BR112017016899A2 - conjunto-guia de vazão de ar de motor de turbina e motor de turbina - Google Patents

conjunto-guia de vazão de ar de motor de turbina e motor de turbina

Info

Publication number
BR112017016899A2
BR112017016899A2 BR112017016899-5A BR112017016899A BR112017016899A2 BR 112017016899 A2 BR112017016899 A2 BR 112017016899A2 BR 112017016899 A BR112017016899 A BR 112017016899A BR 112017016899 A2 BR112017016899 A2 BR 112017016899A2
Authority
BR
Brazil
Prior art keywords
turbine engine
arm
air flow
flow guide
channel
Prior art date
Application number
BR112017016899-5A
Other languages
English (en)
Other versions
BR112017016899B1 (pt
Inventor
Damevin Henri-Marie
Jacques Pierre Fessou Philippe
Christophe Marie Maniere Vianney
Franck Antoine Schvallinger Michaël
Original Assignee
Safran Aircraft Engines
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 Safran Aircraft Engines filed Critical Safran Aircraft Engines
Publication of BR112017016899A2 publication Critical patent/BR112017016899A2/pt
Publication of BR112017016899B1 publication Critical patent/BR112017016899B1/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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F04D29/544—Blade shapes
    • 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
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
    • 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
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2240/123—Fluid guiding means, e.g. vanes related to the pressure side 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
    • F05D2260/00—Function
    • F05D2260/97—Reducing windage losses
    • 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)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Geometry (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

a invenção se refere a um conjunto-guia de vazão de ar de motor de turbina que inclui: um braço estrutural (30) e uma pá-guia (21) na superfície inferior do braço estrutural, que compreende um bordo de ataque (22), um bordo de fuga (23) e uma linha de arqueamento (24), em que a dita pá e o dito braço se estendem radialmente sobre um eixo geométrico (x-x) do motor de turbina e definem entre os mesmos um canal de vazão de ar. o braço estrutural (30) compreende: uma extremidade a montante (31) que tem um perfil de pá-guia (21) e compreende um bordo de ataque (32) alinhado com o da pá; e um ombro (35) localizado na superfície inferior do braço, de modo a definir um gargalo no canal. o conjunto é caracterizado por a área (agargalo) da seção do canal no gargalo ser entre 0,7 e 0,9 vezes a área (aentrada) da seção do canal nos bordos de ataque.
BR112017016899-5A 2015-02-09 2016-02-09 Conjunto-guia de vazão de ar de motor de turbina e motor de turbina BR112017016899B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1551013 2015-02-09
FR1551013A FR3032495B1 (fr) 2015-02-09 2015-02-09 Ensemble de redressement a performances aerodynamiques optimisees
PCT/FR2016/050274 WO2016128664A1 (fr) 2015-02-09 2016-02-09 Ensemble de redressement a performances aerodynamiques optimisees

Publications (2)

Publication Number Publication Date
BR112017016899A2 true BR112017016899A2 (pt) 2018-03-27
BR112017016899B1 BR112017016899B1 (pt) 2022-11-01

Family

ID=52808037

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112017016899-5A BR112017016899B1 (pt) 2015-02-09 2016-02-09 Conjunto-guia de vazão de ar de motor de turbina e motor de turbina

Country Status (9)

Country Link
US (1) US10385708B2 (pt)
EP (1) EP3256741B1 (pt)
JP (1) JP6629337B2 (pt)
CN (1) CN107208660B (pt)
BR (1) BR112017016899B1 (pt)
CA (1) CA2975570C (pt)
FR (1) FR3032495B1 (pt)
RU (1) RU2711204C2 (pt)
WO (1) WO2016128664A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3051832B1 (fr) * 2016-05-26 2019-09-06 Safran Aircraft Engines Procede de fabrication d'un carter d'echappement de turbomachine
FR3059735B1 (fr) * 2016-12-05 2020-09-25 Safran Aircraft Engines Piece de turbomachine a surface non-axisymetrique
GB201703422D0 (en) * 2017-03-03 2017-04-19 Rolls Royce Plc Gas turbine engine vanes
FR3073891B1 (fr) 2017-11-22 2019-11-22 Safran Aircraft Engines Mat d'un ensemble propulsif
FR3083260B1 (fr) * 2018-06-28 2020-06-19 Safran Aircraft Engines Module d’un moteur d’aeronef a double flux dont un bras integre une aube de stator
FR3090033B1 (fr) * 2018-12-18 2020-11-27 Safran Aircraft Engines Ensemble d’aube directrice de sortie et de bifurcation pour turbomachine
FR3092868B1 (fr) 2019-02-19 2021-01-22 Safran Aircraft Engines Roue de stator d’une turbomachine comprenant des aubes présentant des cordes différentes
FR3093756B1 (fr) * 2019-03-15 2021-02-19 Safran Aircraft Engines redresseur de flux secondaire a Tuyère intégréE
FR3109795B1 (fr) * 2020-04-29 2022-03-25 Safran Aircraft Engines Carter intermediaire de redressement avec bras structural monobloc
FR3109796B1 (fr) * 2020-04-29 2022-03-25 Safran Aircraft Engines Carter intermediaire de redressement avec bras structural rapporte
CN112282856B (zh) * 2020-10-26 2021-09-24 上海交通大学 一种用于抑制通道涡的涡轮叶片
CN113123834B (zh) * 2021-06-17 2021-09-28 中国航发上海商用航空发动机制造有限责任公司 发动机的叶片组件及发动机
US11802525B2 (en) 2022-01-07 2023-10-31 General Electric Company Outlet guide vane

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1291235A (en) * 1968-10-02 1972-10-04 Rolls Royce Fluid flow machine
US6561761B1 (en) * 2000-02-18 2003-05-13 General Electric Company Fluted compressor flowpath
DE102004036594A1 (de) * 2004-07-28 2006-03-23 Mtu Aero Engines Gmbh Strömungsstruktur für eine Gasturbine
DE102010014900A1 (de) * 2010-04-14 2011-10-20 Rolls-Royce Deutschland Ltd & Co Kg Nebenstromkanal eines Turbofantriebwerkes
FR2984428B1 (fr) * 2011-12-19 2018-12-07 Safran Aircraft Engines Redresseur de compresseur pour turbomachine.
JP5676825B2 (ja) * 2011-12-27 2015-02-25 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ ガスタービンエンジン圧縮機構造
US9068460B2 (en) * 2012-03-30 2015-06-30 United Technologies Corporation Integrated inlet vane and strut

Also Published As

Publication number Publication date
RU2711204C2 (ru) 2020-01-15
EP3256741B1 (fr) 2019-01-23
EP3256741A1 (fr) 2017-12-20
JP2018504555A (ja) 2018-02-15
RU2017131456A (ru) 2019-03-12
US20180030843A1 (en) 2018-02-01
FR3032495B1 (fr) 2017-01-13
US10385708B2 (en) 2019-08-20
CA2975570A1 (fr) 2016-08-18
FR3032495A1 (fr) 2016-08-12
WO2016128664A1 (fr) 2016-08-18
RU2017131456A3 (pt) 2019-07-17
BR112017016899B1 (pt) 2022-11-01
CN107208660B (zh) 2019-02-01
CN107208660A (zh) 2017-09-26
JP6629337B2 (ja) 2020-01-15
CA2975570C (fr) 2023-03-21

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Legal Events

Date Code Title Description
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 09/02/2016, OBSERVADAS AS CONDICOES LEGAIS