FR2961564B1 - Compresseur et turbomachine a rendement optimise - Google Patents

Compresseur et turbomachine a rendement optimise

Info

Publication number
FR2961564B1
FR2961564B1 FR1054826A FR1054826A FR2961564B1 FR 2961564 B1 FR2961564 B1 FR 2961564B1 FR 1054826 A FR1054826 A FR 1054826A FR 1054826 A FR1054826 A FR 1054826A FR 2961564 B1 FR2961564 B1 FR 2961564B1
Authority
FR
France
Prior art keywords
turbomachine
compressor
optimized
optimized turbomachine
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
FR1054826A
Other languages
English (en)
Other versions
FR2961564A1 (fr
Inventor
Vincent Paul Gabriel Perrot
Agnes Pesteil
Lieven Baert
Vasiliki Iliopoulou
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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
Priority to FR1054826A priority Critical patent/FR2961564B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to CN201180029982.1A priority patent/CN102947598B/zh
Priority to CA2801221A priority patent/CA2801221C/fr
Priority to JP2013514758A priority patent/JP5882311B2/ja
Priority to EP11735463.9A priority patent/EP2582985B1/fr
Priority to US13/703,809 priority patent/US9488179B2/en
Priority to RU2013102076/06A priority patent/RU2568355C2/ru
Priority to BR112012030350-3A priority patent/BR112012030350B1/pt
Priority to PCT/FR2011/051307 priority patent/WO2011157927A1/fr
Publication of FR2961564A1 publication Critical patent/FR2961564A1/fr
Application granted granted Critical
Publication of FR2961564B1 publication Critical patent/FR2961564B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • 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
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
    • 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
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F04D29/522—Casings; Connections of working fluid for axial pumps 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
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
    • F04D29/526—Details of the casing section radially opposing blade tips
    • 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
    • F04D29/545—Ducts
    • 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
    • F04D29/545—Ducts
    • F04D29/547—Ducts having a special shape in order to influence fluid flow
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2212—Improvement of heat transfer by creating turbulence

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)
FR1054826A 2010-06-17 2010-06-17 Compresseur et turbomachine a rendement optimise Expired - Fee Related FR2961564B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR1054826A FR2961564B1 (fr) 2010-06-17 2010-06-17 Compresseur et turbomachine a rendement optimise
CA2801221A CA2801221C (fr) 2010-06-17 2011-06-09 Compresseur et turbomachine a rendement optimise
JP2013514758A JP5882311B2 (ja) 2010-06-17 2011-06-09 最適化された効率性を備えた圧縮機およびタービンエンジン
EP11735463.9A EP2582985B1 (fr) 2010-06-17 2011-06-09 Compresseur et turbomachine a rendement optimise.
CN201180029982.1A CN102947598B (zh) 2010-06-17 2011-06-09 压缩机和具有最佳效率的涡轮发动机
US13/703,809 US9488179B2 (en) 2010-06-17 2011-06-09 Compressor and a turbine engine with optimized efficiency
RU2013102076/06A RU2568355C2 (ru) 2010-06-17 2011-06-09 Компрессор и газотурбинный двигатель с оптимизированным коэффициентом полезного действия
BR112012030350-3A BR112012030350B1 (pt) 2010-06-17 2011-06-09 compressor de turbomáquina de fluxo axial e turbomáquina
PCT/FR2011/051307 WO2011157927A1 (fr) 2010-06-17 2011-06-09 Compresseur et turbomachine a rendement optimise.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1054826A FR2961564B1 (fr) 2010-06-17 2010-06-17 Compresseur et turbomachine a rendement optimise

Publications (2)

Publication Number Publication Date
FR2961564A1 FR2961564A1 (fr) 2011-12-23
FR2961564B1 true FR2961564B1 (fr) 2016-03-04

Family

ID=43414868

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1054826A Expired - Fee Related FR2961564B1 (fr) 2010-06-17 2010-06-17 Compresseur et turbomachine a rendement optimise

Country Status (9)

Country Link
US (1) US9488179B2 (fr)
EP (1) EP2582985B1 (fr)
JP (1) JP5882311B2 (fr)
CN (1) CN102947598B (fr)
BR (1) BR112012030350B1 (fr)
CA (1) CA2801221C (fr)
FR (1) FR2961564B1 (fr)
RU (1) RU2568355C2 (fr)
WO (1) WO2011157927A1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102817873B (zh) * 2012-08-10 2015-07-15 势加透博（北京）科技有限公司 航空发动机压气机的梯状间隙结构
US9568009B2 (en) 2013-03-11 2017-02-14 Rolls-Royce Corporation Gas turbine engine flow path geometry
DE102014212652A1 (de) 2014-06-30 2016-01-14 MTU Aero Engines AG Strömungsmaschine
JP6374760B2 (ja) * 2014-10-24 2018-08-15 三菱重工業株式会社 軸流タービン及び過給機
EP3088672A1 (fr) * 2015-04-27 2016-11-02 Siemens Aktiengesellschaft Procédé de conception d'un moteur à écoulement de fluide et moteur à écoulement de fluide
US10808539B2 (en) 2016-07-25 2020-10-20 Raytheon Technologies Corporation Rotor blade for a gas turbine engine
EP3421725A1 (fr) * 2017-06-26 2019-01-02 Siemens Aktiengesellschaft Aube de compresseur
JP7223570B2 (ja) * 2018-12-06 2023-02-16 三菱重工業株式会社 タービン動翼、タービン及びチップクリアランス計測方法

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191210179A (en) 1911-05-04 1912-06-20 Heinrich Holzer Arrangement for Diminishing Clearance Losses in Turbines and Pumps for Liquids and Elastic Fluids.
FR1348186A (fr) * 1963-02-19 1964-01-04 Hélice carénée
US3300121A (en) * 1965-02-24 1967-01-24 Gen Motors Corp Axial-flow compressor
DE2351308C3 (de) * 1973-10-12 1981-10-08 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen Einrichtung zur Erweiterung des Arbeitsbereichs von Axialströmungsmaschinen
GB1518293A (en) * 1975-09-25 1978-07-19 Rolls Royce Axial flow compressors particularly for gas turbine engines
US4606699A (en) * 1984-02-06 1986-08-19 General Electric Company Compressor casing recess
JPS613998U (ja) * 1984-06-13 1986-01-11 三菱重工業株式会社 流体機械のケ−シングトリ−トメント装置
SU1560812A1 (ru) * 1987-05-13 1990-04-30 Харьковский авиационный институт им.Н.Е.Жуковского Осевой компрессор
JPH0738641Y2 (ja) * 1989-07-26 1995-09-06 三菱重工業株式会社 多段軸流タービン
JP3118136B2 (ja) 1994-03-28 2000-12-18 株式会社先進材料利用ガスジェネレータ研究所 軸流圧縮機のケーシング
KR20010005910A (ko) * 1997-04-01 2001-01-15 칼 하인쯔 호르닝어 유동 채널 또는 터빈 블레이드의 벽 표면 구조
ATE373175T1 (de) * 1999-07-15 2007-09-15 Hitachi Plant Technologies Ltd Turbomaschinen
US6338609B1 (en) * 2000-02-18 2002-01-15 General Electric Company Convex compressor casing
US6499940B2 (en) * 2001-03-19 2002-12-31 Williams International Co., L.L.C. Compressor casing for a gas turbine engine
DE50306028D1 (de) * 2002-02-28 2007-02-01 Mtu Aero Engines Gmbh Rezirkulationsstruktur für turboverdichter
JP3927886B2 (ja) 2002-08-09 2007-06-13 本田技研工業株式会社 軸流圧縮機
DE10355241A1 (de) 2003-11-26 2005-06-30 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidzufuhr
US7287956B2 (en) * 2004-12-22 2007-10-30 General Electric Company Removable abradable seal carriers for sealing between rotary and stationary turbine components
JP5055179B2 (ja) * 2008-03-25 2012-10-24 三菱重工業株式会社 軸流式圧縮機のケーシング
FR2929349B1 (fr) * 2008-03-28 2010-04-16 Snecma Carter pour roue a aubes mobiles de turbomachine
FR2933149B1 (fr) 2008-06-25 2010-08-20 Snecma Injection d'air dans la veine d'un compresseur de turbomachine
FR2933148B1 (fr) 2008-06-25 2010-08-20 Snecma Compresseur de turbomachine
DE102008052401A1 (de) * 2008-10-21 2010-04-22 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Laufspalteinzug
EP2218918A1 (fr) * 2009-02-13 2010-08-18 Siemens Aktiengesellschaft Compresseur turbo axial pour une turbine à gaz ayant des pertes de gaz et des pertes de diffuseur réduites
US8177494B2 (en) * 2009-03-15 2012-05-15 United Technologies Corporation Buried casing treatment strip for a gas turbine engine

Also Published As

Publication number Publication date
US20130156559A1 (en) 2013-06-20
EP2582985B1 (fr) 2020-07-15
RU2013102076A (ru) 2014-07-27
CN102947598B (zh) 2016-05-04
US9488179B2 (en) 2016-11-08
CN102947598A (zh) 2013-02-27
EP2582985A1 (fr) 2013-04-24
BR112012030350A2 (pt) 2016-08-09
JP5882311B2 (ja) 2016-03-09
RU2568355C2 (ru) 2015-11-20
BR112012030350B1 (pt) 2020-11-17
WO2011157927A1 (fr) 2011-12-22
CA2801221C (fr) 2018-09-04
JP2013529740A (ja) 2013-07-22
FR2961564A1 (fr) 2011-12-23
CA2801221A1 (fr) 2011-12-22

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Year of fee payment: 6

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CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170717

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Year of fee payment: 12

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Effective date: 20230205