JP2004332731A5 - - Google Patents

Download PDF

Info

Publication number
JP2004332731A5
JP2004332731A5 JP2004135246A JP2004135246A JP2004332731A5 JP 2004332731 A5 JP2004332731 A5 JP 2004332731A5 JP 2004135246 A JP2004135246 A JP 2004135246A JP 2004135246 A JP2004135246 A JP 2004135246A JP 2004332731 A5 JP2004332731 A5 JP 2004332731A5
Authority
JP
Japan
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.)
Withdrawn
Application number
JP2004135246A
Other languages
Japanese (ja)
Other versions
JP2004332731A (en
Filing date
Publication date
Priority claimed from US10/428,219 external-priority patent/US20040219011A1/en
Application filed filed Critical
Publication of JP2004332731A publication Critical patent/JP2004332731A/en
Publication of JP2004332731A5 publication Critical patent/JP2004332731A5/ja
Withdrawn legal-status Critical Current

Links

JP2004135246A 2003-05-02 2004-04-30 High-pressure turbine elastic clearance control system and method Withdrawn JP2004332731A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/428,219 US20040219011A1 (en) 2003-05-02 2003-05-02 High pressure turbine elastic clearance control system and method

Publications (2)

Publication Number Publication Date
JP2004332731A JP2004332731A (en) 2004-11-25
JP2004332731A5 true JP2004332731A5 (en) 2007-06-14

Family

ID=32990469

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004135246A Withdrawn JP2004332731A (en) 2003-05-02 2004-04-30 High-pressure turbine elastic clearance control system and method

Country Status (4)

Country Link
US (1) US20040219011A1 (en)
EP (1) EP1475516A1 (en)
JP (1) JP2004332731A (en)
CN (1) CN1542259A (en)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2404953A (en) * 2003-08-15 2005-02-16 Rolls Royce Plc Blade tip clearance system
DE102004016222A1 (en) * 2004-03-26 2005-10-06 Rolls-Royce Deutschland Ltd & Co Kg Arrangement for automatic running gap adjustment in a two-stage or multi-stage turbine
DE602005027210D1 (en) * 2004-05-17 2011-05-12 Carlton Forge Works Paramount TURBINE HOUSING REINFORCEMENT IN A GAS TURBINE ENGINE
US7596954B2 (en) * 2004-07-09 2009-10-06 United Technologies Corporation Blade clearance control
US8191254B2 (en) * 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
US8126628B2 (en) * 2007-08-03 2012-02-28 General Electric Company Aircraft gas turbine engine blade tip clearance control
US8434997B2 (en) * 2007-08-22 2013-05-07 United Technologies Corporation Gas turbine engine case for clearance control
FR2933458B1 (en) * 2008-07-01 2010-09-03 Snecma AXIALO-CENTRIFUGAL COMPRESSOR WITH STEERING SYSTEM
CN102272419A (en) * 2009-03-09 2011-12-07 斯奈克玛 Turbine ring assembly
FR2949810B1 (en) 2009-09-04 2013-06-28 Turbomeca DEVICE FOR SUPPORTING A TURBINE RING, TURBINE WITH SUCH A DEVICE AND TURBOMOTOR WITH SUCH A TURBINE
GB0916892D0 (en) 2009-09-28 2009-11-11 Rolls Royce Plc A casing component
FR2952965B1 (en) * 2009-11-25 2012-03-09 Snecma INSULATING A CIRCONFERENTIAL SIDE OF AN EXTERNAL TURBOMACHINE CASTER WITH RESPECT TO A CORRESPONDING RING SECTOR
FR2973069B1 (en) * 2011-03-24 2014-09-12 Snecma TURBOMACHINE STATOR CASTER RING
CN102352778B (en) * 2011-10-20 2013-11-27 西北工业大学 Electronic mechanical actuation device for actively controlling tip clearance of turbine
US9726043B2 (en) 2011-12-15 2017-08-08 General Electric Company Mounting apparatus for low-ductility turbine shroud
BR112015028691A2 (en) 2013-05-17 2017-07-25 Gen Electric housing support system
US9266618B2 (en) 2013-11-18 2016-02-23 Honeywell International Inc. Gas turbine engine turbine blade tip active clearance control system and method
JP6529013B2 (en) 2013-12-12 2019-06-12 ゼネラル・エレクトリック・カンパニイ CMC shroud support system
WO2015191185A1 (en) 2014-06-12 2015-12-17 General Electric Company Shroud hanger assembly
WO2015191169A1 (en) 2014-06-12 2015-12-17 General Electric Company Shroud hanger assembly
WO2015191174A1 (en) 2014-06-12 2015-12-17 General Electric Company Multi-piece shroud hanger assembly
US11008890B2 (en) * 2014-11-25 2021-05-18 Raytheon Technologies Corporation Sealing interface for a case of a gas turbine engine
US9874104B2 (en) * 2015-02-27 2018-01-23 General Electric Company Method and system for a ceramic matrix composite shroud hanger assembly
US9915153B2 (en) * 2015-05-11 2018-03-13 General Electric Company Turbine shroud segment assembly with expansion joints
FR3036432B1 (en) * 2015-05-22 2019-04-19 Safran Ceramics TURBINE RING ASSEMBLY WITH AXIAL RETENTION
US10443417B2 (en) * 2015-09-18 2019-10-15 General Electric Company Ceramic matrix composite ring shroud retention methods-finger seals with stepped shroud interface
FR3041993B1 (en) * 2015-10-05 2019-06-21 Safran Aircraft Engines TURBINE RING ASSEMBLY WITH AXIAL RETENTION
US10344769B2 (en) 2016-07-18 2019-07-09 United Technologies Corporation Clearance control between rotating and stationary structures
EP3332894A1 (en) * 2016-12-08 2018-06-13 Siemens Aktiengesellschaft Method for producing a gas turbine component
US10968782B2 (en) * 2017-01-18 2021-04-06 Raytheon Technologies Corporation Rotatable vanes
US10815816B2 (en) * 2018-09-24 2020-10-27 General Electric Company Containment case active clearance control structure
KR102579798B1 (en) * 2018-10-15 2023-09-15 한화에어로스페이스 주식회사 Turbo Device

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3039737A (en) * 1959-04-13 1962-06-19 Int Harvester Co Device for controlling clearance between rotor and shroud of a turbine
DE2907748A1 (en) * 1979-02-28 1980-09-04 Motoren Turbinen Union DEVICE FOR MINIMIZING AND MAINTAINING THE SHOVEL TIP GAMES EXISTING WITH AXIAL TURBINES, IN PARTICULAR FOR GAS TURBINE ENGINES
US4513567A (en) * 1981-11-02 1985-04-30 United Technologies Corporation Gas turbine engine active clearance control
GB2117843B (en) * 1982-04-01 1985-11-06 Rolls Royce Compressor shrouds
FR2724973B1 (en) * 1982-12-31 1996-12-13 Snecma DEVICE FOR SEALING MOBILE BLADES OF A TURBOMACHINE WITH REAL-TIME ACTIVE GAME CONTROL AND METHOD FOR DETERMINING SAID DEVICE
FR2540939A1 (en) * 1983-02-10 1984-08-17 Snecma SEALING RING FOR A TURBINE ROTOR OF A TURBOMACHINE AND TURBOMACHINE INSTALLATION PROVIDED WITH SUCH RINGS
GB2169962B (en) * 1985-01-22 1988-07-13 Rolls Royce Blade tip clearance control
US4728255A (en) * 1985-02-25 1988-03-01 General Electric Company Removable stiffening disk
JPH06506037A (en) * 1991-04-02 1994-07-07 ロールス・ロイス・ピーエルシー turbine casing
US6116852A (en) * 1997-12-11 2000-09-12 Pratt & Whitney Canada Corp. Turbine passive thermal valve for improved tip clearance control
DE19756734A1 (en) * 1997-12-19 1999-06-24 Bmw Rolls Royce Gmbh Passive gap system of a gas turbine
JP2000220472A (en) * 1998-12-23 2000-08-08 United Technol Corp <Utc> Fan case liner
US6487491B1 (en) * 2001-11-21 2002-11-26 United Technologies Corporation System and method of controlling clearance between turbine engine blades and case based on engine components thermal growth model
GB2388407B (en) * 2002-05-10 2005-10-26 Rolls Royce Plc Gas turbine blade tip clearance control structure

Similar Documents

Publication Publication Date Title
BE2015C038I2 (en)
BRPI0518216C1 (en)
BRPI0515516B8 (en)
BR122015024347A2 (en)
BRPI0508002A (en)
BR122018073034B8 (en)
BRPI0508029A (en)
BRPI0419105B8 (en)
BRPI0508026A (en)
BRPI0508033A (en)
AT501137B8 (en)
AT500847B8 (en)
CN300734497S (zh) 旋转椅子
CN300736473S (zh) 洗手盆
CN300781624S (zh) 电视机
CN300736469S (zh) 净身盆
CN300765733S (zh) 瓶子
CN300765107S (zh) 椅子
CN300764069S (zh) 便携式媒体播放机
CN300779224S (zh) 龙头
CN300729373S (zh) 包装盒（曲面的蛤壳式）
CN300731631S (zh) 衣架
CN300731632S (zh) 衣架
CN300732651S (zh) 起动器的主体
CN300775620S (zh) 太阳能逆变器