GB0507405D0 - A mounting arrangement - Google Patents
A mounting arrangementInfo
- Publication number
- GB0507405D0 GB0507405D0 GB0507405A GB0507405A GB0507405D0 GB 0507405 D0 GB0507405 D0 GB 0507405D0 GB 0507405 A GB0507405 A GB 0507405A GB 0507405 A GB0507405 A GB 0507405A GB 0507405 D0 GB0507405 D0 GB 0507405D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- mounting arrangement
- mounting
- arrangement
- 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.)
- Granted
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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0507405A GB2425155B (en) | 2005-04-13 | 2005-04-13 | A mounting arrangement |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0507405A GB2425155B (en) | 2005-04-13 | 2005-04-13 | A mounting arrangement |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0507405D0 true GB0507405D0 (en) | 2005-05-18 |
GB2425155A GB2425155A (en) | 2006-10-18 |
GB2425155B GB2425155B (en) | 2007-09-19 |
Family
ID=34611013
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0507405A Expired - Fee Related GB2425155B (en) | 2005-04-13 | 2005-04-13 | A mounting arrangement |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2425155B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006050907A1 (en) | 2006-10-28 | 2008-05-15 | Man Turbo Ag | Guide device of a turbomachine and vane for such a guide device |
FR2922950B1 (en) * | 2007-10-31 | 2014-05-09 | Snecma | CARTRIDGE OF ABRADABLE MATERIAL |
GB0922422D0 (en) | 2009-12-23 | 2010-02-03 | Rolls Royce Plc | Annulus Filler Assembly for a Rotor of a Turbomachine |
US8454303B2 (en) * | 2010-01-14 | 2013-06-04 | General Electric Company | Turbine nozzle assembly |
US8864446B2 (en) | 2011-05-23 | 2014-10-21 | Siemens Energy, Inc. | Wear pin gap closure detection system for gas turbine engine |
EP2696039B1 (en) * | 2012-08-10 | 2015-07-29 | MTU Aero Engines GmbH | Gas turbine stage |
US9334756B2 (en) | 2012-09-28 | 2016-05-10 | United Technologies Corporation | Liner and method of assembly |
EP3085900B1 (en) * | 2015-04-21 | 2020-08-05 | Ansaldo Energia Switzerland AG | Abradable lip for a gas turbine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB856599A (en) * | 1958-06-16 | 1960-12-21 | Gen Motors Corp | Improvements relating to axial-flow compressors |
FR2427469A1 (en) * | 1978-06-01 | 1979-12-28 | Snecma | DEVICE FOR FIXING A SEALING GASKET ON A TURBOMACHINE DISTRIBUTOR |
JPS6189908A (en) * | 1984-10-11 | 1986-05-08 | Central Res Inst Of Electric Power Ind | Ceramics metal compound stationary blade structure |
JPH07324601A (en) * | 1994-05-31 | 1995-12-12 | Mitsubishi Heavy Ind Ltd | Diaphragm structure for steam turbine |
US5586864A (en) * | 1994-07-27 | 1996-12-24 | General Electric Company | Turbine nozzle diaphragm and method of assembly |
JP2001123803A (en) * | 1999-10-21 | 2001-05-08 | Toshiba Corp | Sealing device, steam turbine having the device, and power generating plant |
-
2005
- 2005-04-13 GB GB0507405A patent/GB2425155B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2425155A (en) | 2006-10-18 |
GB2425155B (en) | 2007-09-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20130413 |