JP4737879B2 - シュラウド冷却セグメント及び組立体 - Google Patents
シュラウド冷却セグメント及び組立体 Download PDFInfo
- Publication number
- JP4737879B2 JP4737879B2 JP2001225352A JP2001225352A JP4737879B2 JP 4737879 B2 JP4737879 B2 JP 4737879B2 JP 2001225352 A JP2001225352 A JP 2001225352A JP 2001225352 A JP2001225352 A JP 2001225352A JP 4737879 B2 JP4737879 B2 JP 4737879B2
- Authority
- JP
- Japan
- Prior art keywords
- shroud
- cooling
- side panel
- cooling air
- turbine
- 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
- 238000001816 cooling Methods 0.000 title claims description 156
- 239000007789 gas Substances 0.000 description 54
- 238000002485 combustion reaction Methods 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 6
- 238000007254 oxidation reaction Methods 0.000 description 6
- 238000013459 approach Methods 0.000 description 5
- 238000012546 transfer Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000037406 food intake Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
-
- 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
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/14—Casings modified therefor
-
- 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
-
- 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
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
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 |
|---|---|---|---|
| US09/627,050 US6354795B1 (en) | 2000-07-27 | 2000-07-27 | Shroud cooling segment and assembly |
| US09/627050 | 2000-07-27 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2002089206A JP2002089206A (ja) | 2002-03-27 |
| JP2002089206A5 JP2002089206A5 (enExample) | 2008-09-11 |
| JP4737879B2 true JP4737879B2 (ja) | 2011-08-03 |
Family
ID=24512969
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001225352A Expired - Fee Related JP4737879B2 (ja) | 2000-07-27 | 2001-07-26 | シュラウド冷却セグメント及び組立体 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6354795B1 (enExample) |
| EP (1) | EP1176285B1 (enExample) |
| JP (1) | JP4737879B2 (enExample) |
| DE (1) | DE60128865T2 (enExample) |
Families Citing this family (100)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6899518B2 (en) | 2002-12-23 | 2005-05-31 | Pratt & Whitney Canada Corp. | Turbine shroud segment apparatus for reusing cooling air |
| US7186078B2 (en) * | 2003-07-04 | 2007-03-06 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine shroud segment |
| WO2005003520A1 (en) | 2003-07-04 | 2005-01-13 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine shroud segment |
| JP4200846B2 (ja) * | 2003-07-04 | 2008-12-24 | 株式会社Ihi | シュラウドセグメント |
| US7147432B2 (en) * | 2003-11-24 | 2006-12-12 | General Electric Company | Turbine shroud asymmetrical cooling elements |
| US6942445B2 (en) * | 2003-12-04 | 2005-09-13 | Honeywell International Inc. | Gas turbine cooled shroud assembly with hot gas ingestion suppression |
| US6997673B2 (en) * | 2003-12-11 | 2006-02-14 | Honeywell International, Inc. | Gas turbine high temperature turbine blade outer air seal assembly |
| US7434402B2 (en) * | 2005-03-29 | 2008-10-14 | Siemens Power Generation, Inc. | System for actively controlling compressor clearances |
| US7708518B2 (en) * | 2005-06-23 | 2010-05-04 | Siemens Energy, Inc. | Turbine blade tip clearance control |
| EP1744016A1 (de) * | 2005-07-11 | 2007-01-17 | Siemens Aktiengesellschaft | Heissgasführendes Gehäuseelement, Wellenschutzmantel und Gasturbinenanlage |
| US7588412B2 (en) * | 2005-07-28 | 2009-09-15 | General Electric Company | Cooled shroud assembly and method of cooling a shroud |
| US7387488B2 (en) * | 2005-08-05 | 2008-06-17 | General Electric Company | Cooled turbine shroud |
| US7452183B2 (en) * | 2005-08-06 | 2008-11-18 | General Electric Company | Thermally compliant turbine shroud assembly |
| US7448846B2 (en) * | 2005-08-06 | 2008-11-11 | General Electric Company | Thermally compliant turbine shroud mounting |
| US7438520B2 (en) * | 2005-08-06 | 2008-10-21 | General Electric Company | Thermally compliant turbine shroud mounting assembly |
| US7442004B2 (en) * | 2005-08-06 | 2008-10-28 | General Electric Company | Thermally compliant C-clip |
| US7296967B2 (en) * | 2005-09-13 | 2007-11-20 | General Electric Company | Counterflow film cooled wall |
| US7278820B2 (en) * | 2005-10-04 | 2007-10-09 | Siemens Power Generation, Inc. | Ring seal system with reduced cooling requirements |
| US7377742B2 (en) * | 2005-10-14 | 2008-05-27 | General Electric Company | Turbine shroud assembly and method for assembling a gas turbine engine |
| CA2580102A1 (en) * | 2006-03-06 | 2007-09-06 | General Electric Company | System and method for monitoring drilling process parameters and controlling drilling operation |
| US7665960B2 (en) | 2006-08-10 | 2010-02-23 | United Technologies Corporation | Turbine shroud thermal distortion control |
| US7771160B2 (en) * | 2006-08-10 | 2010-08-10 | United Technologies Corporation | Ceramic shroud assembly |
| FR2907841B1 (fr) * | 2006-10-30 | 2011-04-15 | Snecma | Secteur d'anneau de turbine de turbomachine |
| US7740443B2 (en) * | 2006-11-15 | 2010-06-22 | General Electric Company | Transpiration clearance control turbine |
| US7740442B2 (en) * | 2006-11-30 | 2010-06-22 | General Electric Company | Methods and system for cooling integral turbine nozzle and shroud assemblies |
| US7722315B2 (en) * | 2006-11-30 | 2010-05-25 | General Electric Company | Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly |
| US7740444B2 (en) * | 2006-11-30 | 2010-06-22 | General Electric Company | Methods and system for cooling integral turbine shround assemblies |
| US7785067B2 (en) * | 2006-11-30 | 2010-08-31 | General Electric Company | Method and system to facilitate cooling turbine engines |
| US7690885B2 (en) * | 2006-11-30 | 2010-04-06 | General Electric Company | Methods and system for shielding cooling air to facilitate cooling integral turbine nozzle and shroud assemblies |
| US7611324B2 (en) * | 2006-11-30 | 2009-11-03 | General Electric Company | Method and system to facilitate enhanced local cooling of turbine engines |
| US7604453B2 (en) * | 2006-11-30 | 2009-10-20 | General Electric Company | Methods and system for recuperated circumferential cooling of integral turbine nozzle and shroud assemblies |
| US7665953B2 (en) * | 2006-11-30 | 2010-02-23 | General Electric Company | Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies |
| GB2444501B (en) * | 2006-12-06 | 2009-01-28 | Siemens Ag | A gas turbine |
| US8123466B2 (en) * | 2007-03-01 | 2012-02-28 | United Technologies Corporation | Blade outer air seal |
| US7704039B1 (en) | 2007-03-21 | 2010-04-27 | Florida Turbine Technologies, Inc. | BOAS with multiple trenched film cooling slots |
| SI2137382T1 (sl) | 2007-04-19 | 2012-10-30 | Alstom Technology Ltd | Statorski toplotni ščit |
| US7874792B2 (en) | 2007-10-01 | 2011-01-25 | United Technologies Corporation | Blade outer air seals, cores, and manufacture methods |
| US8061979B1 (en) | 2007-10-19 | 2011-11-22 | Florida Turbine Technologies, Inc. | Turbine BOAS with edge cooling |
| US8104292B2 (en) * | 2007-12-17 | 2012-01-31 | General Electric Company | Duplex turbine shroud |
| US8246297B2 (en) | 2008-07-21 | 2012-08-21 | Pratt & Whitney Canada Corp. | Shroud segment cooling configuration |
| CH699232A1 (de) * | 2008-07-22 | 2010-01-29 | Alstom Technology Ltd | Gasturbine. |
| US8147192B2 (en) * | 2008-09-19 | 2012-04-03 | General Electric Company | Dual stage turbine shroud |
| US8123473B2 (en) * | 2008-10-31 | 2012-02-28 | General Electric Company | Shroud hanger with diffused cooling passage |
| US8128344B2 (en) * | 2008-11-05 | 2012-03-06 | General Electric Company | Methods and apparatus involving shroud cooling |
| GB0910177D0 (en) * | 2009-06-15 | 2009-07-29 | Rolls Royce Plc | A cooled component for a gas turbine engine |
| US8167546B2 (en) * | 2009-09-01 | 2012-05-01 | United Technologies Corporation | Ceramic turbine shroud support |
| US8371800B2 (en) * | 2010-03-03 | 2013-02-12 | General Electric Company | Cooling gas turbine components with seal slot channels |
| EP2378071A1 (en) * | 2010-04-16 | 2011-10-19 | Siemens Aktiengesellschaft | Turbine assembly having cooling arrangement and method of cooling |
| GB201012783D0 (en) * | 2010-07-30 | 2010-09-15 | Rolls Royce Plc | Turbine stage shroud segment |
| GB201014802D0 (en) * | 2010-09-07 | 2010-10-20 | Rolls Royce Plc | Turbine stage shroud segment |
| FR2968350B1 (fr) * | 2010-12-06 | 2016-01-29 | Snecma | Anneau sectorise de turbine pour turbomachine, et turbomachine equipee d'un tel anneau |
| US8444372B2 (en) * | 2011-02-07 | 2013-05-21 | General Electric Company | Passive cooling system for a turbomachine |
| US9039350B2 (en) * | 2012-01-09 | 2015-05-26 | General Electric Company | Impingement cooling system for use with contoured surfaces |
| US9103225B2 (en) * | 2012-06-04 | 2015-08-11 | United Technologies Corporation | Blade outer air seal with cored passages |
| US9422824B2 (en) * | 2012-10-18 | 2016-08-23 | General Electric Company | Gas turbine thermal control and related method |
| US9238971B2 (en) * | 2012-10-18 | 2016-01-19 | General Electric Company | Gas turbine casing thermal control device |
| WO2014186005A2 (en) * | 2013-02-15 | 2014-11-20 | United Technologies Corporation | Gas turbine engine component with combined mate face and platform cooling |
| CN103133063A (zh) * | 2013-03-01 | 2013-06-05 | 哈尔滨汽轮机厂有限责任公司 | 重型中低热值燃机涡轮第一级动叶护环冷却机构 |
| EP2971521B1 (en) | 2013-03-11 | 2022-06-22 | Rolls-Royce Corporation | Gas turbine engine flow path geometry |
| GB201308602D0 (en) * | 2013-05-14 | 2013-06-19 | Rolls Royce Plc | A Shroud Arrangement for a Gas Turbine Engine |
| GB201311333D0 (en) | 2013-06-26 | 2013-08-14 | Rolls Royce Plc | Component for use in releasing a flow of material into an environment subject to periodic fluctuations in pressure |
| WO2015013503A1 (en) | 2013-07-24 | 2015-01-29 | United Technologies Corporation | Trough seal for gas turbine engine |
| US9988923B2 (en) | 2013-08-29 | 2018-06-05 | United Technologies Corporation | Seal for gas turbine engine |
| US9518478B2 (en) * | 2013-10-28 | 2016-12-13 | General Electric Company | Microchannel exhaust for cooling and/or purging gas turbine segment gaps |
| JP6233578B2 (ja) * | 2013-12-05 | 2017-11-22 | 株式会社Ihi | タービン |
| US20150198063A1 (en) | 2014-01-14 | 2015-07-16 | Alstom Technology Ltd | Cooled stator heat shield |
| EP3191689B1 (en) | 2014-09-08 | 2019-11-06 | Siemens Energy, Inc. | A cooled turbine vane platform comprising forward, midchord and aft cooling chambers in the platform |
| EP3023596B1 (en) * | 2014-11-20 | 2019-01-02 | United Technologies Corporation | Internally cooled turbine platform |
| US10018068B2 (en) * | 2015-01-13 | 2018-07-10 | United Technologies Corporation | Blade outer air seal with cooling holes |
| US10641099B1 (en) | 2015-02-09 | 2020-05-05 | United Technologies Corporation | Impingement cooling for a gas turbine engine component |
| US20160237850A1 (en) * | 2015-02-16 | 2016-08-18 | United Technologies Corporation | Systems and methods for vane cooling |
| JP6567072B2 (ja) | 2015-03-17 | 2019-08-28 | シーメンス エナジー インコーポレイテッド | 漏れ流調整装置を備えるシュラウド付きタービン翼 |
| US10221713B2 (en) * | 2015-05-26 | 2019-03-05 | Rolls-Royce Corporation | Shroud cartridge having a ceramic matrix composite seal segment |
| US9869202B2 (en) * | 2015-08-14 | 2018-01-16 | United Technologies Corporation | Blade outer air seal for a gas turbine engine |
| RU2706210C2 (ru) | 2016-01-25 | 2019-11-14 | Ансалдо Энерджиа Свитзерлэнд Аг | Тепловой экран статора для газовой турбины, газовая турбина с таким тепловым экраном статора и способ охлаждения теплового экрана статора |
| US10837300B2 (en) * | 2016-11-01 | 2020-11-17 | General Electric Company | Seal pressurization in box shroud |
| US20180355754A1 (en) * | 2017-02-24 | 2018-12-13 | General Electric Company | Spline for a turbine engine |
| US10648362B2 (en) * | 2017-02-24 | 2020-05-12 | General Electric Company | Spline for a turbine engine |
| US10655495B2 (en) * | 2017-02-24 | 2020-05-19 | General Electric Company | Spline for a turbine engine |
| US20180340437A1 (en) * | 2017-02-24 | 2018-11-29 | General Electric Company | Spline for a turbine engine |
| US20180355741A1 (en) * | 2017-02-24 | 2018-12-13 | General Electric Company | Spline for a turbine engine |
| US10436041B2 (en) | 2017-04-07 | 2019-10-08 | General Electric Company | Shroud assembly for turbine systems |
| US10677084B2 (en) | 2017-06-16 | 2020-06-09 | Honeywell International Inc. | Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement |
| US10900378B2 (en) * | 2017-06-16 | 2021-01-26 | Honeywell International Inc. | Turbine tip shroud assembly with plural shroud segments having internal cooling passages |
| FR3070718B1 (fr) * | 2017-09-06 | 2019-08-23 | Safran Aircraft Engines | Ensemble de turbine a secteurs d'anneau |
| FR3070716B1 (fr) * | 2017-09-06 | 2020-10-02 | Safran Aircraft Engines | Languette d'etancheite de segments de stator |
| US10502093B2 (en) * | 2017-12-13 | 2019-12-10 | Pratt & Whitney Canada Corp. | Turbine shroud cooling |
| US10989068B2 (en) | 2018-07-19 | 2021-04-27 | General Electric Company | Turbine shroud including plurality of cooling passages |
| US10907501B2 (en) | 2018-08-21 | 2021-02-02 | General Electric Company | Shroud hanger assembly cooling |
| US10982559B2 (en) * | 2018-08-24 | 2021-04-20 | General Electric Company | Spline seal with cooling features for turbine engines |
| US10907487B2 (en) * | 2018-10-16 | 2021-02-02 | Honeywell International Inc. | Turbine shroud assemblies for gas turbine engines |
| US10837315B2 (en) * | 2018-10-25 | 2020-11-17 | General Electric Company | Turbine shroud including cooling passages in communication with collection plenums |
| GB2584299A (en) | 2019-05-29 | 2020-12-02 | Siemens Ag | Heatshield for gas turbine engine |
| US11187094B2 (en) * | 2019-08-26 | 2021-11-30 | General Electric Company | Spline for a turbine engine |
| FR3108367B1 (fr) | 2020-03-20 | 2023-07-21 | Safran Aircraft Engines | Ensemble de turbine et turbomachine munie d’un tel ensemble |
| US11566532B2 (en) | 2020-12-04 | 2023-01-31 | Ge Avio S.R.L. | Turbine clearance control system |
| KR102510535B1 (ko) * | 2021-02-23 | 2023-03-15 | 두산에너빌리티 주식회사 | 링 세그먼트 및 이를 포함하는 터보머신 |
| KR102675092B1 (ko) * | 2021-11-30 | 2024-06-12 | 두산에너빌리티 주식회사 | 링세그먼트 및 이를 포함하는 터빈 |
| EP4332351A1 (en) * | 2022-09-05 | 2024-03-06 | General Electric Company Polska Sp. Z o.o | Turbine rotor outer casing assembly |
| US12410730B1 (en) * | 2024-04-23 | 2025-09-09 | Ge Infrastructure Technology, Llc | Turbine shroud and turbomachine with cooling circuit |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3777484A (en) | 1971-12-08 | 1973-12-11 | Gen Electric | Shrouded combustion liner |
| US3825364A (en) | 1972-06-09 | 1974-07-23 | Gen Electric | Porous abradable turbine shroud |
| US4127357A (en) | 1977-06-24 | 1978-11-28 | General Electric Company | Variable shroud for a turbomachine |
| US4157232A (en) | 1977-10-31 | 1979-06-05 | General Electric Company | Turbine shroud support |
| US4177004A (en) | 1977-10-31 | 1979-12-04 | General Electric Company | Combined turbine shroud and vane support structure |
| US4303371A (en) | 1978-06-05 | 1981-12-01 | General Electric Company | Shroud support with impingement baffle |
| US4573865A (en) | 1981-08-31 | 1986-03-04 | General Electric Company | Multiple-impingement cooled structure |
| US4526226A (en) | 1981-08-31 | 1985-07-02 | General Electric Company | Multiple-impingement cooled structure |
| US5071313A (en) | 1990-01-16 | 1991-12-10 | General Electric Company | Rotor blade shroud segment |
| US5127793A (en) | 1990-05-31 | 1992-07-07 | General Electric Company | Turbine shroud clearance control assembly |
| US5074748A (en) | 1990-07-30 | 1991-12-24 | General Electric Company | Seal assembly for segmented turbine engine structures |
| US5088888A (en) | 1990-12-03 | 1992-02-18 | General Electric Company | Shroud seal |
| US5116199A (en) | 1990-12-20 | 1992-05-26 | General Electric Company | Blade tip clearance control apparatus using shroud segment annular support ring thermal expansion |
| US5165847A (en) * | 1991-05-20 | 1992-11-24 | General Electric Company | Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines |
| US5169287A (en) * | 1991-05-20 | 1992-12-08 | General Electric Company | Shroud cooling assembly for gas turbine engine |
| US5188506A (en) | 1991-08-28 | 1993-02-23 | General Electric Company | Apparatus and method for preventing leakage of cooling air in a shroud assembly of a gas turbine engine |
| US5273396A (en) | 1992-06-22 | 1993-12-28 | General Electric Company | Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud |
| US5375973A (en) * | 1992-12-23 | 1994-12-27 | United Technologies Corporation | Turbine blade outer air seal with optimized cooling |
| US5391052A (en) | 1993-11-16 | 1995-02-21 | General Electric Co. | Impingement cooling and cooling medium retrieval system for turbine shrouds and methods of operation |
| US5480281A (en) | 1994-06-30 | 1996-01-02 | General Electric Co. | Impingement cooling apparatus for turbine shrouds having ducts of increasing cross-sectional area in the direction of post-impingement cooling flow |
| US5584651A (en) | 1994-10-31 | 1996-12-17 | General Electric Company | Cooled shroud |
| US5641267A (en) | 1995-06-06 | 1997-06-24 | General Electric Company | Controlled leakage shroud panel |
| US5993150A (en) | 1998-01-16 | 1999-11-30 | General Electric Company | Dual cooled shroud |
| EP1022437A1 (de) * | 1999-01-19 | 2000-07-26 | Siemens Aktiengesellschaft | Bauteil zur Verwendung in einer thermischen Machine |
-
2000
- 2000-07-27 US US09/627,050 patent/US6354795B1/en not_active Expired - Fee Related
-
2001
- 2001-07-26 JP JP2001225352A patent/JP4737879B2/ja not_active Expired - Fee Related
- 2001-07-26 DE DE60128865T patent/DE60128865T2/de not_active Expired - Lifetime
- 2001-07-26 EP EP01306419A patent/EP1176285B1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1176285B1 (en) | 2007-06-13 |
| DE60128865D1 (de) | 2007-07-26 |
| JP2002089206A (ja) | 2002-03-27 |
| EP1176285A2 (en) | 2002-01-30 |
| EP1176285A3 (en) | 2004-01-14 |
| US6354795B1 (en) | 2002-03-12 |
| DE60128865T2 (de) | 2008-02-21 |
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