DE602004032192D1 - Rahmenstruktur einer Turbomaschine - Google Patents

Rahmenstruktur einer Turbomaschine

Info

Publication number
DE602004032192D1
DE602004032192D1 DE602004032192T DE602004032192T DE602004032192D1 DE 602004032192 D1 DE602004032192 D1 DE 602004032192D1 DE 602004032192 T DE602004032192 T DE 602004032192T DE 602004032192 T DE602004032192 T DE 602004032192T DE 602004032192 D1 DE602004032192 D1 DE 602004032192D1
Authority
DE
Germany
Prior art keywords
turbomachine
frame structure
frame
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 - Lifetime
Application number
DE602004032192T
Other languages
English (en)
Inventor
Robert P Czachor
Robert E Jones
Thomas L Maclean
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of DE602004032192D1 publication Critical patent/DE602004032192D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602004032192T 2003-05-29 2004-05-27 Rahmenstruktur einer Turbomaschine Expired - Lifetime DE602004032192D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/447,546 US6860716B2 (en) 2003-05-29 2003-05-29 Turbomachine frame structure

Publications (1)

Publication Number Publication Date
DE602004032192D1 true DE602004032192D1 (de) 2011-05-26

Family

ID=33131592

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004032192T Expired - Lifetime DE602004032192D1 (de) 2003-05-29 2004-05-27 Rahmenstruktur einer Turbomaschine

Country Status (5)

Country Link
US (1) US6860716B2 (de)
EP (1) EP1482130B1 (de)
JP (1) JP4400871B2 (de)
CN (1) CN100507238C (de)
DE (1) DE602004032192D1 (de)

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FR2923530B1 (fr) 2007-11-09 2014-04-04 Snecma Raccordement de bras radiaux a une virole circulaire par des axes et des entretoises
FR2923529B1 (fr) * 2007-11-09 2014-05-16 Snecma Raccordement de bras radiaux a une virole circulaire par imbrication de pieces rapportees
DE102008019156A1 (de) * 2008-04-17 2009-10-22 Mtu Aero Engines Gmbh Strebe für ein Turbinenzwischengehäuse, Turbinenzwischengehäuse und Verfahren zur Herstellung eines Turbinenzwischengehäuses
US8347500B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitney Canada Corp. Method of assembly and disassembly of a gas turbine mid turbine frame
US8371812B2 (en) * 2008-11-29 2013-02-12 General Electric Company Turbine frame assembly and method for a gas turbine engine
US8152451B2 (en) * 2008-11-29 2012-04-10 General Electric Company Split fairing 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
FR2940359B1 (fr) * 2008-12-18 2014-11-28 Snecma Carter d'echappement pour turbomachine, comportant une ferrure d'accrochage dissociee de la virole exterieure.
US8794912B2 (en) * 2009-05-07 2014-08-05 Volvo Aero Corporation Strut and a gas turbine structure comprising the strut
US8281602B2 (en) * 2009-09-11 2012-10-09 General Electric Company Circumferentially self expanding combustor support for a turbine engine
WO2011129724A1 (en) * 2010-04-16 2011-10-20 Volvo Aero Corporation A strut, a gas turbine engine frame comprising the strut and a gas turbine engine comprising the frame
US8992167B2 (en) * 2011-09-07 2015-03-31 General Electric Company Turbine casing assembly mounting pin
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
US9765648B2 (en) 2011-12-08 2017-09-19 Gkn Aerospace Sweden Ab Gas turbine engine component
EP2795067B1 (de) 2011-12-20 2019-03-13 GKN Aerospace Sweden AB Verfahren zur herstellung eines gasturbinenmotorbauteils
ES2618786T3 (es) 2011-12-22 2017-06-22 Gkn Aerospace Sweden Ab Componente de motor de turbina de gas
ES2605102T3 (es) 2011-12-23 2017-03-13 Volvo Aero Corporation Estructura de soporte para un motor de turbina de gas, motor de turbina de gas, avión y método de construcción correspondientes
EP2795071B1 (de) 2011-12-23 2017-02-01 GKN Aerospace Sweden AB Gasturbinenmotorkomponente
US8979484B2 (en) 2012-01-05 2015-03-17 Pratt & Whitney Canada Corp. Casing for an aircraft turbofan bypass engine
US9447694B2 (en) * 2012-01-30 2016-09-20 United Technologies Corporation Internal manifold for turning mid-turbine frame flow distribution
US9316117B2 (en) * 2012-01-30 2016-04-19 United Technologies Corporation Internally cooled spoke
US9140137B2 (en) 2012-01-31 2015-09-22 United Technologies Corporation Gas turbine engine mid turbine frame bearing support
JP6002325B2 (ja) * 2012-08-01 2016-10-05 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジンの分割フェアリング用のバックル接合部
US9482115B2 (en) 2012-08-23 2016-11-01 United Technologies Corporation Turbine engine support assembly including self anti-rotating bushing
GB2524220B (en) * 2012-12-31 2020-05-20 United Technologies Corp Turbine exhaust case multi-piece frame
EP2971579B1 (de) * 2013-03-11 2020-04-29 United Technologies Corporation Baugruppe für eine turbinenabgasgehäuseverkleidung
FR3006373B1 (fr) * 2013-05-31 2015-05-22 Snecma Carter de turbomachine comportant un orifice d'endoscopie
EP2837775B1 (de) 2013-08-15 2016-03-30 ALSTOM Technology Ltd Fixiervorrichtung für eine Turbine und Verfahren zum Anbringen der Fixierung
FR3010047B1 (fr) * 2013-09-04 2017-03-31 Snecma Structure de liaison moteur-nacelle a platine a vis
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
JP2015135061A (ja) * 2014-01-16 2015-07-27 株式会社Ihi 翼の連結部構造及びこれを用いたジェットエンジン
WO2015156882A2 (en) * 2014-02-26 2015-10-15 United Technologies Corporation Tie rod connection for mid-turbine frame
CN104564926B (zh) * 2014-12-10 2016-08-24 中国航空工业集团公司金城南京机电液压工程研究中心 一种冲压空气涡轮限位安全装置
US10309308B2 (en) * 2015-01-16 2019-06-04 United Technologies Corporation Cooling passages for a mid-turbine frame
FR3036442B1 (fr) * 2015-05-21 2021-07-16 Snecma Turbomachine comportant un systeme de ventilation
US10443449B2 (en) 2015-07-24 2019-10-15 Pratt & Whitney Canada Corp. Spoke mounting arrangement
US10914193B2 (en) 2015-07-24 2021-02-09 Pratt & Whitney Canada Corp. Multiple spoke cooling system and method
US10247035B2 (en) 2015-07-24 2019-04-02 Pratt & Whitney Canada Corp. Spoke locking architecture
JP6546481B2 (ja) * 2015-08-31 2019-07-17 川崎重工業株式会社 排気ディフューザ
US10273812B2 (en) 2015-12-18 2019-04-30 Pratt & Whitney Canada Corp. Turbine rotor coolant supply system
DE102016201863A1 (de) * 2016-02-08 2017-08-24 MTU Aero Engines AG Gehäuseelement für ein Turbinenzwischengehäuse
FR3054263B1 (fr) * 2016-07-20 2018-08-10 Safran Aircraft Engines Carter intermediaire de turbomachine d'aeronef realise d'une seule piece de fonderie avec une canalisation de lubrifiant
DE102016217320A1 (de) * 2016-09-12 2018-03-15 Siemens Aktiengesellschaft Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse
DE102018132892A1 (de) * 2018-12-19 2020-06-25 Rolls-Royce Deutschland Ltd & Co Kg Zwischengehäusestruktur für eine Verdichtervorrichtung eines Gasturbinentriebwerks und ein Gasturbinentriebwerk
US11047247B2 (en) 2018-12-21 2021-06-29 Rolls-Royce Plc Turbine section of a gas turbine engine with ceramic matrix composite vanes
US10961857B2 (en) 2018-12-21 2021-03-30 Rolls-Royce Plc Turbine section of a gas turbine engine with ceramic matrix composite vanes
US10954802B2 (en) 2019-04-23 2021-03-23 Rolls-Royce Plc Turbine section assembly with ceramic matrix composite vane
US11008880B2 (en) 2019-04-23 2021-05-18 Rolls-Royce Plc Turbine section assembly with ceramic matrix composite vane
US11193393B2 (en) 2019-04-23 2021-12-07 Rolls-Royce Plc Turbine section assembly with ceramic matrix composite vane
US10975708B2 (en) 2019-04-23 2021-04-13 Rolls-Royce Plc Turbine section assembly with ceramic matrix composite vane
US11149559B2 (en) 2019-05-13 2021-10-19 Rolls-Royce Plc Turbine section assembly with ceramic matrix composite vane
FR3097259B1 (fr) * 2019-06-12 2021-05-21 Safran Helicopter Engines Piece annulaire de support d’un palier pour une turbomachine
CN115335588A (zh) * 2020-03-20 2022-11-11 西门子能源全球两合公司 用于涡轮机的支柱罩
CN112360581A (zh) * 2020-11-13 2021-02-12 中国航发沈阳发动机研究所 一种连接式发动机涡轮承力框架
US11732596B2 (en) 2021-12-22 2023-08-22 Rolls-Royce Plc Ceramic matrix composite turbine vane assembly having minimalistic support spars

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US5180282A (en) 1991-09-27 1993-01-19 General Electric Company Gas turbine engine structural frame with multi-yoke attachment of struts to outer casing
US5272869A (en) 1992-12-10 1993-12-28 General Electric Company Turbine frame
US5292227A (en) 1992-12-10 1994-03-08 General Electric Company Turbine frame
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
FR2774358B1 (fr) * 1998-02-04 2000-04-21 Aerospatiale Dispositif d'accrochage d'un moteur d'aeronef
FR2775465B1 (fr) * 1998-03-02 2000-05-26 Aerospatiale Dispositif d'accrochage d'un moteur sur un pylone d'aeronef
US6439841B1 (en) 2000-04-29 2002-08-27 General Electric Company Turbine frame assembly
US6358001B1 (en) * 2000-04-29 2002-03-19 General Electric Company Turbine frame assembly
AU2001273144A1 (en) * 2000-07-06 2002-01-21 Wyeth Use of substituted indole compounds for treating neuropeptide y-related conditions
US6672833B2 (en) * 2001-12-18 2004-01-06 General Electric Company Gas turbine engine frame flowpath liner support

Also Published As

Publication number Publication date
US20040240987A1 (en) 2004-12-02
CN1573053A (zh) 2005-02-02
US6860716B2 (en) 2005-03-01
EP1482130A3 (de) 2009-02-11
JP2005030389A (ja) 2005-02-03
CN100507238C (zh) 2009-07-01
EP1482130B1 (de) 2011-04-13
EP1482130A2 (de) 2004-12-01
JP4400871B2 (ja) 2010-01-20

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