KR20080018118A - 터빈용 단일체 용접 노즐 하이브리드 설계 - Google Patents
터빈용 단일체 용접 노즐 하이브리드 설계 Download PDFInfo
- Publication number
- KR20080018118A KR20080018118A KR1020070083801A KR20070083801A KR20080018118A KR 20080018118 A KR20080018118 A KR 20080018118A KR 1020070083801 A KR1020070083801 A KR 1020070083801A KR 20070083801 A KR20070083801 A KR 20070083801A KR 20080018118 A KR20080018118 A KR 20080018118A
- Authority
- KR
- South Korea
- Prior art keywords
- turbine
- nozzle
- sidewall
- ring
- welded
- Prior art date
Links
Images
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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- 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
-
- 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
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
-
- 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
-
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
- F05D2240/56—Brush seals
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/508,170 | 2006-08-23 | ||
US11/508,170 US20080050222A1 (en) | 2006-08-23 | 2006-08-23 | Singlet welded nozzle hybrid design for a turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
KR20080018118A true KR20080018118A (ko) | 2008-02-27 |
Family
ID=38457865
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020070083801A KR20080018118A (ko) | 2006-08-23 | 2007-08-21 | 터빈용 단일체 용접 노즐 하이브리드 설계 |
Country Status (5)
Country | Link |
---|---|
US (1) | US20080050222A1 (zh) |
EP (1) | EP1898053A2 (zh) |
JP (1) | JP2008051105A (zh) |
KR (1) | KR20080018118A (zh) |
CN (1) | CN101131100A (zh) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8070429B2 (en) * | 2009-03-11 | 2011-12-06 | General Electric Company | Turbine singlet nozzle assembly with mechanical and weld fabrication |
GB201001072D0 (en) * | 2010-01-25 | 2010-03-10 | Rolls Royce Plc | Sealing arrangemant foa a gas turbine engine |
US8562292B2 (en) | 2010-12-02 | 2013-10-22 | General Electric Company | Steam turbine singlet interface for margin stage nozzles with pinned or bolted inner ring |
US8684697B2 (en) | 2010-12-13 | 2014-04-01 | General Electric Company | Steam turbine singlet nozzle design for breech loaded assembly |
US9011078B2 (en) * | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine vane seal carrier with slots for cooling and assembly |
US10436047B2 (en) | 2015-08-18 | 2019-10-08 | General Electric Company | Method for repair of a diaphragm of a rotary machine |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1998951A (en) * | 1933-11-15 | 1935-04-23 | Gen Electric | Nozzle diaphragm |
US3529905A (en) * | 1966-12-12 | 1970-09-22 | Gen Motors Corp | Cellular metal and seal |
DE1551193A1 (de) * | 1967-05-16 | 1970-03-12 | Licentia Gmbh | Schnellstartturbine |
US3501246A (en) * | 1967-12-29 | 1970-03-17 | Westinghouse Electric Corp | Axial fluid-flow machine |
US4889470A (en) * | 1988-08-01 | 1989-12-26 | Westinghouse Electric Corp. | Compressor diaphragm assembly |
US5622475A (en) * | 1994-08-30 | 1997-04-22 | General Electric Company | Double rabbet rotor blade retention assembly |
US5584654A (en) * | 1995-12-22 | 1996-12-17 | General Electric Company | Gas turbine engine fan stator |
JP3477347B2 (ja) * | 1997-07-30 | 2003-12-10 | 三菱重工業株式会社 | ガスタービン段間部シール装置 |
JP4040922B2 (ja) * | 2001-07-19 | 2008-01-30 | 株式会社東芝 | 組立式ノズルダイアフラムおよびその組立方法 |
US6896482B2 (en) * | 2003-09-03 | 2005-05-24 | General Electric Company | Expanding sealing strips for steam turbines |
US7160078B2 (en) * | 2004-09-23 | 2007-01-09 | General Electric Company | Mechanical solution for rail retention of turbine nozzles |
US7287956B2 (en) * | 2004-12-22 | 2007-10-30 | General Electric Company | Removable abradable seal carriers for sealing between rotary and stationary turbine components |
-
2006
- 2006-08-23 US US11/508,170 patent/US20080050222A1/en not_active Abandoned
-
2007
- 2007-08-15 EP EP07114373A patent/EP1898053A2/en not_active Withdrawn
- 2007-08-21 KR KR1020070083801A patent/KR20080018118A/ko not_active Application Discontinuation
- 2007-08-22 JP JP2007215703A patent/JP2008051105A/ja not_active Withdrawn
- 2007-08-23 CN CNA2007101427502A patent/CN101131100A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
JP2008051105A (ja) | 2008-03-06 |
CN101131100A (zh) | 2008-02-27 |
US20080050222A1 (en) | 2008-02-28 |
EP1898053A2 (en) | 2008-03-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3415720B1 (en) | Turbine tip shroud assembly with plural shroud segments having internal cooling passages | |
US11181006B2 (en) | Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement | |
KR20080018118A (ko) | 터빈용 단일체 용접 노즐 하이브리드 설계 | |
US7470109B2 (en) | Machine tooled diaphragm partitions and nozzles | |
JP2017040262A (ja) | ガスタービンエンジン用のスプリット端壁を有するcmcノズル | |
US20090191053A1 (en) | Diaphragm and blades for turbomachinery | |
KR101385799B1 (ko) | 터빈용 노즐 조립체 | |
JP2007198293A (ja) | 軸流圧縮機の静翼環 | |
US20090191050A1 (en) | Sealing band having bendable tang with anti-rotation in a turbine and associated methods | |
CN111868353B (zh) | 十字键防旋转间隔件 | |
JP2009041568A (ja) | 第1段シングレットノズルの外側側壁保持機構 | |
KR100228931B1 (ko) | 복류식 증기 터어빈내의 이용되는 재가열 터브 및 이의 개장방법 | |
US10619743B2 (en) | Splined honeycomb seals | |
US20220228502A1 (en) | Dynamic seal for a turbomachine comprising a multi-layer abradable part | |
KR102048874B1 (ko) | 유연성이 향상된 터빈 베인 | |
US10837316B2 (en) | High thermal response exhaust diffuser strut collar | |
US10208612B2 (en) | Gas turbine sealing band arrangement having an underlap seal | |
US10563528B2 (en) | Turbine vane with ceramic matrix composite airfoil | |
JP6884720B2 (ja) | 蒸気タービンのパッキンヘッド、及び蒸気タービン | |
US2777666A (en) | Turbine nozzle structure | |
US10001134B2 (en) | Rotor disc | |
JP2005113881A (ja) | タービン用シール構造、シールステータ、及びタービンノズルセグメント | |
JPS6261762B2 (zh) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WITN | Application deemed withdrawn, e.g. because no request for examination was filed or no examination fee was paid |