EP2110559A3 - Turbomachine avec réinjection de fluide pour influencer la couche limite - Google Patents

Turbomachine avec réinjection de fluide pour influencer la couche limite Download PDF

Info

Publication number
EP2110559A3
EP2110559A3 EP09003693.0A EP09003693A EP2110559A3 EP 2110559 A3 EP2110559 A3 EP 2110559A3 EP 09003693 A EP09003693 A EP 09003693A EP 2110559 A3 EP2110559 A3 EP 2110559A3
Authority
EP
European Patent Office
Prior art keywords
fluid
injection
influence
boundary layer
turbo machine
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.)
Granted
Application number
EP09003693.0A
Other languages
German (de)
English (en)
Other versions
EP2110559B1 (fr
EP2110559A2 (fr
Inventor
Volker Dr. Gümmer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
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 Rolls Royce Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Publication of EP2110559A2 publication Critical patent/EP2110559A2/fr
Publication of EP2110559A3 publication Critical patent/EP2110559A3/fr
Application granted granted Critical
Publication of EP2110559B1 publication Critical patent/EP2110559B1/fr
Ceased legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
    • F04D29/542—Bladed diffusers
    • 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
    • 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
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP09003693.0A 2008-04-18 2009-03-13 Turbomachine avec réinjection de fluide pour influencer la couche limite Ceased EP2110559B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102008019603A DE102008019603A1 (de) 2008-04-18 2008-04-18 Strömungsmaschine mit schaufelreiheninterner Fluid-Rückführung

Publications (3)

Publication Number Publication Date
EP2110559A2 EP2110559A2 (fr) 2009-10-21
EP2110559A3 true EP2110559A3 (fr) 2015-03-25
EP2110559B1 EP2110559B1 (fr) 2018-12-12

Family

ID=40474926

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09003693.0A Ceased EP2110559B1 (fr) 2008-04-18 2009-03-13 Turbomachine avec réinjection de fluide pour influencer la couche limite

Country Status (3)

Country Link
US (1) US8043046B2 (fr)
EP (1) EP2110559B1 (fr)
DE (1) DE102008019603A1 (fr)

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DE102008011746A1 (de) * 2008-02-28 2009-09-03 Mtu Aero Engines Gmbh Vorrichtung und Verfahren zur Umleitung eines Leckagestroms
FR2931886B1 (fr) * 2008-05-29 2011-10-14 Snecma Collecteur d'air dans une turbomachine.
DE102008029605A1 (de) * 2008-06-23 2009-12-24 Rolls-Royce Deutschland Ltd & Co Kg Schaufeldeckband mit Durchlass
DE102008036294A1 (de) * 2008-08-04 2010-02-11 Mtu Aero Engines Gmbh Axialverdichter mit Verdichtergitter
DE102008060424A1 (de) * 2008-12-04 2010-06-10 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine mit Seitenwand-Grenzschicht-Barriere
US9068507B2 (en) * 2011-11-16 2015-06-30 General Electric Company Compressor having purge circuit and method of purging
CN102556345B (zh) * 2012-01-18 2016-04-13 朱晓义 飞机动力装置
KR101790421B1 (ko) 2013-01-23 2017-10-25 컨셉츠 이티아이 인코포레이티드 터보머신들의 인접한 블레이드 요소들의 흐름장들의 결합을 가하는 구조들 및 방법들, 그리고 그들을 포함하는 터보머신들
DE102013210167A1 (de) * 2013-05-31 2014-12-04 Rolls-Royce Deutschland Ltd & Co Kg Strukturbaugruppe für eine Strömungsmaschine
DE102013210169A1 (de) * 2013-05-31 2014-12-04 Rolls-Royce Deutschland Ltd & Co Kg Strukturbaugruppe für eine Strömungsmaschine
DE102013222514A1 (de) 2013-11-06 2015-05-07 MTU Aero Engines AG Dichtungsanordnung für eine Strömungsmaschine
EP2871368B1 (fr) 2013-11-12 2018-09-12 MTU Aero Engines GmbH Compresseur de turbine à gaz
EP2881548B1 (fr) * 2013-12-09 2018-08-15 MTU Aero Engines GmbH Compresseur de turbine à gaz
WO2015200533A1 (fr) 2014-06-24 2015-12-30 Concepts Eti, Inc. Structures de commande d'écoulement pour turbomachines et procédés de conception associés
DE102015110252A1 (de) * 2015-06-25 2016-12-29 Rolls-Royce Deutschland Ltd & Co Kg Statorvorrichtung für eine Strömungsmaschine mit einer Gehäuseeinrichtung und mehreren Leitschaufeln
DE102015110249A1 (de) * 2015-06-25 2017-01-12 Rolls-Royce Deutschland Ltd & Co Kg Statorvorrichtung für eine Strömungsmaschine mit einer Gehäuseeinrichtung und mehreren Leitschaufeln
DE102015110250A1 (de) * 2015-06-25 2016-12-29 Rolls-Royce Deutschland Ltd & Co Kg Statorvorrichtung für eine Strömungsmaschine mit einer Gehäuseeinrichtung und mehreren Leitschaufeln
US10041500B2 (en) * 2015-12-08 2018-08-07 General Electric Company Venturi effect endwall treatment
CN107150788A (zh) * 2017-04-26 2017-09-12 朱晓义 一种产生更大升力的固定翼飞行器
DE102017118950A1 (de) * 2017-08-18 2019-02-21 Abb Turbo Systems Ag Diffusor für einen Radialverdichter
FR3082558B1 (fr) * 2018-06-15 2021-09-17 Safran Aircraft Engines Distributeur de turbine pour turbomachine, comprenant un systeme passif de reintroduction de gaz de fuite dans une veine d'ecoulement des gaz
FR3084395B1 (fr) * 2018-07-24 2020-10-30 Safran Aircraft Engines Ailettes entrefer pour compresseur de turbomachine
US10876549B2 (en) 2019-04-05 2020-12-29 Pratt & Whitney Canada Corp. Tandem stators with flow recirculation conduit
FR3107917B1 (fr) * 2020-03-04 2022-09-09 Safran Carter de roue mobile pour turbomachine
FR3109959B1 (fr) * 2020-05-06 2022-04-22 Safran Helicopter Engines Compresseur de turbomachine comportant une paroi fixe pourvue d’un traitement de forme
JP2023536998A (ja) 2020-08-07 2023-08-30 コンセプツ エヌアールイーシー，エルエルシー 性能を向上させるための流量制御構造及び当該流量制御構造を組み込んだターボ機械
US11732612B2 (en) 2021-12-22 2023-08-22 Rolls-Royce North American Technologies Inc. Turbine engine fan track liner with tip injection air recirculation passage
US11702945B2 (en) 2021-12-22 2023-07-18 Rolls-Royce North American Technologies Inc. Turbine engine fan case with tip injection air recirculation passage
US11946379B2 (en) 2021-12-22 2024-04-02 Rolls-Royce North American Technologies Inc. Turbine engine fan case with manifolded tip injection air recirculation passages
FR3133063B1 (fr) * 2022-02-25 2024-08-02 Safran Aircraft Engines Aubage de turbomachine, comprenant une pale et une plateforme qui présente un canal interne d’aspiration et d’éjection de flux
FR3152831A1 (fr) * 2023-09-11 2025-03-14 Safran Aircraft Engines Aubage de turbomachine
US12146413B1 (en) 2023-12-12 2024-11-19 Rolls-Royce North American Technologies Inc. Circumferentially variable flow control in fan outlet guide vane assemblies for distortion management and stall margin in gas turbine engines
US12258870B1 (en) 2024-03-08 2025-03-25 Rolls-Royce North American Technologies Inc. Adjustable fan track liner with slotted array active fan tip treatment for distortion tolerance
US12286936B1 (en) 2024-05-09 2025-04-29 Rolls-Royce North American Technologies Inc. Adjustable fan track liner with groove array active fan tip treatment for distortion tolerance
US12209541B1 (en) 2024-05-09 2025-01-28 Rolls-Royce North American Technologies Inc. Adjustable fan track liner with dual slotted array active fan tip treatment for distortion tolerance
US12215712B1 (en) 2024-05-09 2025-02-04 Rolls-Royce North American Technologies Inc. Adjustable fan track liner with dual grooved array active fan tip treatment for distortion tolerance
US12168983B1 (en) 2024-06-28 2024-12-17 Rolls-Royce North American Technologies Inc. Active fan tip treatment using rotating drum array in fan track liner with axial and circumferential channels for distortion tolerance
US12209502B1 (en) 2024-06-28 2025-01-28 Rolls-Royce North American Technologies Inc. Active fan tip treatment using rotating drum array with axial channels in fan track liner for distortion tolerance

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH204331A (de) * 1937-02-24 1939-04-30 Rheinmetall Borsig Ag Einrichtung zur Verhinderung der Strahlablösung bei Turboverdichtern.
US4146352A (en) * 1975-10-31 1979-03-27 Hitachi, Ltd. Diaphragms for axial flow fluid machines
EP0497574A1 (fr) * 1991-01-30 1992-08-05 United Technologies Corporation Virole avec canaux de récirculation pour soufflante
EP1286022A1 (fr) * 2001-08-14 2003-02-26 United Technologies Corporation Traitement de l'enveloppe pour compresseurs
EP1609999A2 (fr) * 2004-06-24 2005-12-28 Rolls-Royce Deutschland Ltd & Co KG Turbo machine
EP1659293A2 (fr) * 2004-11-17 2006-05-24 Rolls-Royce Deutschland Ltd & Co KG Turbomachine
EP1382855B1 (fr) * 2002-07-20 2006-10-25 Rolls-Royce Deutschland Ltd & Co KG Turbomachine avec système de recirculation de fluide intégré

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US5431533A (en) * 1993-10-15 1995-07-11 United Technologies Corporation Active vaned passage casing treatment
US5474417A (en) * 1994-12-29 1995-12-12 United Technologies Corporation Cast casing treatment for compressor blades
US5607284A (en) * 1994-12-29 1997-03-04 United Technologies Corporation Baffled passage casing treatment for compressor blades
US6220012B1 (en) * 1999-05-10 2001-04-24 General Electric Company Booster recirculation passageway and methods for recirculating air
US7186072B2 (en) * 2002-08-23 2007-03-06 Mtu Aero Engines Gmbh Recirculation structure for a turbocompressor
DE10355240A1 (de) * 2003-11-26 2005-07-07 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidentnahme
GB2413158B (en) * 2004-04-13 2006-08-16 Rolls Royce Plc Flow control arrangement
DE102007012119A1 (de) * 2007-03-13 2008-09-18 Rolls-Royce Deutschland Ltd & Co Kg Drosselgradabhängige Schaufelverstellung bei Strömungsarbeitsmaschinen

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH204331A (de) * 1937-02-24 1939-04-30 Rheinmetall Borsig Ag Einrichtung zur Verhinderung der Strahlablösung bei Turboverdichtern.
US4146352A (en) * 1975-10-31 1979-03-27 Hitachi, Ltd. Diaphragms for axial flow fluid machines
EP0497574A1 (fr) * 1991-01-30 1992-08-05 United Technologies Corporation Virole avec canaux de récirculation pour soufflante
EP1286022A1 (fr) * 2001-08-14 2003-02-26 United Technologies Corporation Traitement de l'enveloppe pour compresseurs
EP1382855B1 (fr) * 2002-07-20 2006-10-25 Rolls-Royce Deutschland Ltd & Co KG Turbomachine avec système de recirculation de fluide intégré
EP1609999A2 (fr) * 2004-06-24 2005-12-28 Rolls-Royce Deutschland Ltd & Co KG Turbo machine
EP1659293A2 (fr) * 2004-11-17 2006-05-24 Rolls-Royce Deutschland Ltd & Co KG Turbomachine

Also Published As

Publication number Publication date
US8043046B2 (en) 2011-10-25
EP2110559B1 (fr) 2018-12-12
DE102008019603A1 (de) 2009-10-22
EP2110559A2 (fr) 2009-10-21
US20090263233A1 (en) 2009-10-22

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