DE69205568D1 - Turbinengehaeuse. - Google Patents
Turbinengehaeuse.Info
- Publication number
- DE69205568D1 DE69205568D1 DE69205568T DE69205568T DE69205568D1 DE 69205568 D1 DE69205568 D1 DE 69205568D1 DE 69205568 T DE69205568 T DE 69205568T DE 69205568 T DE69205568 T DE 69205568T DE 69205568 D1 DE69205568 D1 DE 69205568D1
- Authority
- DE
- Germany
- Prior art keywords
- turbine housing
- turbine
- housing
- 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
- 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
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9106810 | 1991-04-02 | ||
PCT/GB1992/000024 WO1992017686A1 (en) | 1991-04-02 | 1992-01-07 | Turbine casing |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69205568D1 true DE69205568D1 (de) | 1995-11-23 |
DE69205568T2 DE69205568T2 (de) | 1996-04-11 |
Family
ID=10692467
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69205568T Expired - Lifetime DE69205568T2 (de) | 1991-04-02 | 1992-01-07 | Turbinengehaeuse. |
Country Status (5)
Country | Link |
---|---|
US (1) | US5407320A (de) |
EP (1) | EP0578639B1 (de) |
JP (1) | JPH06506037A (de) |
DE (1) | DE69205568T2 (de) |
WO (1) | WO1992017686A1 (de) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9306719D0 (en) * | 1993-03-31 | 1993-06-02 | Rolls Royce Plc | A turbine assembly for a gas turbine engine |
GB2313161B (en) * | 1996-05-14 | 2000-05-31 | Rolls Royce Plc | Gas turbine engine casing |
EP0844369B1 (de) * | 1996-11-23 | 2002-01-30 | ROLLS-ROYCE plc | Zusammenbau eines Schaufelrotors und dessen Gehäuses |
US6116852A (en) * | 1997-12-11 | 2000-09-12 | Pratt & Whitney Canada Corp. | Turbine passive thermal valve for improved tip clearance control |
US6227800B1 (en) * | 1998-11-24 | 2001-05-08 | General Electric Company | Bay cooled turbine casing |
GB2378730B (en) * | 2001-08-18 | 2005-03-16 | Rolls Royce Plc | Cooled segments surrounding turbine blades |
US20040219011A1 (en) * | 2003-05-02 | 2004-11-04 | General Electric Company | High pressure turbine elastic clearance control system and method |
GB2401658B (en) * | 2003-05-16 | 2006-07-26 | Rolls Royce Plc | Sealing arrangement |
US6890150B2 (en) * | 2003-08-12 | 2005-05-10 | General Electric Company | Center-located cutter teeth on shrouded turbine blades |
US6905309B2 (en) * | 2003-08-28 | 2005-06-14 | General Electric Company | Methods and apparatus for reducing vibrations induced to compressor airfoils |
US7260892B2 (en) * | 2003-12-24 | 2007-08-28 | General Electric Company | Methods for optimizing turbine engine shell radial clearances |
US8434997B2 (en) | 2007-08-22 | 2013-05-07 | United Technologies Corporation | Gas turbine engine case for clearance control |
FR2923525B1 (fr) * | 2007-11-13 | 2009-12-18 | Snecma | Etancheite d'un anneau de rotor dans un etage de turbine |
US8616827B2 (en) * | 2008-02-20 | 2013-12-31 | Rolls-Royce Corporation | Turbine blade tip clearance system |
US8256228B2 (en) * | 2008-04-29 | 2012-09-04 | Rolls Royce Corporation | Turbine blade tip clearance apparatus and method |
EP2159381A1 (de) * | 2008-08-27 | 2010-03-03 | Siemens Aktiengesellschaft | Turbinenleitschaufelträger für eine Gasturbine |
GB0904118D0 (en) * | 2009-03-11 | 2009-04-22 | Rolls Royce Plc | An impingement cooling arrangement for a gas turbine engine |
US8490408B2 (en) * | 2009-07-24 | 2013-07-23 | Pratt & Whitney Canada Copr. | Continuous slot in shroud |
EP2518278A1 (de) * | 2011-04-28 | 2012-10-31 | Siemens Aktiengesellschaft | Kühlleitung eines Turbinengehäuses mit stromaufwärts fliessender Kühlflüssigkeit |
EP2725203B1 (de) * | 2012-10-23 | 2019-04-03 | MTU Aero Engines AG | Kühlluftführung in einer Gehäusestruktur einer Strömungsmaschine |
US9587507B2 (en) | 2013-02-23 | 2017-03-07 | Rolls-Royce North American Technologies, Inc. | Blade clearance control for gas turbine engine |
US9828880B2 (en) | 2013-03-15 | 2017-11-28 | General Electric Company | Method and apparatus to improve heat transfer in turbine sections of gas turbines |
GB201409991D0 (en) | 2014-07-04 | 2014-07-16 | Rolls Royce Plc | Turbine case cooling system |
US10975721B2 (en) | 2016-01-12 | 2021-04-13 | Pratt & Whitney Canada Corp. | Cooled containment case using internal plenum |
US10329941B2 (en) * | 2016-05-06 | 2019-06-25 | United Technologies Corporation | Impingement manifold |
US10753222B2 (en) | 2017-09-11 | 2020-08-25 | Raytheon Technologies Corporation | Gas turbine engine blade outer air seal |
US11702951B1 (en) * | 2022-06-10 | 2023-07-18 | Pratt & Whitney Canada Corp. | Passive cooling system for tip clearance optimization |
US20230417150A1 (en) * | 2022-06-22 | 2023-12-28 | Pratt & Whitney Canada Corp. | Augmented cooling for tip clearance optimization |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB589541A (en) * | 1941-09-22 | 1947-06-24 | Hayne Constant | Improvements in axial flow turbines, compressors and the like |
US2783965A (en) * | 1949-02-01 | 1957-03-05 | Birmann Rudolph | Turbines |
US2639579A (en) * | 1949-06-21 | 1953-05-26 | Hartford Nat Bank & Trust Co | Turbojet engine having tail pipe ejector to induce flow of cooling air |
US2759700A (en) * | 1950-02-04 | 1956-08-21 | Gen Motors Corp | Bearing cooling system |
GB2062117B (en) * | 1980-10-20 | 1983-05-05 | Gen Electric | Clearance control for turbine blades |
GB2108586B (en) * | 1981-11-02 | 1985-08-07 | United Technologies Corp | Gas turbine engine active clearance control |
DE3540943A1 (de) * | 1985-11-19 | 1987-05-21 | Mtu Muenchen Gmbh | Gasturbinenstrahltriebwerk in mehr-wellen-zweistrom-bauweise |
US5100291A (en) * | 1990-03-28 | 1992-03-31 | General Electric Company | Impingement manifold |
US5152666A (en) * | 1991-05-03 | 1992-10-06 | United Technologies Corporation | Stator assembly for a rotary machine |
-
1992
- 1992-01-07 US US08/122,422 patent/US5407320A/en not_active Expired - Lifetime
- 1992-01-07 JP JP4502167A patent/JPH06506037A/ja active Pending
- 1992-01-07 DE DE69205568T patent/DE69205568T2/de not_active Expired - Lifetime
- 1992-01-07 EP EP92901583A patent/EP0578639B1/de not_active Expired - Lifetime
- 1992-01-07 WO PCT/GB1992/000024 patent/WO1992017686A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
JPH06506037A (ja) | 1994-07-07 |
WO1992017686A1 (en) | 1992-10-15 |
EP0578639B1 (de) | 1995-10-18 |
DE69205568T2 (de) | 1996-04-11 |
US5407320A (en) | 1995-04-18 |
EP0578639A1 (de) | 1994-01-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8365 | Fully valid after opposition proceedings |