EP1013890A2 - Anstreifdichtung für Turbomaschinen - Google Patents
Anstreifdichtung für Turbomaschinen Download PDFInfo
- Publication number
- EP1013890A2 EP1013890A2 EP99124032A EP99124032A EP1013890A2 EP 1013890 A2 EP1013890 A2 EP 1013890A2 EP 99124032 A EP99124032 A EP 99124032A EP 99124032 A EP99124032 A EP 99124032A EP 1013890 A2 EP1013890 A2 EP 1013890A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- foamed
- gas turbine
- seal
- sealing
- foam
- 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.)
- Granted
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
- F01D11/127—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 a deformable or crushable structure, e.g. honeycomb
-
- 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
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/612—Foam
Definitions
- the invention relates to a brush seal between a wall section and the blade tips of a gas turbine.
- the invention further relates to a Method for producing a gas turbine with such a sealing seal.
- the technical environment in particular refer to EP 0 605 417 B1 and to US 5,388,959.
- Brush seals from or in gas turbines essentially have two Fulfill tasks, namely firstly a flow around the individual running stages prevent the gas turbine and secondly the housing structure or thermally isolate the hot gas in the gas turbine wall sections or control the heat flow passing into the wall sections in such a way that the thermal expansion of the casing is simultaneous with the thermal expansion of the rotating blades or the discs carrying them.
- the so-called gap between the tips of the turbine blades and the these surrounding wall sections or that on the wall sections The intended sealing seal should be over the entire operating range the gas turbine should be as small as possible because of any enlargement of the gap dimension a reduction in thrust and thus a reduced Efficiency.
- the object of the present invention to show an improved sealing seal between a wall section and the blade tips of a gas turbine.
- the solution to this problem is characterized in that the brush seal consists entirely of a foamed, metallic, corrosion-resistant high-temperature alloy.
- two advantageous methods for producing a gas turbine with such a metal foam brush seal are specified.
- the invention proposed here replaces the above. known Sealing systems through a metal foam.
- a uniformly foamed, corrosion-resistant high-temperature alloy such as. Hastalloy X, IN 601, ODS alloys are the ones mentioned Requirements met in an excellent way.
- the one is younger Metal foam technology that has become up to date to the specialist basically known.
- a suitable metal alloy is used
- the present invention is a metallic corrosion-resistant High temperature alloy - foamed using known methods, so that an essentially fine foam structure forms, whereby thin metal walls enclose a variety of cavities between them.
- a foaming method for example, a metal powder mixed with a metal hydrite and then extruded, after which this primary material is thermally foamed.
- one is Appropriate manufacture from prefabricated hollow metal spheres possible. In general, this produces a mainly closed-pore foam Structure with high porosity and good thermal insulation properties educated.
- solder does not migrate (as for example in the case of open-pore structures or metal felts) from the joint into the sealing structure due to capillary forces; so that the foam is easy to solder.
- An alternative production method is to connect the unfoamed primary material to the respective wall section or to the housing structure in a first process step and to foam this primary material in a second process step. This is followed by machining, of course, to bring the metal foam or the sealing gasket into the desired shape.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Material Composition (AREA)
- Sealing With Elastic Sealing Lips (AREA)
Abstract
Description
Die Lösung dieser Aufgabe ist dadurch gekennzeichnet, daß die Anstreifdichtung vollständig aus einer aufgeschäumten, metallischen, korrosionsbeständigen Hochtemperaturlegierung besteht. In den Unteransprüchen sind zwei vorteilhafte Verfahren zum Herstellen einer Gasturbine mit einer derartigen Metallschaum-Anstreifdichtung angegeben.
Ein alternativer Herstellweg besteht darin, in einem ersten Prozeßschritt das ungeschäumte Vormaterial mit dem jeweiligen Wandabschnitt bzw. mit der Gehäusestruktur zu verbinden und in einem zweiten Prozeßschritt dieses Vormaterial zu schäumen. Danach erfolgt selbstverständlich eine spanende Bearbeitung, um den Metallschaum bzw. die Anstreifdichtung in die gewünschte Form zu bringen.
Claims (3)
- Anstreifdichtung zwischen einem Wandabschnitt und den Schaufelspitzen einer Gasturbine, die vollständig aus einer aufgeschäumten, metallischen, korrosionsbeständigen Hochtemperaturlegierung besteht.
- Verfahren zum Herstellen einer Gasturbine mit einer Anstreifdichtung nach Anspruch 1,
dadurch gekennzeichnet, daß vorgefertigte Metallschaumelemente durch Hochtemperaturlöten mit den Wandabschnitten verbunden werden. - Verfahren zum Herstellen einer Gasturbine mit einer Anstreifdichtung nach Anspruch 1,
dadurch gekennzeichnet, daß das nicht aufgeschäumte Vormaterial der Ansteifdichtung zunächst mit den Wandabschnitten verbunden und anschließend daran aufgeschäumt wird.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19858031 | 1998-12-16 | ||
DE19858031A DE19858031A1 (de) | 1998-12-16 | 1998-12-16 | Anstreifdichtung zwischen einem Wandabschnitt und den Schaufelspitzen einer Gasturbine |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1013890A2 true EP1013890A2 (de) | 2000-06-28 |
EP1013890A3 EP1013890A3 (de) | 2001-11-07 |
EP1013890B1 EP1013890B1 (de) | 2004-02-04 |
Family
ID=7891283
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP99124032A Expired - Lifetime EP1013890B1 (de) | 1998-12-16 | 1999-12-09 | Anstreifdichtung für Turbomaschinen |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1013890B1 (de) |
AT (1) | ATE259027T1 (de) |
DE (2) | DE19858031A1 (de) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005061855A1 (de) * | 2003-12-20 | 2005-07-07 | Mtu Aero Engines Gmbh | Gasturbinenbauteil |
DE102013219766A1 (de) | 2013-09-30 | 2015-04-16 | Siemens Aktiengesellschaft | Anstreifdichtung und Dichtungsanordnung |
US9200567B2 (en) | 2009-07-23 | 2015-12-01 | Cummins Turbo Technologies Limited | Compressor, turbine and turbocharger |
US10519792B2 (en) | 2013-11-19 | 2019-12-31 | MTU Aero Engines AG | Run-in coating based on metal fibers |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE50211431D1 (de) | 2001-09-25 | 2008-02-07 | Alstom Technology Ltd | Dichtungsanordnung zur dichtspaltreduzierung innerhalb einer strömungsrotationsmaschine |
DE102007032707A1 (de) | 2007-07-13 | 2009-01-15 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen eines Einlaufbelags |
DE102008007321A1 (de) | 2008-02-02 | 2009-08-13 | Mtu Aero Engines Gmbh | Vorrichtung mit Rotor, Gehäuse und Anstreifdichtung |
DE102008019331A1 (de) * | 2008-04-16 | 2009-10-22 | Rolls-Royce Deutschland Ltd & Co Kg | Einlaufdichtung für den Kompressor eines Gasturbinentriebwerks |
GB0822416D0 (en) | 2008-12-10 | 2009-01-14 | Rolls Royce Plc | A seal and a method of manufacturing a seal |
DE102009016803A1 (de) | 2009-04-09 | 2010-10-14 | Rolls-Royce Deutschland Ltd & Co Kg | Labyrinth-Anstreifdichtung für eine Strömungsmaschine |
DE102011014292A1 (de) * | 2011-03-17 | 2012-09-20 | Rolls-Royce Deutschland Ltd & Co Kg | Zwischenstufendichtungsring sowie Verfahren zu dessen Herstellung |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3235745C2 (de) | 1981-09-29 | 1993-11-11 | United Technologies Corp | Turbinenschaufelabdichtung für Gasturbinenmaschinen |
US5388959A (en) | 1993-08-23 | 1995-02-14 | General Electric Company | Seal including a non-metallic abradable material |
EP0605417B1 (de) | 1991-09-23 | 1997-03-05 | Technetics Corporation | Abschleifbare und undurchlässige dichtung und verfahren zur herstellung |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4177308A (en) * | 1978-08-10 | 1979-12-04 | The United States Of America As Represented By The Secretary Of The Air Force | Non-combustible high temperature abradable seal material |
FR2468741A1 (fr) * | 1979-10-26 | 1981-05-08 | Snecma | Perfectionnements aux anneaux a joint d'etancheite refroidi par l'air pour roues de turbine a gaz |
DE3203869C2 (de) * | 1982-02-05 | 1984-05-10 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turbinenlaufschaufel für Strömungsmaschinen, insbesondere Gasturbinentriebwerke |
DE4241420C1 (de) * | 1992-12-09 | 1993-11-25 | Mtu Muenchen Gmbh | Verfahren zur Herstellung von Bauteilen oder Substraten mit Verbundbeschichtungen und dessen Anwendung |
DE19750516A1 (de) * | 1997-11-14 | 1999-05-20 | Asea Brown Boveri | Abreibbare Dichtung |
-
1998
- 1998-12-16 DE DE19858031A patent/DE19858031A1/de not_active Withdrawn
-
1999
- 1999-12-09 AT AT99124032T patent/ATE259027T1/de not_active IP Right Cessation
- 1999-12-09 EP EP99124032A patent/EP1013890B1/de not_active Expired - Lifetime
- 1999-12-09 DE DE59908461T patent/DE59908461D1/de not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3235745C2 (de) | 1981-09-29 | 1993-11-11 | United Technologies Corp | Turbinenschaufelabdichtung für Gasturbinenmaschinen |
EP0605417B1 (de) | 1991-09-23 | 1997-03-05 | Technetics Corporation | Abschleifbare und undurchlässige dichtung und verfahren zur herstellung |
US5388959A (en) | 1993-08-23 | 1995-02-14 | General Electric Company | Seal including a non-metallic abradable material |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005061855A1 (de) * | 2003-12-20 | 2005-07-07 | Mtu Aero Engines Gmbh | Gasturbinenbauteil |
US7775766B2 (en) | 2003-12-20 | 2010-08-17 | Mtu Aero Engines Gmbh | Gas turbine component |
US9200567B2 (en) | 2009-07-23 | 2015-12-01 | Cummins Turbo Technologies Limited | Compressor, turbine and turbocharger |
US10662806B2 (en) | 2009-07-23 | 2020-05-26 | Cummins Turbo Technologies Limited | Compressor, turbine and turbocharger |
DE102013219766A1 (de) | 2013-09-30 | 2015-04-16 | Siemens Aktiengesellschaft | Anstreifdichtung und Dichtungsanordnung |
US10519792B2 (en) | 2013-11-19 | 2019-12-31 | MTU Aero Engines AG | Run-in coating based on metal fibers |
Also Published As
Publication number | Publication date |
---|---|
EP1013890A3 (de) | 2001-11-07 |
ATE259027T1 (de) | 2004-02-15 |
EP1013890B1 (de) | 2004-02-04 |
DE19858031A1 (de) | 2000-06-21 |
DE59908461D1 (de) | 2004-03-11 |
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