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FR2607198B1 - Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication - Google Patents

Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication

Info

Publication number
FR2607198B1
FR2607198B1 FR8616448A FR8616448A FR2607198B1 FR 2607198 B1 FR2607198 B1 FR 2607198B1 FR 8616448 A FR8616448 A FR 8616448A FR 8616448 A FR8616448 A FR 8616448A FR 2607198 B1 FR2607198 B1 FR 2607198B1
Authority
FR
France
Prior art keywords
pilotage
expansions
active
manufacturing
compressor 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
FR8616448A
Other languages
English (en)
Other versions
FR2607198A1 (fr
Inventor
Alain Marie Joseph Lardellier
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR8616448A priority Critical patent/FR2607198B1/fr
Priority to US07/124,599 priority patent/US4762462A/en
Priority to DE8787402660T priority patent/DE3761493D1/de
Priority to EP87402660A priority patent/EP0273790B1/fr
Publication of FR2607198A1 publication Critical patent/FR2607198A1/fr
Application granted granted Critical
Publication of FR2607198B1 publication Critical patent/FR2607198B1/fr
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
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified therefor
    • F01D25/145—Thermally insulated 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
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/58—Cooling; Heating; Diminishing heat transfer
    • F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/584—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling or heating the machine

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8616448A 1986-11-26 1986-11-26 Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication Expired - Lifetime FR2607198B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8616448A FR2607198B1 (fr) 1986-11-26 1986-11-26 Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication
US07/124,599 US4762462A (en) 1986-11-26 1987-11-24 Housing for an axial compressor
DE8787402660T DE3761493D1 (de) 1986-11-26 1987-11-25 Kompressorgehaeuse, dessen ausdehnung sich thermisch steuern laesst und seine herstellungsweise.
EP87402660A EP0273790B1 (fr) 1986-11-26 1987-11-25 Carter de compresseur adapté pour le pilotage actif de ses dilatations et son procédé de fabrication

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8616448A FR2607198B1 (fr) 1986-11-26 1986-11-26 Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication

Publications (2)

Publication Number Publication Date
FR2607198A1 FR2607198A1 (fr) 1988-05-27
FR2607198B1 true FR2607198B1 (fr) 1990-05-04

Family

ID=9341216

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8616448A Expired - Lifetime FR2607198B1 (fr) 1986-11-26 1986-11-26 Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication

Country Status (4)

Country Link
US (1) US4762462A (fr)
EP (1) EP0273790B1 (fr)
DE (1) DE3761493D1 (fr)
FR (1) FR2607198B1 (fr)

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US5224824A (en) * 1990-09-12 1993-07-06 United Technologies Corporation Compressor case construction
US5180281A (en) * 1990-09-12 1993-01-19 United Technologies Corporation Case tying means for gas turbine engine
US5238365A (en) * 1991-07-09 1993-08-24 General Electric Company Assembly for thermal shielding of low pressure turbine
US5174714A (en) * 1991-07-09 1992-12-29 General Electric Company Heat shield mechanism for turbine engines
US5201847A (en) * 1991-11-21 1993-04-13 Westinghouse Electric Corp. Shroud design
US5540547A (en) * 1994-06-23 1996-07-30 General Electric Company Method and apparatus for damping vibrations of external tubing of a gas turbine engine
DE4442157A1 (de) * 1994-11-26 1996-05-30 Abb Management Ag Verfahren und Vorrichtung zur Beeinflussung des Radialspieles der Beschaufelung in axialdurchströmten Verdichtern
US5655876A (en) * 1996-01-02 1997-08-12 General Electric Company Low leakage turbine nozzle
US5735671A (en) * 1996-11-29 1998-04-07 General Electric Company Shielded turbine rotor
DE59807765D1 (de) 1997-11-03 2003-05-08 Siemens Ag Turbinengehäuse sowie verfahren zu dessen herstellung
US6185925B1 (en) * 1999-02-12 2001-02-13 General Electric Company External cooling system for turbine frame
US6589600B1 (en) * 1999-06-30 2003-07-08 General Electric Company Turbine engine component having enhanced heat transfer characteristics and method for forming same
GB0116988D0 (en) 2000-08-11 2001-09-05 Rolls Royce Plc A gas turbine engine blade containment assembly
GB2365925B (en) * 2000-08-11 2005-02-23 Rolls Royce Plc A gas turbine engine blade containment assembly
GB2365926B (en) * 2000-08-12 2004-12-08 Rolls Royce Plc A gas turbine engine blade containment assembly
US6530744B2 (en) * 2001-05-29 2003-03-11 General Electric Company Integral nozzle and shroud
US6896483B2 (en) * 2001-07-02 2005-05-24 Allison Advanced Development Company Blade track assembly
DE10343049B3 (de) * 2003-09-16 2005-04-14 Eads Space Transportation Gmbh Brennkammer mit Kühleinrichtung und Verfahren zur Herstellung der Brennkammer
US8393855B2 (en) * 2007-06-29 2013-03-12 General Electric Company Flange with axially curved impingement surface for gas turbine engine clearance control
US8197186B2 (en) 2007-06-29 2012-06-12 General Electric Company Flange with axially extending holes for gas turbine engine clearance control
US8434997B2 (en) * 2007-08-22 2013-05-07 United Technologies Corporation Gas turbine engine case for clearance control
DE102008043605B4 (de) * 2007-11-16 2015-05-07 Alstom Technology Ltd. Verfahren zur Herstellung eines Turbinengehäuses
EP2159384A1 (fr) * 2008-08-27 2010-03-03 Siemens Aktiengesellschaft Support statorique d'aubes directrices pour une turbine à gaz
US20110097199A1 (en) * 2009-10-27 2011-04-28 Ballard Jr Henry G System and method to insulate turbines and associated piping
US9115600B2 (en) * 2011-08-30 2015-08-25 Siemens Energy, Inc. Insulated wall section
US9157331B2 (en) * 2011-12-08 2015-10-13 Siemens Aktiengesellschaft Radial active clearance control for a gas turbine engine
ITTO20120519A1 (it) * 2012-06-14 2013-12-15 Avio Spa Turbina a gas per motori aeronautici
JP5306532B1 (ja) * 2012-10-24 2013-10-02 三菱電機株式会社 内燃機関の制御装置および制御方法
ITFI20130118A1 (it) * 2013-05-21 2014-11-22 Nuovo Pignone Srl "compressor with a thermal shield and methods of operation"
US10202870B2 (en) 2013-11-14 2019-02-12 United Technologies Corporation Flange relief for split casing
US20160326915A1 (en) * 2015-05-08 2016-11-10 General Electric Company System and method for waste heat powered active clearance control
EP3153671A1 (fr) 2015-10-08 2017-04-12 MTU Aero Engines GmbH Dispositif de protection pour turbomachine
US10683772B2 (en) * 2016-06-21 2020-06-16 Rolls-Royce North American Technologies Inc. Intercooling for an axial compressor with radially outer annulus
US10822991B2 (en) * 2016-08-01 2020-11-03 General Electric Company Method and apparatus for active clearance control on gas turbine engines
EP3712380A1 (fr) * 2019-03-19 2020-09-23 MTU Aero Engines GmbH Composant pour moteur d'avion, un module d'un moteur d'avion avec un tel composant et procédé de fabrication du composant par fabrication additive

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR975879A (fr) * 1948-12-06 1951-03-12 Const Et D Equipements Mecaniq Perfectionnement dans la construction des cylindres pour turbines à gaz
US3319930A (en) * 1961-12-19 1967-05-16 Gen Electric Stator assembly for turbomachines
US3335483A (en) * 1961-12-19 1967-08-15 Gen Electric Method of manufacturing a stator assembly for turbomachines
GB1335145A (en) * 1972-01-12 1973-10-24 Rolls Royce Turbine casing for a gas turbine engine
US3892497A (en) * 1974-05-14 1975-07-01 Westinghouse Electric Corp Axial flow turbine stationary blade and blade ring locking arrangement
GB1501916A (en) * 1975-06-20 1978-02-22 Rolls Royce Matching thermal expansions of components of turbo-machines
GB1553038A (en) * 1977-04-28 1979-09-19 Snecma Drum for an axial flow compressor rotor and process for its manufacture
US4131388A (en) * 1977-05-26 1978-12-26 United Technologies Corporation Outer air seal
GB2019954B (en) * 1978-04-04 1982-08-04 Rolls Royce Turbomachine housing
US4411594A (en) * 1979-06-30 1983-10-25 Rolls-Royce Limited Support member and a component supported thereby
DE3018621C2 (de) * 1980-05-16 1982-06-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Außengehäuse für Axialverdichter oder -turbinen von Strömungsmaschinen, insbesondere Gasturbinentriebwerken
US4431373A (en) * 1980-05-16 1984-02-14 United Technologies Corporation Flow directing assembly for a gas turbine engine
US4426191A (en) * 1980-05-16 1984-01-17 United Technologies Corporation Flow directing assembly for a gas turbine engine
GB2076071B (en) * 1980-05-16 1983-11-02 United Technologies Corp Flow directing assembly for a gas turbine engine
GB2110306B (en) * 1981-11-26 1985-02-13 Roll Royce Limited Turbomachine housing
GB2115487B (en) * 1982-02-19 1986-02-05 Gen Electric Double wall compressor casing
US4522559A (en) * 1982-02-19 1985-06-11 General Electric Company Compressor casing
FR2534982A1 (fr) * 1982-10-22 1984-04-27 Snecma Dispositif de controle des jeux d'un compresseur haute pression
FR2535795B1 (fr) * 1982-11-08 1987-04-10 Snecma Dispositif de suspension d'aubes statoriques de compresseur axial pour le controle actif des jeux entre rotor et stator
FR2577282B1 (fr) * 1985-02-13 1987-04-17 Snecma Carter de turbomachine associe a un dispositif pour ajuster le jeu entre rotor et stator

Also Published As

Publication number Publication date
US4762462A (en) 1988-08-09
EP0273790B1 (fr) 1990-01-24
EP0273790A1 (fr) 1988-07-06
DE3761493D1 (de) 1990-03-01
FR2607198A1 (fr) 1988-05-27

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ST Notification of lapse