DE50214035D1 - Lagerring zur Lagerung von Schaufelfüssen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine - Google Patents
Lagerring zur Lagerung von Schaufelfüssen von verstellbaren Statorschaufeln im Hochdruckverdichter einer GasturbineInfo
- Publication number
- DE50214035D1 DE50214035D1 DE50214035T DE50214035T DE50214035D1 DE 50214035 D1 DE50214035 D1 DE 50214035D1 DE 50214035 T DE50214035 T DE 50214035T DE 50214035 T DE50214035 T DE 50214035T DE 50214035 D1 DE50214035 D1 DE 50214035D1
- Authority
- DE
- Germany
- Prior art keywords
- storage
- gas turbine
- bearing ring
- pressure compressor
- stator blades
- 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.)
- Expired - Lifetime
Links
Classifications
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
-
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10161292A DE10161292A1 (de) | 2001-12-13 | 2001-12-13 | Lagerring zur Lagerung von Schaufelfüßen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE50214035D1 true DE50214035D1 (de) | 2010-01-14 |
Family
ID=7709105
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10161292A Withdrawn DE10161292A1 (de) | 2001-12-13 | 2001-12-13 | Lagerring zur Lagerung von Schaufelfüßen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine |
DE50214035T Expired - Lifetime DE50214035D1 (de) | 2001-12-13 | 2002-10-16 | Lagerring zur Lagerung von Schaufelfüssen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10161292A Withdrawn DE10161292A1 (de) | 2001-12-13 | 2001-12-13 | Lagerring zur Lagerung von Schaufelfüßen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine |
Country Status (3)
Country | Link |
---|---|
US (1) | US6790000B2 (de) |
EP (1) | EP1319844B1 (de) |
DE (2) | DE10161292A1 (de) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10353810A1 (de) | 2003-11-17 | 2005-06-23 | Rolls-Royce Deutschland Ltd & Co Kg | Innendeckband für die Statorschaufeln des Verdichters einer Gasturbine |
DE10358421A1 (de) * | 2003-12-13 | 2005-07-07 | Mtu Aero Engines Gmbh | Rotor für eine Turbomaschine |
GB0504588D0 (en) | 2005-03-05 | 2005-04-13 | Rolls Royce Plc | Pivot ring |
US7665959B2 (en) * | 2005-07-20 | 2010-02-23 | United Technologies Corporation | Rack and pinion variable vane synchronizing mechanism for inner diameter vane shroud |
US7753647B2 (en) * | 2005-07-20 | 2010-07-13 | United Technologies Corporation | Lightweight cast inner diameter vane shroud for variable stator vanes |
US7628579B2 (en) * | 2005-07-20 | 2009-12-08 | United Technologies Corporation | Gear train variable vane synchronizing mechanism for inner diameter vane shroud |
US7690889B2 (en) * | 2005-07-20 | 2010-04-06 | United Technologies Corporation | Inner diameter variable vane actuation mechanism |
US7588415B2 (en) * | 2005-07-20 | 2009-09-15 | United Technologies Corporation | Synch ring variable vane synchronizing mechanism for inner diameter vane shroud |
US7510369B2 (en) | 2005-09-02 | 2009-03-31 | United Technologies Corporation | Sacrificial inner shroud liners for gas turbine engines |
EP1811134A1 (de) * | 2006-01-23 | 2007-07-25 | ABB Turbo Systems AG | Verstellbare Leitvorrichtung |
DE102006024085B4 (de) | 2006-05-23 | 2020-04-16 | MTU Aero Engines AG | Turboverdichter in Axialbauweise |
US7713022B2 (en) * | 2007-03-06 | 2010-05-11 | United Technologies Operations | Small radial profile shroud for variable vane structure in a gas turbine engine |
US8328512B2 (en) * | 2009-06-05 | 2012-12-11 | United Technologies Corporation | Inner diameter shroud assembly for variable inlet guide vane structure in a gas turbine engine |
US8777561B2 (en) | 2010-11-05 | 2014-07-15 | Hamilton Sundstrand Corporation | Compressor shroud having a retention cover channel for receiving a retention cover |
US9957832B2 (en) | 2012-02-28 | 2018-05-01 | United Technologies Corporation | Variable area turbine |
EP2644833A1 (de) * | 2012-03-26 | 2013-10-02 | Alstom Technology Ltd | Trägerring |
WO2014046965A1 (en) * | 2012-09-20 | 2014-03-27 | United Technologies Corporation | Fan drive gear system module and inlet guide vane coupling mechanism |
WO2014143445A2 (en) * | 2013-02-10 | 2014-09-18 | United Technologies Corporation | Variable vane overlap shroud |
FR3009335B1 (fr) | 2013-07-30 | 2015-09-04 | Snecma | Dispositif de guidage d'aubes de redresseur a angle de calage variable de turbomachine |
WO2015077011A1 (en) | 2013-11-19 | 2015-05-28 | United Technologies Corporation | Multi-element inner shroud extension for a turbo-machine |
FR3014152B1 (fr) * | 2013-11-29 | 2015-12-25 | Snecma | Dispositif de guidage d'aubes de redresseur a angle de calage variable de turbomachine et procede d'assemblage d'un tel dispositif |
DE102014205986B4 (de) | 2014-03-31 | 2021-03-18 | MTU Aero Engines AG | Leitschaufelkranz und Strömungsmaschine |
DE102014223975A1 (de) * | 2014-11-25 | 2016-05-25 | MTU Aero Engines AG | Leitschaufelkranz und Strömungsmaschine |
US10072746B2 (en) * | 2015-05-05 | 2018-09-11 | Valeo Embrayages | Stator assembly of hydrokinetic torque converter, and method for making the same |
EP3176386B1 (de) | 2015-12-04 | 2021-01-27 | MTU Aero Engines GmbH | Innenringsystem, zugehöriger innenring, zwichengehäuse und strömungsmaschine |
DE102016215807A1 (de) * | 2016-08-23 | 2018-03-01 | MTU Aero Engines AG | Innenring für einen Leitschaufelkranz einer Strömungsmaschine |
DE102017109952A1 (de) * | 2017-05-09 | 2018-11-15 | Rolls-Royce Deutschland Ltd & Co Kg | Rotorvorrichtung einer Strömungsmaschine |
DE102017209682A1 (de) | 2017-06-08 | 2018-12-13 | MTU Aero Engines AG | Axial geteilter Turbomaschinen-Innenring |
US10526911B2 (en) * | 2017-06-22 | 2020-01-07 | United Technologies Corporation | Split synchronization ring for variable vane assembly |
DE102018203442A1 (de) * | 2018-03-07 | 2019-09-12 | MTU Aero Engines AG | Innenring für eine Turbomaschine, Leitschaufelkranz mit einem Innenring, Turbomaschine und Verfahren zur Herstellung eines Innenrings |
BE1026411B1 (fr) * | 2018-06-21 | 2020-01-30 | Safran Aero Boosters Sa | Virole extérieure de turbomachine |
DE102018210601A1 (de) * | 2018-06-28 | 2020-01-02 | MTU Aero Engines AG | Segmentring zur montage in einer strömungsmaschine |
US11572794B2 (en) | 2021-01-07 | 2023-02-07 | General Electric Company | Inner shroud damper for vibration reduction |
US11608747B2 (en) | 2021-01-07 | 2023-03-21 | General Electric Company | Split shroud for vibration reduction |
US11629606B2 (en) * | 2021-05-26 | 2023-04-18 | General Electric Company | Split-line stator vane assembly |
CN113898419A (zh) * | 2021-10-10 | 2022-01-07 | 中国航发沈阳发动机研究所 | 一种进气机匣结构及其组装方法 |
US11879480B1 (en) | 2023-04-07 | 2024-01-23 | Rolls-Royce North American Technologies Inc. | Sectioned compressor inner band for variable pitch vane assemblies in gas turbine engines |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2868439A (en) * | 1954-05-07 | 1959-01-13 | Goodyear Aircraft Corp | Plastic axial-flow compressor for gas turbines |
DE2121707C3 (de) * | 1971-05-03 | 1974-06-20 | Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Leitschaufelkranz |
FR2524934B1 (fr) * | 1982-04-08 | 1986-12-26 | Snecma | Dispositif de butee de securite pour pivot d'aubes de stator a calage variable |
FR2582720B1 (fr) * | 1985-05-29 | 1989-06-02 | Snecma | Procede de realisation de pivot d'aube de turbomachine et aube de stator le comportant |
US4792277A (en) * | 1987-07-08 | 1988-12-20 | United Technologies Corporation | Split shroud compressor |
US4834613A (en) * | 1988-02-26 | 1989-05-30 | United Technologies Corporation | Radially constrained variable vane shroud |
US5279031A (en) * | 1988-12-06 | 1994-01-18 | Alliedsignal Inc. | High temperature turbine engine structure |
US5062767A (en) * | 1990-04-27 | 1991-11-05 | The United States Of America As Represented By The Secretary Of The Air Force | Segmented composite inner shrouds |
FR2685033B1 (fr) * | 1991-12-11 | 1994-02-11 | Snecma | Stator dirigeant l'entree de l'air a l'interieur d'une turbomachine et procede de montage d'une aube de ce stator. |
US5421703A (en) | 1994-05-25 | 1995-06-06 | General Electric Company | Positively retained vane bushing for an axial flow compressor |
FR2723614B1 (fr) * | 1994-08-10 | 1996-09-13 | Snecma | Dispositif d'assemblage d'un etage circulaire d'aubes pivotantes. |
CA2231986A1 (en) * | 1997-01-10 | 1999-09-12 | Masahito Kataoka | Stationary blade of integrated segment construction and manufacturing method therefor |
FR2775731B1 (fr) * | 1998-03-05 | 2000-04-07 | Snecma | Etage circulaire d'aubes aux extremites interieures unies par un anneau de liaison |
US6164903A (en) * | 1998-12-22 | 2000-12-26 | United Technologies Corporation | Turbine vane mounting arrangement |
US6086327A (en) * | 1999-01-20 | 2000-07-11 | Mack Plastics Corporation | Bushing for a jet engine vane |
-
2001
- 2001-12-13 DE DE10161292A patent/DE10161292A1/de not_active Withdrawn
-
2002
- 2002-10-16 EP EP02023209A patent/EP1319844B1/de not_active Expired - Fee Related
- 2002-10-16 DE DE50214035T patent/DE50214035D1/de not_active Expired - Lifetime
- 2002-12-12 US US10/316,845 patent/US6790000B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US6790000B2 (en) | 2004-09-14 |
US20030113204A1 (en) | 2003-06-19 |
EP1319844A1 (de) | 2003-06-18 |
DE10161292A1 (de) | 2003-06-26 |
EP1319844B1 (de) | 2009-12-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |