MX2009000257A - Metodo de fabricacion de un elemento de turbomaquina y dispositivo obtenido de esta manera. - Google Patents
Metodo de fabricacion de un elemento de turbomaquina y dispositivo obtenido de esta manera.Info
- Publication number
- MX2009000257A MX2009000257A MX2009000257A MX2009000257A MX2009000257A MX 2009000257 A MX2009000257 A MX 2009000257A MX 2009000257 A MX2009000257 A MX 2009000257A MX 2009000257 A MX2009000257 A MX 2009000257A MX 2009000257 A MX2009000257 A MX 2009000257A
- Authority
- MX
- Mexico
- Prior art keywords
- manufacturing
- way
- device obtained
- abradable material
- turbomachine element
- Prior art date
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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C39/00—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor
- B29C39/02—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor for making articles of definite length, i.e. discrete articles
- B29C39/10—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor for making articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. casting around inserts or for coating articles
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C67/00—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
- B29C67/24—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 characterised by the choice of material
- B29C67/246—Moulding high reactive monomers or prepolymers, e.g. by reaction injection moulding [RIM], liquid injection moulding [LIM]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2083/00—Use of polymers having silicon, with or without sulfur, nitrogen, oxygen, or carbon only, in the main chain, as moulding material
-
- 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
- F05D2230/60—Assembly 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
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Uso de plataformas de aspas de estator para la deposicián de una pista de material abrasible adyacente dentro de un forro de turbomáquina externo. Las aspas (13) de estator se unen al forro (11) de manera que definen un borde (33) anular que es sustancialmente continuo y el material abrasible se deposita utilizando este borde para delimitar un límite de la pista de material (15) abrasible.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP07150429A EP2075416B1 (fr) | 2007-12-27 | 2007-12-27 | Procédé de fabrication d'un élément de turbomachine et dispositif ainsi obtenu |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2009000257A true MX2009000257A (es) | 2009-06-26 |
Family
ID=39717788
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2009000257A MX2009000257A (es) | 2007-12-27 | 2009-01-07 | Metodo de fabricacion de un elemento de turbomaquina y dispositivo obtenido de esta manera. |
Country Status (8)
Country | Link |
---|---|
US (1) | US8192150B2 (es) |
EP (1) | EP2075416B1 (es) |
JP (1) | JP5575392B2 (es) |
CN (1) | CN101497976B (es) |
BR (1) | BRPI0805624A2 (es) |
CA (1) | CA2648862C (es) |
MX (1) | MX2009000257A (es) |
RU (1) | RU2485326C2 (es) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2977521B1 (fr) * | 2011-07-04 | 2013-08-23 | Snecma | Dispositif et procede de moulage d'une piste de materiau abradable sur une virole d'un ensemble annulaire aubage pour turbomachine |
EP2586989B1 (fr) * | 2011-10-27 | 2015-04-29 | Techspace Aero S.A. | Virole composite co-injectée de compresseur de turbomachine axiale |
EP2735706B8 (fr) * | 2012-11-21 | 2016-12-07 | Safran Aero Booster S.A. | Redresseur à aubes de compresseur de turbomachine axiale et procédé de fabrication |
EP2738356B1 (fr) * | 2012-11-29 | 2019-05-01 | Safran Aero Boosters SA | Aube de redresseur de turbomachine, redresseur de turbomachine et procédé de montage associé |
EP2811121B1 (fr) * | 2013-06-03 | 2019-07-31 | Safran Aero Boosters SA | Carter composite de compresseur de turbomachine axiale avec bride de fixation métallique |
EP2883688B1 (fr) * | 2013-12-13 | 2021-09-22 | Safran Aero Boosters SA | Carter annulaire composite de compresseur de turbomachine et procédé d'obtention de celui-ci |
BE1022497B1 (fr) * | 2014-06-05 | 2016-05-12 | Techspace Aero S.A. | Moule pour piste d'abradable sous virole interne de compresseur de turbomachine axiale |
BE1023290B1 (fr) * | 2015-07-22 | 2017-01-24 | Safran Aero Boosters S.A. | Aube composite de compresseur de turbomachine axiale |
CN107542499B (zh) * | 2017-09-30 | 2019-12-20 | 中国航发沈阳发动机研究所 | 风扇机匣 |
CN107747563B (zh) * | 2017-09-30 | 2020-04-10 | 中国航发沈阳发动机研究所 | 带阻尼的风扇机匣 |
CN107642504B (zh) * | 2017-09-30 | 2019-08-23 | 中国航发沈阳发动机研究所 | 螺纹装配的风扇机匣 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3070353A (en) * | 1958-12-03 | 1962-12-25 | Gen Motors Corp | Shroud assembly |
FR2535795B1 (fr) * | 1982-11-08 | 1987-04-10 | Snecma | Dispositif de suspension d'aubes statoriques de compresseur axial pour le controle actif des jeux entre rotor et stator |
DE8507551U1 (es) * | 1985-03-14 | 1990-10-11 | Mtu Muenchen Gmbh | |
GB2207629B (en) * | 1987-07-22 | 1991-01-02 | Rolls Royce Plc | Method of manufacture of an axial flow compressor assembly |
DE4100777A1 (de) * | 1990-12-18 | 1992-06-25 | Asea Brown Boveri | Einlassgehaeuse fuer dampfturbine |
US5304032A (en) * | 1991-07-22 | 1994-04-19 | Bosna Alexander A | Abradable non-metallic seal for rotating turbine engines |
DE4242851A1 (de) * | 1992-12-18 | 1994-06-23 | Mtu Muenchen Gmbh | Verfahren zur Herstellung eines Leitgitters für Turbomaschinen, insbesondere für Axialverdichter |
US5429478A (en) * | 1994-03-31 | 1995-07-04 | United Technologies Corporation | Airfoil having a seal and an integral heat shield |
DE19543764A1 (de) * | 1995-11-24 | 1997-05-28 | Asea Brown Boveri | Berührungsdichtung für Strömungsmaschinen |
DE10020673C2 (de) * | 2000-04-27 | 2002-06-27 | Mtu Aero Engines Gmbh | Ringstruktur in Metallbauweise |
GB2388161A (en) * | 2002-05-02 | 2003-11-05 | Rolls Royce Plc | Gas turbine engine compressor casing |
US20040086635A1 (en) * | 2002-10-30 | 2004-05-06 | Grossklaus Warren Davis | Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
US7025563B2 (en) * | 2003-12-19 | 2006-04-11 | United Technologies Corporation | Stator vane assembly for a gas turbine engine |
US20070197719A1 (en) * | 2006-02-21 | 2007-08-23 | United Technologies Corporation | Turbine friendly abradable material |
US20070237629A1 (en) * | 2006-04-05 | 2007-10-11 | General Electric Company | Gas turbine compressor casing flowpath rings |
US20070248457A1 (en) * | 2006-04-25 | 2007-10-25 | General Electric Company | Rub coating for gas turbine engine compressors |
US20080081109A1 (en) * | 2006-09-29 | 2008-04-03 | General Electric Company | Porous abradable coating and method for applying the same |
US7908867B2 (en) * | 2007-09-14 | 2011-03-22 | Siemens Energy, Inc. | Wavy CMC wall hybrid ceramic apparatus |
-
2007
- 2007-12-27 EP EP07150429A patent/EP2075416B1/fr active Active
-
2008
- 2008-12-23 CA CA2648862A patent/CA2648862C/fr not_active Expired - Fee Related
- 2008-12-24 US US12/343,675 patent/US8192150B2/en active Active
- 2008-12-26 BR BRPI0805624-2A patent/BRPI0805624A2/pt not_active IP Right Cessation
- 2008-12-26 JP JP2008332353A patent/JP5575392B2/ja not_active Expired - Fee Related
- 2008-12-26 RU RU2008151973/06A patent/RU2485326C2/ru not_active IP Right Cessation
- 2008-12-29 CN CN2008101891578A patent/CN101497976B/zh active Active
-
2009
- 2009-01-07 MX MX2009000257A patent/MX2009000257A/es active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
US8192150B2 (en) | 2012-06-05 |
BRPI0805624A2 (pt) | 2009-09-15 |
CA2648862A1 (fr) | 2009-06-27 |
CA2648862C (fr) | 2015-12-01 |
EP2075416A1 (fr) | 2009-07-01 |
CN101497976B (zh) | 2013-06-19 |
CN101497976A (zh) | 2009-08-05 |
RU2008151973A (ru) | 2010-07-10 |
EP2075416B1 (fr) | 2011-05-18 |
US20090175719A1 (en) | 2009-07-09 |
JP2009156263A (ja) | 2009-07-16 |
JP5575392B2 (ja) | 2014-08-20 |
RU2485326C2 (ru) | 2013-06-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant or registration |