DE69707556T2 - Spitzspielkontrolle für Turbomaschinen - Google Patents
Spitzspielkontrolle für TurbomaschinenInfo
- Publication number
- DE69707556T2 DE69707556T2 DE69707556T DE69707556T DE69707556T2 DE 69707556 T2 DE69707556 T2 DE 69707556T2 DE 69707556 T DE69707556 T DE 69707556T DE 69707556 T DE69707556 T DE 69707556T DE 69707556 T2 DE69707556 T2 DE 69707556T2
- Authority
- DE
- Germany
- Prior art keywords
- turbomachinery
- play control
- sharp
- sharp play
- control
- 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
- F01D11/20—Actively adjusting tip-clearance
- F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9610916A GB2313414B (en) | 1996-05-24 | 1996-05-24 | Gas turbine engine blade tip clearance control |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69707556D1 DE69707556D1 (de) | 2001-11-29 |
DE69707556T2 true DE69707556T2 (de) | 2002-04-25 |
Family
ID=10794267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69707556T Expired - Lifetime DE69707556T2 (de) | 1996-05-24 | 1997-04-24 | Spitzspielkontrolle für Turbomaschinen |
Country Status (4)
Country | Link |
---|---|
US (1) | US5871333A (de) |
EP (1) | EP0808991B1 (de) |
DE (1) | DE69707556T2 (de) |
GB (1) | GB2313414B (de) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2323269A (en) | 1997-03-18 | 1998-09-23 | Applied Sweepers Ltd | Pedestrian operated suction sweeping machine |
GB9725623D0 (en) | 1997-12-03 | 2006-09-20 | Rolls Royce Plc | Improvements in or relating to a blade tip clearance system |
US6382905B1 (en) | 2000-04-28 | 2002-05-07 | General Electric Company | Fan casing liner support |
US6409471B1 (en) | 2001-02-16 | 2002-06-25 | General Electric Company | Shroud assembly and method of machining same |
US6896483B2 (en) | 2001-07-02 | 2005-05-24 | Allison Advanced Development Company | Blade track assembly |
GB2388407B (en) * | 2002-05-10 | 2005-10-26 | Rolls Royce Plc | Gas turbine blade tip clearance control structure |
GB0218060D0 (en) | 2002-08-03 | 2002-09-11 | Alstom Switzerland Ltd | Sealing arrangements |
US6877952B2 (en) * | 2002-09-09 | 2005-04-12 | Florida Turbine Technologies, Inc | Passive clearance control |
GB2404953A (en) * | 2003-08-15 | 2005-02-16 | Rolls Royce Plc | Blade tip clearance system |
US20050135923A1 (en) * | 2003-12-22 | 2005-06-23 | Todd Coons | Cooled vane cluster |
US7596954B2 (en) * | 2004-07-09 | 2009-10-06 | United Technologies Corporation | Blade clearance control |
US7246989B2 (en) * | 2004-12-10 | 2007-07-24 | Pratt & Whitney Canada Corp. | Shroud leading edge cooling |
DE102005030426A1 (de) * | 2005-06-30 | 2007-01-04 | Mtu Aero Engines Gmbh | Rotorspalt Steuervorrichtung für einen Verdichter |
US7575409B2 (en) * | 2005-07-01 | 2009-08-18 | Allison Advanced Development Company | Apparatus and method for active control of blade tip clearance |
US20080025838A1 (en) * | 2006-07-25 | 2008-01-31 | Siemens Power Generation, Inc. | Ring seal for a turbine engine |
DE102006038753A1 (de) * | 2006-08-17 | 2008-03-13 | Mtu Aero Engines Gmbh | Anordnung zur Laufspaltoptimierung für Turbomaschinen |
US7740442B2 (en) * | 2006-11-30 | 2010-06-22 | General Electric Company | Methods and system for cooling integral turbine nozzle and shroud assemblies |
US7686569B2 (en) | 2006-12-04 | 2010-03-30 | Siemens Energy, Inc. | Blade clearance system for a turbine engine |
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 |
GB0812306D0 (en) | 2008-07-07 | 2008-08-13 | Rolls Royce Plc | A clearance arrangement |
US8092153B2 (en) * | 2008-12-16 | 2012-01-10 | Pratt & Whitney Canada Corp. | Bypass air scoop for gas turbine engine |
GB0909470D0 (en) * | 2009-06-03 | 2009-07-15 | Rolls Royce Plc | A guide vane assembly |
GB0910070D0 (en) | 2009-06-12 | 2009-07-22 | Rolls Royce Plc | System and method for adjusting rotor-stator clearance |
US8454303B2 (en) * | 2010-01-14 | 2013-06-04 | General Electric Company | Turbine nozzle assembly |
RU2543101C2 (ru) * | 2010-11-29 | 2015-02-27 | Альстом Текнолоджи Лтд | Осевая газовая турбина |
RU2547351C2 (ru) * | 2010-11-29 | 2015-04-10 | Альстом Текнолоджи Лтд | Осевая газовая турбина |
GB201109143D0 (en) * | 2011-06-01 | 2011-07-13 | Rolls Royce Plc | Flap seal spring and sealing apparatus |
US8944756B2 (en) * | 2011-07-15 | 2015-02-03 | United Technologies Corporation | Blade outer air seal assembly |
US20130315716A1 (en) * | 2012-05-22 | 2013-11-28 | General Electric Company | Turbomachine having clearance control capability and system therefor |
US9255524B2 (en) * | 2012-12-20 | 2016-02-09 | United Technologies Corporation | Variable outer air seal fluid control |
WO2014130159A1 (en) | 2013-02-23 | 2014-08-28 | Ottow Nathan W | Blade clearance control for gas turbine engine |
US9850822B2 (en) * | 2013-03-15 | 2017-12-26 | United Technologies Corporation | Shroudless adaptive fan with free turbine |
WO2014186003A2 (en) * | 2013-04-12 | 2014-11-20 | United Technologies Corporation | Gas turbine engine rapid response clearance control system with variable volume turbine case |
US9617917B2 (en) | 2013-07-31 | 2017-04-11 | General Electric Company | Flow control assembly and methods of assembling the same |
US10364694B2 (en) | 2013-12-17 | 2019-07-30 | United Technologies Corporation | Turbomachine blade clearance control system |
WO2015102949A2 (en) * | 2013-12-30 | 2015-07-09 | United Technologies Corporation | Accessible rapid response clearance control system |
US9915153B2 (en) * | 2015-05-11 | 2018-03-13 | General Electric Company | Turbine shroud segment assembly with expansion joints |
GB201616197D0 (en) * | 2016-09-23 | 2016-11-09 | Rolls Royce Plc | Gas turbine engine |
US10704408B2 (en) | 2018-05-03 | 2020-07-07 | Rolls-Royce North American Technologies Inc. | Dual response blade track system |
WO2020013837A1 (en) * | 2018-07-13 | 2020-01-16 | Siemens Aktiengesellschaft | Sealing apparatus for sealing a radial clearance between stationary and rotatable components of a gas turbine engine and corresponding operating method |
US11346237B1 (en) * | 2021-05-25 | 2022-05-31 | Rolls-Royce Corporation | Turbine shroud assembly with axially biased ceramic matrix composite shroud segment |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3452542A (en) * | 1966-09-30 | 1969-07-01 | Gen Electric | Gas turbine engine cooling system |
FR2280791A1 (fr) * | 1974-07-31 | 1976-02-27 | Snecma | Perfectionnements au reglage du jeu entre les aubes et le stator d'une turbine |
US3936217A (en) * | 1975-01-31 | 1976-02-03 | Westinghouse Electric Corporation | Inspection port for turbines |
US4214851A (en) * | 1978-04-20 | 1980-07-29 | General Electric Company | Structural cooling air manifold for a gas turbine engine |
GB2042646B (en) * | 1979-02-20 | 1982-09-22 | Rolls Royce | Rotor blade tip clearance control for gas turbine engine |
DE2922835C2 (de) * | 1979-06-06 | 1985-06-05 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Umfangsspaltdichtung an Axialströmungsmaschinen |
GB2103294B (en) * | 1981-07-11 | 1984-08-30 | Rolls Royce | Shroud assembly for a gas turbine engine |
GB2117451B (en) * | 1982-03-05 | 1985-11-06 | Rolls Royce | Gas turbine shroud |
GB2169962B (en) * | 1985-01-22 | 1988-07-13 | Rolls Royce | Blade tip clearance control |
US5601402A (en) * | 1986-06-06 | 1997-02-11 | The United States Of America As Represented By The Secretary Of The Air Force | Turbo machine shroud-to-rotor blade dynamic clearance control |
GB2195715B (en) * | 1986-10-08 | 1990-10-10 | Rolls Royce Plc | Gas turbine engine rotor blade clearance control |
GB9103809D0 (en) * | 1991-02-23 | 1991-04-10 | Rolls Royce Plc | Blade tip clearance control apparatus |
US5685693A (en) * | 1995-03-31 | 1997-11-11 | General Electric Co. | Removable inner turbine shell with bucket tip clearance control |
-
1996
- 1996-05-24 GB GB9610916A patent/GB2313414B/en not_active Expired - Fee Related
-
1997
- 1997-04-24 EP EP97302799A patent/EP0808991B1/de not_active Expired - Lifetime
- 1997-04-24 DE DE69707556T patent/DE69707556T2/de not_active Expired - Lifetime
- 1997-04-28 US US08/848,026 patent/US5871333A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5871333A (en) | 1999-02-16 |
GB2313414B (en) | 2000-05-17 |
EP0808991A3 (de) | 1997-12-03 |
GB2313414A (en) | 1997-11-26 |
EP0808991A2 (de) | 1997-11-26 |
EP0808991B1 (de) | 2001-10-24 |
GB9610916D0 (en) | 1996-07-31 |
DE69707556D1 (de) | 2001-11-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |