BR112015000676A2 - pá de turbomáquina, ventoinha da turbomáquina, compressor de alta pressão de uma turbomáquina, compressor de baixa pressão de uma turbomáquina, e, turbomáquina. - Google Patents

pá de turbomáquina, ventoinha da turbomáquina, compressor de alta pressão de uma turbomáquina, compressor de baixa pressão de uma turbomáquina, e, turbomáquina.

Info

Publication number
BR112015000676A2
BR112015000676A2 BR112015000676A BR112015000676A BR112015000676A2 BR 112015000676 A2 BR112015000676 A2 BR 112015000676A2 BR 112015000676 A BR112015000676 A BR 112015000676A BR 112015000676 A BR112015000676 A BR 112015000676A BR 112015000676 A2 BR112015000676 A2 BR 112015000676A2
Authority
BR
Brazil
Prior art keywords
turbocharger
pressure compressor
fan
blade
low
Prior art date
Application number
BR112015000676A
Other languages
English (en)
Other versions
BR112015000676B1 (pt
Inventor
Reiss Hanna
Talbotec Jérôme
Jablonski Laurent
Quevreux Sandrine
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 BR112015000676A2 publication Critical patent/BR112015000676A2/pt
Publication of BR112015000676B1 publication Critical patent/BR112015000676B1/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324Blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/36Application in turbines specially adapted for the fan of turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BR112015000676-0A 2012-07-12 2013-06-28 Pá de turbomáquina, ventoinha da turbomáquina, compressor de alta pressão de uma turbomáquina, compressor de baixa pressão de uma turbomáquina, e, turbomáquina BR112015000676B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1256746A FR2993323B1 (fr) 2012-07-12 2012-07-12 Aube de turbomachine ayant un profil configure de maniere a obtenir des proprietes aerodynamiques et mecaniques ameliorees
FR1256746 2012-07-12
PCT/FR2013/051522 WO2014009628A1 (fr) 2012-07-12 2013-06-28 Aube de turbomachine ayant un profil configuré de manière à obtenir des propriétés aérodynamiques et mécaniques améliorées

Publications (2)

Publication Number Publication Date
BR112015000676A2 true BR112015000676A2 (pt) 2017-06-27
BR112015000676B1 BR112015000676B1 (pt) 2021-09-28

Family

ID=46826816

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015000676-0A BR112015000676B1 (pt) 2012-07-12 2013-06-28 Pá de turbomáquina, ventoinha da turbomáquina, compressor de alta pressão de uma turbomáquina, compressor de baixa pressão de uma turbomáquina, e, turbomáquina

Country Status (9)

Country Link
US (1) US9995156B2 (pt)
EP (1) EP2872782B1 (pt)
JP (2) JP2015522132A (pt)
CN (1) CN104583604B (pt)
BR (1) BR112015000676B1 (pt)
CA (1) CA2878827C (pt)
FR (1) FR2993323B1 (pt)
RU (1) RU2624677C2 (pt)
WO (1) WO2014009628A1 (pt)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3043428B1 (fr) * 2015-11-10 2020-05-29 Safran Aircraft Engines Aube de redresseur de turbomachine
JP6959589B2 (ja) * 2018-11-05 2021-11-02 株式会社Ihi 軸流流体機械の動翼
FR3129686B1 (fr) * 2021-11-29 2024-07-12 Safran Aircraft Engines Aube pour une soufflante carénée d’une turbomachine

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB680036A (en) * 1949-04-26 1952-10-01 Francis Henry Keast Blading for rotary compressors, turbines and the like
US4012172A (en) * 1975-09-10 1977-03-15 Avco Corporation Low noise blades for axial flow compressors
SU1613701A1 (ru) * 1988-07-15 1990-12-15 Харьковский авиационный институт им.Н.Е.Жуковского Лопатка осевой турбомашины
US5088892A (en) 1990-02-07 1992-02-18 United Technologies Corporation Bowed airfoil for the compression section of a rotary machine
JPH07139302A (ja) * 1993-11-17 1995-05-30 Ishikawajima Harima Heavy Ind Co Ltd ブレードの構造
DE19812624A1 (de) * 1998-03-23 1999-09-30 Bmw Rolls Royce Gmbh Rotor-Schaufelblatt einer Axialströmungsmaschine
US6331100B1 (en) * 1999-12-06 2001-12-18 General Electric Company Doubled bowed compressor airfoil
DE10054244C2 (de) * 2000-11-02 2002-10-10 Honda Motor Co Ltd Turbinenblattanordnung und Turbinenblatt für eine Axialturbine
US6508630B2 (en) * 2001-03-30 2003-01-21 General Electric Company Twisted stator vane
FR2851798B1 (fr) * 2003-02-27 2005-04-29 Snecma Moteurs Aube en fleche de turboreacteur
DE102005025213B4 (de) * 2005-06-01 2014-05-15 Honda Motor Co., Ltd. Schaufel einer Axialströmungsmaschine
FR2908152B1 (fr) * 2006-11-08 2009-02-06 Snecma Sa Aube en fleche de turbomachine
GB0701866D0 (en) * 2007-01-31 2007-03-14 Rolls Royce Plc Tone noise reduction in turbomachines
US8083487B2 (en) * 2007-07-09 2011-12-27 General Electric Company Rotary airfoils and method for fabricating same
EP2017466A1 (en) * 2007-07-20 2009-01-21 Siemens Aktiengesellschaft Wind turbine rotor blade and turbine rotor
RU2354854C1 (ru) * 2007-12-20 2009-05-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Рабочее колесо высокооборотного осевого вентилятора или компрессора
US8167567B2 (en) * 2008-12-17 2012-05-01 United Technologies Corporation Gas turbine engine airfoil
JP4923073B2 (ja) * 2009-02-25 2012-04-25 株式会社日立製作所 遷音速翼
FR2969230B1 (fr) * 2010-12-15 2014-11-21 Snecma Aube de compresseur a loi d'empilage amelioree
JP5703750B2 (ja) * 2010-12-28 2015-04-22 株式会社Ihi ファン動翼及びファン
US9062554B2 (en) * 2012-01-03 2015-06-23 General Electric Company Gas turbine nozzle with a flow groove

Also Published As

Publication number Publication date
CN104583604B (zh) 2017-04-12
US20150192024A1 (en) 2015-07-09
FR2993323B1 (fr) 2014-08-15
RU2015104651A (ru) 2016-08-27
RU2624677C2 (ru) 2017-07-05
EP2872782A1 (fr) 2015-05-20
CA2878827A1 (fr) 2014-01-16
US9995156B2 (en) 2018-06-12
CA2878827C (fr) 2019-08-27
JP2018155248A (ja) 2018-10-04
JP6649981B2 (ja) 2020-02-19
WO2014009628A1 (fr) 2014-01-16
BR112015000676B1 (pt) 2021-09-28
EP2872782B1 (fr) 2017-03-08
JP2015522132A (ja) 2015-08-03
FR2993323A1 (fr) 2014-01-17
CN104583604A (zh) 2015-04-29

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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: 20 (VINTE) ANOS CONTADOS A PARTIR DE 28/06/2013, OBSERVADAS AS CONDICOES LEGAIS.