BRPI1013840A2 - virola para estator de módulo de turbomotor de aeronave, parte de estator, módulo de turbomotor de aeronave, e, turbomotor para aeronave - Google Patents

virola para estator de módulo de turbomotor de aeronave, parte de estator, módulo de turbomotor de aeronave, e, turbomotor para aeronave

Info

Publication number
BRPI1013840A2
BRPI1013840A2 BRPI1013840A BRPI1013840A BRPI1013840A2 BR PI1013840 A2 BRPI1013840 A2 BR PI1013840A2 BR PI1013840 A BRPI1013840 A BR PI1013840A BR PI1013840 A BRPI1013840 A BR PI1013840A BR PI1013840 A2 BRPI1013840 A2 BR PI1013840A2
Authority
BR
Brazil
Prior art keywords
aircraft turbo
module
stator
aircraft
ferrule
Prior art date
Application number
BRPI1013840A
Other languages
English (en)
Inventor
Vincenzo Bertoli
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 BRPI1013840A2 publication Critical patent/BRPI1013840A2/pt
Publication of BRPI1013840B1 publication Critical patent/BRPI1013840B1/pt

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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • 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
    • 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
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/114—Purpose of the control system to prolong engine life by limiting mechanical stresses
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BRPI1013840-4A 2009-05-07 2010-05-04 Virola para estator de módulo de turbomotor de aeronave, parte de estator, módulo de turbomotor de aeronave, e, turbomotor para aeronave BRPI1013840B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0953055A FR2945331B1 (fr) 2009-05-07 2009-05-07 Virole pour stator de turbomoteur d'aeronef a fentes de dechargement mecanique d'aubes.
FR0953055 2009-05-07
PCT/EP2010/055998 WO2010128025A1 (fr) 2009-05-07 2010-05-04 Virole pour stator de turbomoteur d'aeronef a fentes de dechargement mecanique d'aubes

Publications (2)

Publication Number Publication Date
BRPI1013840A2 true BRPI1013840A2 (pt) 2016-04-12
BRPI1013840B1 BRPI1013840B1 (pt) 2020-06-23

Family

ID=41059728

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1013840-4A BRPI1013840B1 (pt) 2009-05-07 2010-05-04 Virola para estator de módulo de turbomotor de aeronave, parte de estator, módulo de turbomotor de aeronave, e, turbomotor para aeronave

Country Status (9)

Country Link
US (1) US9017022B2 (pt)
EP (1) EP2427659B1 (pt)
JP (1) JP5699132B2 (pt)
CN (1) CN102422027B (pt)
BR (1) BRPI1013840B1 (pt)
CA (1) CA2760667C (pt)
FR (1) FR2945331B1 (pt)
RU (1) RU2527809C2 (pt)
WO (1) WO2010128025A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2984428B1 (fr) 2011-12-19 2018-12-07 Safran Aircraft Engines Redresseur de compresseur pour turbomachine.
US10550699B2 (en) * 2013-03-06 2020-02-04 United Technologies Corporation Pretrenched rotor for gas turbine engine
US9938840B2 (en) * 2015-02-10 2018-04-10 United Technologies Corporation Stator vane with platform having sloped face
US9988918B2 (en) 2015-05-01 2018-06-05 General Electric Company Compressor system and airfoil assembly
FR3048017B1 (fr) 2016-02-24 2019-05-31 Safran Aircraft Engines Redresseur pour compresseur de turbomachine d'aeronef, comprenant des orifices de prelevement d'air de forme etiree selon la direction circonferentielle
FR3056630B1 (fr) * 2016-09-26 2018-12-07 Safran Aircraft Engines Disque aubage monobloc de soufflante pour turbomachine d'aeronef

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2143466A (en) * 1937-12-31 1939-01-10 Westinghouse Electric & Mfg Co Turbine apparatus
FR994013A (fr) * 1944-12-05 1951-11-09 Rateau Soc Perfectionnement à l'exécution des distributeurs et tuyères de turbines
GB1100384A (en) * 1965-03-10 1968-01-24 Bristol Siddeley Engines Ltd Stator blade assemblies for axial flow compressors or turbines
DE1801475B2 (de) * 1968-10-05 1971-08-12 Daimler Benz Ag, 7000 Stuttgart Luftgekuehlte turbinenschaufel
JPH10299408A (ja) * 1997-04-22 1998-11-10 Hitachi Ltd ガスタービン静翼
JPH1113406A (ja) * 1997-06-23 1999-01-19 Hitachi Ltd ガスタービン静翼
JP3559152B2 (ja) * 1997-10-13 2004-08-25 新潟原動機株式会社 ターボ機械の静翼及びその組立方法
JPH11141352A (ja) * 1997-11-07 1999-05-25 Hitachi Ltd ガスタービン高温部品の保守管理装置およびその方法
US6290466B1 (en) * 1999-09-17 2001-09-18 General Electric Company Composite blade root attachment
US6478537B2 (en) * 2001-02-16 2002-11-12 Siemens Westinghouse Power Corporation Pre-segmented squealer tip for turbine blades
US6550254B2 (en) * 2001-08-17 2003-04-22 General Electric Company Gas turbine engine bleed scoops
SE519781C2 (sv) * 2001-08-29 2003-04-08 Volvo Aero Corp Förfarande för framställning av en stator-eller rotorkomponent
WO2004044387A1 (de) * 2002-11-13 2004-05-27 Abb Turbo Systems Ag Geschlitzte strömungsleitschaufel
FR2874403B1 (fr) * 2004-08-23 2006-09-29 Snecma Moteurs Sa Aube de compresseur ou de turbune a gaz
EP1724443A1 (de) * 2005-05-20 2006-11-22 ABB Turbo Systems AG Düsenring
US7329087B2 (en) * 2005-09-19 2008-02-12 General Electric Company Seal-less CMC vane to platform interfaces
EP1857636A1 (de) * 2006-05-18 2007-11-21 Siemens Aktiengesellschaft Schaufel einer Strömungsmaschine und Verfahren zur Anpassung der Steifigkeit von Schaufelblatt und Plattform
US7597536B1 (en) * 2006-06-14 2009-10-06 Florida Turbine Technologies, Inc. Turbine airfoil with de-coupled platform
US8292567B2 (en) * 2006-09-14 2012-10-23 Caterpillar Inc. Stator assembly including bleed ports for turbine engine compressor
US7686576B2 (en) 2006-10-24 2010-03-30 General Electric Company Method and apparatus for assembling gas turbine engines
US8177502B2 (en) * 2008-11-25 2012-05-15 General Electric Company Vane with reduced stress

Also Published As

Publication number Publication date
JP2012526228A (ja) 2012-10-25
US20120051938A1 (en) 2012-03-01
JP5699132B2 (ja) 2015-04-08
CA2760667C (fr) 2016-08-30
EP2427659B1 (fr) 2017-10-11
CA2760667A1 (fr) 2010-11-11
WO2010128025A1 (fr) 2010-11-11
CN102422027A (zh) 2012-04-18
EP2427659A1 (fr) 2012-03-14
BRPI1013840B1 (pt) 2020-06-23
US9017022B2 (en) 2015-04-28
CN102422027B (zh) 2015-05-13
RU2011149631A (ru) 2013-06-20
RU2527809C2 (ru) 2014-09-10
FR2945331B1 (fr) 2011-07-22
FR2945331A1 (fr) 2010-11-12

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 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 23/06/2020, OBSERVADAS AS CONDICOES LEGAIS.