JP2006170209A - 自動心出し回転アクチュエータリングによって作動されるステータ翼ステージ - Google Patents

自動心出し回転アクチュエータリングによって作動されるステータ翼ステージ Download PDF

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Publication number
JP2006170209A
JP2006170209A JP2005361306A JP2005361306A JP2006170209A JP 2006170209 A JP2006170209 A JP 2006170209A JP 2005361306 A JP2005361306 A JP 2005361306A JP 2005361306 A JP2005361306 A JP 2005361306A JP 2006170209 A JP2006170209 A JP 2006170209A
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JP
Japan
Prior art keywords
casing
moving device
stage
wing
actuator ring
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
Application number
JP2005361306A
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English (en)
Japanese (ja)
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JP2006170209A5 (https=
Inventor
Michel Andre Bouru
ミシエル・アンドレ・ブリユ
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of JP2006170209A publication Critical patent/JP2006170209A/ja
Publication of JP2006170209A5 publication Critical patent/JP2006170209A5/ja
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/56Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162Final 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/90Variable geometry
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2005361306A 2004-12-16 2005-12-15 自動心出し回転アクチュエータリングによって作動されるステータ翼ステージ Pending JP2006170209A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0413387A FR2879686B1 (fr) 2004-12-16 2004-12-16 Turbomachine a stator comportant un etage d'aubes de redresseur actionnees par une couronne rotative a centrage automatique

Publications (2)

Publication Number Publication Date
JP2006170209A true JP2006170209A (ja) 2006-06-29
JP2006170209A5 JP2006170209A5 (https=) 2009-04-09

Family

ID=34952058

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005361306A Pending JP2006170209A (ja) 2004-12-16 2005-12-15 自動心出し回転アクチュエータリングによって作動されるステータ翼ステージ

Country Status (7)

Country Link
US (2) US7300245B2 (https=)
EP (1) EP1672223A3 (https=)
JP (1) JP2006170209A (https=)
CN (1) CN100547228C (https=)
CA (1) CA2530137C (https=)
FR (1) FR2879686B1 (https=)
RU (1) RU2416724C2 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013096341A (ja) * 2011-11-02 2013-05-20 Mitsubishi Heavy Ind Ltd 軸流流体機械、及びその可変静翼駆動装置

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2902454A1 (fr) 2006-06-16 2007-12-21 Snecma Sa Stator de turbomachine comportant un etage d'aubes de redresseurs actionnees par une couronne rotative a centrage automatique
FR2922257B1 (fr) * 2007-10-12 2014-03-28 Snecma Perfectionnement a un anneau de commande de calage des aubes fixes d'une turbomachine
US8864449B2 (en) 2010-11-02 2014-10-21 Hamilton Sundstrand Corporation Drive ring bearing for compressor diffuser assembly
RU2470834C1 (ru) * 2011-07-27 2012-12-27 Николай Борисович Болотин Летательный аппарат
CN102373965B (zh) * 2011-11-24 2015-12-02 成都发动机(集团)有限公司 高温高尘含量烟气轮机可调式静叶组件
FR2983924B1 (fr) * 2011-12-09 2013-11-22 Snecma Carter annulaire pour un compresseur de turbomachine
US8920109B2 (en) * 2013-03-12 2014-12-30 Siemens Aktiengesellschaft Vane carrier thermal management arrangement and method for clearance control
US9932851B2 (en) 2013-12-30 2018-04-03 Rolls-Royce North American Technologies, Inc. Active synchronizing ring
US9644491B2 (en) 2014-06-13 2017-05-09 Pratt & Whitney Canada Corp. Single bolting flange arrangement for variable guide vane connection
DE102016122639A1 (de) * 2016-11-23 2018-05-24 Rolls-Royce Deutschland Ltd & Co Kg Leitschaufelbaugruppe mit Ausgleichseinrichtung
FR3063779B1 (fr) * 2017-03-07 2022-11-04 Safran Aircraft Engines Anneau de commande de calage d'un etage d'aube d'un stator
US10724543B2 (en) 2017-08-11 2020-07-28 Raytheon Technologies Corporation Bridge bracket for variable-pitch vane system
GB201803649D0 (en) * 2018-03-07 2018-04-25 Rolls Royce Plc A variable vane actuation arrangement
US11092167B2 (en) * 2018-08-28 2021-08-17 Pratt & Whitney Canada Corp. Variable vane actuating system
US11092032B2 (en) * 2018-08-28 2021-08-17 Pratt & Whitney Canada Corp. Variable vane actuating system
US11149567B2 (en) * 2018-09-17 2021-10-19 Rolls-Royce Corporation Ceramic matrix composite load transfer roller joint
US11578611B2 (en) * 2020-11-26 2023-02-14 Pratt & Whitney Canada Corp. Variable guide vane assembly and bushings therefor
US11371380B2 (en) 2020-12-01 2022-06-28 Pratt & Whitney Canada Corp. Variable guide vane assembly and vane arms therefor
FR3119859B1 (fr) * 2021-02-15 2024-01-12 Safran Aircraft Engines Anneau de commande d’un etage d’aubes a calage variable pour une turbomachine
CN115507063A (zh) * 2021-06-22 2022-12-23 中国航发商用航空发动机有限责任公司 压气机的静叶调节机构和压气机
CN115704400B (zh) * 2021-08-16 2025-11-25 中国航发商用航空发动机有限责任公司 可调静子叶片调节机构及包含其的航空发动机
FR3127782B1 (fr) * 2021-10-04 2024-04-05 Safran Aircraft Engines Patin de guidage pour un anneau de transmission d’un système de commande de vannes de décharge d’une turbomachine pour aéronef, système de commande et turbomachine
CN116255358B (zh) * 2023-02-27 2024-11-05 中国航发湖南动力机械研究所 一种压气机调节机构的支撑限位装置
EP4534806A1 (fr) * 2023-10-02 2025-04-09 Safran Aero Boosters Dispositif de commande de calage d'aubes d'une grille d'aubes à calage variable de turbomachine d'aéronef

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02215936A (ja) * 1988-12-21 1990-08-28 United Technol Corp <Utc> 調節自在スペーサ
JPH04107500U (ja) * 1991-02-27 1992-09-17 三菱重工業株式会社 軸流送風機または圧縮機
JP2002005096A (ja) * 2000-06-20 2002-01-09 Mitsubishi Heavy Ind Ltd 軸流圧縮機、及び、ガスタービン
JP2004124942A (ja) * 2002-09-30 2004-04-22 United Technol Corp <Utc> バンパーシステム

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FR965869A (https=) * 1950-09-23
US2933234A (en) * 1954-12-28 1960-04-19 Gen Electric Compressor stator assembly
CH363661A (de) * 1958-02-14 1962-08-15 Int Stal Company Ab Verbindung zwischen zwei ringförmigen Maschinenelementen
CH558477A (de) * 1972-11-27 1975-01-31 Bbc Sulzer Turbomaschinen Verstellvorrichtung fuer drehbare leitschaufeln.
US3990809A (en) * 1975-07-24 1976-11-09 United Technologies Corporation High ratio actuation linkage
CA1034509A (en) * 1975-10-14 1978-07-11 Westinghouse Canada Limited Vane rotator assembly for a gas turbine
GB1499531A (en) * 1976-05-24 1978-02-01 Secr Defence Apparatus for varying the incidence of turbomachinery stator blades
GB2078865B (en) * 1980-06-28 1983-06-08 Rolls Royce A variable stator vane operating mechanism for a gas turbine engine
US4373859A (en) * 1981-09-23 1983-02-15 General Motors Corporation Unison ring support system
US4755104A (en) * 1986-04-29 1988-07-05 United Technologies Corporation Stator vane linkage
SU1649875A1 (ru) * 1987-05-22 1996-05-20 Производственное Объединение "Турбомоторный Завод" Им.К.Е.Ворошилова Механизм для поворота лопаток направляющего аппарата
DE69010519T2 (de) * 1989-02-02 1994-11-10 Hitachi Ltd Leitschaufel-Regler.
US4979874A (en) * 1989-06-19 1990-12-25 United Technologies Corporation Variable van drive mechanism

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02215936A (ja) * 1988-12-21 1990-08-28 United Technol Corp <Utc> 調節自在スペーサ
JPH04107500U (ja) * 1991-02-27 1992-09-17 三菱重工業株式会社 軸流送風機または圧縮機
JP2002005096A (ja) * 2000-06-20 2002-01-09 Mitsubishi Heavy Ind Ltd 軸流圧縮機、及び、ガスタービン
JP2004124942A (ja) * 2002-09-30 2004-04-22 United Technol Corp <Utc> バンパーシステム

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013096341A (ja) * 2011-11-02 2013-05-20 Mitsubishi Heavy Ind Ltd 軸流流体機械、及びその可変静翼駆動装置
US9309897B2 (en) 2011-11-02 2016-04-12 Mitsubishi Hitachi Power Systems, Ltd. Axial-flow fluid machinery, and variable vane drive device thereof

Also Published As

Publication number Publication date
EP1672223A2 (fr) 2006-06-21
FR2879686A1 (fr) 2006-06-23
CN100547228C (zh) 2009-10-07
CA2530137C (fr) 2013-07-23
USRE42523E1 (en) 2011-07-05
CA2530137A1 (fr) 2006-06-16
US20060133925A1 (en) 2006-06-22
FR2879686B1 (fr) 2007-04-06
EP1672223A3 (fr) 2014-01-22
US7300245B2 (en) 2007-11-27
RU2005139358A (ru) 2007-06-20
CN1804376A (zh) 2006-07-19
RU2416724C2 (ru) 2011-04-20

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