DE60114697D1 - Turbinengehäuse - Google Patents

Turbinengehäuse

Info

Publication number
DE60114697D1
DE60114697D1 DE60114697T DE60114697T DE60114697D1 DE 60114697 D1 DE60114697 D1 DE 60114697D1 DE 60114697 T DE60114697 T DE 60114697T DE 60114697 T DE60114697 T DE 60114697T DE 60114697 D1 DE60114697 D1 DE 60114697D1
Authority
DE
Germany
Prior art keywords
turbine housing
turbine
housing
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
DE60114697T
Other languages
English (en)
Other versions
DE60114697T2 (de
Inventor
Tod Kenneth Bosel
Moses William Warnow
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
Application granted granted Critical
Publication of DE60114697D1 publication Critical patent/DE60114697D1/de
Publication of DE60114697T2 publication Critical patent/DE60114697T2/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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
  • Connection Of Plates (AREA)
DE60114697T 2000-04-29 2001-04-26 Turbinengehäuseanordnung Expired - Lifetime DE60114697T2 (de)

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
US561771 2000-04-29

Publications (2)

Publication Number Publication Date
DE60114697D1 true DE60114697D1 (de) 2005-12-15
DE60114697T2 DE60114697T2 (de) 2006-07-20

Family

ID=24243390

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60114697T Expired - Lifetime DE60114697T2 (de) 2000-04-29 2001-04-26 Turbinengehäuseanordnung

Country Status (4)

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

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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
EP1619354B1 (de) * 2004-07-22 2008-04-09 Siemens Aktiengesellschaft 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
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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
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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
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US8371812B2 (en) * 2008-11-29 2013-02-12 General Electric Company Turbine frame assembly and method for a gas turbine engine
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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
US9982561B2 (en) 2012-12-29 2018-05-29 United Technologies Corporation Heat shield for cooling a strut
US10240532B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Frame junction cooling holes
US9903224B2 (en) 2012-12-29 2018-02-27 United Technologies Corporation Scupper channelling in gas turbine modules
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
US10378370B2 (en) 2012-12-29 2019-08-13 United Technologies Corporation Mechanical linkage for segmented heat shield
EP2938868B1 (de) 2012-12-29 2019-08-07 United Technologies Corporation Anordnung zur strömungsumlenkung
US10294819B2 (en) 2012-12-29 2019-05-21 United Technologies Corporation Multi-piece heat shield
WO2014105602A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Heat shield for a casing
US9828867B2 (en) 2012-12-29 2017-11-28 United Technologies Corporation Bumper for seals in a turbine exhaust case
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
GB2524211B (en) 2012-12-29 2021-05-26 United Technologies Corp Turbine frame assembly and method of designing turbine frame 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
US9845695B2 (en) 2012-12-29 2017-12-19 United Technologies Corporation Gas turbine seal assembly and seal support
US10060279B2 (en) 2012-12-29 2018-08-28 United Technologies Corporation Seal support disk and assembly
EP2938845A4 (de) 2012-12-29 2016-01-13 United Technologies Corp Turbinenabgasgehäusearchitektur
US10087843B2 (en) 2012-12-29 2018-10-02 United Technologies Corporation Mount with deflectable tabs
US10240481B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Angled cut to direct radiative heat load
US10329956B2 (en) 2012-12-29 2019-06-25 United Technologies Corporation Multi-function boss for a turbine exhaust case
GB2524443B (en) 2012-12-31 2020-02-12 United Technologies Corp Turbine exhaust case multi-piece frame
EP2938860B1 (de) 2012-12-31 2018-08-29 United Technologies Corporation Turbinenabgasgehäuse mit mehrteiligem rahmen
JP6249499B2 (ja) 2012-12-31 2017-12-20 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
US10330011B2 (en) * 2013-03-11 2019-06-25 United Technologies Corporation Bench aft 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
US10920612B2 (en) 2015-07-24 2021-02-16 Pratt & Whitney Canada Corp. Mid-turbine frame spoke cooling system and method
US10443449B2 (en) 2015-07-24 2019-10-15 Pratt & Whitney Canada Corp. Spoke mounting arrangement
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

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Also Published As

Publication number Publication date
JP2002047902A (ja) 2002-02-15
EP1149987A2 (de) 2001-10-31
DE60114697T2 (de) 2006-07-20
EP1149987A3 (de) 2003-11-19
JP4582471B2 (ja) 2010-11-17
US6358001B1 (en) 2002-03-19
EP1149987B1 (de) 2005-11-09

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Legal Events

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