DE69312657D1 - Turbinenrahmen - Google Patents

Turbinenrahmen

Info

Publication number
DE69312657D1
DE69312657D1 DE69312657T DE69312657T DE69312657D1 DE 69312657 D1 DE69312657 D1 DE 69312657D1 DE 69312657 T DE69312657 T DE 69312657T DE 69312657 T DE69312657 T DE 69312657T DE 69312657 D1 DE69312657 D1 DE 69312657D1
Authority
DE
Germany
Prior art keywords
turbine frame
turbine
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 - Fee Related
Application number
DE69312657T
Other languages
English (en)
Other versions
DE69312657T2 (de
Inventor
Robert Paul Czachor
Christopher Charles Glynn
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 DE69312657D1 publication Critical patent/DE69312657D1/de
Application granted granted Critical
Publication of DE69312657T2 publication Critical patent/DE69312657T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69312657T 1992-12-10 1993-12-09 Turbinenrahmen Expired - Fee Related DE69312657T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/988,637 US5292227A (en) 1992-12-10 1992-12-10 Turbine frame

Publications (2)

Publication Number Publication Date
DE69312657D1 true DE69312657D1 (de) 1997-09-04
DE69312657T2 DE69312657T2 (de) 1998-02-19

Family

ID=25534346

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69312657T Expired - Fee Related DE69312657T2 (de) 1992-12-10 1993-12-09 Turbinenrahmen

Country Status (4)

Country Link
US (1) US5292227A (de)
EP (1) EP0601864B1 (de)
JP (1) JPH076408B2 (de)
DE (1) DE69312657T2 (de)

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ATE230065T1 (de) * 1996-06-21 2003-01-15 Siemens Ag Turbinenwelle sowie verfahren zur kühlung einer turbinenwelle
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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
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US6708482B2 (en) * 2001-11-29 2004-03-23 General Electric Company Aircraft engine with inter-turbine engine frame
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FR2887931B1 (fr) * 2005-06-29 2007-08-17 Snecma Dispositif de support et de logement de servitudes dans un turboreacteur a double flux
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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
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EP2321499B1 (de) * 2008-08-29 2017-12-13 GKN Aerospace Sweden AB Komponente und gasturbinenmotor mit der komponente
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US8152451B2 (en) * 2008-11-29 2012-04-10 General Electric Company Split fairing for a 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
US8371127B2 (en) * 2009-10-01 2013-02-12 Pratt & Whitney Canada Corp. Cooling air system for mid turbine frame
FR2952403B1 (fr) * 2009-11-12 2012-01-13 Snecma Structure annulaire metallique de raccord pour turbomachine d'aeronef
US8256229B2 (en) 2010-04-09 2012-09-04 United Technologies Corporation Rear hub cooling for high pressure compressor
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US8992173B2 (en) * 2011-11-04 2015-03-31 United Technologies Corporation Tie-rod nut including a nut flange with a plurality of mounting apertures
US10094285B2 (en) 2011-12-08 2018-10-09 Siemens Aktiengesellschaft Gas turbine outer case active ambient cooling including air exhaust into sub-ambient cavity
CN104053859B (zh) * 2011-12-20 2016-03-23 Gkn航空公司 用于制造燃气轮机部件的方法
US10012108B2 (en) 2011-12-23 2018-07-03 Gkn Aerospace Sweden Ab Gas turbine engine component
US8979484B2 (en) 2012-01-05 2015-03-17 Pratt & Whitney Canada Corp. Casing for an aircraft turbofan bypass engine
US9316117B2 (en) 2012-01-30 2016-04-19 United Technologies Corporation Internally cooled spoke
US9447694B2 (en) * 2012-01-30 2016-09-20 United Technologies Corporation Internal manifold for turning mid-turbine frame flow distribution
US9140137B2 (en) 2012-01-31 2015-09-22 United Technologies Corporation Gas turbine engine mid turbine frame bearing support
US9347374B2 (en) * 2012-02-27 2016-05-24 United Technologies Corporation Gas turbine engine buffer cooling system
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
US8863531B2 (en) * 2012-07-02 2014-10-21 United Technologies Corporation Cooling apparatus for a mid-turbine frame
US20140003920A1 (en) * 2012-07-02 2014-01-02 United Technologies Corporation Flow metering anti-rotation outer diameter (od) hex nut
EP2900956B1 (de) 2012-09-26 2019-11-20 United Technologies Corporation Gasturbinentriebwerk mit einer dichtungsanordnung für eine statische struktur
US10240481B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Angled cut to direct radiative heat load
US10087843B2 (en) 2012-12-29 2018-10-02 United Technologies Corporation Mount with deflectable tabs
US10053998B2 (en) 2012-12-29 2018-08-21 United Technologies Corporation Multi-purpose gas turbine seal support and assembly
US9845695B2 (en) 2012-12-29 2017-12-19 United Technologies Corporation Gas turbine seal assembly and seal support
US10329956B2 (en) * 2012-12-29 2019-06-25 United Technologies Corporation Multi-function boss for a turbine exhaust case
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US10294819B2 (en) 2012-12-29 2019-05-21 United Technologies Corporation Multi-piece heat shield
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WO2014143329A2 (en) 2012-12-29 2014-09-18 United Technologies Corporation Frame junction cooling holes
US9982561B2 (en) 2012-12-29 2018-05-29 United Technologies Corporation Heat shield for cooling a strut
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US10006306B2 (en) 2012-12-29 2018-06-26 United Technologies Corporation Turbine exhaust case architecture
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
US10138742B2 (en) 2012-12-29 2018-11-27 United Technologies Corporation Multi-ply finger seal
WO2014105512A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Mechanical linkage for segmented heat shield
US9903216B2 (en) 2012-12-29 2018-02-27 United Technologies Corporation Gas turbine seal assembly and seal support
EP2938836B1 (de) 2012-12-29 2020-02-05 United Technologies Corporation Dichtungsträgerscheibe und anordnung
EP2938868B1 (de) 2012-12-29 2019-08-07 United Technologies Corporation Anordnung zur strömungsumlenkung
US10472987B2 (en) 2012-12-29 2019-11-12 United Technologies Corporation Heat shield for a casing
DE112013006315T5 (de) * 2012-12-31 2015-09-17 United Technologies Corporation Mehrteiliger Rahmen eines Turbinenabgasgehäuses
US9890663B2 (en) 2012-12-31 2018-02-13 United Technologies Corporation Turbine exhaust case multi-piece frame
JP6232446B2 (ja) * 2012-12-31 2017-11-15 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ タービン排気ケースのマルチピース型フレーム
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CN105378226B (zh) * 2013-07-19 2017-11-10 通用电气公司 带有冲击挡板的涡轮喷嘴
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CN106460559B (zh) * 2014-04-11 2018-06-12 通用电气公司 涡轮中央框架整流罩组件
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JP2017525883A (ja) 2014-07-18 2017-09-07 シーメンス エナジー インコーポレイテッド 取り外し可能なストラットを備えたタービンアッセンブリ
US10443498B2 (en) * 2014-08-15 2019-10-15 United Technologies Corporation Gas turbine engine cooling fluid metering system
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US9869204B2 (en) * 2015-03-06 2018-01-16 United Technologies Corporation Integrated inner case heat shield
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US9822667B2 (en) 2015-04-06 2017-11-21 United Technologies Corporation Tri-tab lock washer
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Also Published As

Publication number Publication date
EP0601864B1 (de) 1997-07-30
JPH06235331A (ja) 1994-08-23
JPH076408B2 (ja) 1995-01-30
US5292227A (en) 1994-03-08
EP0601864A1 (de) 1994-06-15
DE69312657T2 (de) 1998-02-19

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN

8339 Ceased/non-payment of the annual fee