MX2015007582A - Álabe, de turbomaquina turbomáquina correspondiente y método para fabricar un álabe de turbina. - Google Patents
Álabe, de turbomaquina turbomáquina correspondiente y método para fabricar un álabe de turbina.Info
- Publication number
- MX2015007582A MX2015007582A MX2015007582A MX2015007582A MX2015007582A MX 2015007582 A MX2015007582 A MX 2015007582A MX 2015007582 A MX2015007582 A MX 2015007582A MX 2015007582 A MX2015007582 A MX 2015007582A MX 2015007582 A MX2015007582 A MX 2015007582A
- Authority
- MX
- Mexico
- Prior art keywords
- blade
- airfoil portion
- turbomachine
- manufacturing
- rotor
- 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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/02—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
-
- 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
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/10—Formation of a green body
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
-
- 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
- Y10T29/49339—Hollow blade
- Y10T29/49341—Hollow blade with cooling passage
Abstract
Un álabe 20 de una turbomáquina comprende una porción aerodinámica 21; la porción aerodinámica 21 se extiende en dirección longitudinal; la porción aerodinámica está definida lateralmente por una superficie externa; la porción aerodinámica tiene una forma tridimensional y torcida y tiene una cavidad interna 24 ; el álabe está en una sola pieza; además, el álabe está diseñado para una disposición de rotor o de estator; el rotor o estator define una dirección radial y una dirección axial; la superficie externa de la porción aerodinámica tiene un borde delantero y un borde trasero; el borde frontal y/o el borde trasero cambian hacia atrás o hacia adelante en la dirección axial que se mueve en la dirección radial; la cavidad interna se extiende sustancialmente a lo largo de toda la longitud longitudinal de la porción aerodinámica; la fabricación aditiva es particularmente eficaz y ventajas para tal álabe.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000059A ITCO20120059A1 (it) | 2012-12-13 | 2012-12-13 | Metodi per produrre pale cave sagomate in 3d di turbomacchine mediante produzione additiva, pale cave di turbomacchina e turbomacchine |
PCT/EP2013/076294 WO2014090907A1 (en) | 2012-12-13 | 2013-12-11 | Turbomachine blade, corresponding turbomachine and method of manufacturing a turbine blade |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2015007582A true MX2015007582A (es) | 2015-10-22 |
Family
ID=47631578
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2015007582A MX2015007582A (es) | 2012-12-13 | 2013-12-11 | Álabe, de turbomaquina turbomáquina correspondiente y método para fabricar un álabe de turbina. |
Country Status (10)
Country | Link |
---|---|
US (1) | US20150337664A1 (es) |
EP (1) | EP2932041A1 (es) |
JP (1) | JP2016505754A (es) |
KR (1) | KR20150093784A (es) |
CN (1) | CN105121787B (es) |
CA (1) | CA2894828A1 (es) |
IT (1) | ITCO20120059A1 (es) |
MX (1) | MX2015007582A (es) |
RU (1) | RU2015122163A (es) |
WO (1) | WO2014090907A1 (es) |
Families Citing this family (22)
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US20150003995A1 (en) * | 2012-11-14 | 2015-01-01 | United Technologies Corporation | Aircraft engine component with locally tailored materials |
US9649690B2 (en) * | 2014-02-25 | 2017-05-16 | General Electric Company | System having layered structure and method of making the same |
PL3206816T3 (pl) | 2014-11-21 | 2020-11-16 | Siemens Aktiengesellschaft | Sposób wytwarzania elementu składowego i element składowy |
DE102015201782A1 (de) | 2015-02-02 | 2016-08-18 | MTU Aero Engines AG | Leitschaufelring für eine Strömungsmaschine |
EP3081751B1 (en) | 2015-04-14 | 2020-10-21 | Ansaldo Energia Switzerland AG | Cooled airfoil and method for manufacturing said airfoil |
US9850763B2 (en) * | 2015-07-29 | 2017-12-26 | General Electric Company | Article, airfoil component and method for forming article |
CN105626163B (zh) * | 2015-12-28 | 2017-09-26 | 无锡透平叶片有限公司 | 一种隔板静叶锻造转角的确定方法 |
WO2017147499A1 (en) * | 2016-02-25 | 2017-08-31 | Eaton Corporation | Additively manufactured rotors for superchargers and expanders |
US20180147655A1 (en) * | 2016-11-30 | 2018-05-31 | Arcam Ab | Additive manufacturing of three-dimensional articles |
US10487660B2 (en) * | 2016-12-19 | 2019-11-26 | General Electric Company | Additively manufactured blade extension with internal features |
JP6349449B1 (ja) * | 2017-09-19 | 2018-06-27 | 三菱日立パワーシステムズ株式会社 | タービン翼の製造方法、及びタービン翼 |
US10822981B2 (en) | 2017-10-30 | 2020-11-03 | General Electric Company | Variable guide vane sealing |
GB201718144D0 (en) * | 2017-11-02 | 2017-12-20 | Rolls Royce Plc | Manufacturing method |
US10793943B2 (en) * | 2018-03-15 | 2020-10-06 | Raytheon Technologies Corporation | Method of producing a gas turbine engine component |
FR3079265B1 (fr) * | 2018-03-23 | 2020-04-17 | Safran Aircraft Engines | Support de palier de turboreacteur obtenu par fabrication additive |
FR3082554B1 (fr) * | 2018-06-15 | 2021-06-04 | Safran Aircraft Engines | Aube de turbine comprenant un systeme passif de reduction des phenomenes tourbillonaires dans un flux d'air qui la parcourt |
FR3084695A1 (fr) * | 2018-07-31 | 2020-02-07 | Safran Aircraft Engines | Aube composite a armature metallique et son procede de fabrication |
US10815821B2 (en) | 2018-08-31 | 2020-10-27 | General Electric Company | Variable airfoil with sealed flowpath |
JP7260845B2 (ja) * | 2019-01-16 | 2023-04-19 | 株式会社Ihi | タービン動翼 |
JP7144374B2 (ja) * | 2019-07-29 | 2022-09-29 | 日立Geニュークリア・エナジー株式会社 | トランジションピースの製造方法およびトランジションピース |
GB201913394D0 (en) * | 2019-09-17 | 2019-10-30 | Rolls Royce Plc | A vane |
US11686210B2 (en) | 2021-03-24 | 2023-06-27 | General Electric Company | Component assembly for variable airfoil systems |
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CH541065A (de) * | 1972-01-20 | 1973-08-31 | Bbc Brown Boveri & Cie | Verdrillte Laufschaufel einer axial durchströmten Turbomaschine |
US4512069A (en) * | 1983-02-04 | 1985-04-23 | Motoren-Und Turbinen-Union Munchen Gmbh | Method of manufacturing hollow flow profiles |
FR2556409B1 (fr) * | 1983-12-12 | 1991-07-12 | Gen Electric | Aube perfectionnee pour moteur a turbine a gaz et procede de fabrication |
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DE102009048665A1 (de) * | 2009-09-28 | 2011-03-31 | Siemens Aktiengesellschaft | Turbinenschaufel und Verfahren zu deren Herstellung |
FR2955609B1 (fr) * | 2010-01-26 | 2012-04-27 | Snecma | Aube composite a canaux internes |
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US11000899B2 (en) * | 2012-01-29 | 2021-05-11 | Raytheon Technologies Corporation | Hollow airfoil construction utilizing functionally graded materials |
US9249668B2 (en) * | 2012-04-24 | 2016-02-02 | United Technologies Corporation | Airfoil with break-way, free-floating damper member |
US9120144B2 (en) * | 2013-02-06 | 2015-09-01 | Siemens Aktiengesellschaft | Casting core for twisted gas turbine engine airfoil having a twisted rib |
-
2012
- 2012-12-13 IT IT000059A patent/ITCO20120059A1/it unknown
-
2013
- 2013-12-11 US US14/651,893 patent/US20150337664A1/en not_active Abandoned
- 2013-12-11 WO PCT/EP2013/076294 patent/WO2014090907A1/en active Application Filing
- 2013-12-11 CN CN201380065444.7A patent/CN105121787B/zh not_active Expired - Fee Related
- 2013-12-11 JP JP2015547008A patent/JP2016505754A/ja active Pending
- 2013-12-11 MX MX2015007582A patent/MX2015007582A/es unknown
- 2013-12-11 RU RU2015122163A patent/RU2015122163A/ru unknown
- 2013-12-11 EP EP13802671.1A patent/EP2932041A1/en not_active Withdrawn
- 2013-12-11 CA CA2894828A patent/CA2894828A1/en not_active Abandoned
- 2013-12-11 KR KR1020157018154A patent/KR20150093784A/ko not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
JP2016505754A (ja) | 2016-02-25 |
US20150337664A1 (en) | 2015-11-26 |
KR20150093784A (ko) | 2015-08-18 |
CN105121787A (zh) | 2015-12-02 |
CN105121787B (zh) | 2018-02-09 |
ITCO20120059A1 (it) | 2014-06-14 |
WO2014090907A1 (en) | 2014-06-19 |
CA2894828A1 (en) | 2014-06-19 |
RU2015122163A (ru) | 2017-01-16 |
EP2932041A1 (en) | 2015-10-21 |
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