JP5461828B2 - 半径方向間隙を改善するための装置を備えるターボ機械モジュール - Google Patents

半径方向間隙を改善するための装置を備えるターボ機械モジュール Download PDF

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Publication number
JP5461828B2
JP5461828B2 JP2008310568A JP2008310568A JP5461828B2 JP 5461828 B2 JP5461828 B2 JP 5461828B2 JP 2008310568 A JP2008310568 A JP 2008310568A JP 2008310568 A JP2008310568 A JP 2008310568A JP 5461828 B2 JP5461828 B2 JP 5461828B2
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Japan
Prior art keywords
turbomachine
annular
shock absorbing
cover plate
module according
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Active
Application number
JP2008310568A
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English (en)
Japanese (ja)
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JP2009144706A (ja
JP2009144706A5 (https=
Inventor
アントワーヌ・ブルネ
クロード・シヨメール
セバスチヤン・ジユスト
エマニユエル・ウラドウ
ドミニク・ロラン
フレデリツク・ルノー
ジユリアン・セドラツク
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
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Publication date
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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
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/105—Final actuators by passing part of the fluid
    • 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
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP2008310568A 2007-12-14 2008-12-05 半径方向間隙を改善するための装置を備えるターボ機械モジュール Active JP5461828B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0708709 2007-12-14
FR0708709A FR2925109B1 (fr) 2007-12-14 2007-12-14 Module de turbomachine muni d'un dispositif d'amelioration des jeux radiaux

Publications (3)

Publication Number Publication Date
JP2009144706A JP2009144706A (ja) 2009-07-02
JP2009144706A5 JP2009144706A5 (https=) 2013-08-22
JP5461828B2 true JP5461828B2 (ja) 2014-04-02

Family

ID=39689054

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008310568A Active JP5461828B2 (ja) 2007-12-14 2008-12-05 半径方向間隙を改善するための装置を備えるターボ機械モジュール

Country Status (6)

Country Link
US (1) US8052381B2 (https=)
EP (1) EP2071133B1 (https=)
JP (1) JP5461828B2 (https=)
CA (1) CA2646297C (https=)
FR (1) FR2925109B1 (https=)
RU (1) RU2472000C2 (https=)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2078837A1 (de) * 2008-01-11 2009-07-15 Siemens Aktiengesellschaft Zapfluftentnahmevorrichtung für einen Verdichter eines Gasturbinentriebwerks
RU2525384C2 (ru) * 2012-11-07 2014-08-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Статор компрессора газотурбинного двигателя
WO2014204629A1 (en) 2013-06-19 2014-12-24 United Technologies Corporation Windback heat shield
CN106704266B (zh) * 2016-12-21 2023-04-25 浙江理工大学 一种双涵道轴流通风机
US20180313364A1 (en) * 2017-04-27 2018-11-01 General Electric Company Compressor apparatus with bleed slot including turning vanes
FR3071561B1 (fr) * 2017-09-25 2021-09-24 Safran Aircraft Engines Module de compresseur de turbomachine a flasque evide
US11242764B2 (en) * 2018-05-17 2022-02-08 Raytheon Technologies Corporation Seal assembly with baffle for gas turbine engine

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3407945A1 (de) * 1984-03-03 1985-09-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Verfahren und mittel zur vermeidung der entstehung von titanfeuer
US5160241A (en) * 1991-09-09 1992-11-03 General Electric Company Multi-port air channeling assembly
FR2688539A1 (fr) * 1992-03-11 1993-09-17 Snecma Stator de turbomachine comprenant des dispositifs de reglage de jeu entre le stator et les aubes du rotor.
GB9210642D0 (en) 1992-05-19 1992-07-08 Rolls Royce Plc Rotor shroud assembly
US5653581A (en) * 1994-11-29 1997-08-05 United Technologies Corporation Case-tied joint for compressor stators
US5685693A (en) * 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control
US5562408A (en) * 1995-06-06 1996-10-08 General Electric Company Isolated turbine shroud
FR2766231B1 (fr) 1997-07-18 1999-08-20 Snecma Dispositif d'echauffement ou de refroidissement d'un carter circulaire
US6116852A (en) * 1997-12-11 2000-09-12 Pratt & Whitney Canada Corp. Turbine passive thermal valve for improved tip clearance control
RU2151886C1 (ru) * 1998-08-04 2000-06-27 Открытое акционерное общество "Авиадвигатель" Статор многоступенчатой газовой турбины
FR2794816B1 (fr) * 1999-06-10 2001-07-06 Snecma Stator de compresseur a haute pression
GB2388407B (en) 2002-05-10 2005-10-26 Rolls Royce Plc Gas turbine blade tip clearance control structure
US6732530B2 (en) * 2002-05-31 2004-05-11 Mitsubishi Heavy Industries, Ltd. Gas turbine compressor and clearance controlling method therefor
US6783324B2 (en) * 2002-08-15 2004-08-31 General Electric Company Compressor bleed case
FR2860041B1 (fr) * 2003-09-22 2005-11-25 Snecma Moteurs Realisation de l'etancheite dans un turboreacteur pour le prelevement cabine par tube a double rotule
US7249929B2 (en) * 2003-11-13 2007-07-31 United Technologies Corporation Bleed housing
FR2866079B1 (fr) * 2004-02-05 2006-03-17 Snecma Moteurs Diffuseur pour turboreacteur
GB2417762B (en) * 2004-09-04 2006-10-04 Rolls Royce Plc Turbine case cooling
FR2882573B1 (fr) * 2005-02-25 2007-04-13 Snecma Moteurs Sa Carter interne de turbomachine equipe d'un bouclier thermique

Also Published As

Publication number Publication date
RU2008149153A (ru) 2010-06-20
FR2925109B1 (fr) 2015-05-15
CA2646297A1 (en) 2009-06-14
US20090202341A1 (en) 2009-08-13
US8052381B2 (en) 2011-11-08
CA2646297C (en) 2015-06-16
EP2071133B1 (fr) 2018-06-13
RU2472000C2 (ru) 2013-01-10
EP2071133A1 (fr) 2009-06-17
JP2009144706A (ja) 2009-07-02
FR2925109A1 (fr) 2009-06-19

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