JP4731156B2 - タービンシュラウドの非対称冷却要素 - Google Patents
タービンシュラウドの非対称冷却要素 Download PDFInfo
- Publication number
- JP4731156B2 JP4731156B2 JP2004337529A JP2004337529A JP4731156B2 JP 4731156 B2 JP4731156 B2 JP 4731156B2 JP 2004337529 A JP2004337529 A JP 2004337529A JP 2004337529 A JP2004337529 A JP 2004337529A JP 4731156 B2 JP4731156 B2 JP 4731156B2
- Authority
- JP
- Japan
- Prior art keywords
- cooling
- opening
- shroud
- symmetrical
- impingement
- 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
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
- 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
-
- 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
- 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
- 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
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S165/00—Heat exchange
- Y10S165/908—Fluid jets
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 |
|---|---|---|---|
| US10/720,430 | 2003-11-24 | ||
| US10/720,430 US7147432B2 (en) | 2003-11-24 | 2003-11-24 | Turbine shroud asymmetrical cooling elements |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2005155626A JP2005155626A (ja) | 2005-06-16 |
| JP2005155626A5 JP2005155626A5 (enExample) | 2010-10-07 |
| JP4731156B2 true JP4731156B2 (ja) | 2011-07-20 |
Family
ID=34435822
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004337529A Expired - Fee Related JP4731156B2 (ja) | 2003-11-24 | 2004-11-22 | タービンシュラウドの非対称冷却要素 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7147432B2 (enExample) |
| EP (1) | EP1533478A3 (enExample) |
| JP (1) | JP4731156B2 (enExample) |
| CN (1) | CN100507234C (enExample) |
Families Citing this family (79)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7296966B2 (en) * | 2004-12-20 | 2007-11-20 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| US7438520B2 (en) * | 2005-08-06 | 2008-10-21 | General Electric Company | Thermally compliant turbine shroud mounting assembly |
| US7296967B2 (en) * | 2005-09-13 | 2007-11-20 | General Electric Company | Counterflow film cooled wall |
| FR2891862B1 (fr) * | 2005-10-12 | 2011-02-25 | Snecma | Plaque perforee a disposer dans une cavite de refroidissement d'anneau de turbine |
| US7607885B2 (en) * | 2006-07-31 | 2009-10-27 | General Electric Company | Methods and apparatus for operating gas turbine engines |
| FR2907841B1 (fr) * | 2006-10-30 | 2011-04-15 | Snecma | Secteur d'anneau de turbine de turbomachine |
| 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 |
| US7611324B2 (en) * | 2006-11-30 | 2009-11-03 | General Electric Company | Method and system to facilitate enhanced local cooling of turbine engines |
| 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 |
| US7836703B2 (en) * | 2007-06-20 | 2010-11-23 | General Electric Company | Reciprocal cooled turbine nozzle |
| US8393855B2 (en) * | 2007-06-29 | 2013-03-12 | General Electric Company | Flange with axially curved impingement surface for gas turbine engine clearance control |
| US8197186B2 (en) * | 2007-06-29 | 2012-06-12 | General Electric Company | Flange with axially extending holes for gas turbine engine clearance control |
| US20090053045A1 (en) * | 2007-08-22 | 2009-02-26 | General Electric Company | Turbine Shroud for Gas Turbine Assemblies and Processes for Forming the Shroud |
| US8104292B2 (en) * | 2007-12-17 | 2012-01-31 | General Electric Company | Duplex turbine shroud |
| US8281604B2 (en) * | 2007-12-17 | 2012-10-09 | General Electric Company | Divergent turbine nozzle |
| US8205458B2 (en) * | 2007-12-31 | 2012-06-26 | General Electric Company | Duplex turbine nozzle |
| US8439639B2 (en) * | 2008-02-24 | 2013-05-14 | United Technologies Corporation | Filter system for blade outer air seal |
| US8147192B2 (en) * | 2008-09-19 | 2012-04-03 | General Electric Company | Dual stage turbine shroud |
| DE102008052409A1 (de) * | 2008-10-21 | 2010-04-22 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsarbeitsmaschine mit saugseitennaher Randenergetisierung |
| CN102272419A (zh) * | 2009-03-09 | 2011-12-07 | 斯奈克玛 | 涡轮环组件 |
| US8677763B2 (en) * | 2009-03-10 | 2014-03-25 | General Electric Company | Method and apparatus for gas turbine engine temperature management |
| FR2957093B1 (fr) | 2010-03-02 | 2012-03-23 | Snecma | Preforme fibreuse pour un secteur d'anneau de turbine et son procede de fabrication. |
| US8371800B2 (en) * | 2010-03-03 | 2013-02-12 | General Electric Company | Cooling gas turbine components with seal slot channels |
| US10337404B2 (en) * | 2010-03-08 | 2019-07-02 | General Electric Company | Preferential cooling of gas turbine nozzles |
| US8550778B2 (en) * | 2010-04-20 | 2013-10-08 | Mitsubishi Heavy Industries, Ltd. | Cooling system of ring segment and gas turbine |
| JP5683573B2 (ja) * | 2010-04-20 | 2015-03-11 | 三菱重工業株式会社 | 分割環冷却構造およびガスタービン |
| GB201014802D0 (en) * | 2010-09-07 | 2010-10-20 | Rolls Royce Plc | Turbine stage shroud segment |
| US9458855B2 (en) * | 2010-12-30 | 2016-10-04 | Rolls-Royce North American Technologies Inc. | Compressor tip clearance control and gas turbine engine |
| US8887508B2 (en) * | 2011-03-15 | 2014-11-18 | General Electric Company | Impingement sleeve and methods for designing and forming impingement sleeve |
| US8826668B2 (en) * | 2011-08-02 | 2014-09-09 | Siemens Energy, Inc. | Two stage serial impingement cooling for isogrid structures |
| US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
| US9039350B2 (en) * | 2012-01-09 | 2015-05-26 | General Electric Company | Impingement cooling system for use with contoured surfaces |
| US9403600B2 (en) | 2012-05-01 | 2016-08-02 | Lockheed Martin Corporation | Integrated thermal protection and leakage reduction in a supersonic air intake system |
| US20130340966A1 (en) | 2012-06-21 | 2013-12-26 | United Technologies Corporation | Blade outer air seal hybrid casting core |
| EP2716787A1 (en) | 2012-10-05 | 2014-04-09 | Siemens Aktiengesellschaft | Method for manufacturing a turbine assembly |
| US9422824B2 (en) * | 2012-10-18 | 2016-08-23 | General Electric Company | Gas turbine thermal control and related method |
| JP5518235B2 (ja) * | 2013-05-10 | 2014-06-11 | 三菱重工業株式会社 | 分割環冷却構造およびガスタービン |
| GB201308603D0 (en) * | 2013-05-14 | 2013-06-19 | Rolls Royce Plc | A Shroud Arrangement for a Gas Turbine Engine |
| JP6114878B2 (ja) | 2013-05-17 | 2017-04-12 | ゼネラル・エレクトリック・カンパニイ | Cmcシュラウド支持システム |
| 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 |
| JP6529013B2 (ja) | 2013-12-12 | 2019-06-12 | ゼネラル・エレクトリック・カンパニイ | Cmcシュラウド支持システム |
| US9657642B2 (en) * | 2014-03-27 | 2017-05-23 | Honeywell International Inc. | Turbine sections of gas turbine engines with dual use of cooling air |
| JP6466647B2 (ja) * | 2014-03-27 | 2019-02-06 | 三菱日立パワーシステムズ株式会社 | ガスタービンの分割環の冷却構造及びこれを有するガスタービン |
| CA2951431C (en) | 2014-06-12 | 2019-03-26 | General Electric Company | Multi-piece shroud hanger assembly |
| US11668207B2 (en) | 2014-06-12 | 2023-06-06 | General Electric Company | Shroud hanger assembly |
| US10400619B2 (en) | 2014-06-12 | 2019-09-03 | General Electric Company | Shroud hanger assembly |
| JP5676040B1 (ja) * | 2014-06-30 | 2015-02-25 | 三菱日立パワーシステムズ株式会社 | 静翼、これを備えているガスタービン、静翼の製造方法、及び静翼の改造方法 |
| FR3024884B1 (fr) * | 2014-08-14 | 2019-07-05 | Safran Aircraft Engines | Procede de realisation d'un anneau sectorise d'etancheite et d'une turbine de turbomachine |
| US9963996B2 (en) | 2014-08-22 | 2018-05-08 | Siemens Aktiengesellschaft | Shroud cooling system for shrouds adjacent to airfoils within gas turbine engines |
| GB201417150D0 (en) | 2014-09-29 | 2014-11-12 | Rolls Royce Plc | Carriers for turbine components |
| US10100659B2 (en) * | 2014-12-16 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Hanger system for a turbine engine component |
| US10018068B2 (en) * | 2015-01-13 | 2018-07-10 | United Technologies Corporation | Blade outer air seal with cooling holes |
| US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
| WO2016152573A1 (ja) | 2015-03-26 | 2016-09-29 | 三菱日立パワーシステムズ株式会社 | 翼、及びこれを備えているガスタービン |
| US20170198602A1 (en) * | 2016-01-11 | 2017-07-13 | General Electric Company | Gas turbine engine with a cooled nozzle segment |
| 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 |
| EP3232002A1 (en) * | 2016-04-11 | 2017-10-18 | Rolls-Royce Corporation | Impingement plate with stress relief feature |
| CN106246238A (zh) * | 2016-07-25 | 2016-12-21 | 西北工业大学 | 一种台阶型收缩气膜孔结构 |
| GB2559739A (en) * | 2017-02-15 | 2018-08-22 | Rolls Royce Plc | Stator vane section |
| US10900378B2 (en) | 2017-06-16 | 2021-01-26 | Honeywell International Inc. | Turbine tip shroud assembly with plural shroud segments having internal cooling passages |
| US10677084B2 (en) * | 2017-06-16 | 2020-06-09 | Honeywell International Inc. | Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement |
| FR3072711B1 (fr) * | 2017-10-19 | 2021-07-16 | Safran Aircraft Engines | Element de repartition d'un fluide de refroidissement et ensemble d'anneau de turbine associe |
| US10619504B2 (en) | 2017-10-31 | 2020-04-14 | United Technologies Corporation | Gas turbine engine blade outer air seal cooling hole configuration |
| US10533454B2 (en) | 2017-12-13 | 2020-01-14 | Pratt & Whitney Canada Corp. | Turbine shroud cooling |
| US10502093B2 (en) * | 2017-12-13 | 2019-12-10 | Pratt & Whitney Canada Corp. | Turbine shroud cooling |
| US10570773B2 (en) | 2017-12-13 | 2020-02-25 | Pratt & Whitney Canada Corp. | Turbine shroud cooling |
| US10738637B2 (en) | 2017-12-22 | 2020-08-11 | Raytheon Technologies Corporation | Airflow deflector and assembly |
| JP7065941B2 (ja) * | 2018-03-07 | 2022-05-12 | 川崎重工業株式会社 | ガスタービンのシュラウド取付構造、シュラウド集合体及びシュラウド要素 |
| US10941709B2 (en) * | 2018-09-28 | 2021-03-09 | Pratt & Whitney Canada Corp. | Gas turbine engine and cooling air configuration for turbine section thereof |
| JP6508499B1 (ja) * | 2018-10-18 | 2019-05-08 | 三菱日立パワーシステムズ株式会社 | ガスタービン静翼、これを備えているガスタービン、及びガスタービン静翼の製造方法 |
| US10830050B2 (en) * | 2019-01-31 | 2020-11-10 | General Electric Company | Unitary body turbine shrouds including structural breakdown and collapsible features |
| US10927694B2 (en) * | 2019-03-13 | 2021-02-23 | Raytheon Technologies Corporation | BOAS carrier with cooling supply |
| US11047250B2 (en) * | 2019-04-05 | 2021-06-29 | Raytheon Technologies Corporation | CMC BOAS transverse hook arrangement |
| FR3096395B1 (fr) * | 2019-05-21 | 2021-04-23 | Safran Aircraft Engines | Turbine pour une turbomachine, telle qu’un turboréacteur ou un turbopropulseur d’avion |
| US20210246829A1 (en) * | 2020-02-10 | 2021-08-12 | General Electric Company | Hot gas path components including aft end exhaust conduits and aft end flanges |
| US11525401B2 (en) | 2021-01-11 | 2022-12-13 | Honeywell International Inc. | Impingement baffle for gas turbine engine |
| KR102510535B1 (ko) * | 2021-02-23 | 2023-03-15 | 두산에너빌리티 주식회사 | 링 세그먼트 및 이를 포함하는 터보머신 |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4693667A (en) * | 1980-04-29 | 1987-09-15 | Teledyne Industries, Inc. | Turbine inlet nozzle with cooling means |
| US5167487A (en) * | 1991-03-11 | 1992-12-01 | General Electric Company | Cooled shroud support |
| US5241827A (en) * | 1991-05-03 | 1993-09-07 | General Electric Company | Multi-hole film cooled combuster linear with differential cooling |
| US5169287A (en) * | 1991-05-20 | 1992-12-08 | General Electric Company | Shroud cooling assembly for gas turbine engine |
| 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 |
| JPH06173706A (ja) * | 1992-12-08 | 1994-06-21 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービンエンジンのシュラウドハウジング構造 |
| US5759012A (en) * | 1996-12-13 | 1998-06-02 | Caterpillar Inc. | Turbine disc ingress prevention method and apparatus |
| US6205789B1 (en) * | 1998-11-13 | 2001-03-27 | General Electric Company | Multi-hole film cooled combuster liner |
| US6155778A (en) * | 1998-12-30 | 2000-12-05 | General Electric Company | Recessed turbine shroud |
| US6196792B1 (en) * | 1999-01-29 | 2001-03-06 | General Electric Company | Preferentially cooled turbine shroud |
| US6354795B1 (en) * | 2000-07-27 | 2002-03-12 | General Electric Company | Shroud cooling segment and assembly |
| FR2832178B1 (fr) * | 2001-11-15 | 2004-07-09 | Snecma Moteurs | Dispositif de refroidissement pour anneaux de turbine a gaz |
-
2003
- 2003-11-24 US US10/720,430 patent/US7147432B2/en not_active Expired - Lifetime
-
2004
- 2004-11-22 JP JP2004337529A patent/JP4731156B2/ja not_active Expired - Fee Related
- 2004-11-24 CN CNB2004101023238A patent/CN100507234C/zh not_active Expired - Lifetime
- 2004-11-24 EP EP04257275A patent/EP1533478A3/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| EP1533478A2 (en) | 2005-05-25 |
| JP2005155626A (ja) | 2005-06-16 |
| US20050111965A1 (en) | 2005-05-26 |
| US7147432B2 (en) | 2006-12-12 |
| CN1644891A (zh) | 2005-07-27 |
| EP1533478A3 (en) | 2012-11-07 |
| CN100507234C (zh) | 2009-07-01 |
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