FR2522067B1 - Carter de compresseur - Google Patents

Carter de compresseur

Info

Publication number
FR2522067B1
FR2522067B1 FR838302568A FR8302568A FR2522067B1 FR 2522067 B1 FR2522067 B1 FR 2522067B1 FR 838302568 A FR838302568 A FR 838302568A FR 8302568 A FR8302568 A FR 8302568A FR 2522067 B1 FR2522067 B1 FR 2522067B1
Authority
FR
France
Prior art keywords
compressor housing
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
Application number
FR838302568A
Other languages
English (en)
Other versions
FR2522067A1 (fr
Inventor
Joseph Clayton Burge
Julius Bathori
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 FR2522067A1 publication Critical patent/FR2522067A1/fr
Application granted granted Critical
Publication of FR2522067B1 publication Critical patent/FR2522067B1/fr
Expired 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
    • F01D25/08—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
    • 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
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
    • 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
    • F04D29/5853—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps heat insulation or conduction

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)
  • Separation By Low-Temperature Treatments (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR838302568A 1982-02-19 1983-02-17 Carter de compresseur Expired FR2522067B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US35049082A 1982-02-19 1982-02-19

Publications (2)

Publication Number Publication Date
FR2522067A1 FR2522067A1 (fr) 1983-08-26
FR2522067B1 true FR2522067B1 (fr) 1989-01-27

Family

ID=23376950

Family Applications (1)

Application Number Title Priority Date Filing Date
FR838302568A Expired FR2522067B1 (fr) 1982-02-19 1983-02-17 Carter de compresseur

Country Status (5)

Country Link
JP (1) JPS58152108A (fr)
DE (1) DE3305170C2 (fr)
FR (1) FR2522067B1 (fr)
GB (1) GB2115487B (fr)
IT (1) IT1168258B (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4728255A (en) * 1985-02-25 1988-03-01 General Electric Company Removable stiffening disk
DE3509192A1 (de) * 1985-03-14 1986-09-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Stroemungsmaschine mit mitteln zur kontrolle des radialspaltes
DE3509193A1 (de) * 1985-03-14 1986-09-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Stroemungsmaschine mit innengehaeuse
KR950008505B1 (ko) * 1985-11-04 1995-07-31 카롤 앤 맥키 윤활유 제한장치
US4728257A (en) * 1986-06-18 1988-03-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal stress minimized, two component, turbine shroud seal
FR2607198B1 (fr) * 1986-11-26 1990-05-04 Snecma Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication
FR2635562B1 (fr) * 1988-08-18 1993-12-24 Snecma Anneau de stator de turbine associe a un support de liaison au carter de turbine
GB2225587B (en) * 1988-10-29 1992-07-15 Ishikawajima Harima Heavy Ind Interior material for fan case of turbo-fan engine
GB8903000D0 (en) * 1989-02-10 1989-03-30 Rolls Royce Plc A blade tip clearance control arrangement for a gas turbine engine
CA2039756A1 (fr) * 1990-05-31 1991-12-01 Larry Wayne Plemmons Aube fixe a revetement applique selectivement selon la conductivite thermique dudit revetement
US5165848A (en) * 1991-07-09 1992-11-24 General Electric Company Vane liner with axially positioned heat shields
US5195868A (en) * 1991-07-09 1993-03-23 General Electric Company Heat shield for a compressor/stator structure
FR2683851A1 (fr) * 1991-11-20 1993-05-21 Snecma Turbomachine equipee de moyens facilitant le reglage des jeux du stator entree stator et rotor.
JPH0568603U (ja) * 1992-02-26 1993-09-17 正静 平出 鉋
FR2711730B1 (fr) * 1993-10-27 1995-12-01 Snecma Turbomachine équipée de moyens de pilotage des jeux entre rotor et stator.
DE4442157A1 (de) * 1994-11-26 1996-05-30 Abb Management Ag Verfahren und Vorrichtung zur Beeinflussung des Radialspieles der Beschaufelung in axialdurchströmten Verdichtern
GB9820226D0 (en) 1998-09-18 1998-11-11 Rolls Royce Plc Gas turbine engine casing
GB0107973D0 (en) 2001-03-30 2001-05-23 Rolls Royce Plc A gas turbine engine blade containment assembly
FR2829176B1 (fr) 2001-08-30 2005-06-24 Snecma Moteurs Carter de stator de turbomachine
FR2852053B1 (fr) * 2003-03-06 2007-12-28 Snecma Moteurs Turbine haute pression pour turbomachine
GB2415017A (en) * 2004-06-08 2005-12-14 Rolls Royce Plc Heat shield for attachment to a casing of a gas turbine engine
FR2882573B1 (fr) * 2005-02-25 2007-04-13 Snecma Moteurs Sa Carter interne de turbomachine equipe d'un bouclier thermique
FR2923529B1 (fr) 2007-11-09 2014-05-16 Snecma Raccordement de bras radiaux a une virole circulaire par imbrication de pieces rapportees
US8784061B2 (en) * 2011-01-31 2014-07-22 General Electric Company Methods and systems for controlling thermal differential in turbine systems
US8647055B2 (en) * 2011-04-18 2014-02-11 General Electric Company Ceramic matrix composite shroud attachment system
GB2501918B (en) 2012-05-11 2014-06-18 Rolls Royce Plc Casing
DE102012213622A1 (de) * 2012-08-02 2014-02-06 Siemens Aktiengesellschaft Turbomaschine
ITFI20130118A1 (it) * 2013-05-21 2014-11-22 Nuovo Pignone Srl "compressor with a thermal shield and methods of operation"
DE102013213834A1 (de) 2013-07-15 2015-02-19 MTU Aero Engines AG Verfahren zum Herstellen eines Isolationselements und Isolationselement für ein Gehäuse eines Flugtriebwerks
FR3086691B1 (fr) 2018-09-28 2020-12-11 Safran Aircraft Engines Ensemble annulaire pour turbomachine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2858104A (en) * 1954-02-04 1958-10-28 A V Roe Canada Ltd Adjustable gas turbine shroud ring segments
CH397360A (de) * 1961-11-28 1965-08-15 Licentia Gmbh Rotordichtung mit radial beweglichen Dichtringsegmenten, insbesondere bei Turbomaschinen
US3425665A (en) * 1966-02-24 1969-02-04 Curtiss Wright Corp Gas turbine rotor blade shroud
GB1501916A (en) * 1975-06-20 1978-02-22 Rolls Royce Matching thermal expansions of components of turbo-machines
US4087199A (en) * 1976-11-22 1978-05-02 General Electric Company Ceramic turbine shroud assembly
US4131388A (en) * 1977-05-26 1978-12-26 United Technologies Corporation Outer air seal
US4247248A (en) * 1978-12-20 1981-01-27 United Technologies Corporation Outer air seal support structure for gas turbine engine
US4398866A (en) * 1981-06-24 1983-08-16 Avco Corporation Composite ceramic/metal cylinder for gas turbine engine

Also Published As

Publication number Publication date
IT1168258B (it) 1987-05-20
DE3305170A1 (de) 1983-08-25
GB8300210D0 (en) 1983-02-09
IT8319599A1 (it) 1984-08-15
GB2115487A (en) 1983-09-07
IT8319599A0 (it) 1983-02-15
JPH0261603B2 (fr) 1990-12-20
DE3305170C2 (de) 1994-07-21
GB2115487B (en) 1986-02-05
JPS58152108A (ja) 1983-09-09
FR2522067A1 (fr) 1983-08-26

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