DE60017486D1 - Verriegelte Statorbeschaufelung eines Kompressors - Google Patents
Verriegelte Statorbeschaufelung eines KompressorsInfo
- Publication number
- DE60017486D1 DE60017486D1 DE60017486T DE60017486T DE60017486D1 DE 60017486 D1 DE60017486 D1 DE 60017486D1 DE 60017486 T DE60017486 T DE 60017486T DE 60017486 T DE60017486 T DE 60017486T DE 60017486 D1 DE60017486 D1 DE 60017486D1
- Authority
- DE
- Germany
- Prior art keywords
- compressor
- stator blading
- locked
- locked stator
- blading
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/267,259 US6234750B1 (en) | 1999-03-12 | 1999-03-12 | Interlocked compressor stator |
Publications (1)
Publication Number | Publication Date |
---|---|
DE60017486D1 true DE60017486D1 (de) | 2005-02-24 |
Family
ID=23018012
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60017486T Expired - Fee Related DE60017486D1 (de) | 1999-03-12 | 2000-01-25 | Verriegelte Statorbeschaufelung eines Kompressors |
Country Status (4)
Country | Link |
---|---|
US (1) | US6234750B1 (de) |
EP (1) | EP1041249B1 (de) |
JP (1) | JP2000320497A (de) |
DE (1) | DE60017486D1 (de) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7008170B2 (en) * | 2004-03-26 | 2006-03-07 | Siemens Westinghouse Power Corporation | Compressor diaphragm with axial preload |
US7097420B2 (en) * | 2004-04-14 | 2006-08-29 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
FR2906296A1 (fr) * | 2006-09-26 | 2008-03-28 | Snecma Sa | Dispositif de fixation d'une aube fixe dans un carter annulaire de turbomachine, turboreacteur incorporant le dispositif et procede de montage de l'aube. |
US7758307B2 (en) * | 2007-05-17 | 2010-07-20 | Siemens Energy, Inc. | Wear minimization system for a compressor diaphragm |
US8047778B2 (en) * | 2009-01-06 | 2011-11-01 | General Electric Company | Method and apparatus for insuring proper installation of stators in a compressor case |
US8070429B2 (en) * | 2009-03-11 | 2011-12-06 | General Electric Company | Turbine singlet nozzle assembly with mechanical and weld fabrication |
US9863321B2 (en) | 2011-12-29 | 2018-01-09 | Elliott Company | Hot gas expander inlet casing assembly and method |
US9097124B2 (en) * | 2012-01-24 | 2015-08-04 | United Technologies Corporation | Gas turbine engine stator vane assembly with inner shroud |
US20140030083A1 (en) * | 2012-07-24 | 2014-01-30 | General Electric Company | Article of manufacture for turbomachine |
EP2966264B1 (de) * | 2014-07-07 | 2021-09-22 | Safran Aero Boosters SA | Laufradschaufelsegment eines Verdichters eines axialen Turbotriebwerks |
US10072516B2 (en) * | 2014-09-24 | 2018-09-11 | United Technologies Corporation | Clamped vane arc segment having load-transmitting features |
WO2016068859A1 (en) * | 2014-10-28 | 2016-05-06 | Siemens Energy, Inc. | Modular turbine vane |
US10378371B2 (en) * | 2014-12-18 | 2019-08-13 | United Technologies Corporation | Anti-rotation vane |
US10309240B2 (en) * | 2015-07-24 | 2019-06-04 | General Electric Company | Method and system for interfacing a ceramic matrix composite component to a metallic component |
US11073033B2 (en) * | 2018-10-18 | 2021-07-27 | Honeywell International Inc. | Stator attachment system for gas turbine engine |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2799473A (en) * | 1955-04-27 | 1957-07-16 | Gen Electric | Gas turbine nozzle ring |
US3085398A (en) * | 1961-01-10 | 1963-04-16 | Gen Electric | Variable-clearance shroud structure for gas turbine engines |
US3142475A (en) * | 1962-12-28 | 1964-07-28 | Gen Electric | Stator assembly |
US3302926A (en) * | 1965-12-06 | 1967-02-07 | Gen Electric | Segmented nozzle diaphragm for high temperature turbine |
US3443791A (en) * | 1966-11-23 | 1969-05-13 | United Aircraft Corp | Turbine vane assembly |
US3423071A (en) * | 1967-07-17 | 1969-01-21 | United Aircraft Corp | Turbine vane retention |
DE2121707C3 (de) * | 1971-05-03 | 1974-06-20 | Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Leitschaufelkranz |
US3728041A (en) * | 1971-10-04 | 1973-04-17 | Gen Electric | Fluidic seal for segmented nozzle diaphragm |
US3918832A (en) * | 1974-07-29 | 1975-11-11 | United Technologies Corp | Stator construction for an axial flow compressor |
US3985465A (en) * | 1975-06-25 | 1976-10-12 | United Technologies Corporation | Turbomachine with removable stator vane |
US3970318A (en) * | 1975-09-26 | 1976-07-20 | General Electric Company | Sealing means for a segmented ring |
US4126405A (en) | 1976-12-16 | 1978-11-21 | General Electric Company | Turbine nozzle |
IT1167241B (it) | 1983-10-03 | 1987-05-13 | Nuovo Pignone Spa | Sistema perfezionato per il fissaggio degli ugelli statorici alla cassa di una turbina di potenza |
US4639189A (en) * | 1984-02-27 | 1987-01-27 | Rockwell International Corporation | Hollow, thermally-conditioned, turbine stator nozzle |
US4621976A (en) * | 1985-04-23 | 1986-11-11 | United Technologies Corporation | Integrally cast vane and shroud stator with damper |
US5154577A (en) * | 1991-01-17 | 1992-10-13 | General Electric Company | Flexible three-piece seal assembly |
US5149250A (en) * | 1991-02-28 | 1992-09-22 | General Electric Company | Gas turbine vane assembly seal and support system |
US5197856A (en) * | 1991-06-24 | 1993-03-30 | General Electric Company | Compressor stator |
US5176496A (en) | 1991-09-27 | 1993-01-05 | General Electric Company | Mounting arrangements for turbine nozzles |
US5248240A (en) * | 1993-02-08 | 1993-09-28 | General Electric Company | Turbine stator vane assembly |
US5846050A (en) * | 1997-07-14 | 1998-12-08 | General Electric Company | Vane sector spring |
-
1999
- 1999-03-12 US US09/267,259 patent/US6234750B1/en not_active Expired - Fee Related
-
2000
- 2000-01-24 JP JP2000013791A patent/JP2000320497A/ja not_active Withdrawn
- 2000-01-25 DE DE60017486T patent/DE60017486D1/de not_active Expired - Fee Related
- 2000-01-25 EP EP00300523A patent/EP1041249B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP2000320497A (ja) | 2000-11-21 |
US6234750B1 (en) | 2001-05-22 |
EP1041249B1 (de) | 2005-01-19 |
EP1041249A2 (de) | 2000-10-04 |
EP1041249A3 (de) | 2000-10-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8339 | Ceased/non-payment of the annual fee |