ATE557244T1 - Diffusor für einen turbinenmotor mit gekerbten ringförmigen netzen - Google Patents

Diffusor für einen turbinenmotor mit gekerbten ringförmigen netzen

Info

Publication number
ATE557244T1
ATE557244T1 AT09722143T AT09722143T ATE557244T1 AT E557244 T1 ATE557244 T1 AT E557244T1 AT 09722143 T AT09722143 T AT 09722143T AT 09722143 T AT09722143 T AT 09722143T AT E557244 T1 ATE557244 T1 AT E557244T1
Authority
AT
Austria
Prior art keywords
diffuser
turbine engine
notched
annual
mesh
Prior art date
Application number
AT09722143T
Other languages
English (en)
Inventor
Patrice Commaret
Didier Hernandez
Romain Lunel
Original Assignee
Snecma
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 filed Critical Snecma
Application granted granted Critical
Publication of ATE557244T1 publication Critical patent/ATE557244T1/de

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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • 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
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • 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
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444—Bladed diffusers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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)
  • Fuel-Injection Apparatus (AREA)
AT09722143T 2008-02-27 2009-02-20 Diffusor für einen turbinenmotor mit gekerbten ringförmigen netzen ATE557244T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0801059A FR2927949B1 (fr) 2008-02-27 2008-02-27 Diffuseur de turbomachine comportant des voiles annulaires echancres
PCT/FR2009/000192 WO2009115690A1 (fr) 2008-02-27 2009-02-20 Diffuseur de turbomachine comportant des voiles annulaires echancres

Publications (1)

Publication Number Publication Date
ATE557244T1 true ATE557244T1 (de) 2012-05-15

Family

ID=40139285

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09722143T ATE557244T1 (de) 2008-02-27 2009-02-20 Diffusor für einen turbinenmotor mit gekerbten ringförmigen netzen

Country Status (11)

Country Link
US (1) US8875517B2 (de)
EP (1) EP2245314B1 (de)
JP (1) JP5258905B2 (de)
CN (1) CN101960151B (de)
AT (1) ATE557244T1 (de)
BR (1) BRPI0907645B1 (de)
CA (1) CA2712669C (de)
ES (1) ES2386246T3 (de)
FR (1) FR2927949B1 (de)
RU (1) RU2488718C2 (de)
WO (1) WO2009115690A1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2927951B1 (fr) * 2008-02-27 2011-08-19 Snecma Ensemble diffuseur-redresseur pour une turbomachine
FR3019879A1 (fr) * 2014-04-09 2015-10-16 Turbomeca Moteur d'aeronef comprenant un calage azimutal du diffuseur, par rapport a la chambre de combustion
FR3020865B1 (fr) * 2014-05-12 2016-05-20 Snecma Chambre annulaire de combustion
DE102014012764A1 (de) * 2014-09-02 2016-03-03 Man Diesel & Turbo Se Radialverdichterstufe
CN104449471A (zh) * 2014-12-18 2015-03-25 贵州新三荣包装印务有限公司 一种环保粘结剂
CN104449475A (zh) * 2014-12-18 2015-03-25 贵州新三荣包装印务有限公司 一种不干胶粘结剂制备方法
FR3057015B1 (fr) * 2016-09-30 2018-12-07 Safran Aircraft Engines Disque de rotor comportant une toile a epaisseur variable
US10718222B2 (en) 2017-03-27 2020-07-21 General Electric Company Diffuser-deswirler for a gas turbine engine
UA131257U (uk) * 2018-07-02 2019-01-10 Публічне Акціонерне Товариство "Мотор Січ" Дифузор відцентрового компресора
US11098730B2 (en) * 2019-04-12 2021-08-24 Rolls-Royce Corporation Deswirler assembly for a centrifugal compressor

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5079611A (de) * 1973-11-15 1975-06-28
US4327547A (en) * 1978-11-23 1982-05-04 Rolls-Royce Limited Fuel injectors
US4416111A (en) * 1981-02-25 1983-11-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Air modulation apparatus
GB2100409B (en) * 1981-04-24 1984-10-03 Rolls Royce Gas turbine engine fuel burners
US4462204A (en) * 1982-07-23 1984-07-31 General Electric Company Gas turbine engine cooling airflow modulator
CN2033059U (zh) * 1988-02-02 1989-02-22 丹尼尔·C·斯坎皮尼 可变扩散器
FR2694962B1 (fr) * 1992-08-19 1994-10-21 Snecma Turboréacteur dont la chambre de combustion est protégée contre les effets d'une ingestion massive d'eau.
DE4438611C2 (de) * 1994-10-28 1998-02-19 Bmw Rolls Royce Gmbh Radialverdichter oder Radialturbine mit einem Leitschaufeln aufweisenden Diffusor oder Turbinenleitkranz
US6035627A (en) * 1998-04-21 2000-03-14 Pratt & Whitney Canada Inc. Turbine engine with cooled P3 air to impeller rear cavity
US6564555B2 (en) * 2001-05-24 2003-05-20 Allison Advanced Development Company Apparatus for forming a combustion mixture in a gas turbine engine
US6647730B2 (en) * 2001-10-31 2003-11-18 Pratt & Whitney Canada Corp. Turbine engine having turbine cooled with diverted compressor intermediate pressure air
US6880341B2 (en) * 2002-12-18 2005-04-19 Pratt & Whitney Canada Corp. Low cost combustor floating collar with improved sealing and damping
US6976363B2 (en) * 2003-08-11 2005-12-20 General Electric Company Combustor dome assembly of a gas turbine engine having a contoured swirler
US7581397B2 (en) * 2005-08-26 2009-09-01 Honeywell International Inc. Diffuser particle separator
FR2891314B1 (fr) * 2005-09-28 2015-04-24 Snecma Bras d'injecteur anti-cokefaction.
US7874158B2 (en) * 2005-11-29 2011-01-25 United Technologies Corporation Dirt separator for compressor diffuser in gas turbine engine
US20070183890A1 (en) * 2006-02-09 2007-08-09 Honeywell International, Inc. Leaned deswirl vanes behind a centrifugal compressor in a gas turbine engine
JP2007224866A (ja) * 2006-02-24 2007-09-06 Mitsubishi Heavy Ind Ltd 遠心圧縮機
FR2904033B1 (fr) * 2006-07-19 2011-01-21 Snecma Ensemble diffuseur-redresseur pour une turbomachine
FR2911669B1 (fr) 2007-01-23 2011-09-16 Snecma Carenage pour chambre de combustion, chambre de combustion en etant equipee et turboreacteur les comportant.
US8438855B2 (en) * 2008-07-24 2013-05-14 General Electric Company Slotted compressor diffuser and related method

Also Published As

Publication number Publication date
EP2245314B1 (de) 2012-05-09
BRPI0907645B1 (pt) 2019-11-26
CA2712669A1 (fr) 2009-09-24
EP2245314A1 (de) 2010-11-03
ES2386246T3 (es) 2012-08-14
JP5258905B2 (ja) 2013-08-07
WO2009115690A1 (fr) 2009-09-24
JP2011513624A (ja) 2011-04-28
CA2712669C (fr) 2016-07-05
FR2927949B1 (fr) 2010-03-26
RU2488718C2 (ru) 2013-07-27
BRPI0907645A2 (pt) 2015-07-21
US20110056207A1 (en) 2011-03-10
US8875517B2 (en) 2014-11-04
CN101960151A (zh) 2011-01-26
FR2927949A1 (fr) 2009-08-28
RU2010139405A (ru) 2012-04-20
CN101960151B (zh) 2012-10-24

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