DE102011053433A1 - Verstell-Leitapparatanordnung für einen Turbinenverdichter - Google Patents
Verstell-Leitapparatanordnung für einen Turbinenverdichter Download PDFInfo
- Publication number
- DE102011053433A1 DE102011053433A1 DE102011053433A DE102011053433A DE102011053433A1 DE 102011053433 A1 DE102011053433 A1 DE 102011053433A1 DE 102011053433 A DE102011053433 A DE 102011053433A DE 102011053433 A DE102011053433 A DE 102011053433A DE 102011053433 A1 DE102011053433 A1 DE 102011053433A1
- Authority
- DE
- Germany
- Prior art keywords
- lever arms
- several
- adjustment
- leitapparatanordnung
- synchronizing 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
Links
Images
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
- F04D29/40—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
- 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
-
- 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
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/24—Three-dimensional ellipsoidal
- F05D2250/241—Three-dimensional ellipsoidal spherical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/892,269 US8714916B2 (en) | 2010-09-28 | 2010-09-28 | Variable vane assembly for a turbine compressor |
| US12/892,269 | 2010-09-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE102011053433A1 true DE102011053433A1 (de) | 2012-03-29 |
Family
ID=45804819
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE102011053433A Pending DE102011053433A1 (de) | 2010-09-28 | 2011-09-09 | Verstell-Leitapparatanordnung für einen Turbinenverdichter |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8714916B2 (enExample) |
| JP (1) | JP5941259B2 (enExample) |
| CN (1) | CN102418712B (enExample) |
| CH (1) | CH703871B1 (enExample) |
| DE (1) | DE102011053433A1 (enExample) |
Families Citing this family (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8668444B2 (en) * | 2010-09-28 | 2014-03-11 | General Electric Company | Attachment stud for a variable vane assembly of a turbine compressor |
| US8714916B2 (en) * | 2010-09-28 | 2014-05-06 | General Electric Company | Variable vane assembly for a turbine compressor |
| EP2525048A1 (en) * | 2011-05-18 | 2012-11-21 | Siemens Aktiengesellschaft | Drive lever arrangement |
| US20140023502A1 (en) * | 2012-07-20 | 2014-01-23 | General Electric Company | Variable vane assembly for turbine system |
| US9404384B2 (en) | 2012-09-12 | 2016-08-02 | United Technologies Corporation | Gas turbine engine synchronizing ring with multi-axis joint |
| US20140093362A1 (en) | 2012-09-28 | 2014-04-03 | United Technologies Corporation | Gas turbine engine components and method of assembly |
| JP6185781B2 (ja) | 2013-07-23 | 2017-08-23 | 三菱日立パワーシステムズ株式会社 | 軸流圧縮機 |
| JP5736443B1 (ja) | 2013-12-19 | 2015-06-17 | 川崎重工業株式会社 | 可変静翼機構 |
| US9932851B2 (en) | 2013-12-30 | 2018-04-03 | Rolls-Royce North American Technologies, Inc. | Active synchronizing ring |
| JP2017527733A (ja) | 2014-09-12 | 2017-09-21 | ゼネラル・エレクトリック・カンパニイ | 可変式出力ガイドベーンを備えた軸流−遠心圧縮機 |
| FR3027635B1 (fr) * | 2014-10-27 | 2016-11-04 | Snecma | Systeme de commande d'aubes a calage variable pour une turbomachine |
| FR3038666B1 (fr) * | 2015-07-09 | 2017-07-07 | Snecma | Anneau de commande d'aubes a calage variable pour une turbomachine |
| CN106640226A (zh) | 2015-10-30 | 2017-05-10 | 西门子公司 | 驱动环偏移感测系统、压气机及燃气轮机 |
| US10533436B2 (en) * | 2015-11-04 | 2020-01-14 | General Electric Company | Centerline-mounted hydraulic pitch change mechanism actuator |
| GB2557565A (en) * | 2016-07-18 | 2018-06-27 | Rolls Royce Plc | Variable stator vane mechanism |
| US10563670B2 (en) | 2016-07-29 | 2020-02-18 | Rolls-Royce Corporation | Vane actuation system for a gas turbine engine |
| GB201614803D0 (en) * | 2016-09-01 | 2016-10-19 | Rolls Royce Plc | Variable stator vane rigging |
| DE102016224523A1 (de) * | 2016-12-08 | 2018-06-14 | MTU Aero Engines AG | Leitschaufelverstellung mit seitlich montiertem Verstellhebel |
| US10815818B2 (en) * | 2017-07-18 | 2020-10-27 | Raytheon Technologies Corporation | Variable-pitch vane assembly |
| US11486304B2 (en) * | 2017-11-03 | 2022-11-01 | Borgwarner Inc. | Lever with pre-attached self locking nut for a variable turbine geometry turbocharger |
| US11002142B2 (en) * | 2019-01-21 | 2021-05-11 | Raytheon Technologies Corporation | Thermally compensated synchronization ring of a variable stator vane assembly |
| FR3099518B1 (fr) | 2019-07-31 | 2021-08-06 | Safran Aircraft Engines | Ensemble redresseur pour un compresseur de turbomachine |
| CN110529197B (zh) * | 2019-10-10 | 2024-09-17 | 兰州长城机械工程有限公司 | 一种适用于高温烟气轮机的可调静叶装置 |
| US11215117B2 (en) * | 2019-11-08 | 2022-01-04 | Raytheon Technologies Corporation | Gas turbine engine having electric motor applying power to the high pressure spool shaft and method for operating same |
| US20210254557A1 (en) * | 2020-02-13 | 2021-08-19 | Honeywell International Inc. | Variable vane system for turbomachine with linkage having tapered receiving aperture for unison ring pin |
| JP7431640B2 (ja) * | 2020-03-31 | 2024-02-15 | 川崎重工業株式会社 | ガスタービンエンジンのユニゾンリング |
| CN112065743B (zh) * | 2020-08-21 | 2025-01-28 | 山东钢铁股份有限公司 | 高炉轴流鼓风机可调式信号反馈连杆的使用方法 |
| CN112360815B (zh) * | 2020-11-10 | 2022-05-24 | 沈观清 | 用于多级涵道风扇的可调节定片机构及该机构的控制系统 |
| US11686210B2 (en) | 2021-03-24 | 2023-06-27 | General Electric Company | Component assembly for variable airfoil systems |
| DE102021128979A1 (de) * | 2021-11-08 | 2023-05-11 | MTU Aero Engines AG | Verstellhebel für eine strömungsmaschine |
| US12416262B2 (en) | 2023-02-17 | 2025-09-16 | General Electric Company | Reverse flow gas turbine engine having electric machine |
| US12221894B2 (en) | 2023-03-20 | 2025-02-11 | General Electric Company Polska Sp. Z O.O. | Compressor with anti-ice inlet |
| EP4435235A1 (en) * | 2023-03-20 | 2024-09-25 | General Electric Company Polska Sp. Z o.o | Compressor and turboprop engine |
Family Cites Families (53)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2842305A (en) * | 1955-11-01 | 1958-07-08 | Gen Electric | Compressor stator assembly |
| US3031049A (en) * | 1958-03-31 | 1962-04-24 | A V R Achat Ventes Representat | Fastening device for metal constructions |
| US3563669A (en) * | 1969-07-10 | 1971-02-16 | Gen Motors Corp | Variable area nozzle |
| US3736070A (en) | 1971-06-22 | 1973-05-29 | Curtiss Wright Corp | Variable stator blade assembly for axial flow, fluid expansion engine |
| US3788763A (en) * | 1972-11-01 | 1974-01-29 | Gen Motors Corp | Variable vanes |
| US3799694A (en) | 1972-11-20 | 1974-03-26 | Gen Motors Corp | Variable diffuser |
| US4050844A (en) | 1976-06-01 | 1977-09-27 | United Technologies Corporation | Connection between vane arm and unison ring in variable area stator ring |
| US4193738A (en) * | 1977-09-19 | 1980-03-18 | General Electric Company | Floating seal for a variable area turbine nozzle |
| US4295784A (en) | 1979-09-26 | 1981-10-20 | United Technologies Corporation | Variable stator |
| JPS5843421A (ja) | 1981-09-09 | 1983-03-14 | Toshiba Corp | 回転鏡光偏向器 |
| DE3540401A1 (de) * | 1985-11-14 | 1987-05-21 | Mtu Muenchen Gmbh | Leitschaufelkranz fuer turbomaschinen, insbesondere fuer gasturbinen |
| US4668165A (en) * | 1986-03-27 | 1987-05-26 | The United States Of America As Represented By The Secretary Of The Air Force | Super gripper variable vane arm |
| US4755104A (en) | 1986-04-29 | 1988-07-05 | United Technologies Corporation | Stator vane linkage |
| US4767264A (en) | 1986-10-31 | 1988-08-30 | United Technologies Corporation | Vane lever arm construction |
| US4792277A (en) * | 1987-07-08 | 1988-12-20 | United Technologies Corporation | Split shroud compressor |
| IT1217437B (it) * | 1988-04-21 | 1990-03-22 | Nuovo Pignone Spa | Sistema perfezionato di registrazione in posizione degli ugelli orientabili di una turbina a gas |
| US4925364A (en) | 1988-12-21 | 1990-05-15 | United Technologies Corporation | Adjustable spacer |
| GB8913988D0 (en) * | 1989-06-17 | 1989-08-09 | Rolls Royce Plc | Improvements in or relating to control of variable stator vanes |
| US4979874A (en) * | 1989-06-19 | 1990-12-25 | United Technologies Corporation | Variable van drive mechanism |
| US5035573A (en) | 1990-03-21 | 1991-07-30 | General Electric Company | Blade tip clearance control apparatus with shroud segment position adjustment by unison ring movement |
| JPH06159343A (ja) * | 1992-11-20 | 1994-06-07 | Sekisui Chem Co Ltd | 木質材連結ボルト |
| FR2699595B1 (fr) * | 1992-12-23 | 1995-01-20 | Snecma | Dispositif de guidage en rotation d'un anneau de commande d'aubes pivotantes. |
| US5549448A (en) | 1995-02-08 | 1996-08-27 | United Technolgies Corporation | Variable stator vane linkage system and method |
| US5593275A (en) * | 1995-08-01 | 1997-01-14 | General Electric Company | Variable stator vane mounting and vane actuation system for an axial flow compressor of a gas turbine engine |
| US5622473A (en) | 1995-11-17 | 1997-04-22 | General Electric Company | Variable stator vane assembly |
| US5601401A (en) * | 1995-12-21 | 1997-02-11 | United Technologies Corporation | Variable stage vane actuating apparatus |
| JP4211087B2 (ja) * | 1998-05-27 | 2009-01-21 | 株式会社Ihi | 可動ベーンの駆動機構 |
| US6019574A (en) | 1998-08-13 | 2000-02-01 | General Electric Company | Mismatch proof variable stator vane |
| JP2000266029A (ja) * | 1999-03-16 | 2000-09-26 | Hitachi Ltd | フランジ付スタッドボルト |
| US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
| US6457938B1 (en) | 2001-03-30 | 2002-10-01 | General Electric Company | Wide angle guide vane |
| JP4834931B2 (ja) * | 2001-07-18 | 2011-12-14 | 株式会社Ihi | 圧縮機可変翼の支持装置 |
| US6984104B2 (en) * | 2002-12-16 | 2006-01-10 | United Technologies Corporation | Variable vane arm/unison ring attachment system |
| GB0312098D0 (en) * | 2003-05-27 | 2004-05-05 | Rolls Royce Plc | A variable arrangement for a turbomachine |
| US7246484B2 (en) | 2003-08-25 | 2007-07-24 | General Electric Company | FLADE gas turbine engine with counter-rotatable fans |
| DE10352099B4 (de) * | 2003-11-08 | 2017-08-24 | MTU Aero Engines AG | Vorrichtung zum Verstellen von Leitschaufeln |
| US7096657B2 (en) | 2003-12-30 | 2006-08-29 | Honeywell International, Inc. | Gas turbine engine electromechanical variable inlet guide vane actuation system |
| GB2416194B (en) | 2004-07-15 | 2006-08-16 | Rolls Royce Plc | A spacer arrangement |
| US7114911B2 (en) | 2004-08-25 | 2006-10-03 | General Electric Company | Variable camber and stagger airfoil and method |
| FR2875559B1 (fr) * | 2004-09-21 | 2007-02-23 | Snecma Moteurs Sa | Levier de commande du calage angulaire d'une aube de stator dans une turbomachine |
| WO2006060000A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method |
| FR2879695B1 (fr) * | 2004-12-16 | 2007-04-06 | Snecma Moteurs Sa | Dispositif de liaison, de longueur ajustable, entre deux pieces |
| FR2882570B1 (fr) * | 2005-02-25 | 2007-04-13 | Snecma Moteurs Sa | Dipositif de commande d'aubes a calage variable dans une turbomachine |
| US7588415B2 (en) | 2005-07-20 | 2009-09-15 | United Technologies Corporation | Synch ring variable vane synchronizing mechanism for inner diameter vane shroud |
| US7413401B2 (en) * | 2006-01-17 | 2008-08-19 | General Electric Company | Methods and apparatus for controlling variable stator vanes |
| EP1867877A1 (en) * | 2006-06-16 | 2007-12-19 | Ansaldo Energia S.P.A. | Gas turbine compressor |
| GB2440346A (en) * | 2006-07-25 | 2008-01-30 | Rolls Royce Plc | Bearing assembly for a variable vane |
| US7594794B2 (en) | 2006-08-24 | 2009-09-29 | United Technologies Corporation | Leaned high pressure compressor inlet guide vane |
| US8092157B2 (en) | 2007-12-19 | 2012-01-10 | United Technologies Corporation | Variable turbine vane actuation mechanism having a bumper ring |
| GB0811286D0 (en) | 2008-06-20 | 2008-07-30 | Rolls Royce Plc | Multi-rotational crankshaft |
| GB2470586A (en) * | 2009-05-29 | 2010-12-01 | Rolls Royce Plc | Eccentric joint for actuator connection rod. |
| US8714916B2 (en) * | 2010-09-28 | 2014-05-06 | General Electric Company | Variable vane assembly for a turbine compressor |
| US8668444B2 (en) * | 2010-09-28 | 2014-03-11 | General Electric Company | Attachment stud for a variable vane assembly of a turbine compressor |
-
2010
- 2010-09-28 US US12/892,269 patent/US8714916B2/en active Active
-
2011
- 2011-09-09 DE DE102011053433A patent/DE102011053433A1/de active Pending
- 2011-09-21 CH CH01568/11A patent/CH703871B1/de not_active IP Right Cessation
- 2011-09-26 JP JP2011208361A patent/JP5941259B2/ja active Active
- 2011-09-28 CN CN201110309554.6A patent/CN102418712B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN102418712A (zh) | 2012-04-18 |
| CH703871B1 (de) | 2016-04-15 |
| US8714916B2 (en) | 2014-05-06 |
| US20120076641A1 (en) | 2012-03-29 |
| JP5941259B2 (ja) | 2016-06-29 |
| CH703871A2 (de) | 2012-03-30 |
| JP2012072763A (ja) | 2012-04-12 |
| CN102418712B (zh) | 2016-09-07 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| R012 | Request for examination validly filed | ||
| R016 | Response to examination communication | ||
| R081 | Change of applicant/patentee |
Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH, CH Free format text: FORMER OWNER: GENERAL ELECTRIC COMPANY, SCHENECTADY, NY, US |
|
| R016 | Response to examination communication |