DE602006006268D1 - Ringförmige Schneidendichtung für eine Labyrinthdichtung und sein Herstellungsverfahren - Google Patents

Ringförmige Schneidendichtung für eine Labyrinthdichtung und sein Herstellungsverfahren

Info

Publication number
DE602006006268D1
DE602006006268D1 DE602006006268T DE602006006268T DE602006006268D1 DE 602006006268 D1 DE602006006268 D1 DE 602006006268D1 DE 602006006268 T DE602006006268 T DE 602006006268T DE 602006006268 T DE602006006268 T DE 602006006268T DE 602006006268 D1 DE602006006268 D1 DE 602006006268D1
Authority
DE
Germany
Prior art keywords
seal
manufacturing
ring
shaped cutting
labyrinth
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.)
Active
Application number
DE602006006268T
Other languages
English (en)
Inventor
Claude Mons
Joel Vigneau
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 DE602006006268D1 publication Critical patent/DE602006006268D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23HWORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
    • B23H9/00Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
    • B23H9/10Working turbine blades or nozzles
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • 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
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/081Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/28Arrangement of seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/44Free-space packings
    • F16J15/445Free-space packings with means for adjusting the clearance
    • 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
    • F05D2230/00Manufacture
    • F05D2230/10Manufacture by removing material
    • F05D2230/12Manufacture by removing material by spark erosion methods
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/22Manufacture essentially without removing material by sintering
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • F05D2230/237Brazing
    • 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
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/18Two-dimensional patterned
    • F05D2250/181Two-dimensional patterned ridged
    • 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
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/18Two-dimensional patterned
    • F05D2250/182Two-dimensional patterned crenellated, notched
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/21Oxide ceramics
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
DE602006006268T 2005-11-15 2006-11-15 Ringförmige Schneidendichtung für eine Labyrinthdichtung und sein Herstellungsverfahren Active DE602006006268D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0511579A FR2893359A1 (fr) 2005-11-15 2005-11-15 Lechette annulaire destinee a un laryrinthe d'etancheite, et son procede de fabrication

Publications (1)

Publication Number Publication Date
DE602006006268D1 true DE602006006268D1 (de) 2009-05-28

Family

ID=36781968

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006006268T Active DE602006006268D1 (de) 2005-11-15 2006-11-15 Ringförmige Schneidendichtung für eine Labyrinthdichtung und sein Herstellungsverfahren

Country Status (6)

Country Link
US (1) US7857581B2 (de)
EP (1) EP1785651B1 (de)
CA (1) CA2567892C (de)
DE (1) DE602006006268D1 (de)
FR (1) FR2893359A1 (de)
RU (1) RU2454547C2 (de)

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* Cited by examiner, † Cited by third party
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FR2884550B1 (fr) * 2005-04-15 2010-09-17 Snecma Moteurs Piece pour proteger le bord d'attaque d'une pale
US8790085B2 (en) * 2005-07-13 2014-07-29 Beacon Lighting International Limited Combined ceiling fan and light fitting
FR2922263B1 (fr) 2007-10-11 2009-12-11 Snecma Stator de turbine pour turbomachine d'aeronef integrant un dispositif d'amortissement de vibrations
DE102008061800A1 (de) * 2008-12-11 2010-06-17 Rolls-Royce Deutschland Ltd & Co Kg Segmentierte Dichtlippen für Labyrinthdichtungsringe
FR2946687B1 (fr) * 2009-06-10 2011-07-01 Snecma Turbomachine comprenant des moyens ameliores de reglage du debit d'un flux d'air de refroidissement preleve en sortie de compresseur haute pression
FR2950656B1 (fr) 2009-09-25 2011-09-23 Snecma Ventilation d'une roue de turbine dans une turbomachine
DE102009055913A1 (de) * 2009-11-27 2011-06-09 Rolls-Royce Deutschland Ltd & Co Kg Labyrinthdichtung aus in eine Einlaufschicht eingreifenden Dichtringen
US8529736B2 (en) 2010-05-25 2013-09-10 General Electric Company System and method for metal cutting
US8002286B1 (en) * 2010-06-14 2011-08-23 Florida Turbine Technologies, Inc. Aerodynamically mistuned labyrinth seal
US20120027573A1 (en) * 2010-08-02 2012-02-02 General Electric Company Seal teeth for seal assembly
US20120177484A1 (en) * 2011-01-07 2012-07-12 General Electric Company Elliptical Sealing System
US8784037B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment with integrated impingement plate
US8784044B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment
US9079245B2 (en) 2011-08-31 2015-07-14 Pratt & Whitney Canada Corp. Turbine shroud segment with inter-segment overlap
US9028744B2 (en) 2011-08-31 2015-05-12 Pratt & Whitney Canada Corp. Manufacturing of turbine shroud segment with internal cooling passages
US8784041B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment with integrated seal
FR3021348B1 (fr) * 2014-05-20 2016-06-10 Snecma Rotor de turbine pour un moteur a turbine a gaz
DE102015206516A1 (de) 2015-04-13 2016-10-13 MTU Aero Engines AG Labyrinthdichtung mit verbesserten Dichtrippen
EP3124742B1 (de) * 2015-07-28 2018-11-07 MTU Aero Engines GmbH Gasturbine
DE102015217670A1 (de) 2015-09-15 2017-03-16 Rolls-Royce Deutschland Ltd & Co Kg Dichtungselement, Dichtungssystem mit einem Dichtungselement, Turbomaschine mit einem Dichtungssystem und Verfahren zur Herstellung eines Dichtungselements
RU178381U1 (ru) * 2017-08-16 2018-04-02 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ БЮДЖЕТНОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Брянский государственный технический университет" Амортизатор для гашения вибраций статора турбореактивного двигателя
FR3072121B1 (fr) * 2017-10-06 2021-07-30 Safran Aircraft Engines Dispositif d'etancheite entre rotor et stator de turbomachine
FR3073595B1 (fr) * 2017-11-15 2020-02-07 Safran Helicopter Engines Joint a labyrinthe comprenant une lechette dotee d'un deflecteur
US11274569B2 (en) 2017-12-13 2022-03-15 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10570773B2 (en) 2017-12-13 2020-02-25 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10502093B2 (en) * 2017-12-13 2019-12-10 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10533454B2 (en) 2017-12-13 2020-01-14 Pratt & Whitney Canada Corp. Turbine shroud cooling
WO2019168501A1 (en) * 2018-02-27 2019-09-06 Siemens Aktiengesellschaft Turbine cooling air delivery system
CN109202254B (zh) * 2018-03-13 2020-10-16 中国航空制造技术研究院 一种外环面的密集长方形环焊缝的电子束焊接方法
FR3081498B1 (fr) * 2018-05-23 2022-12-23 Safran Aircraft Engines Joint labyrinthe de turbomachine avec lechette revetue
FR3109182B1 (fr) * 2020-04-10 2023-03-24 Safran Aircraft Engines Ensemble d’etancheite pour une turbomachine
US11365645B2 (en) 2020-10-07 2022-06-21 Pratt & Whitney Canada Corp. Turbine shroud cooling
US11773773B1 (en) * 2022-07-26 2023-10-03 Rolls-Royce North American Technologies Inc. Gas turbine engine centrifugal compressor with impeller load and cooling control

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DE474361C (de) * 1926-11-07 1929-03-30 Bergmann Elek Citaets Werke Ak Einrichtung zur Abdichtung umlaufender Teile, insbesondere der Wellen von Dampf- oder Gasturbinen
US3537713A (en) * 1968-02-21 1970-11-03 Garrett Corp Wear-resistant labyrinth seal
JPS5590229A (en) * 1978-12-12 1980-07-08 Toshiba Corp Electrochemical machining method for turbine blade wheel
SU792014A1 (ru) * 1978-12-13 1980-12-30 Предприятие П/Я М-5906 Лабиринтное уплотнение
US4608145A (en) * 1984-07-23 1986-08-26 General Electric Company Electroplating tape
JPS6161720A (ja) * 1984-09-03 1986-03-29 Nissan Motor Co Ltd タ−ビンロ−タの加工方法
SU1576757A1 (ru) * 1988-09-22 1990-07-07 Всесоюзный научно-исследовательский и конструкторско-технологический институт компрессорного машиностроения Лабиринтное ступенчатое уплотнение турбомашины
DE4341216C2 (de) * 1993-12-03 1997-01-16 Mtu Muenchen Gmbh Dichtungsbauteil für Spalt- oder Labyrinthdichtungen und Verfahren zu seiner Herstellung
DE4439950C2 (de) * 1994-11-09 2001-03-01 Mtu Muenchen Gmbh Metallisches Bauteil mit einer Verbundbeschichtung, Verwendung, sowie Verfahren zur Herstellung von metallischen Bauteilen
DE19933445C2 (de) * 1999-07-16 2001-12-13 Mtu Aero Engines Gmbh Dichtring für nicht- hermetische Fluiddichtungen
DE10047307A1 (de) * 2000-09-25 2002-08-01 Alstom Switzerland Ltd Dichtungsanordnung

Also Published As

Publication number Publication date
CA2567892C (fr) 2014-12-30
EP1785651B1 (de) 2009-04-15
CA2567892A1 (fr) 2007-05-15
US7857581B2 (en) 2010-12-28
RU2454547C2 (ru) 2012-06-27
EP1785651A1 (de) 2007-05-16
US20070110562A1 (en) 2007-05-17
FR2893359A1 (fr) 2007-05-18
RU2006140332A (ru) 2008-05-20

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Legal Events

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8364 No opposition during term of opposition