CN103195516B - 涡轮机械系统及其部件和将盖板连接到涡轮机械部件的方法 - Google Patents
涡轮机械系统及其部件和将盖板连接到涡轮机械部件的方法 Download PDFInfo
- Publication number
- CN103195516B CN103195516B CN201310007885.3A CN201310007885A CN103195516B CN 103195516 B CN103195516 B CN 103195516B CN 201310007885 A CN201310007885 A CN 201310007885A CN 103195516 B CN103195516 B CN 103195516B
- Authority
- CN
- China
- Prior art keywords
- mounting
- fastener
- cover plate
- mounting member
- component
- 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.)
- Active
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
- 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
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49236—Fluid pump or compressor making
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 (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/345,959 US9133724B2 (en) | 2012-01-09 | 2012-01-09 | Turbomachine component including a cover plate |
| US13/345,959 | 2012-01-09 | ||
| US13/345959 | 2012-01-09 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103195516A CN103195516A (zh) | 2013-07-10 |
| CN103195516B true CN103195516B (zh) | 2017-03-01 |
Family
ID=47678561
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310007885.3A Active CN103195516B (zh) | 2012-01-09 | 2013-01-09 | 涡轮机械系统及其部件和将盖板连接到涡轮机械部件的方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9133724B2 (https=) |
| EP (1) | EP2613005B1 (https=) |
| JP (1) | JP6604600B2 (https=) |
| CN (1) | CN103195516B (https=) |
| RU (1) | RU2614474C2 (https=) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201213109D0 (en) * | 2012-07-24 | 2012-09-05 | Rolls Royce Plc | Seal segment |
| JP6209375B2 (ja) | 2013-07-08 | 2017-10-04 | 株式会社日本マイクロニクス | 電気的接続装置 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1164252A2 (en) * | 2000-06-13 | 2001-12-19 | General Electric Company | Support pedestals for a wall cover in a gas turbine nozzle segment |
| US6382906B1 (en) * | 2000-06-16 | 2002-05-07 | General Electric Company | Floating spoolie cup impingement baffle |
| US7326030B2 (en) * | 2005-02-02 | 2008-02-05 | Siemens Power Generation, Inc. | Support system for a composite airfoil in a turbine engine |
Family Cites Families (56)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4187054A (en) | 1978-04-20 | 1980-02-05 | General Electric Company | Turbine band cooling system |
| JPS6166802A (ja) | 1984-09-10 | 1986-04-05 | Mitsubishi Heavy Ind Ltd | ガスタ−ビンのタ−ビン翼 |
| JP3142850B2 (ja) | 1989-03-13 | 2001-03-07 | 株式会社東芝 | タービンの冷却翼および複合発電プラント |
| US5197852A (en) | 1990-05-31 | 1993-03-30 | General Electric Company | Nozzle band overhang cooling |
| US5320483A (en) | 1992-12-30 | 1994-06-14 | General Electric Company | Steam and air cooling for stator stage of a turbine |
| WO1996015357A1 (en) | 1994-11-10 | 1996-05-23 | Westinghouse Electric Corporation | Gas turbine vane with a cooled inner shroud |
| US6383602B1 (en) | 1996-12-23 | 2002-05-07 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture |
| JP3316415B2 (ja) | 1997-05-01 | 2002-08-19 | 三菱重工業株式会社 | ガスタービン冷却静翼 |
| US6217279B1 (en) | 1997-06-19 | 2001-04-17 | Mitsubishi Heavy Industries, Ltd. | Device for sealing gas turbine stator blades |
| US6227798B1 (en) | 1999-11-30 | 2001-05-08 | General Electric Company | Turbine nozzle segment band cooling |
| US6386825B1 (en) | 2000-04-11 | 2002-05-14 | General Electric Company | Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment |
| US6419445B1 (en) | 2000-04-11 | 2002-07-16 | General Electric Company | Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment |
| US6418618B1 (en) | 2000-04-11 | 2002-07-16 | General Electric Company | Method of controlling the side wall thickness of a turbine nozzle segment for improved cooling |
| DE10131073A1 (de) * | 2000-12-16 | 2002-06-20 | Alstom Switzerland Ltd | Vorrichtung zur Kühlung eines Deckbandes einer Gasturbinenschaufel |
| US6530744B2 (en) | 2001-05-29 | 2003-03-11 | General Electric Company | Integral nozzle and shroud |
| US6503051B2 (en) | 2001-06-06 | 2003-01-07 | General Electric Company | Overlapping interference seal and methods for forming the seal |
| US6652220B2 (en) | 2001-11-15 | 2003-11-25 | General Electric Company | Methods and apparatus for cooling gas turbine nozzles |
| US6769865B2 (en) | 2002-03-22 | 2004-08-03 | General Electric Company | Band cooled turbine nozzle |
| US6761529B2 (en) | 2002-07-25 | 2004-07-13 | Mitshubishi Heavy Industries, Ltd. | Cooling structure of stationary blade, and gas turbine |
| US6843479B2 (en) | 2002-07-30 | 2005-01-18 | General Electric Company | Sealing of nozzle slashfaces in a steam turbine |
| DE60313979T2 (de) * | 2002-08-14 | 2008-03-13 | Volvo Aero Corp. | Verfahren zur herstellung einer statorkomponente |
| US6877952B2 (en) * | 2002-09-09 | 2005-04-12 | Florida Turbine Technologies, Inc | Passive clearance control |
| US6884026B2 (en) * | 2002-09-30 | 2005-04-26 | General Electric Company | Turbine engine shroud assembly including axially floating shroud segment |
| US7008185B2 (en) | 2003-02-27 | 2006-03-07 | General Electric Company | Gas turbine engine turbine nozzle bifurcated impingement baffle |
| US6932568B2 (en) | 2003-02-27 | 2005-08-23 | General Electric Company | Turbine nozzle segment cantilevered mount |
| FR2852053B1 (fr) * | 2003-03-06 | 2007-12-28 | Snecma Moteurs | Turbine haute pression pour turbomachine |
| CN1573018B (zh) * | 2003-05-20 | 2010-09-15 | 株式会社东芝 | 蒸汽涡轮机 |
| US6984101B2 (en) | 2003-07-14 | 2006-01-10 | Siemens Westinghouse Power Corporation | Turbine vane plate assembly |
| US7029228B2 (en) | 2003-12-04 | 2006-04-18 | General Electric Company | Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
| US7044709B2 (en) * | 2004-01-15 | 2006-05-16 | General Electric Company | Methods and apparatus for coupling ceramic matrix composite turbine components |
| US7094026B2 (en) | 2004-04-29 | 2006-08-22 | General Electric Company | System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor |
| US7252481B2 (en) | 2004-05-14 | 2007-08-07 | Pratt & Whitney Canada Corp. | Natural frequency tuning of gas turbine engine blades |
| US7219498B2 (en) | 2004-09-10 | 2007-05-22 | Honeywell International, Inc. | Waffled impingement effusion method |
| US7160078B2 (en) | 2004-09-23 | 2007-01-09 | General Electric Company | Mechanical solution for rail retention of turbine nozzles |
| US7140835B2 (en) | 2004-10-01 | 2006-11-28 | General Electric Company | Corner cooled turbine nozzle |
| US7494317B2 (en) * | 2005-06-23 | 2009-02-24 | Siemens Energy, Inc. | Ring seal attachment system |
| US20070009349A1 (en) * | 2005-07-11 | 2007-01-11 | General Electric Company | Impingement box for gas turbine shroud |
| US7338253B2 (en) | 2005-09-15 | 2008-03-04 | General Electric Company | Resilient seal on trailing edge of turbine inner shroud and method for shroud post impingement cavity sealing |
| US7278820B2 (en) * | 2005-10-04 | 2007-10-09 | Siemens Power Generation, Inc. | Ring seal system with reduced cooling requirements |
| US7918024B2 (en) | 2006-01-20 | 2011-04-05 | General Electric Company | Methods and apparatus for manufacturing components |
| US7534086B2 (en) * | 2006-05-05 | 2009-05-19 | Siemens Energy, Inc. | Multi-layer ring seal |
| US7726936B2 (en) * | 2006-07-25 | 2010-06-01 | Siemens Energy, Inc. | Turbine engine ring seal |
| US7669422B2 (en) | 2006-07-26 | 2010-03-02 | General Electric Company | Combustor liner and method of fabricating same |
| US7900433B2 (en) | 2006-08-31 | 2011-03-08 | United Technologies Corporation | Fan exhaust nozzle for turbofan engine |
| US8801370B2 (en) | 2006-10-12 | 2014-08-12 | General Electric Company | Turbine case impingement cooling for heavy duty gas turbines |
| US7950234B2 (en) * | 2006-10-13 | 2011-05-31 | Siemens Energy, Inc. | Ceramic matrix composite turbine engine components with unitary stiffening frame |
| US7798775B2 (en) | 2006-12-21 | 2010-09-21 | General Electric Company | Cantilevered nozzle with crowned flange to improve outer band low cycle fatigue |
| US7946801B2 (en) | 2007-12-27 | 2011-05-24 | General Electric Company | Multi-source gas turbine cooling |
| US8439639B2 (en) * | 2008-02-24 | 2013-05-14 | United Technologies Corporation | Filter system for blade outer air seal |
| US8118548B2 (en) | 2008-09-15 | 2012-02-21 | General Electric Company | Shroud for a turbomachine |
| US8142138B2 (en) | 2009-05-01 | 2012-03-27 | General Electric Company | Turbine engine having cooling pin |
| US20100284800A1 (en) | 2009-05-11 | 2010-11-11 | General Electric Company | Turbine nozzle with sidewall cooling plenum |
| EP2282012B1 (en) | 2009-07-03 | 2015-11-25 | Alstom Technology Ltd | Method for replacing a cover plate of a guide vane of a gas turbine |
| US8740551B2 (en) | 2009-08-18 | 2014-06-03 | Pratt & Whitney Canada Corp. | Blade outer air seal cooling |
| US8651802B2 (en) * | 2010-03-17 | 2014-02-18 | United Technologies Corporation | Cover plate for turbine vane assembly |
| US9011079B2 (en) | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine nozzle compartmentalized cooling system |
-
2012
- 2012-01-09 US US13/345,959 patent/US9133724B2/en active Active
- 2012-12-25 JP JP2012280447A patent/JP6604600B2/ja active Active
- 2012-12-27 RU RU2012158306A patent/RU2614474C2/ru active
-
2013
- 2013-01-03 EP EP13150157.9A patent/EP2613005B1/en active Active
- 2013-01-09 CN CN201310007885.3A patent/CN103195516B/zh active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1164252A2 (en) * | 2000-06-13 | 2001-12-19 | General Electric Company | Support pedestals for a wall cover in a gas turbine nozzle segment |
| US6382906B1 (en) * | 2000-06-16 | 2002-05-07 | General Electric Company | Floating spoolie cup impingement baffle |
| US7326030B2 (en) * | 2005-02-02 | 2008-02-05 | Siemens Power Generation, Inc. | Support system for a composite airfoil in a turbine engine |
Also Published As
| Publication number | Publication date |
|---|---|
| RU2614474C2 (ru) | 2017-03-28 |
| JP6604600B2 (ja) | 2019-11-13 |
| EP2613005A1 (en) | 2013-07-10 |
| US20130177408A1 (en) | 2013-07-11 |
| JP2013142390A (ja) | 2013-07-22 |
| US9133724B2 (en) | 2015-09-15 |
| EP2613005B1 (en) | 2015-11-04 |
| RU2012158306A (ru) | 2014-07-10 |
| CN103195516A (zh) | 2013-07-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2669579B1 (en) | Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same | |
| US9309783B2 (en) | Seal assembly for turbine system | |
| EP3415720B1 (en) | Turbine tip shroud assembly with plural shroud segments having internal cooling passages | |
| EP2587002B1 (en) | Turbomachine including an inner-to-outer turbine casing seal assembly and corresponding method of sealing | |
| CN102418602B (zh) | 包括cmc桥的涡轮机及其输送燃烧气体的方法 | |
| US9115808B2 (en) | Transition piece seal assembly for a turbomachine | |
| US10267162B2 (en) | Platform core feed for a multi-wall blade | |
| US10260362B2 (en) | Turbine vane assembly with ceramic matrix composite airfoil and friction fit metallic attachment features | |
| EP2581664A1 (en) | Annular Flow Conditioning Member for Gas Turbomachine Combustor Assembly | |
| US9303515B2 (en) | Turbomachine diaphragm and method of repairing a turbomachine diaphragm | |
| CN103195516B (zh) | 涡轮机械系统及其部件和将盖板连接到涡轮机械部件的方法 | |
| US8683805B2 (en) | Injector seal for a gas turbomachine | |
| US9915428B2 (en) | Cylinder of combustor, method of manufacturing of cylinder of combustor, and pressure vessel | |
| EP2617948A2 (en) | Near flow path seal for a turbomachine | |
| EP3048258A1 (en) | Inner seal for a turbomachine transition piece frame assembly | |
| US20160047313A1 (en) | Bushing for joining turbomachine components | |
| EP2530385A2 (en) | Turbomachine combustor assembly including a liner stop | |
| US20150047358A1 (en) | Inner barrel member with integrated diffuser for a gas turbomachine | |
| Lacy et al. | Shim for sealing transition pieces |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240103 Address after: Swiss Baden Patentee after: GENERAL ELECTRIC CO. LTD. Address before: New York State, USA Patentee before: General Electric Co. |