BRPI0907645A2 - Difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião - Google Patents

Difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião

Info

Publication number
BRPI0907645A2
BRPI0907645A2 BRPI0907645-0A BRPI0907645A BRPI0907645A2 BR PI0907645 A2 BRPI0907645 A2 BR PI0907645A2 BR PI0907645 A BRPI0907645 A BR PI0907645A BR PI0907645 A2 BRPI0907645 A2 BR PI0907645A2
Authority
BR
Brazil
Prior art keywords
turbomachine
diffuser
turboreator
airplane turboprop
turboprop
Prior art date
Application number
BRPI0907645-0A
Other languages
English (en)
Inventor
Patrice André Commaret
Didier Hippolyte Hernandez
Romain Nicolas 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
Publication of BRPI0907645A2 publication Critical patent/BRPI0907645A2/pt
Publication of BRPI0907645B1 publication Critical patent/BRPI0907645B1/pt

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)
BRPI0907645-0 2008-02-27 2009-02-20 difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião BRPI0907645B1 (pt)

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 (2)

Publication Number Publication Date
BRPI0907645A2 true BRPI0907645A2 (pt) 2015-07-21
BRPI0907645B1 BRPI0907645B1 (pt) 2019-11-26

Family

ID=40139285

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0907645-0 BRPI0907645B1 (pt) 2008-02-27 2009-02-20 difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião

Country Status (11)

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

Families Citing this family (11)

* 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
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
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
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
CN119983326B (zh) * 2025-02-17 2025-10-21 中国航发湖南动力机械研究所 一种进气均匀的扩压器及径流燃烧室

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5079611A (pt) * 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
BRPI0907645B1 (pt) 2019-11-26
JP2011513624A (ja) 2011-04-28
EP2245314B1 (fr) 2012-05-09
ATE557244T1 (de) 2012-05-15
EP2245314A1 (fr) 2010-11-03
FR2927949B1 (fr) 2010-03-26
US8875517B2 (en) 2014-11-04
CA2712669A1 (fr) 2009-09-24
CN101960151A (zh) 2011-01-26
US20110056207A1 (en) 2011-03-10
WO2009115690A1 (fr) 2009-09-24
ES2386246T3 (es) 2012-08-14
JP5258905B2 (ja) 2013-08-07
RU2488718C2 (ru) 2013-07-27
RU2010139405A (ru) 2012-04-20
FR2927949A1 (fr) 2009-08-28
CA2712669C (fr) 2016-07-05
CN101960151B (zh) 2012-10-24

Similar Documents

Publication Publication Date Title
BRPI0907645A2 (pt) Difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião
WO2014055435A3 (en) Flow divider mechanism for a multi-stage combustor
WO2014028095A3 (en) Blade outer air seal with cored passages
ATE556195T1 (de) Ringförmige schaufelanordnung für einen gasturbinenmotor
BRPI0908165A2 (pt) distribuidor satorizado para uma turbomáquina, turbina baixa-pressão de turbomáquina e turbomáquina tal como um turborreator ou um turbopropulsor de avião
EP2369135A3 (en) Blade outer air seal for a gas turbine engine and corresponding gas turbine engine
WO2014133644A3 (en) Blade outer air seal system for controlled tip clearance
WO2014011246A3 (en) Integrated inlet vane and strut
WO2014186001A3 (en) Flexible feather seal for blade outer air seal gas turbine engine rapid response clearance control system
RU2012108735A (ru) Вибрационно-демпфирующая прокладка для лопасти вентилятора
EP2775098A3 (en) Integrated strut-vane
BRPI0911686A2 (pt) rotor de compressor de uma turbomáquina e turbomáquina, tal como um turborreator ou um turbopropulsor de avião
GB201312222D0 (en) Turbomachine with variable-pitch vortex generator
WO2014186015A3 (en) Actuator for gas turbine engine blade outer air seal
BR112014029523A8 (pt) Pá de ventilador para turborreator de avião, ventilador de turborreator de avião, e, turborreator de avião
WO2015112227A3 (en) Multiple injector holes for gas turbine engine vane
IN2014DN07487A (pt)
IN2014DN10840A (pt)
EP4293198A3 (en) Airfoil platform impingement cooling holes
WO2014186005A3 (en) Gas turbine engine component with combined mate face and platform cooling
EP4047274A3 (en) Main mixer in an axial staged combustor for a gas turbine engine
BR112015018470A2 (pt) anel de suporte híbrido para um motor de aeronave
BR112017012436B8 (pt) Turbomáquina
WO2011128551A3 (fr) Dispositif redresseur pour turbomachine
WO2015069334A3 (en) Variable area turbine arrangement for a gas turbine engine

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 26/11/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 26/11/2019, OBSERVADAS AS CONDICOES LEGAIS