DE69001233T2 - Turbokompressorgehaeuse mit spielkontrollvorrichtung fuer den inneren durchmesser. - Google Patents
Turbokompressorgehaeuse mit spielkontrollvorrichtung fuer den inneren durchmesser.Info
- Publication number
- DE69001233T2 DE69001233T2 DE9090402910T DE69001233T DE69001233T2 DE 69001233 T2 DE69001233 T2 DE 69001233T2 DE 9090402910 T DE9090402910 T DE 9090402910T DE 69001233 T DE69001233 T DE 69001233T DE 69001233 T2 DE69001233 T2 DE 69001233T2
- Authority
- DE
- Germany
- Prior art keywords
- control device
- inner diameter
- game control
- compressor housing
- turbo compressor
- 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 - Fee Related
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
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 |
---|---|---|---|
FR8913585A FR2653171B1 (fr) | 1989-10-18 | 1989-10-18 | Carter de compresseur de turbomachine muni d'un dispositif de pilotage de son diametre interne. |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69001233D1 DE69001233D1 (de) | 1993-05-06 |
DE69001233T2 true DE69001233T2 (de) | 1993-09-23 |
Family
ID=9386499
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE9090402910T Expired - Fee Related DE69001233T2 (de) | 1989-10-18 | 1990-10-17 | Turbokompressorgehaeuse mit spielkontrollvorrichtung fuer den inneren durchmesser. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5154578A (de) |
EP (1) | EP0424253B1 (de) |
DE (1) | DE69001233T2 (de) |
FR (1) | FR2653171B1 (de) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5219268A (en) * | 1992-03-06 | 1993-06-15 | General Electric Company | Gas turbine engine case thermal control flange |
FR2708669B1 (fr) * | 1993-08-05 | 1995-09-08 | Snecma | Système de ventilation des disques et du stator de turbine d'un turboréacteur. |
US5685693A (en) * | 1995-03-31 | 1997-11-11 | General Electric Co. | Removable inner turbine shell with bucket tip clearance control |
US5779436A (en) * | 1996-08-07 | 1998-07-14 | Solar Turbines Incorporated | Turbine blade clearance control system |
US5791872A (en) * | 1997-04-22 | 1998-08-11 | Rolls-Royce Inc. | Blade tip clearence control apparatus |
DE19824766C2 (de) * | 1998-06-03 | 2000-05-11 | Siemens Ag | Gasturbine sowie Verfahren zur Kühlung einer Turbinenstufe |
GB2388407B (en) * | 2002-05-10 | 2005-10-26 | Rolls Royce Plc | Gas turbine blade tip clearance control structure |
EP1426563A1 (de) * | 2002-12-03 | 2004-06-09 | BorgWarner Inc. | Turbolader mit keramischer oder metallischer Hitzeisolierung zwischen Turbinen- und Lagergehäuse |
US6925814B2 (en) * | 2003-04-30 | 2005-08-09 | Pratt & Whitney Canada Corp. | Hybrid turbine tip clearance control system |
US20050109016A1 (en) * | 2003-11-21 | 2005-05-26 | Richard Ullyott | Turbine tip clearance control system |
EP1566531A1 (de) * | 2004-02-19 | 2005-08-24 | Siemens Aktiengesellschaft | Gasturbine mit einem gegen Auskühlen geschützten Verdichtergehäuse und Verfahren zum Betrieb einer Gasturbine |
US8240979B2 (en) * | 2007-10-24 | 2012-08-14 | United Technologies Corp. | Gas turbine engine systems involving integrated fluid conduits |
US8177494B2 (en) * | 2009-03-15 | 2012-05-15 | United Technologies Corporation | Buried casing treatment strip for a gas turbine engine |
US8342798B2 (en) * | 2009-07-28 | 2013-01-01 | General Electric Company | System and method for clearance control in a rotary machine |
US20110103939A1 (en) * | 2009-10-30 | 2011-05-05 | General Electric Company | Turbine rotor blade tip and shroud clearance control |
FR3034465B1 (fr) | 2015-04-03 | 2017-05-05 | Snecma | Turbomoteur comportant deux flux de ventilation distincts |
US20170350597A1 (en) * | 2016-06-07 | 2017-12-07 | General Electric Company | Heat transfer device, turbomachine casing and related storage medium |
US10422237B2 (en) * | 2017-04-11 | 2019-09-24 | United Technologies Corporation | Flow diverter case attachment for gas turbine engine |
US10815814B2 (en) * | 2017-05-08 | 2020-10-27 | Raytheon Technologies Corporation | Re-use and modulated cooling from tip clearance control system for gas turbine engine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1259142B (de) * | 1962-02-14 | 1968-01-18 | Licentia Gmbh | Ringflansch des rohrfoermigen Innen- oder Aussengehaeuses einer Axialgas- oder -dampfturbine |
US3275294A (en) * | 1963-11-14 | 1966-09-27 | Westinghouse Electric Corp | Elastic fluid apparatus |
US3551068A (en) * | 1968-10-25 | 1970-12-29 | Westinghouse Electric Corp | Rotor structure for an axial flow machine |
GB1519590A (en) * | 1974-11-11 | 1978-08-02 | Rolls Royce | Gas turbine engine |
GB1605255A (en) * | 1975-12-02 | 1986-08-13 | Rolls Royce | Clearance control apparatus for bladed fluid flow machine |
GB2042646B (en) * | 1979-02-20 | 1982-09-22 | Rolls Royce | Rotor blade tip clearance control for gas turbine engine |
FR2473621A1 (fr) * | 1980-01-10 | 1981-07-17 | Snecma | Aube de distributeur de turbine |
FR2534982A1 (fr) * | 1982-10-22 | 1984-04-27 | Snecma | Dispositif de controle des jeux d'un compresseur haute pression |
FR2535795B1 (fr) * | 1982-11-08 | 1987-04-10 | Snecma | Dispositif de suspension d'aubes statoriques de compresseur axial pour le controle actif des jeux entre rotor et stator |
FR2577282B1 (fr) * | 1985-02-13 | 1987-04-17 | Snecma | Carter de turbomachine associe a un dispositif pour ajuster le jeu entre rotor et stator |
FR2591674B1 (fr) * | 1985-12-18 | 1988-02-19 | Snecma | Dispositif de reglage des jeux radiaux entre rotor et stator d'un compresseur |
FR2614073B1 (fr) * | 1987-04-15 | 1992-02-14 | Snecma | Dispositif d'ajustement en temps reel du jeu radial entre un rotor et un stator de turbomachine |
US4826397A (en) * | 1988-06-29 | 1989-05-02 | United Technologies Corporation | Stator assembly for a gas turbine engine |
FR2640687B1 (fr) * | 1988-12-21 | 1991-02-08 | Snecma | Carter de compresseur de turbomachine a pilotage de son diametre interne |
-
1989
- 1989-10-18 FR FR8913585A patent/FR2653171B1/fr not_active Expired - Lifetime
-
1990
- 1990-10-15 US US07/597,024 patent/US5154578A/en not_active Expired - Lifetime
- 1990-10-17 DE DE9090402910T patent/DE69001233T2/de not_active Expired - Fee Related
- 1990-10-17 EP EP90402910A patent/EP0424253B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2653171B1 (fr) | 1991-12-27 |
EP0424253B1 (de) | 1993-03-31 |
US5154578A (en) | 1992-10-13 |
FR2653171A1 (fr) | 1991-04-19 |
EP0424253A1 (de) | 1991-04-24 |
DE69001233D1 (de) | 1993-05-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: SNECMA MOTEURS, PARIS, FR |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: SNECMA, PARIS, FR |
|
8339 | Ceased/non-payment of the annual fee |