DE602006006268D1 - Ringförmige Schneidendichtung für eine Labyrinthdichtung und sein Herstellungsverfahren - Google Patents
Ringförmige Schneidendichtung für eine Labyrinthdichtung und sein HerstellungsverfahrenInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23H—WORKING 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
- B23H9/00—Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
- B23H9/10—Working turbine blades or nozzles
-
- 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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- 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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
- F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, 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
- F02C7/28—Arrangement of seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/445—Free-space packings with means for adjusting the clearance
-
- 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
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/12—Manufacture by removing material by spark erosion methods
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/22—Manufacture essentially without removing material by sintering
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/237—Brazing
-
- 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
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/181—Two-dimensional patterned ridged
-
- 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
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/182—Two-dimensional patterned crenellated, notched
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- 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)
- 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)
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) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
-
2005
- 2005-11-15 FR FR0511579A patent/FR2893359A1/fr active Pending
-
2006
- 2006-11-14 CA CA2567892A patent/CA2567892C/fr active Active
- 2006-11-15 RU RU2006140332/06A patent/RU2454547C2/ru active
- 2006-11-15 DE DE602006006268T patent/DE602006006268D1/de active Active
- 2006-11-15 US US11/560,100 patent/US7857581B2/en active Active
- 2006-11-15 EP EP06124101A patent/EP1785651B1/de active Active
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
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |