DE60313929D1 - Gehäuse, Verdichter, Turbine und Triebwerk mit einem solchen Gehäuse - Google Patents

Gehäuse, Verdichter, Turbine und Triebwerk mit einem solchen Gehäuse

Info

Publication number
DE60313929D1
DE60313929D1 DE60313929T DE60313929T DE60313929D1 DE 60313929 D1 DE60313929 D1 DE 60313929D1 DE 60313929 T DE60313929 T DE 60313929T DE 60313929 T DE60313929 T DE 60313929T DE 60313929 D1 DE60313929 D1 DE 60313929D1
Authority
DE
Germany
Prior art keywords
housing
turbine
compressor
engine
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 - Lifetime
Application number
DE60313929T
Other languages
English (en)
Other versions
DE60313929T2 (de
Inventor
Biez Philippe Le
Yann Lebret
Claude Mons
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
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of DE60313929D1 publication Critical patent/DE60313929D1/de
Application granted granted Critical
Publication of DE60313929T2 publication Critical patent/DE60313929T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • F01D11/125—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material with a reinforcing structure
    • 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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • 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
    • F04D29/08—Sealings
    • F04D29/16—Sealings between pressure and suction sides
    • F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • 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
    • F04D29/66—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
    • F04D29/685—Inducing localised fluid recirculation in the stator-rotor interface
    • 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
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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)
  • Fluid Mechanics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60313929T 2002-10-22 2003-10-21 Gehäuse, Verdichter, Turbine und Triebwerk mit einem solchen Gehäuse Expired - Lifetime DE60313929T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0213144 2002-10-22
FR0213144A FR2846034B1 (fr) 2002-10-22 2002-10-22 Carter, compresseur, turbine et turbomoteur a combustion comprenant un tel carter

Publications (2)

Publication Number Publication Date
DE60313929D1 true DE60313929D1 (de) 2007-07-05
DE60313929T2 DE60313929T2 (de) 2008-01-17

Family

ID=32050624

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60313929T Expired - Lifetime DE60313929T2 (de) 2002-10-22 2003-10-21 Gehäuse, Verdichter, Turbine und Triebwerk mit einem solchen Gehäuse

Country Status (7)

Country Link
US (1) US6881029B2 (de)
EP (1) EP1413771B1 (de)
JP (1) JP4148872B2 (de)
CA (1) CA2444982C (de)
DE (1) DE60313929T2 (de)
FR (1) FR2846034B1 (de)
RU (1) RU2324076C2 (de)

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US7370467B2 (en) * 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
EP1649145B1 (de) * 2003-07-29 2008-05-28 Pratt & Whitney Canada Corp. Turbofan-Triebwerksgehäuse, Turbofantriebwerk und entsprechendes Verfahren
DE102004055439A1 (de) * 2004-11-17 2006-05-24 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit dynamischer Strömungsbeeinflussung
FR2887890B1 (fr) * 2005-06-30 2007-10-12 Snecma Composition de materiau abradable, piece thermomecanique ou carter comprenant un revetement et procede de fabrication ou de reparation d'un revetement presentant cette composition
US7722316B2 (en) * 2005-09-13 2010-05-25 Rolls-Royce Power Engineering Plc Acoustic viscous damper for centrifugal gas compressor
US8602156B2 (en) * 2006-05-19 2013-12-10 United Technologies Corporation Multi-splice acoustic liner
US7686570B2 (en) * 2006-08-01 2010-03-30 Siemens Energy, Inc. Abradable coating system
EP2171283A4 (de) * 2007-02-14 2013-01-30 Borgwarner Inc Verdichtergehäuse
FR2912789B1 (fr) * 2007-02-21 2009-10-02 Snecma Sa Carter avec traitement de carter, compresseur et turbomachine comportant un tel carter.
DE102007037924A1 (de) * 2007-08-10 2009-02-12 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Ringkanalwandausnehmung
FR2921100B1 (fr) * 2007-09-13 2009-12-04 Snecma Levier d'entrainement en rotation autour de son pivot d'aube de stator a calage variable de turbomachine
DE102008011644A1 (de) * 2008-02-28 2009-09-03 Rolls-Royce Deutschland Ltd & Co Kg Gehäusestrukturierung für Axialverdichter im Nabenbereich
DE102008031982A1 (de) * 2008-07-07 2010-01-14 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Nut an einem Laufspalt eines Schaufelendes
DE102008037154A1 (de) 2008-08-08 2010-02-11 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine
EP2418387B1 (de) * 2010-08-11 2015-04-01 Techspace Aero S.A. Gehäusering eines Kompressors eines axialen Turbotriebwerks
EP2532898A1 (de) * 2011-06-08 2012-12-12 Siemens Aktiengesellschaft Axialturboverdichter
GB201116029D0 (en) * 2011-09-16 2011-10-26 Rolls Royce Plc Abradable panel and method of forming the same
EP2938843B1 (de) * 2012-12-28 2020-04-08 United Technologies Corporation Axialspannungssystem für ein gehäuse einer gasturbine
EP2951241A4 (de) * 2013-01-29 2016-08-24 United Technologies Corp Klingenabriebmaterial
JP6184173B2 (ja) * 2013-05-29 2017-08-23 三菱日立パワーシステムズ株式会社 ガスタービン
GB201311460D0 (en) * 2013-06-27 2013-08-14 Rolls Royce Plc An abradable liner for a gas turbine engine
EP2886804B1 (de) * 2013-12-20 2017-08-16 Safran Aero Boosters SA Dichtungsanordnung für einen Verdicther eines Turbotriebwerks
US8939716B1 (en) * 2014-02-25 2015-01-27 Siemens Aktiengesellschaft Turbine abradable layer with nested loop groove pattern
US9151175B2 (en) 2014-02-25 2015-10-06 Siemens Aktiengesellschaft Turbine abradable layer with progressive wear zone multi level ridge arrays
RU2662003C2 (ru) 2014-02-25 2018-07-23 Сименс Акциенгезелльшафт Компонент газовой турбины, газотурбинный двигатель, способ изготовления компонента газотурбинного двигателя
US9243511B2 (en) 2014-02-25 2016-01-26 Siemens Aktiengesellschaft Turbine abradable layer with zig zag groove pattern
BE1022170B1 (fr) * 2014-10-15 2016-02-24 Techspace Aero S.A. Capot moteur isolant pour test de turbomachine sur banc d'essais
US10273192B2 (en) 2015-02-17 2019-04-30 Rolls-Royce Corporation Patterned abradable coating and methods for the manufacture thereof
WO2016133583A1 (en) 2015-02-18 2016-08-25 Siemens Aktiengesellschaft Turbine shroud with abradable layer having ridges with holes
US10408079B2 (en) 2015-02-18 2019-09-10 Siemens Aktiengesellschaft Forming cooling passages in thermal barrier coated, combustion turbine superalloy components
US10107307B2 (en) * 2015-04-14 2018-10-23 Pratt & Whitney Canada Corp. Gas turbine engine rotor casing treatment
RU2596894C1 (ru) * 2015-06-02 2016-09-10 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Барабан ротора турбомашины
RU2596895C1 (ru) * 2015-06-02 2016-09-10 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Барабан ротора турбомашины
DE102018208040A1 (de) * 2018-05-23 2019-11-28 MTU Aero Engines AG Dichtungsträger und Strömungsmaschine
US10914318B2 (en) 2019-01-10 2021-02-09 General Electric Company Engine casing treatment for reducing circumferentially variable distortion
EP3996889B1 (de) * 2019-07-11 2024-01-10 Safran Aircraft Engines Verfahren zur herstellung eines teils aus einem verbundmaterial durch injektion einer gefüllten schlämme in eine faserige textur
CN111535869B (zh) * 2020-04-29 2022-07-29 中国航发湖南动力机械研究所 涡轮导向器
BE1028335B1 (fr) * 2020-05-20 2021-12-20 Safran Aero Boosters Sous-ensemble de compresseur basse pression d'une turbomachine d'aéronef

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DE1022745B (de) * 1956-07-20 1958-01-16 Maschf Augsburg Nuernberg Ag Anordnung zur Verminderung des Spaltverlustes in Stroemungsmaschinen
US3425665A (en) * 1966-02-24 1969-02-04 Curtiss Wright Corp Gas turbine rotor blade shroud
FR1533120A (fr) * 1966-11-02 1968-07-12 Gen Electric Chemise à refroidissement par l'air pour turbine de moteur à turbine à gaz
US3867061A (en) * 1973-12-26 1975-02-18 Curtiss Wright Corp Shroud structure for turbine rotor blades and the like
US4639388A (en) * 1985-02-12 1987-01-27 Chromalloy American Corporation Ceramic-metal composites
US5161942A (en) * 1990-10-24 1992-11-10 Westinghouse Electric Corp. Moisture drainage of honeycomb seals
US5520508A (en) * 1994-12-05 1996-05-28 United Technologies Corporation Compressor endwall treatment
JP3544471B2 (ja) * 1998-05-12 2004-07-21 日本碍子株式会社 六角セルハニカム構造体とその把持方法
US6203927B1 (en) * 1999-02-05 2001-03-20 Siemens Westinghouse Power Corporation Thermal barrier coating resistant to sintering
US6485025B1 (en) * 2000-11-27 2002-11-26 Neomet Limited Metallic cellular structure

Also Published As

Publication number Publication date
RU2003131385A (ru) 2005-04-10
EP1413771B1 (de) 2007-05-23
JP2004278516A (ja) 2004-10-07
US6881029B2 (en) 2005-04-19
FR2846034A1 (fr) 2004-04-23
EP1413771A1 (de) 2004-04-28
FR2846034B1 (fr) 2006-06-23
DE60313929T2 (de) 2008-01-17
JP4148872B2 (ja) 2008-09-10
RU2324076C2 (ru) 2008-05-10
US20050058541A1 (en) 2005-03-17
CA2444982A1 (fr) 2004-04-22
CA2444982C (fr) 2011-08-30

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