JP2002047902A5 - - Google Patents

Download PDF

Info

Publication number
JP2002047902A5
JP2002047902A5 JP2001130539A JP2001130539A JP2002047902A5 JP 2002047902 A5 JP2002047902 A5 JP 2002047902A5 JP 2001130539 A JP2001130539 A JP 2001130539A JP 2001130539 A JP2001130539 A JP 2001130539A JP 2002047902 A5 JP2002047902 A5 JP 2002047902A5
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.)
Granted
Application number
JP2001130539A
Other versions
JP2002047902A (ja
JP4582471B2 (ja
Filing date
Publication date
Priority claimed from US09/561,771 external-priority patent/US6358001B1/en
Application filed filed Critical
Publication of JP2002047902A publication Critical patent/JP2002047902A/ja
Publication of JP2002047902A5 publication Critical patent/JP2002047902A5/ja
Application granted granted Critical
Publication of JP4582471B2 publication Critical patent/JP4582471B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

JP2001130539A 2000-04-29 2001-04-27 タービンフレーム組立体 Expired - Fee Related JP4582471B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/561,771 US6358001B1 (en) 2000-04-29 2000-04-29 Turbine frame assembly
US09/561771 2000-04-29

Publications (3)

Publication Number Publication Date
JP2002047902A JP2002047902A (ja) 2002-02-15
JP2002047902A5 true JP2002047902A5 (ja) 2008-06-19
JP4582471B2 JP4582471B2 (ja) 2010-11-17

Family

ID=24243390

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001130539A Expired - Fee Related JP4582471B2 (ja) 2000-04-29 2001-04-27 タービンフレーム組立体

Country Status (4)

Country Link
US (1) US6358001B1 (ja)
EP (1) EP1149987B1 (ja)
JP (1) JP4582471B2 (ja)
DE (1) DE60114697T2 (ja)

Families Citing this family (72)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6796765B2 (en) * 2001-12-27 2004-09-28 General Electric Company Methods and apparatus for assembling gas turbine engine struts
DE10213402A1 (de) * 2002-03-26 2003-12-24 Mtu Aero Engines Gmbh Anordnung zur Befestigung von als Lagerträger für den Rotor einer Fluggasturbine dienenden Streben an der Gehäusestruktur der Fluggasturbine
US6773228B2 (en) * 2002-07-03 2004-08-10 General Electric Company Methods and apparatus for turbine nozzle locks
US6935837B2 (en) * 2003-02-27 2005-08-30 General Electric Company Methods and apparatus for assembling gas turbine engines
US6860716B2 (en) 2003-05-29 2005-03-01 General Electric Company Turbomachine frame structure
ATE391835T1 (de) * 2004-07-22 2008-04-15 Siemens Ag Sicherungsvorrichtung für eine an einer drehbaren rotorscheibe angeordneten laufschaufel einer strömungsmaschine, strömungsmaschine und verfahren zur montage und demontage einer laufschaufel an einer rotorscheibe einer strömungsmaschine
US7124572B2 (en) * 2004-09-14 2006-10-24 Honeywell International, Inc. Recuperator and turbine support adapter for recuperated gas turbine engines
FR2875855B1 (fr) * 2004-09-27 2006-12-22 Snecma Moteurs Sa Turboreacteur avec un bras monobloc de raccord de servitudes et le bras monobloc de raccord de servitudes
US7383686B2 (en) * 2004-12-13 2008-06-10 Honeywell International Inc. Secondary flow, high pressure turbine module cooling air system for recuperated gas turbine engines
GB2448116B (en) * 2007-04-05 2009-05-27 Rolls Royce Plc Means for cooling a bearing assembly
FR2917458B1 (fr) * 2007-06-13 2009-09-25 Snecma Sa Moyeu de carter d'echappement comportant des nervures de repartition de contraintes
FR2923530B1 (fr) * 2007-11-09 2014-04-04 Snecma Raccordement de bras radiaux a une virole circulaire par des axes et des entretoises
DE102008019156A1 (de) * 2008-04-17 2009-10-22 Mtu Aero Engines Gmbh Strebe für ein Turbinenzwischengehäuse, Turbinenzwischengehäuse und Verfahren zur Herstellung eines Turbinenzwischengehäuses
FR2933130B1 (fr) * 2008-06-25 2012-02-24 Snecma Carter structural pour turbomachine
ES2370307B1 (es) * 2008-11-04 2012-11-27 Industria De Turbo Propulsores, S.A. Estructura soporte de rodamiento para turbina.
US20100132377A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Fabricated itd-strut and vane ring for gas turbine engine
US8371812B2 (en) * 2008-11-29 2013-02-12 General Electric Company Turbine frame assembly and method for a gas turbine engine
US8177488B2 (en) * 2008-11-29 2012-05-15 General Electric Company Integrated service tube and impingement baffle for a gas turbine engine
US8152451B2 (en) * 2008-11-29 2012-04-10 General Electric Company Split fairing for a gas turbine engine
US8231142B2 (en) * 2009-02-17 2012-07-31 Pratt & Whitney Canada Corp. Fluid conduit coupling with leakage detection
US20100275572A1 (en) * 2009-04-30 2010-11-04 Pratt & Whitney Canada Corp. Oil line insulation system for mid turbine frame
FR2950416B1 (fr) * 2009-09-23 2012-04-20 Snecma Dispositif accroche-flammes comprenant un support de bras et un ecran de protection thermique monoblocs
US8316523B2 (en) 2009-10-01 2012-11-27 Pratt & Whitney Canada Corp. Method for centering engine structures
US9097141B2 (en) 2011-09-15 2015-08-04 Pratt & Whitney Canada Corp. Axial bolting arrangement for mid turbine frame
US9279341B2 (en) 2011-09-22 2016-03-08 Pratt & Whitney Canada Corp. Air system architecture for a mid-turbine frame module
US9316117B2 (en) 2012-01-30 2016-04-19 United Technologies Corporation Internally cooled spoke
US9316108B2 (en) * 2012-03-05 2016-04-19 General Electric Company Gas turbine frame stiffening rails
FR2988777B1 (fr) * 2012-03-29 2014-04-25 Snecma Propulsion Solide Integration de pieces d'arriere-corps de moteur aeronautique
US9482115B2 (en) 2012-08-23 2016-11-01 United Technologies Corporation Turbine engine support assembly including self anti-rotating bushing
EP2719870B1 (de) * 2012-10-12 2016-12-07 MTU Aero Engines AG Lagerstern, zugehöriges Herstellungsverfahren und entsprechende Strömungsmaschine
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
WO2014105657A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Mount with deflectable tabs
US9828867B2 (en) 2012-12-29 2017-11-28 United Technologies Corporation Bumper for seals in a turbine exhaust case
WO2014105619A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-function boss for a turbine exhaust case
WO2014143329A2 (en) 2012-12-29 2014-09-18 United Technologies Corporation Frame junction cooling holes
US10006306B2 (en) 2012-12-29 2018-06-26 United Technologies Corporation Turbine exhaust case architecture
US10138742B2 (en) 2012-12-29 2018-11-27 United Technologies Corporation Multi-ply finger seal
WO2014105780A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-purpose gas turbine seal support and assembly
JP6271582B2 (ja) 2012-12-29 2018-01-31 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation ガスタービンシールアセンブリおよびシール支持体
US9903224B2 (en) 2012-12-29 2018-02-27 United Technologies Corporation Scupper channelling in gas turbine modules
US10240481B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Angled cut to direct radiative heat load
US9850774B2 (en) 2012-12-29 2017-12-26 United Technologies Corporation Flow diverter element and assembly
WO2014105425A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Turbine frame assembly and method of designing turbine frame assembly
WO2014105602A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Heat shield for a casing
US9845695B2 (en) 2012-12-29 2017-12-19 United Technologies Corporation Gas turbine seal assembly and seal support
WO2014105599A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Heat shield for cooling a strut
WO2014105603A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Multi-piece heat shield
EP2938863B1 (en) 2012-12-29 2019-09-25 United Technologies Corporation Mechanical linkage for segmented heat shield
US10060279B2 (en) 2012-12-29 2018-08-28 United Technologies Corporation Seal support disk and assembly
WO2014105682A1 (en) 2012-12-31 2014-07-03 United Technologies Corporation Turbine exhaust case multi-piece frame
GB2524443B (en) 2012-12-31 2020-02-12 United Technologies Corp Turbine exhaust case multi-piece frame
US9890663B2 (en) 2012-12-31 2018-02-13 United Technologies Corporation Turbine exhaust case multi-piece frame
EP2971579B1 (en) * 2013-03-11 2020-04-29 United Technologies Corporation Aft fairing sub-assembly for turbine exhaust case fairing
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
CN103949686A (zh) * 2013-12-19 2014-07-30 重庆赛力盟电机有限责任公司 水轮机转轮上冠泄水孔加工工艺
JP6392371B2 (ja) * 2014-04-11 2018-09-19 ゼネラル・エレクトリック・カンパニイ タービン中央フレームフェアリングアセンブリ
US20160201512A1 (en) * 2015-01-09 2016-07-14 United Technologies Corporation Gas turbine engine mid-turbine frame tie rod arrangement
US9995171B2 (en) * 2015-01-16 2018-06-12 United Technologies Corporation Cooling passages for a mid-turbine frame
FR3034465B1 (fr) * 2015-04-03 2017-05-05 Snecma Turbomoteur comportant deux flux de ventilation distincts
US10247035B2 (en) 2015-07-24 2019-04-02 Pratt & Whitney Canada Corp. Spoke locking architecture
US10443449B2 (en) 2015-07-24 2019-10-15 Pratt & Whitney Canada Corp. Spoke mounting arrangement
CA2936182C (en) 2015-07-24 2023-08-15 Pratt & Whitney Canada Corp. Mid-turbine frame spoke cooling system and method
US10378379B2 (en) 2015-08-27 2019-08-13 General Electric Company Gas turbine engine cooling air manifolds with spoolies
US10273812B2 (en) 2015-12-18 2019-04-30 Pratt & Whitney Canada Corp. Turbine rotor coolant supply system
US10458339B2 (en) 2016-01-12 2019-10-29 United Technologies Corporation Gas turbine engine case flow blocking covers
DE102016201863A1 (de) * 2016-02-08 2017-08-24 MTU Aero Engines AG Gehäuseelement für ein Turbinenzwischengehäuse
GB201612293D0 (en) * 2016-07-15 2016-08-31 Rolls Royce Plc Assembly for supprting an annulus
PL419827A1 (pl) * 2016-12-16 2018-06-18 General Electric Company Rozpórki do ram wylotowych systemów turbin
US11401835B2 (en) 2017-06-12 2022-08-02 General Electric Company Turbine center frame
BE1025975B1 (fr) * 2018-02-02 2019-09-03 Safran Aero Boosters S.A. Carter structural pour turbomachine axiale
US10724390B2 (en) * 2018-03-16 2020-07-28 General Electric Company Collar support assembly for airfoils
CN112392564A (zh) * 2020-11-13 2021-02-23 中国航发沈阳发动机研究所 一种外环机匣与辐板的连接结构

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2819871A (en) * 1954-09-07 1958-01-14 John R Mcveigh Vane structure
US3084849A (en) * 1960-05-18 1963-04-09 United Aircraft Corp Inlet and bearing support for axial flow compressors
US3371697A (en) * 1966-04-22 1968-03-05 Newton Insert Co Threaded elements with locking keys
DE3003470C2 (de) * 1980-01-31 1982-02-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Turbinenleitschaufelaufhängung für Gasturbinenstrahltriebwerke
US4987736A (en) * 1988-12-14 1991-01-29 General Electric Company Lightweight gas turbine engine frame with free-floating heat shield
GB2236809B (en) * 1989-09-22 1994-03-16 Rolls Royce Plc Improvements in or relating to gas turbine engines
FR2685383B1 (fr) * 1991-12-18 1994-02-11 Snecma Bras structural du carter d'une turbomachine.
US5232323A (en) * 1992-09-28 1993-08-03 General Electric Company Removable threaded fastener with locking plate
US5292227A (en) 1992-12-10 1994-03-08 General Electric Company Turbine frame
US5272869A (en) 1992-12-10 1993-12-28 General Electric Company Turbine frame
US5273397A (en) 1993-01-13 1993-12-28 General Electric Company Turbine casing and radiation shield
US5483792A (en) 1993-05-05 1996-01-16 General Electric Company Turbine frame stiffening rails
US5438756A (en) 1993-12-17 1995-08-08 General Electric Company Method for assembling a turbine frame assembly
FR2738283B1 (fr) * 1995-08-30 1997-09-26 Snecma Agencement de turbomachine comprenant une grille d'aubes et un carter intermediaire
US5634767A (en) 1996-03-29 1997-06-03 General Electric Company Turbine frame having spindle mounted liner
US5630700A (en) * 1996-04-26 1997-05-20 General Electric Company Floating vane turbine nozzle
US6053680A (en) * 1998-02-16 2000-04-25 Menke; Manfred Sleeve nut

Similar Documents

Publication Publication Date Title
BE2022C531I2 (ja)
BE2022C502I2 (ja)
BE2017C057I2 (ja)
BE2017C051I2 (ja)
BE2017C032I2 (ja)
BE2016C051I2 (ja)
BE2017C050I2 (ja)
JP2002047902A5 (ja)
JP2002208307A5 (ja)
BRPI0209186B1 (ja)
BRPI0204884A2 (ja)
CH1379220H1 (ja)
JP2002189475A5 (ja)
BE2017C059I2 (ja)
DE60230025D1 (ja)
HU0202414D0 (ja)
HU0201722D0 (ja)
BRPI0101486B8 (ja)
DE60232394D1 (ja)
BRPI0210463A2 (ja)
JP2002091960A5 (ja)
JP2001298417A5 (ja)
JP2001353683A5 (ja)
JP2002029508A5 (ja)
JP2002251268A5 (ja)