FR2619161B1 - Chassis assemble pour moteur a turbine a gaz - Google Patents

Chassis assemble pour moteur a turbine a gaz

Info

Publication number
FR2619161B1
FR2619161B1 FR8810174A FR8810174A FR2619161B1 FR 2619161 B1 FR2619161 B1 FR 2619161B1 FR 8810174 A FR8810174 A FR 8810174A FR 8810174 A FR8810174 A FR 8810174A FR 2619161 B1 FR2619161 B1 FR 2619161B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
chassis assembly
chassis
assembly
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
FR8810174A
Other languages
English (en)
Other versions
FR2619161A1 (fr
Inventor
William Schonewald Roger
Arman Legault Albert
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 FR2619161A1 publication Critical patent/FR2619161A1/fr
Application granted granted Critical
Publication of FR2619161B1 publication Critical patent/FR2619161B1/fr
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
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR8810174A 1987-08-06 1988-07-28 Chassis assemble pour moteur a turbine a gaz Expired - Fee Related FR2619161B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/082,409 US4793770A (en) 1987-08-06 1987-08-06 Gas turbine engine frame assembly

Publications (2)

Publication Number Publication Date
FR2619161A1 FR2619161A1 (fr) 1989-02-10
FR2619161B1 true FR2619161B1 (fr) 1994-04-15

Family

ID=22171032

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8810174A Expired - Fee Related FR2619161B1 (fr) 1987-08-06 1988-07-28 Chassis assemble pour moteur a turbine a gaz

Country Status (8)

Country Link
US (1) US4793770A (fr)
JP (1) JP2581742B2 (fr)
CA (1) CA1284588C (fr)
DE (1) DE3810600C2 (fr)
FR (1) FR2619161B1 (fr)
GB (1) GB2207707B (fr)
IT (1) IT1216546B (fr)
SE (1) SE8801248D0 (fr)

Families Citing this family (88)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4989406A (en) * 1988-12-29 1991-02-05 General Electric Company Turbine engine assembly with aft mounted outlet guide vanes
US5160251A (en) * 1991-05-13 1992-11-03 General Electric Company Lightweight engine turbine bearing support assembly for withstanding radial and axial loads
US5249418A (en) * 1991-09-16 1993-10-05 General Electric Company Gas turbine engine polygonal structural frame with axially curved panels
FR2685381B1 (fr) * 1991-12-18 1994-02-11 Snecma Carter de turbine delimitant une veine d'ecoulement annulaire de gaz divisee par des bras radiaux.
GB2267736B (en) * 1992-06-09 1995-08-09 Gen Electric Segmented turbine flowpath assembly
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
FR2738283B1 (fr) * 1995-08-30 1997-09-26 Snecma Agencement de turbomachine comprenant une grille d'aubes et un carter intermediaire
US5746574A (en) * 1997-05-27 1998-05-05 General Electric Company Low profile fluid joint
JP3622462B2 (ja) * 1997-12-16 2005-02-23 株式会社日立製作所 半導体装置
US5961278A (en) * 1997-12-17 1999-10-05 Pratt & Whitney Canada Inc. Housing for turbine assembly
GB9805030D0 (en) * 1998-03-11 1998-05-06 Rolls Royce Plc A stator vane assembly for a turbomachine
DE19852603A1 (de) * 1998-11-14 2000-05-18 Asea Brown Boveri Verfahren zur Montage eines Abgasgehäuses für eine Wärmekraftmaschine, vorzugsweise eine Gasturbinenanlage
JP4611512B2 (ja) * 2000-12-19 2011-01-12 本田技研工業株式会社 航空機用ガスタービン・エンジンのファンダクト構造
DE10233881B4 (de) * 2002-07-25 2010-02-18 Rolls-Royce Deutschland Ltd & Co Kg Durch thermische Effekte radial veränderbares Ringelement
US6983608B2 (en) * 2003-12-22 2006-01-10 General Electric Company Methods and apparatus for assembling gas turbine engines
US7510371B2 (en) * 2005-06-06 2009-03-31 General Electric Company Forward tilted turbine nozzle
US7594388B2 (en) 2005-06-06 2009-09-29 General Electric Company Counterrotating turbofan engine
FR2891301B1 (fr) * 2005-09-29 2007-11-02 Snecma Sa Carter structural de turbomoteur
US20100303608A1 (en) * 2006-09-28 2010-12-02 Mitsubishi Heavy Industries, Ltd. Two-shaft gas turbine
US7419352B2 (en) * 2006-10-03 2008-09-02 General Electric Company Methods and apparatus for assembling turbine engines
US7824152B2 (en) * 2007-05-09 2010-11-02 Siemens Energy, Inc. Multivane segment mounting arrangement for a gas turbine
FR2923530B1 (fr) * 2007-11-09 2014-04-04 Snecma Raccordement de bras radiaux a une virole circulaire par des axes et des entretoises
JP2009215897A (ja) * 2008-03-07 2009-09-24 Mitsubishi Heavy Ind Ltd ガスタービンエンジン
US8221071B2 (en) * 2008-09-30 2012-07-17 General Electric Company Integrated guide vane assembly
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
WO2010123410A1 (fr) * 2009-04-23 2010-10-28 Volvo Aero Corporation Procédé de fabrication d'un composant de moteur à turbine à gaz et composant d'un moteur à turbine à gaz
US9528382B2 (en) * 2009-11-10 2016-12-27 General Electric Company Airfoil heat shield
US9284887B2 (en) 2009-12-31 2016-03-15 Rolls-Royce North American Technologies, Inc. Gas turbine engine and frame
DE102010014900A1 (de) * 2010-04-14 2011-10-20 Rolls-Royce Deutschland Ltd & Co Kg Nebenstromkanal eines Turbofantriebwerkes
ITTO20110728A1 (it) * 2011-08-04 2013-02-05 Avio Spa Segmento palettato statorico di una turbina a gas per motori aeronautici
US9279341B2 (en) 2011-09-22 2016-03-08 Pratt & Whitney Canada Corp. Air system architecture for a mid-turbine frame module
US8920113B2 (en) 2011-11-28 2014-12-30 United Technologies Corporation Thermal gradiant tolerant turbomachine coupling member
US9951692B2 (en) * 2011-12-23 2018-04-24 Gkn Aerospace Sweden Ab Support structure for a gas turbine engine
US20130170969A1 (en) * 2012-01-04 2013-07-04 General Electric Company Turbine Diffuser
US9068460B2 (en) 2012-03-30 2015-06-30 United Technologies Corporation Integrated inlet vane and strut
CA2870762A1 (fr) * 2012-04-27 2013-10-31 General Electric Company Agrafe de retenue, carcasse de turbine et procede de limitation de mouvement radial
EP2669474B1 (fr) * 2012-06-01 2019-08-07 MTU Aero Engines AG Canal de passage pour une turbomachine et turbomachine
US9303528B2 (en) * 2012-07-06 2016-04-05 United Technologies Corporation Mid-turbine frame thermal radiation shield
CN104508250B (zh) * 2012-08-01 2017-06-09 通用电气公司 用于燃气涡轮发动机中的支柱的整流片
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
WO2014105621A1 (fr) * 2012-12-29 2014-07-03 United Technologies Corporation Carénage d'aube moulé et fendu
WO2014105616A1 (fr) 2012-12-29 2014-07-03 United Technologies Corporation Architecture de carter de sortie de turbine
WO2014105780A1 (fr) 2012-12-29 2014-07-03 United Technologies Corporation Ensemble et support de joint de turbine à gaz à usages multiples
US10087843B2 (en) 2012-12-29 2018-10-02 United Technologies Corporation Mount with deflectable tabs
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
EP2938868B1 (fr) 2012-12-29 2019-08-07 United Technologies Corporation Ensemble de déviation de flux
US10138742B2 (en) 2012-12-29 2018-11-27 United Technologies Corporation Multi-ply finger seal
US10378370B2 (en) 2012-12-29 2019-08-13 United Technologies Corporation Mechanical linkage for segmented heat shield
WO2014105577A1 (fr) 2012-12-29 2014-07-03 United Technologies Corporation Canalisation de dalot dans des modules de turbine à gaz
US10329956B2 (en) 2012-12-29 2019-06-25 United Technologies Corporation Multi-function boss for a turbine exhaust case
WO2014105603A1 (fr) 2012-12-29 2014-07-03 United Technologies Corporation Bouclier thermique en plusieurs pièces
US10472987B2 (en) 2012-12-29 2019-11-12 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
WO2014105604A1 (fr) 2012-12-29 2014-07-03 United Technologies Corporation Découpe oblique permettant de diriger une charge de chaleur par rayonnement
WO2014105800A1 (fr) 2012-12-29 2014-07-03 United Technologies Corporation Ensemble d'étanchéité de turbine à gaz et support d'étanchéité
GB2524211B (en) 2012-12-29 2021-05-26 United Technologies Corp Turbine frame assembly and method of designing turbine frame assembly
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
EP2938836B1 (fr) 2012-12-29 2020-02-05 United Technologies Corporation Disque et ensemble de support d'étanchéité
WO2014105688A1 (fr) 2012-12-31 2014-07-03 United Technologies Corporation Cadre à multiples pièces de compartiment d'échappement de turbine
DE112013006325T5 (de) 2012-12-31 2015-11-19 United Technologies Corporation Mehrteiliger Rahmen eines Turbinenabgasgehäuses
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
US10221707B2 (en) 2013-03-07 2019-03-05 Pratt & Whitney Canada Corp. Integrated strut-vane
WO2014197037A2 (fr) * 2013-03-11 2014-12-11 United Technologies Corporation Sous-ensemble arrière de banc pour un carénage de carter d'échappement de turbine
EP3022400B1 (fr) 2013-07-15 2023-06-21 Raytheon Technologies Corporation Aubes de turbine à congés de raccordement variables
US9835038B2 (en) 2013-08-07 2017-12-05 Pratt & Whitney Canada Corp. Integrated strut and vane arrangements
US10202869B2 (en) 2013-08-22 2019-02-12 United Technologies Corporation Connection for a fairing in a mid-turbine frame of a gas turbine engine
US9556746B2 (en) 2013-10-08 2017-01-31 Pratt & Whitney Canada Corp. Integrated strut and turbine vane nozzle arrangement
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
US20160186614A1 (en) * 2014-08-27 2016-06-30 United Technologies Corporation Turbine exhaust case assembly
US9784133B2 (en) 2015-04-01 2017-10-10 General Electric Company Turbine frame and airfoil for turbine frame
US9771828B2 (en) * 2015-04-01 2017-09-26 General Electric Company Turbine exhaust frame and method of vane assembly
GB201512838D0 (en) 2015-07-21 2015-09-02 Rolls Royce Plc A turbine stator vane assembly for a turbomachine
US9909434B2 (en) 2015-07-24 2018-03-06 Pratt & Whitney Canada Corp. Integrated strut-vane nozzle (ISV) with uneven vane axial chords
US10247035B2 (en) 2015-07-24 2019-04-02 Pratt & Whitney Canada Corp. Spoke locking architecture
CN107849937B (zh) 2015-07-24 2020-06-19 普拉特-惠特尼加拿大公司 涡轮中间框架辐条冷却系统及方法
US10443449B2 (en) 2015-07-24 2019-10-15 Pratt & Whitney Canada Corp. Spoke mounting arrangement
US10273812B2 (en) 2015-12-18 2019-04-30 Pratt & Whitney Canada Corp. Turbine rotor coolant supply system
US10975721B2 (en) * 2016-01-12 2021-04-13 Pratt & Whitney Canada Corp. Cooled containment case using internal plenum
US10443451B2 (en) 2016-07-18 2019-10-15 Pratt & Whitney Canada Corp. Shroud housing supported by vane segments
DE102017212311A1 (de) 2017-07-19 2019-01-24 MTU Aero Engines AG Umströmungsanordung zum Anordnen im Heißgaskanal einer Strömungsmaschine
US10781721B2 (en) * 2018-02-09 2020-09-22 General Electric Company Integral turbine center frame
US11136995B2 (en) 2019-04-05 2021-10-05 Raytheon Technologies Corporation Pre-diffuser for a gas turbine engine
US11384936B2 (en) 2019-04-05 2022-07-12 Raytheon Technologies Corporation Pre-diffuser for a gas turbine engine
US11371704B2 (en) 2019-04-05 2022-06-28 Raytheon Technologies Corporation Pre-diffuser for a gas turbine engine
BE1027876B1 (fr) * 2019-12-18 2021-07-26 Safran Aero Boosters Sa Module pour turbomachine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB742241A (en) * 1951-02-15 1955-12-21 Power Jets Res & Dev Ltd Improvements in the cooling of turbines
US2771622A (en) * 1952-05-09 1956-11-27 Westinghouse Electric Corp Diaphragm apparatus
GB736800A (en) * 1952-07-10 1955-09-14 Havilland Engine Co Ltd Improvements in or relating to stationary blade rings of axial flow turbines or compressors
US2928648A (en) * 1954-03-01 1960-03-15 United Aircraft Corp Turbine bearing support
US2941781A (en) * 1955-10-13 1960-06-21 Westinghouse Electric Corp Guide vane array for turbines
US2936999A (en) * 1956-12-07 1960-05-17 United Aircraft Corp Tangential bearing supports
US2869941A (en) * 1957-04-29 1959-01-20 United Aircraft Corp Turbine bearing support
GB846329A (en) * 1957-12-12 1960-08-31 Napier & Son Ltd Combustion turbine power units
FR1385893A (fr) * 1964-03-06 1965-01-15 Daimler Benz Ag Montage du carter entourant la chambre d'installation d'un palier d'arbre de turbine dans le carter du moteur d'un groupe moto-propulseur à turbine à gaz
US3764226A (en) * 1972-04-05 1973-10-09 Avco Corp Piloting device for split housings having different thermal coefficients of expansion
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
US4033792A (en) * 1974-12-23 1977-07-05 United Technologies Corporation Composite single crystal article
US4208777A (en) * 1978-11-27 1980-06-24 United Technologies Corporation Method for manufacturing a split engine casing from a cylinder
US4369016A (en) * 1979-12-21 1983-01-18 United Technologies Corporation Turbine intermediate case
US4321007A (en) * 1979-12-21 1982-03-23 United Technologies Corporation Outer case cooling for a turbine intermediate case
US4417850A (en) * 1982-12-20 1983-11-29 Allis-Chalmers Corporation Vertical column pump
GB2149022A (en) * 1983-10-27 1985-06-05 Rolls Royce Warpable guide vanes for turbomachines
US4611464A (en) * 1984-05-02 1986-09-16 United Technologies Corporation Rotor assembly for a gas turbine engine and method of disassembly

Also Published As

Publication number Publication date
GB8807804D0 (en) 1988-05-05
SE8801248D0 (sv) 1988-04-05
DE3810600A1 (de) 1989-02-16
CA1284588C (fr) 1991-06-04
GB2207707A (en) 1989-02-08
US4793770A (en) 1988-12-27
JP2581742B2 (ja) 1997-02-12
IT8820094A0 (it) 1988-04-05
JPS6441621A (en) 1989-02-13
DE3810600C2 (de) 2001-03-08
GB2207707B (en) 1992-03-18
FR2619161A1 (fr) 1989-02-10
IT1216546B (it) 1990-03-08

Similar Documents

Publication Publication Date Title
FR2619161B1 (fr) Chassis assemble pour moteur a turbine a gaz
FR2617907B1 (fr) Moteur a turbine a gaz
FR2586453B1 (fr) Carburateur pour moteur a turbine a gaz
FR2557212B1 (fr) Structure de stator pour un moteur a turbine a gaz
GB2165964B (en) Combustion system for a gas turbine engine
EP0319246A3 (en) Emissions control for gas turbine engine
GB2203801B (en) A gas turbine engine
FR2575221B1 (fr) Stator refroidissable pour un moteur a turbine a gaz
GB2221979B (en) A combustion chamber for a gas turbine engine
DE3665627D1 (en) Combustion liner for a gas turbine engine
GB2220711B (en) Stator assembly for a gas turbine engine
FR2628982B1 (fr) Filtre a air perfectionne pour moteurs thermiques
FR2632015B1 (fr) Syste me d'injecteurs pour moteur a turbine a gaz
GB2199900B (en) A turbopropeller or turbofan gas turbine engine
FR2594886B1 (fr) Module propulsif pour un moteur aeronautique a turbine a gaz
IT1240296B (it) Assieme rotorico per turbomotore a gas
FR2533620B1 (fr) Assemblage de rotor pour un moteur a turbine a gaz
FR2632014B1 (fr) Injecteur de carburant pour moteur a turbine a gaz
FR2624954B1 (fr) Structure de chambre de combustion pour moteur a turbine a gaz
FR2586755B1 (fr) Systeme de carburant pour un moteur a turbine a gaz
FR2621650B1 (fr) Assemblage d'injecteur de carburant pour moteur a turbine a gaz
FR2527268B1 (fr) Prediffuseur pour un moteur a turbine a gaz
FR2601068B1 (fr) Turbine de puissance pour moteur a turbine a gaz.
FR2460390B1 (fr) Diffuseur pour moteur a turbine a gaz
EP0335168A3 (en) Method of operating a combustion engine

Legal Events

Date Code Title Description
ST Notification of lapse