NO20002768L - Stötte og låseinnretning for dyser i et höytrykkstrinn i gassturbiner - Google Patents
Stötte og låseinnretning for dyser i et höytrykkstrinn i gassturbinerInfo
- Publication number
- NO20002768L NO20002768L NO20002768A NO20002768A NO20002768L NO 20002768 L NO20002768 L NO 20002768L NO 20002768 A NO20002768 A NO 20002768A NO 20002768 A NO20002768 A NO 20002768A NO 20002768 L NO20002768 L NO 20002768L
- Authority
- NO
- Norway
- Prior art keywords
- high pressure
- locking device
- pressure stage
- gas turbines
- nozzle support
- Prior art date
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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Nozzles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT1999MI001206A ITMI991206A1 (it) | 1999-05-31 | 1999-05-31 | Dispositivo di supporto e bloccaggio per ugelli di uno stadio ad altapressione in turbine a gas |
Publications (3)
Publication Number | Publication Date |
---|---|
NO20002768D0 NO20002768D0 (no) | 2000-05-30 |
NO20002768L true NO20002768L (no) | 2000-12-01 |
NO330517B1 NO330517B1 (no) | 2011-05-09 |
Family
ID=11383081
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO20002768A NO330517B1 (no) | 1999-05-31 | 2000-05-30 | Stotte og laseinnretning for dyser i et hoytrykkstrinn i gassturbiner |
Country Status (12)
Country | Link |
---|---|
US (1) | US6343463B1 (no) |
EP (1) | EP1057975B1 (no) |
AR (1) | AR024169A1 (no) |
BR (1) | BR0002531A (no) |
DE (1) | DE60034993T2 (no) |
DZ (1) | DZ3087A1 (no) |
EG (1) | EG22056A (no) |
ES (1) | ES2286985T3 (no) |
IT (1) | ITMI991206A1 (no) |
MX (1) | MXPA00005372A (no) |
NO (1) | NO330517B1 (no) |
RU (1) | RU2223406C2 (no) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6742987B2 (en) * | 2002-07-16 | 2004-06-01 | General Electric Company | Cradle mounted turbine nozzle |
US7510367B2 (en) * | 2006-08-24 | 2009-03-31 | Siemens Energy, Inc. | Turbine airfoil with endwall horseshoe cooling slot |
US7419352B2 (en) * | 2006-10-03 | 2008-09-02 | General Electric Company | Methods and apparatus for assembling turbine engines |
US7960482B2 (en) | 2006-12-11 | 2011-06-14 | Dupont Powder Coatings France Sas | Low gloss coil powder coating composition for coil coating |
US8708643B2 (en) * | 2007-08-14 | 2014-04-29 | General Electric Company | Counter-rotatable fan gas turbine engine with axial flow positive displacement worm gas generator |
US20090169369A1 (en) * | 2007-12-29 | 2009-07-02 | General Electric Company | Turbine nozzle segment and assembly |
US20090169376A1 (en) * | 2007-12-29 | 2009-07-02 | General Electric Company | Turbine Nozzle Segment and Method for Repairing a Turbine Nozzle Segment |
FR2928961B1 (fr) * | 2008-03-19 | 2015-11-13 | Snecma | Distributeur sectorise pour une turbomachine. |
US8206096B2 (en) * | 2009-07-08 | 2012-06-26 | General Electric Company | Composite turbine nozzle |
US9528392B2 (en) * | 2013-05-10 | 2016-12-27 | General Electric Company | System for supporting a turbine nozzle |
US9863259B2 (en) * | 2015-05-11 | 2018-01-09 | United Technologies Corporation | Chordal seal |
GB201612293D0 (en) | 2016-07-15 | 2016-08-31 | Rolls Royce Plc | Assembly for supprting an annulus |
CN110206591A (zh) * | 2019-06-04 | 2019-09-06 | 中国船舶重工集团公司第七0三研究所 | 一种用于涡轮动叶供气的槽道式冷却空气导向装置 |
US11686210B2 (en) | 2021-03-24 | 2023-06-27 | General Electric Company | Component assembly for variable airfoil systems |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3262677A (en) * | 1963-11-27 | 1966-07-26 | Gen Electric | Stator assembly |
GB1086432A (en) * | 1965-09-21 | 1967-10-11 | Bristol Siddeley Engines Ltd | Gas turbine engines |
US3302926A (en) * | 1965-12-06 | 1967-02-07 | Gen Electric | Segmented nozzle diaphragm for high temperature turbine |
GB1385666A (en) * | 1973-07-06 | 1975-02-26 | Rolls Royce | Sealing of vaned assemblies of gas turbine engines |
US4153386A (en) * | 1974-12-11 | 1979-05-08 | United Technologies Corporation | Air cooled turbine vanes |
US4126405A (en) * | 1976-12-16 | 1978-11-21 | General Electric Company | Turbine nozzle |
GB2163218B (en) * | 1981-07-07 | 1986-07-16 | Rolls Royce | Cooled vane or blade for a gas turbine engine |
US5118120A (en) * | 1989-07-10 | 1992-06-02 | General Electric Company | Leaf seals |
US5211536A (en) * | 1991-05-13 | 1993-05-18 | General Electric Company | Boltless turbine nozzle/stationary seal mounting |
US5224822A (en) * | 1991-05-13 | 1993-07-06 | General Electric Company | Integral turbine nozzle support and discourager seal |
CA2070511C (en) * | 1991-07-22 | 2001-08-21 | Steven Milo Toborg | Turbine nozzle support |
US5271714A (en) * | 1992-07-09 | 1993-12-21 | General Electric Company | Turbine nozzle support arrangement |
US5372476A (en) * | 1993-06-18 | 1994-12-13 | General Electric Company | Turbine nozzle support assembly |
US5622475A (en) * | 1994-08-30 | 1997-04-22 | General Electric Company | Double rabbet rotor blade retention assembly |
US6095750A (en) * | 1998-12-21 | 2000-08-01 | General Electric Company | Turbine nozzle assembly |
-
1999
- 1999-05-31 IT IT1999MI001206A patent/ITMI991206A1/it unknown
-
2000
- 2000-05-26 US US09/579,521 patent/US6343463B1/en not_active Expired - Lifetime
- 2000-05-29 DZ DZ000097A patent/DZ3087A1/xx active
- 2000-05-30 NO NO20002768A patent/NO330517B1/no not_active IP Right Cessation
- 2000-05-30 RU RU2000113795/06A patent/RU2223406C2/ru active
- 2000-05-31 AR ARP000102688A patent/AR024169A1/es not_active Application Discontinuation
- 2000-05-31 EP EP00304617A patent/EP1057975B1/en not_active Expired - Lifetime
- 2000-05-31 ES ES00304617T patent/ES2286985T3/es not_active Expired - Lifetime
- 2000-05-31 BR BR0002531-3A patent/BR0002531A/pt not_active IP Right Cessation
- 2000-05-31 DE DE60034993T patent/DE60034993T2/de not_active Expired - Lifetime
- 2000-05-31 MX MXPA00005372A patent/MXPA00005372A/es unknown
- 2000-05-31 EG EG20000716A patent/EG22056A/xx active
Also Published As
Publication number | Publication date |
---|---|
ITMI991206A1 (it) | 2000-12-01 |
ITMI991206A0 (it) | 1999-05-31 |
EP1057975A3 (en) | 2004-03-24 |
EP1057975B1 (en) | 2007-05-30 |
EG22056A (en) | 2002-06-30 |
NO20002768D0 (no) | 2000-05-30 |
NO330517B1 (no) | 2011-05-09 |
US6343463B1 (en) | 2002-02-05 |
DE60034993D1 (de) | 2007-07-12 |
ES2286985T3 (es) | 2007-12-16 |
AR024169A1 (es) | 2002-09-04 |
MXPA00005372A (es) | 2002-04-24 |
RU2223406C2 (ru) | 2004-02-10 |
DE60034993T2 (de) | 2007-12-20 |
EP1057975A2 (en) | 2000-12-06 |
BR0002531A (pt) | 2001-01-02 |
DZ3087A1 (fr) | 2004-06-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM1K | Lapsed by not paying the annual fees |