-flow, and communicates this processed part into an output fluid interface means. The output fluid interface is itself provided as a step-vortex that feeds into a rearward streaming tip-vortex filament. The rearward streaming tip-vortex filament is tightly bound onto an output surface and/or the rearward streaming tip-vortex filament provides a re-laminarization effect on the output surface downstream of the flow-angled step-down that is adjacent to said rearward streaming tip-vortex filament. In this manner, flow is controlled as the conformal vortex generator reduces downstream flow separation and/or thins a downstream boundary layer. Prior art Vortex Generators have high drag (e.g. protruding ramp types) are structurally delicate, do not produce persistent and submerged vortices (e.g. dimples) or vortices subject to secondary flows and effects. Prior art active flow control devices are generally more complex and do not exhibit significant reduction over baseline unmodified geometry
NZ710406A 2013-01-25 2013-01-25 Energy efficiency improvements for turbomachinery NZ710406A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2013/050676 WO2014114988A1 (en) 2013-01-25 2013-01-25 Energy efficiency improvements for turbomachinery

Publications (1)

Publication Number Publication Date
NZ710406A true NZ710406A (en) 2017-11-24

Family

ID=51226975

Family Applications (1)

Application Number Title Priority Date Filing Date
NZ710406A NZ710406A (en) 2013-01-25 2013-01-25 Energy efficiency improvements for turbomachinery

Country Status (9)

Country Link
EP (1) EP2948369A4 (en)
JP (1) JP2016509651A (en)
CN (1) CN105307931A (en)
AU (1) AU2013375126A1 (en)
BR (1) BR112015017808A2 (en)
CA (1) CA2899238A1 (en)
NZ (1) NZ710406A (en)
RU (1) RU2642203C2 (en)
WO (1) WO2014114988A1 (en)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104462768B (en) * 2014-11-06 2017-08-01 上海电气电站设备有限公司 The efficiency and power consumption of a kind of large turbo-type generator aerofoil fan determine method
US10132498B2 (en) 2015-01-20 2018-11-20 United Technologies Corporation Thermal barrier coating of a combustor dilution hole
EP3354904B1 (en) 2015-04-08 2020-09-16 Horton, Inc. Fan blade surface features
US10507906B2 (en) 2015-04-28 2019-12-17 The Boeing Company Aerodynamic surface assembly defining a fluidic actuation orifice
AU2016338382B2 (en) * 2015-09-02 2021-04-01 Jetoptera, Inc. Ejector and airfoil configurations
US10450867B2 (en) 2016-02-12 2019-10-22 General Electric Company Riblets for a flowpath surface of a turbomachine
CN105841191B (en) * 2016-03-30 2018-07-06 中国科学院工程热物理研究所 A kind of V-flame stabilizer trailing edge structures
CN106226044B (en) * 2016-07-06 2018-12-14 浙江大学宁波理工学院 A kind of Reliable Evaluating Methods of Their Performance of marine tidal-current energy capture blade
US11286787B2 (en) 2016-09-15 2022-03-29 Raytheon Technologies Corporation Gas turbine engine airfoil with showerhead cooling holes near leading edge
CN106564585B (en) * 2016-10-26 2019-12-10 北京航空航天大学 High-performance deep stall wing structure and aircraft
EP3330614B1 (en) 2016-11-30 2019-10-02 Ansaldo Energia Switzerland AG Vortex generating device
WO2018129721A1 (en) * 2017-01-13 2018-07-19 深圳市大疆创新科技有限公司 Propeller of aircraft, power set and unmanned aerial vehicle
DE112017006296B4 (en) * 2017-01-24 2023-02-02 Hitachi, Ltd. FLUID DEVICE
US20200063718A1 (en) * 2017-02-17 2020-02-27 Mhi Vestas Offshore Wind A/S Leading edge protection of a wind turbine blade
US11701616B2 (en) 2017-09-22 2023-07-18 Dehlsen Associates Of The Pacific Limited Sorbent emitter for direct air capture of carbon dioxide
WO2019087236A1 (en) * 2017-10-30 2019-05-09 株式会社Ｑｐｓ研究所 Reflector, developed antenna, and aerospace vehicle
US11053888B2 (en) * 2017-11-01 2021-07-06 The Boeing Company Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode
CN108216617B (en) * 2017-12-29 2020-04-24 厦门大学 Method for suppressing helicopter propeller-vortex interference noise
CN109236731B (en) * 2018-10-18 2020-08-28 江苏大学 Wear-resistant blade based on coupling bionic optimization
CN109726440B (en) * 2018-12-04 2023-04-18 中国航空工业集团公司西安飞机设计研究所 Aeroelasticity analysis method considering dynamic characteristics of internal fluid
ES2767024B2 (en) * 2018-12-14 2021-09-17 Univ Sevilla VORTE GENERATOR DEVICE IN CHANNELS OR DUCTS
CN109649642B (en) * 2018-12-21 2022-04-12 中国航天空气动力技术研究院 Control device for inhibiting shear flow density pulsation
US11645043B2 (en) * 2019-02-11 2023-05-09 Dynatrace Llc Method and system for calculating minwise hash signatures from weighted sets
CN109895983A (en) * 2019-03-20 2019-06-18 西北工业大学 A kind of sawtooth trailing edge denoising structure suitable for ducted propeller
FR3103215B1 (en) * 2019-11-20 2021-10-15 Safran Aircraft Engines Turbomachine rotary fan blade, fan and turbomachine fitted therewith
EP3842336B1 (en) * 2019-12-27 2023-06-28 Bombardier Inc. Variable wing leading edge camber
US11686208B2 (en) 2020-02-06 2023-06-27 Rolls-Royce Corporation Abrasive coating for high-temperature mechanical systems
RU2742558C1 (en) * 2020-05-11 2021-02-08 Общество С Ограниченной Ответственностью "Биопрактика" Device for degassing of liquid media
CN113932249B (en) * 2020-06-29 2022-10-18 中国航发商用航空发动机有限责任公司 Combustion chamber and pre-diffuser
CN112084725B (en) * 2020-09-09 2022-06-24 中自环保科技股份有限公司 Method for evaluating performance of SCR mixer of diesel internal combustion engine
CN112555556A (en) * 2020-10-27 2021-03-26 中国原子能科学研究院 Inverted tooth type throttling element
CN112253314A (en) * 2020-11-10 2021-01-22 上海海事大学 Gas turbine fan and compressor blade drag reduction structure based on shark gill jet flow
RU2753586C1 (en) * 2020-12-02 2021-08-18 Сергей Николаевич Низов Group of vortex generators and method for installing vortex generators
CN112696710B (en) * 2020-12-29 2022-11-22 中国航发沈阳发动机研究所 Method and system for determining size of mixing hole of flame tube with funnel
CN113153868B (en) * 2021-03-17 2022-12-09 太原理工大学 Method for enhancing robustness of turbulent industrial fluid
CN112977713B (en) * 2021-04-07 2021-12-21 浙江海洋大学 Vortex generator for propeller type ship and ship
CN113190786B (en) * 2021-05-13 2024-03-15 岳聪 Vibration prediction method for large-scale rotating equipment by utilizing multidimensional assembly parameters
FR3123380A1 (en) * 2021-05-28 2022-12-02 Safran Aircraft Engines Improved leading edge shield
EP4112451A1 (en) * 2021-06-28 2023-01-04 BAE SYSTEMS plc Duct arrangement and method
CA3222957A1 (en) * 2021-06-28 2023-01-05 Bae Systems Plc Duct arrangement and method
US20230034004A1 (en) * 2021-07-29 2023-02-02 General Electric Company Mixer vanes
CN114738054B (en) * 2022-05-20 2023-05-02 西北工业大学 Design method of bionic turbine blade of aero-engine
CN115355369A (en) * 2022-08-26 2022-11-18 武汉理工大学 Water pipeline connecting device based on bionic principle and installation method
CN116658451B (en) * 2023-08-02 2023-10-03 中国航发四川燃气涡轮研究院 Method for correcting total pressure of outlet of air compressor in core machine environment based on wake loss
CN117408187B (en) * 2023-12-14 2024-03-01 中国科学院合肥物质科学研究院 Guide structure for controlling cavitation of hydraulic machinery

Family Cites Families (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899150A (en) * 1959-08-11 Bound vortex skin
US2800291A (en) * 1950-10-24 1957-07-23 Stephens Arthur Veryan Solid boundary surface for contact with a relatively moving fluid medium
US3779199A (en) * 1969-09-25 1973-12-18 R Mayer Boundary layer control means
US4852355A (en) * 1980-12-22 1989-08-01 General Electric Company Dispensing arrangement for pressurized air
US4434957A (en) * 1982-03-30 1984-03-06 Rolls-Royce Incorporated Low drag surface
DE3325663C2 (en) * 1983-07-15 1985-08-22 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Axial flow through a blade grille of a gas or steam powered turbine
DE3342421A1 (en) * 1983-11-24 1985-06-05 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn METHOD FOR THE STABILIZING INFLUENCE OF DETACHED LAMINARY BORDER LAYERS
GB8626371D0 (en) * 1986-11-04 1987-03-18 British Aerospace Aerodynamic/hydrodynamic surfaces
US5088665A (en) * 1989-10-31 1992-02-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Serrated trailing edges for improving lift and drag characteristics of lifting surfaces
US4984626A (en) * 1989-11-24 1991-01-15 Carrier Corporation Embossed vortex generator enhanced plate fin
US5598990A (en) * 1994-12-15 1997-02-04 University Of Kansas Center For Research Inc. Supersonic vortex generator
RU2094313C1 (en) * 1995-04-20 1997-10-27 Виктор Павлович Винокуров Lifting surface
US6820430B1 (en) * 1999-07-12 2004-11-23 Bruce A. Tassone Method and apparatus for providing evaporative cooling and power augmentation in gas turbines
GB0001399D0 (en) * 2000-01-22 2000-03-08 Rolls Royce Plc An aerofoil for an axial flow turbomachine
US7048505B2 (en) * 2002-06-21 2006-05-23 Darko Segota Method and system for regulating fluid flow over an airfoil or a hydrofoil
US6629674B1 (en) * 2002-07-24 2003-10-07 General Electric Company Method and apparatus for modulating airfoil lift
DE10237341A1 (en) * 2002-08-14 2004-02-26 Siemens Ag Finite vortex model for use in fluid flow numerical simulation, especially for modeling unsteady flows, whereby a general roll-off model is used to model the finite edge vortex
DE102005054248A1 (en) * 2005-11-15 2007-05-24 Airbus Deutschland Gmbh Braking flap for deceleration of aircraft against air-flow which surrounds aircraft, comprises many vortex edges, which resolve individual edge section into number of vortex part, are arranged at free edge
US7748958B2 (en) * 2006-12-13 2010-07-06 The Boeing Company Vortex generators on rotor blades to delay an onset of large oscillatory pitching moments and increase maximum lift
US8016567B2 (en) * 2007-01-17 2011-09-13 United Technologies Corporation Separation resistant aerodynamic article
JP5474279B2 (en) * 2007-03-06 2014-04-16 株式会社Ｉｈｉ Cooling turbine blade
US7900871B2 (en) * 2007-07-20 2011-03-08 Textron Innovations, Inc. Wing leading edge having vortex generators
US20100008759A1 (en) * 2008-07-10 2010-01-14 General Electric Company Methods and apparatuses for providing film cooling to turbine components
DE102008033861A1 (en) * 2008-07-19 2010-01-21 Mtu Aero Engines Gmbh Shovel of a turbomachine with vortex generator
US20110006165A1 (en) * 2009-07-10 2011-01-13 Peter Ireland Application of conformal sub boundary layer vortex generators to a foil or aero/ hydrodynamic surface
US8656957B2 (en) * 2009-09-30 2014-02-25 The Board Of Trustees Of The University Of Illinois Vortex generators to control boundary layer interactions
JP2011163123A (en) * 2010-02-04 2011-08-25 Ihi Corp Turbine moving blade
US8453445B2 (en) * 2010-04-19 2013-06-04 Honeywell International Inc. Axial turbine with parallel flow compressor
US8434723B2 (en) * 2010-06-01 2013-05-07 Applied University Research, Inc. Low drag asymmetric tetrahedral vortex generators
US8690536B2 (en) * 2010-09-28 2014-04-08 Siemens Energy, Inc. Turbine blade tip with vortex generators
US9435537B2 (en) * 2010-11-30 2016-09-06 General Electric Company System and method for premixer wake and vortex filling for enhanced flame-holding resistance
US8820084B2 (en) * 2011-06-28 2014-09-02 Siemens Aktiengesellschaft Apparatus for controlling a boundary layer in a diffusing flow path of a power generating machine
US8657238B2 (en) * 2011-07-05 2014-02-25 The Boeing Company Retractable vortex generator for reducing stall speed
CN102705264A (en) * 2012-06-15 2012-10-03 美的集团有限公司 Axial flow wind wheel

Also Published As

Publication number Publication date
WO2014114988A1 (en) 2014-07-31
RU2642203C2 (en) 2018-01-24
CN105307931A (en) 2016-02-03
EP2948369A1 (en) 2015-12-02
AU2013375126A1 (en) 2015-08-13
BR112015017808A2 (en) 2017-07-11
CA2899238A1 (en) 2014-07-31
JP2016509651A (en) 2016-03-31
EP2948369A4 (en) 2017-01-18
RU2015131056A (en) 2017-02-28

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