JP4648575B2 - 浮動スプーリーカップ衝突邪魔板 - Google Patents
浮動スプーリーカップ衝突邪魔板 Download PDFInfo
- Publication number
- JP4648575B2 JP4648575B2 JP2001180941A JP2001180941A JP4648575B2 JP 4648575 B2 JP4648575 B2 JP 4648575B2 JP 2001180941 A JP2001180941 A JP 2001180941A JP 2001180941 A JP2001180941 A JP 2001180941A JP 4648575 B2 JP4648575 B2 JP 4648575B2
- Authority
- JP
- Japan
- Prior art keywords
- cup
- flange
- cap
- nozzle
- pulley
- 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
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
-
- 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
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection 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
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 |
|---|---|---|---|
| US09/595,867 US6382906B1 (en) | 2000-06-16 | 2000-06-16 | Floating spoolie cup impingement baffle |
| US09/595867 | 2000-06-16 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2002106304A JP2002106304A (ja) | 2002-04-10 |
| JP2002106304A5 JP2002106304A5 (enExample) | 2008-07-24 |
| JP4648575B2 true JP4648575B2 (ja) | 2011-03-09 |
Family
ID=24385005
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001180941A Expired - Fee Related JP4648575B2 (ja) | 2000-06-16 | 2001-06-15 | 浮動スプーリーカップ衝突邪魔板 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6382906B1 (enExample) |
| EP (1) | EP1164250B1 (enExample) |
| JP (1) | JP4648575B2 (enExample) |
| DE (1) | DE60130066D1 (enExample) |
Families Citing this family (59)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6652220B2 (en) * | 2001-11-15 | 2003-11-25 | General Electric Company | Methods and apparatus for cooling gas turbine nozzles |
| ITMI20021465A1 (it) * | 2002-07-03 | 2004-01-05 | Nuovo Pignone Spa | Dispositivo di schermatura termica di facile montaggio per un accoppiamento tra una tubazione di raffreddamento ed una foratura passante rea |
| US7008185B2 (en) * | 2003-02-27 | 2006-03-07 | General Electric Company | Gas turbine engine turbine nozzle bifurcated impingement baffle |
| US6969233B2 (en) * | 2003-02-27 | 2005-11-29 | General Electric Company | Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity |
| US6932568B2 (en) * | 2003-02-27 | 2005-08-23 | General Electric Company | Turbine nozzle segment cantilevered mount |
| FR2856729B1 (fr) * | 2003-06-30 | 2005-09-23 | Snecma Moteurs | Aubes refroidies de moteur a turbine a gaz. |
| FR2862338B1 (fr) * | 2003-11-17 | 2007-07-20 | Snecma Moteurs | Dispositif de liaison entre un distributeur et une enceinte d'alimentation pour injecteurs de fluide de refroidissement dans une turbomachine |
| GB0413672D0 (en) * | 2004-06-18 | 2004-07-21 | Kohler Mira Ltd | Improvements in or relating to ablutionary installations |
| US7007488B2 (en) * | 2004-07-06 | 2006-03-07 | General Electric Company | Modulated flow turbine nozzle |
| US7278828B2 (en) * | 2004-09-22 | 2007-10-09 | General Electric Company | Repair method for plenum cover in a gas turbine engine |
| FR2883599B1 (fr) | 2005-03-23 | 2010-04-23 | Snecma Moteurs | Dispositif de liaison entre une enceinte de passage d'air de refroidissement et un aubage de distributeur dans une turbomachine |
| US20070160475A1 (en) * | 2006-01-12 | 2007-07-12 | Siemens Power Generation, Inc. | Tilted turbine vane with impingement cooling |
| US10286407B2 (en) | 2007-11-29 | 2019-05-14 | General Electric Company | Inertial separator |
| GB0800345D0 (en) * | 2008-01-10 | 2008-02-20 | Boomerang Innovative Technolog | Pipe coupling |
| EP2483529B1 (en) * | 2009-09-28 | 2013-08-28 | Siemens Aktiengesellschaft | Gas turbine nozzle arrangement and gas turbine |
| US10337404B2 (en) * | 2010-03-08 | 2019-07-02 | General Electric Company | Preferential cooling of gas turbine nozzles |
| US20120070302A1 (en) * | 2010-09-20 | 2012-03-22 | Ching-Pang Lee | Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles |
| US9347324B2 (en) * | 2010-09-20 | 2016-05-24 | Siemens Aktiengesellschaft | Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles |
| FR2976616B1 (fr) * | 2011-06-17 | 2015-01-09 | Snecma | Systeme de ventilation pour une pale creuse d un distributeur de turbine dans une turbomachine |
| US8915701B2 (en) | 2011-09-08 | 2014-12-23 | General Electric Company | Piping assembly and method for connecting inner and outer shell in turbine system |
| US9011078B2 (en) | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine vane seal carrier with slots for cooling and assembly |
| US9011079B2 (en) * | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine nozzle compartmentalized cooling system |
| US9039350B2 (en) | 2012-01-09 | 2015-05-26 | General Electric Company | Impingement cooling system for use with contoured surfaces |
| US8944751B2 (en) | 2012-01-09 | 2015-02-03 | General Electric Company | Turbine nozzle cooling assembly |
| US8864445B2 (en) * | 2012-01-09 | 2014-10-21 | General Electric Company | Turbine nozzle assembly methods |
| US9133724B2 (en) * | 2012-01-09 | 2015-09-15 | General Electric Company | Turbomachine component including a cover plate |
| US20140075947A1 (en) * | 2012-09-18 | 2014-03-20 | United Technologies Corporation | Gas turbine engine component cooling circuit |
| US9371735B2 (en) * | 2012-11-29 | 2016-06-21 | Solar Turbines Incorporated | Gas turbine engine turbine nozzle impingement cover |
| CN102979584A (zh) * | 2012-12-06 | 2013-03-20 | 哈尔滨汽轮机厂有限责任公司 | 燃机涡轮首级导叶上端壁冷却系统 |
| CN102996187A (zh) * | 2012-12-06 | 2013-03-27 | 哈尔滨汽轮机厂有限责任公司 | 燃机涡轮首级导叶下端壁冷却系统 |
| US10400616B2 (en) * | 2013-07-19 | 2019-09-03 | General Electric Company | Turbine nozzle with impingement baffle |
| WO2016032585A2 (en) | 2014-05-29 | 2016-03-03 | General Electric Company | Turbine engine, components, and methods of cooling same |
| US11033845B2 (en) | 2014-05-29 | 2021-06-15 | General Electric Company | Turbine engine and particle separators therefore |
| CA2949547A1 (en) | 2014-05-29 | 2016-02-18 | General Electric Company | Turbine engine and particle separators therefore |
| US9915176B2 (en) | 2014-05-29 | 2018-03-13 | General Electric Company | Shroud assembly for turbine engine |
| GB2530763A (en) * | 2014-10-01 | 2016-04-06 | Rolls Royce Plc | A heat shield |
| US10036319B2 (en) | 2014-10-31 | 2018-07-31 | General Electric Company | Separator assembly for a gas turbine engine |
| US10167725B2 (en) | 2014-10-31 | 2019-01-01 | General Electric Company | Engine component for a turbine engine |
| DE102015215144B4 (de) * | 2015-08-07 | 2017-11-09 | MTU Aero Engines AG | Vorrichtung und Verfahren zum Beeinflussen der Temperaturen in Innenringsegmenten einer Gasturbine |
| US10378379B2 (en) | 2015-08-27 | 2019-08-13 | General Electric Company | Gas turbine engine cooling air manifolds with spoolies |
| US9988936B2 (en) | 2015-10-15 | 2018-06-05 | General Electric Company | Shroud assembly for a gas turbine engine |
| US10428664B2 (en) | 2015-10-15 | 2019-10-01 | General Electric Company | Nozzle for a gas turbine engine |
| JP6725273B2 (ja) * | 2016-03-11 | 2020-07-15 | 三菱日立パワーシステムズ株式会社 | 翼、これを備えているガスタービン |
| US10704425B2 (en) | 2016-07-14 | 2020-07-07 | General Electric Company | Assembly for a gas turbine engine |
| DE102016216858A1 (de) * | 2016-09-06 | 2018-03-08 | Rolls-Royce Deutschland Ltd & Co Kg | Laufschaufel für eine Turbomaschine und Verfahren für den Zusammenbau einer Laufschaufel für eine Turbomaschine |
| PL421120A1 (pl) * | 2017-04-04 | 2018-10-08 | General Electric Company Polska Spolka Z Ograniczona Odpowiedzialnoscia | Silnik turbinowy i części składowe do stosowania w nim |
| US10822981B2 (en) | 2017-10-30 | 2020-11-03 | General Electric Company | Variable guide vane sealing |
| US10684149B2 (en) * | 2018-03-09 | 2020-06-16 | Rolls-Royce Corporation | System and method of measuring turbine vane cooling air consumption during engine operation |
| US10738620B2 (en) * | 2018-04-18 | 2020-08-11 | Raytheon Technologies Corporation | Cooling arrangement for engine components |
| US10815821B2 (en) | 2018-08-31 | 2020-10-27 | General Electric Company | Variable airfoil with sealed flowpath |
| US11692485B2 (en) | 2021-02-18 | 2023-07-04 | Generai, Electric Company | Gas turbine engine with spoolie fluid transfer connection |
| US11686210B2 (en) | 2021-03-24 | 2023-06-27 | General Electric Company | Component assembly for variable airfoil systems |
| CN116104650B (zh) * | 2023-01-20 | 2025-08-29 | 中国航发沈阳发动机研究所 | 一种涡轮内冷气接嘴结构 |
| US20240410284A1 (en) * | 2023-06-07 | 2024-12-12 | Raytheon Technologies Corporation | Turbine vane baffle chimney |
| US12025029B1 (en) * | 2023-08-21 | 2024-07-02 | Rtx Corporation | Bathtub seal for damping CMC vane platform |
| US12281597B2 (en) | 2023-08-21 | 2025-04-22 | Rtx Corporation | CMC vane with rotatable baffle design to accommodate re-stagger |
| US12326099B2 (en) | 2023-08-21 | 2025-06-10 | Rtx Corporation | Bathtub seal integrated into CMC vane load path |
| US12467366B2 (en) * | 2023-12-01 | 2025-11-11 | General Electric Company | Turbine engine with a nozzle having cooling features |
| US20250257665A1 (en) * | 2024-02-09 | 2025-08-14 | Rtx Corporation | Cooling nozzle vanes of a turbine engine |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB803137A (en) * | 1955-08-05 | 1958-10-22 | Rolls Royce | Improvements in or relating to axial-flow fluid machines for example turbines and compressors of gas-turbine engines |
| US3540810A (en) * | 1966-03-17 | 1970-11-17 | Gen Electric | Slanted partition for hollow airfoil vane insert |
| US4288201A (en) * | 1979-09-14 | 1981-09-08 | United Technologies Corporation | Vane cooling structure |
| FR2519374B1 (fr) * | 1982-01-07 | 1986-01-24 | Snecma | Dispositif de refroidissement des talons d'aubes mobiles d'une turbine |
| US4962640A (en) * | 1989-02-06 | 1990-10-16 | Westinghouse Electric Corp. | Apparatus and method for cooling a gas turbine vane |
| US5224818A (en) * | 1991-11-01 | 1993-07-06 | General Electric Company | Air transfer bushing |
| US5207556A (en) * | 1992-04-27 | 1993-05-04 | General Electric Company | Airfoil having multi-passage baffle |
| FR2746141B1 (fr) * | 1996-03-14 | 1998-04-17 | Dispositif de commande pour pivot integre dans un collecteur | |
| JP3233871B2 (ja) * | 1997-05-14 | 2001-12-04 | 三菱重工業株式会社 | ガスタービン静翼 |
| FR2771446B1 (fr) * | 1997-11-27 | 1999-12-31 | Snecma | Aube de distributeur de turbine refroidie |
| SE512085C2 (sv) * | 1998-05-28 | 2000-01-24 | Abb Ab | Rotormaskininrättning |
| US6065928A (en) * | 1998-07-22 | 2000-05-23 | General Electric Company | Turbine nozzle having purge air circuit |
| US6158955A (en) * | 1999-06-03 | 2000-12-12 | General Electric Company | Welding method and assembly therefor |
-
2000
- 2000-06-16 US US09/595,867 patent/US6382906B1/en not_active Expired - Lifetime
-
2001
- 2001-06-13 EP EP01305145A patent/EP1164250B1/en not_active Expired - Lifetime
- 2001-06-13 DE DE60130066T patent/DE60130066D1/de not_active Expired - Lifetime
- 2001-06-15 JP JP2001180941A patent/JP4648575B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| DE60130066D1 (de) | 2007-10-04 |
| JP2002106304A (ja) | 2002-04-10 |
| EP1164250B1 (en) | 2007-08-22 |
| EP1164250A3 (en) | 2004-09-29 |
| EP1164250A2 (en) | 2001-12-19 |
| US6382906B1 (en) | 2002-05-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4648575B2 (ja) | 浮動スプーリーカップ衝突邪魔板 | |
| JP4439053B2 (ja) | ベイ冷却タービンケーシング | |
| JP4641916B2 (ja) | 隅部が冷却されるタービンノズル | |
| EP1347152B1 (en) | Cooled turbine nozzle sector | |
| US4573865A (en) | Multiple-impingement cooled structure | |
| JP4464247B2 (ja) | デフレクタ埋込み式インピンジメントバッフル | |
| US4761116A (en) | Turbine blade with tip vent | |
| JP4486201B2 (ja) | 優先冷却タービンシュラウド | |
| EP2187019B1 (en) | Gas turbine with exhaust section structure | |
| EP0959230B1 (en) | Shroud cooling assembly for gas turbine engine | |
| EP1205636B1 (en) | Turbine blade for a gas turbine and method of cooling said blade | |
| US8177492B2 (en) | Passage obstruction for improved inlet coolant filling | |
| US5503528A (en) | Rim seal for turbine wheel | |
| JP5383973B2 (ja) | ガスタービンエンジンアクティブクリアランス制御の使用済み冷却空気を排気するシステム及び方法 | |
| EP1185765B1 (en) | Apparatus for reducing combustor exit duct cooling | |
| JP4781244B2 (ja) | タービンノズル及びタービンエンジン | |
| JP2000130760A (ja) | ディンプルを設けたインピンジメントバッフル | |
| JP2010255629A (ja) | フランジ冷却式タービンノズル | |
| EP1350018B1 (en) | Combustor turbine successive dual cooling | |
| CN104334833B (zh) | 用于喷嘴导向叶片和燃气轮机的密封装置 | |
| EP3461995B1 (en) | Gas turbine blade | |
| GB2054046A (en) | Cooling turbine rotors | |
| KR20060046516A (ko) | 성곽 형상을 가지는 단부를 구비한 에어포일 삽입체 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20080609 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20080609 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20100727 |
|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20101025 |
|
| RD02 | Notification of acceptance of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7422 Effective date: 20101025 |
|
| RD04 | Notification of resignation of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7424 Effective date: 20101025 |
|
| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20101116 |
|
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20101210 |
|
| FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20131217 Year of fee payment: 3 |
|
| R150 | Certificate of patent or registration of utility model |
Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| LAPS | Cancellation because of no payment of annual fees |