FR2643416B1 - Carter pour machine tournante, notamment pour un turbomoteur, et son procede d'assemblage - Google Patents

Carter pour machine tournante, notamment pour un turbomoteur, et son procede d'assemblage

Info

Publication number
FR2643416B1
FR2643416B1 FR909002283A FR9002283A FR2643416B1 FR 2643416 B1 FR2643416 B1 FR 2643416B1 FR 909002283 A FR909002283 A FR 909002283A FR 9002283 A FR9002283 A FR 9002283A FR 2643416 B1 FR2643416 B1 FR 2643416B1
Authority
FR
France
Prior art keywords
turbomotor
housing
rotating machine
assembly method
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
FR909002283A
Other languages
English (en)
Other versions
FR2643416A1 (fr
Inventor
Theodore W Hall
Kenneth H Klapproth
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of FR2643416A1 publication Critical patent/FR2643416A1/fr
Application granted granted Critical
Publication of FR2643416B1 publication Critical patent/FR2643416B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/21—Utilizing thermal characteristic, e.g., expansion or contraction, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR909002283A 1989-02-23 1990-02-23 Carter pour machine tournante, notamment pour un turbomoteur, et son procede d'assemblage Expired - Fee Related FR2643416B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/314,535 US4921401A (en) 1989-02-23 1989-02-23 Casting for a rotary machine

Publications (2)

Publication Number Publication Date
FR2643416A1 FR2643416A1 (fr) 1990-08-24
FR2643416B1 true FR2643416B1 (fr) 1992-05-07

Family

ID=23220341

Family Applications (1)

Application Number Title Priority Date Filing Date
FR909002283A Expired - Fee Related FR2643416B1 (fr) 1989-02-23 1990-02-23 Carter pour machine tournante, notamment pour un turbomoteur, et son procede d'assemblage

Country Status (5)

Country Link
US (1) US4921401A (fr)
JP (1) JP2792990B2 (fr)
KR (1) KR970011034B1 (fr)
FR (1) FR2643416B1 (fr)
GB (1) GB2228539B (fr)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5088775A (en) * 1990-07-27 1992-02-18 General Electric Company Seal ring with flanged end portions
US5154577A (en) * 1991-01-17 1992-10-13 General Electric Company Flexible three-piece seal assembly
FR2683851A1 (fr) * 1991-11-20 1993-05-21 Snecma Turbomachine equipee de moyens facilitant le reglage des jeux du stator entree stator et rotor.
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
US5451116A (en) * 1992-06-09 1995-09-19 General Electric Company Tripod plate for turbine flowpath
US5271714A (en) * 1992-07-09 1993-12-21 General Electric Company Turbine nozzle support arrangement
FR2699970B1 (fr) * 1992-12-30 1995-03-17 Europ Propulsion Dispositif de liaison glissante entre deux pièces soumises à de fortes sollicitations mécaniques et thermiques.
DE4329623A1 (de) * 1993-09-02 1995-03-09 Abb Management Ag Abgasdiffusor
KR980002705A (ko) * 1996-06-12 1998-03-30 이대원 터빈 케이싱 냉각장치
FR2761119B1 (fr) * 1997-03-20 1999-04-30 Snecma Stator de compresseur de turbomachine
DE19855130A1 (de) * 1998-11-30 2000-05-31 Abb Alstom Power Ch Ag Kühlbarer Mantel einer Gasturbine oder dergleichen
GB0117550D0 (en) * 2001-07-19 2001-09-12 Rolls Royce Plc Joint arrangement
GB2384829A (en) * 2002-01-31 2003-08-06 Rolls Royce Plc Casing arrangement
US6918743B2 (en) * 2002-10-23 2005-07-19 Pratt & Whitney Canada Ccorp. Sheet metal turbine or compressor static shroud
GB0321056D0 (en) * 2003-09-09 2003-10-08 Rolls Royce Plc Joint arrangement
US7681601B2 (en) * 2005-08-24 2010-03-23 Alstom Technology Ltd. Inner casing of a rotating thermal machine
FR2922589B1 (fr) * 2007-10-22 2009-12-04 Snecma Controle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine
FR2927951B1 (fr) * 2008-02-27 2011-08-19 Snecma Ensemble diffuseur-redresseur pour une turbomachine
WO2009123302A2 (fr) 2008-03-31 2009-10-08 Mitsubishi Heavy Industries, Ltd. Structure d'isolation thermique pour élément structurel et structure hélicoïdale
US8235345B2 (en) * 2008-04-30 2012-08-07 United Technologies Corp. Gas turbine engine systems and related methods involving thermally isolated retention
CH700679A1 (de) * 2009-03-17 2010-09-30 Alstom Technology Ltd Abstützung für eine turbine.
WO2011047693A1 (fr) * 2009-10-19 2011-04-28 Siemens Aktiengesellschaft Agencement d'aubes distributrices et moteur à turbine
US8668431B2 (en) * 2010-03-29 2014-03-11 United Technologies Corporation Seal clearance control on non-cowled gas turbine engines
US8651809B2 (en) * 2010-10-13 2014-02-18 General Electric Company Apparatus and method for aligning a turbine casing
US9284969B2 (en) 2012-02-24 2016-03-15 Pratt & Whitney Canada Corp. Thermal expansion joint connection for sheet metal assembly
US9498850B2 (en) * 2012-03-27 2016-11-22 Pratt & Whitney Canada Corp. Structural case for aircraft gas turbine engine
US9896971B2 (en) * 2012-09-28 2018-02-20 United Technologies Corporation Lug for preventing rotation of a stator vane arrangement relative to a turbine engine case
FR2998546B1 (fr) * 2012-11-23 2016-01-01 Airbus Operations Sas Nacelle d'aeronef incorporant une liaison amelioree entre une entree d'air et une motorisation
US9850780B2 (en) * 2012-12-29 2017-12-26 United Technologies Corporation Plate for directing flow and film cooling of components
US9963989B2 (en) * 2013-06-12 2018-05-08 United Technologies Corporation Gas turbine engine vane-to-transition duct seal
WO2014201247A1 (fr) * 2013-06-14 2014-12-18 United Technologies Corporation Ensemble écran thermique à double joint de recouvrement pour moteur à turbine à gaz
US9676469B2 (en) * 2014-04-10 2017-06-13 Lockheed Martin Corporation System and method for fastening structures
US9976431B2 (en) * 2014-07-22 2018-05-22 United Technologies Corporation Mid-turbine frame and gas turbine engine including same
EP3006681B1 (fr) * 2014-10-10 2020-12-09 Ansaldo Energia Switzerland AG Diffuseur pour une turbine à gaz
US10018064B2 (en) * 2015-03-02 2018-07-10 United Technologies Corporation Floating panel for a gas powered turbine
EP3208431B1 (fr) * 2016-02-16 2022-01-05 MTU Aero Engines AG Système de raccordement pour élément d'un boîtier intermediaire de turbine
FR3072715B1 (fr) * 2017-10-20 2020-04-17 Safran Aircraft Engines Carter pour turbomachine, equipe d'une enveloppe de protection thermique et d'une bande anti-usures
GB2571591B (en) * 2018-03-03 2020-08-05 Rolls Royce Plc Rear outer discharge nozzle
JP7411458B2 (ja) * 2020-03-11 2024-01-11 三菱重工業株式会社 燃焼筒の取付方法、及び燃焼筒取付治具

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472062A (en) * 1943-08-24 1949-06-07 Jarvis C Marble Turbine casing construction
GB761829A (en) * 1954-02-04 1956-11-21 George Frederick Kelk Stator ring assembly for a rotary bladed fluid flow machine
NL103792C (fr) * 1954-12-16
US2915280A (en) * 1957-04-18 1959-12-01 Gen Electric Nozzle and seal assembly
US3387820A (en) * 1965-05-24 1968-06-11 Continental Aviat & Engineerin Turbine engine construction
US3759038A (en) * 1971-12-09 1973-09-18 Westinghouse Electric Corp Self aligning combustor and transition structure for a gas turbine
US3892497A (en) * 1974-05-14 1975-07-01 Westinghouse Electric Corp Axial flow turbine stationary blade and blade ring locking arrangement
US4184689A (en) * 1978-10-02 1980-01-22 United Technologies Corporation Seal structure for an axial flow rotary machine
US4247248A (en) * 1978-12-20 1981-01-27 United Technologies Corporation Outer air seal support structure for gas turbine engine
SU842244A1 (ru) * 1979-08-06 1981-06-30 Макеевский Инженерно-Строительныйинститут Соединение деталей
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
US4431373A (en) * 1980-05-16 1984-02-14 United Technologies Corporation Flow directing assembly for a gas turbine engine
US4502809A (en) * 1981-08-31 1985-03-05 Carrier Corporation Method and apparatus for controlling thermal growth
US4411134A (en) * 1981-10-26 1983-10-25 Moir David L Apparatus for the repair and replacement of transition ducts on jet engines and bracket therefor
US4477086A (en) * 1982-11-01 1984-10-16 United Technologies Corporation Seal ring with slidable inner element bridging circumferential gap
US4627233A (en) * 1983-08-01 1986-12-09 United Technologies Corporation Stator assembly for bounding the working medium flow path of a gas turbine engine
SU1168755A1 (ru) * 1983-11-11 1985-07-23 Nii Mostov Болтовое соединение
US4635332A (en) * 1985-09-13 1987-01-13 Solar Turbines Incorporated Sealed telescopic joint and method of assembly
FR2591674B1 (fr) * 1985-12-18 1988-02-19 Snecma Dispositif de reglage des jeux radiaux entre rotor et stator d'un compresseur
US4764084A (en) * 1987-11-23 1988-08-16 Westinghouse Electric Corp. Inlet flow guide for a low pressure turbine

Also Published As

Publication number Publication date
JPH02248629A (ja) 1990-10-04
GB2228539B (en) 1993-09-01
FR2643416A1 (fr) 1990-08-24
JP2792990B2 (ja) 1998-09-03
KR970011034B1 (ko) 1997-07-05
US4921401A (en) 1990-05-01
GB2228539A (en) 1990-08-29
KR900013183A (ko) 1990-09-03
GB9002265D0 (en) 1990-03-28

Similar Documents

Publication Publication Date Title
FR2643416B1 (fr) Carter pour machine tournante, notamment pour un turbomoteur, et son procede d'assemblage
IT9020294A0 (it) Sistema visualizzatore di lavorazione a macchina
DE3560371D1 (en) Carter for a turbo machine
DE69021243T2 (de) In-line rotierende Kuvertiervorrichtung.
DE58908610D1 (de) Spinnmaschine.
AU626467B2 (en) System for monitoring the operation of a cage moving in a mine shaft
FR2577575B1 (fr) Dispositif porte-fils pour metier a tisser.
IT8619707A0 (it) Filatoio.
FR2570791B1 (fr) Robinet a obturateur tournant perfectionne, procede pour son assemblage et obturateur equipant un tel robinet
CS47389A1 (en) Device of attendance travelling automaton for spindleless spinning machine
DE59004956D1 (de) Selbstkassierender automat.
FR2533294B1 (fr) Procede d'assemblage d'une machine tournante et machine correspondante
FR2653654B1 (fr) Boitier a raccord tournant pour suceur d'aspirateur.
DE58904847D1 (de) Drehfeldmaschine.
GB8925868D0 (en) Oscillatory rotating engine
IT8622010A0 (it) Filatoio.
FI910100A0 (fi) Metod och arrangemang foer rengoering av fibersuspensioner av laetta orenheter.
IT8722194A0 (it) Filatoio a frizione.
GB9021848D0 (en) Drag machine
FI922591A0 (fi) Foerfarande och anordning foer rening av foerbraenningsgas.
IT8621215A0 (it) Filatoio.
FR2656058B3 (fr) Disposition d'etancheite pour arbre tournant.
FR2512599B1 (fr) Dispositif d'isolement d'encoche pour machine tournante electrique, et son procede de fabrication
IT8947781A0 (it) Filatoio
IT8622008A0 (it) Filatoio.

Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20081031