ES2324858T3 - Estructura disco-alabes unitaria ranurada. - Google Patents
Estructura disco-alabes unitaria ranurada. Download PDFInfo
- Publication number
- ES2324858T3 ES2324858T3 ES02251636T ES02251636T ES2324858T3 ES 2324858 T3 ES2324858 T3 ES 2324858T3 ES 02251636 T ES02251636 T ES 02251636T ES 02251636 T ES02251636 T ES 02251636T ES 2324858 T3 ES2324858 T3 ES 2324858T3
- Authority
- ES
- Spain
- Prior art keywords
- flange
- unitary
- grooved
- blades
- alabes
- 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.)
- Expired - Lifetime
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
- F01D5/02—Blade-carrying members, e.g. rotors
-
- 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
- F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
- B23K20/129—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding specially adapted for particular articles or workpieces
-
- 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/001—Turbines
-
- 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
-
- 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
- Y10T29/49318—Repairing or disassembling
-
- 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
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
-
- 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
- Y10T29/49325—Shaping integrally bladed rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Ceramic Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Una estructura disco-álabes unitaria (10), que comprende: un disco (16) que incluye un reborde (16a); una fila de álabes (18) que se extiende en dirección radial hacia fuera desde dicho reborde en una estructura unitaria con éste para delimitar entre ellos unos correspondientes pasos de flujo (20); incluyendo el reborde (16a) del disco unos talones solidarios (40) que presentan una superficie de soldadura plana (42) que se complementa con una correspondiente raíz (34) del álabe y dicho reborde del disco incluye unos canales interiores (22) de vía de flujo ranurados que se extienden axialmente entre dichos álabes para deslindar dichos pasos (20) y Caracterizado por extenderse cada uno de dichos canales ranurados en círculo entre los álabes adyacentes y presentar entre ellos un contorno circularmente cóncavo.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US801119 | 2001-03-07 | ||
US09/801,119 US6478545B2 (en) | 2001-03-07 | 2001-03-07 | Fluted blisk |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2324858T3 true ES2324858T3 (es) | 2009-08-18 |
ES2324858T5 ES2324858T5 (es) | 2014-01-30 |
Family
ID=25180237
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES02251636.3T Expired - Lifetime ES2324858T5 (es) | 2001-03-07 | 2002-03-07 | Rotor ranurado con álabes integrados |
Country Status (6)
Country | Link |
---|---|
US (1) | US6478545B2 (es) |
EP (1) | EP1239116B2 (es) |
JP (1) | JP4267856B2 (es) |
KR (1) | KR100785543B1 (es) |
DE (1) | DE60232285D1 (es) |
ES (1) | ES2324858T5 (es) |
Families Citing this family (113)
Publication number | Priority date | Publication date | Assignee | Title |
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US6902096B2 (en) | 2001-10-29 | 2005-06-07 | United Technologies Corporation | Method of joining material |
US6910616B2 (en) * | 2002-03-07 | 2005-06-28 | The Boeing Company | Preforms for forming machined structural assemblies |
GB0316158D0 (en) * | 2003-07-10 | 2003-08-13 | Rolls Royce Plc | Method of making aerofoil blisks |
DE10336587A1 (de) * | 2003-08-08 | 2005-02-24 | Mtu Aero Engines Gmbh | Laufschaufel für Gasturbinenrotoren und Verfahren zur Herstellung von Gasturbinenrotoren mit integraler Beschaufelung |
FR2859933B1 (fr) * | 2003-09-19 | 2006-02-10 | Snecma Moteurs | Procede de fabrication ou de reparation d'un disque aubage monobloc |
US6969238B2 (en) * | 2003-10-21 | 2005-11-29 | General Electric Company | Tri-property rotor assembly of a turbine engine, and method for its preparation |
JP4913326B2 (ja) * | 2004-01-05 | 2012-04-11 | 株式会社Ihi | シール構造及びタービンノズル |
GB0412775D0 (en) * | 2004-06-09 | 2004-07-07 | Rolls Royce Plc | Method of replacing damaged aerofoil |
DE102004032461A1 (de) * | 2004-06-30 | 2006-02-02 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren und Reparatur-Schaufelteil zur BLISK-Reparatur oder zur Neuherstellung von BLISKs |
GB0414913D0 (en) * | 2004-07-01 | 2004-08-04 | Rolls Royce Plc | A method of welding onto thin components |
DE102004043746B4 (de) * | 2004-09-10 | 2008-09-25 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung eines mit Hohlschaufeln integral beschaufelten Gasturbinenrotors |
EP1760257B1 (en) * | 2004-09-24 | 2012-12-26 | IHI Corporation | Wall shape of axial flow machine and gas turbine engine |
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DE102005026497A1 (de) * | 2005-06-09 | 2006-12-14 | Mtu Aero Engines Gmbh | Verfahren zum Fügen von Bauteilen |
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EP1785590A1 (de) * | 2005-11-10 | 2007-05-16 | Sulzer Markets and Technology AG | Werkstück sowie Schweissverfahren zur Herstellung eines Werkstücks |
FR2903921B1 (fr) * | 2006-07-19 | 2009-06-05 | Snecma Sa | Procede de fabrication d'un disque aubage monobloc et moule pour la mise en oeuvre du procede |
GB0615671D0 (en) | 2006-08-08 | 2006-09-13 | Rolls Royce Plc | A method of friction welding |
US7758311B2 (en) * | 2006-10-12 | 2010-07-20 | General Electric Company | Part span shrouded fan blisk |
US7784182B2 (en) * | 2006-11-08 | 2010-08-31 | General Electric Company | System for manufacturing a rotor having an MMC ring component and a unitary airfoil component |
US11486311B2 (en) | 2007-08-01 | 2022-11-01 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11149650B2 (en) | 2007-08-01 | 2021-10-19 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US20150377123A1 (en) | 2007-08-01 | 2015-12-31 | United Technologies Corporation | Turbine section of high bypass turbofan |
US8844265B2 (en) | 2007-08-01 | 2014-09-30 | United Technologies Corporation | Turbine section of high bypass turbofan |
US11346289B2 (en) | 2007-08-01 | 2022-05-31 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11242805B2 (en) | 2007-08-01 | 2022-02-08 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US8356980B2 (en) * | 2007-10-09 | 2013-01-22 | Hamilton Sundstrand Corporation | Method of manufacturing a turbine rotor |
DE102007059155A1 (de) * | 2007-12-06 | 2009-06-10 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Herstellung von in Integralbauweise ausgebildeten Laufrädern für Verdichter und Turbinen |
DE102007062559A1 (de) * | 2007-12-22 | 2009-06-25 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung und Reparatur eines Bauteils und Bauteil einer Gasturbine |
DE102007062557A1 (de) * | 2007-12-22 | 2009-06-25 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen eines integral beschaufelten Rotors sowie Rotor |
US20090185908A1 (en) * | 2008-01-21 | 2009-07-23 | Honeywell International, Inc. | Linear friction welded blisk and method of fabrication |
FR2928172B1 (fr) * | 2008-02-28 | 2015-07-17 | Snecma | Aube avec plateforme non axisymetrique lineaire. |
FR2928174B1 (fr) * | 2008-02-28 | 2011-05-06 | Snecma | Aube avec plateforme non axisymetrique : creux et bosse sur extrados. |
FR2928173B1 (fr) * | 2008-02-28 | 2015-06-26 | Snecma | Aube avec plateforme 3d comportant un bulbe interaubes. |
DE102008021053A1 (de) * | 2008-04-26 | 2009-10-29 | Mtu Aero Engines Gmbh | Nachgeformter Strömungspfad einer Axialströmungsmaschine zur Verringerung von Sekundärströmung |
US8231353B2 (en) * | 2008-12-31 | 2012-07-31 | General Electric Company | Methods and apparatus relating to improved turbine blade platform contours |
DE102009011963A1 (de) * | 2009-03-05 | 2010-09-09 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung eines integral beschaufelten Rotors |
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GB8910452D0 (en) * | 1989-05-06 | 1989-06-21 | Allwood Searle & Timney | Friction welding |
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US5197190A (en) * | 1991-03-04 | 1993-03-30 | United Technologies Corporation | Fabrication of repair method for an integrally bladed rotor |
GB2271816B (en) * | 1992-10-23 | 1995-07-05 | Rolls Royce Plc | Linear friction welding of blades |
GB9309864D0 (en) * | 1993-05-13 | 1993-06-23 | Allwood Searle & Timney | Improvements relating to friction welding |
GB9309819D0 (en) * | 1993-05-13 | 1993-06-23 | Allwood Searle & Timney | Imprivements relating to friction welding |
US5397215A (en) | 1993-06-14 | 1995-03-14 | United Technologies Corporation | Flow directing assembly for the compression section of a rotary machine |
FR2716397B1 (fr) * | 1994-02-23 | 1996-04-05 | Snecma | Procédé de soudage de deux parties d'aube. |
US5755031A (en) * | 1996-11-12 | 1998-05-26 | United Technologies Corporation | Method for attaching a rotor blade to an integrally bladed rotor |
US5813593A (en) * | 1996-11-15 | 1998-09-29 | General Electric Company | Translational friction welding apparatus and method |
DE19650656C1 (de) | 1996-12-06 | 1998-06-10 | Mtu Muenchen Gmbh | Turbomaschine mit transsonischer Verdichterstufe |
US5865364A (en) * | 1996-12-24 | 1999-02-02 | United Technologies Corporation | Process for linear friction welding |
DE59806445D1 (de) * | 1997-04-01 | 2003-01-09 | Siemens Ag | Oberflächenstruktur für die wand eines strömungskanals oder einer turbinenschaufel |
GB9713395D0 (en) * | 1997-06-25 | 1997-08-27 | Rolls Royce Plc | Improvements in or relating to the friction welding of components |
US6219916B1 (en) * | 1997-12-19 | 2001-04-24 | United Technologies Corporation | Method for linear friction welding and product made by such method |
DE19807637C2 (de) * | 1998-02-23 | 2001-01-11 | Mtu Muenchen Gmbh | Reibschweißverfahren zur Beschaufelung eines Rotors für eine Strömungsmaschine |
-
2001
- 2001-03-07 US US09/801,119 patent/US6478545B2/en not_active Expired - Lifetime
-
2002
- 2002-03-06 KR KR1020020011936A patent/KR100785543B1/ko not_active IP Right Cessation
- 2002-03-06 JP JP2002059620A patent/JP4267856B2/ja not_active Expired - Fee Related
- 2002-03-07 ES ES02251636.3T patent/ES2324858T5/es not_active Expired - Lifetime
- 2002-03-07 DE DE60232285T patent/DE60232285D1/de not_active Expired - Lifetime
- 2002-03-07 EP EP02251636.3A patent/EP1239116B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1239116A3 (en) | 2004-02-11 |
JP4267856B2 (ja) | 2009-05-27 |
EP1239116B1 (en) | 2009-05-13 |
US6478545B2 (en) | 2002-11-12 |
EP1239116A2 (en) | 2002-09-11 |
ES2324858T5 (es) | 2014-01-30 |
EP1239116B2 (en) | 2013-12-04 |
DE60232285D1 (de) | 2009-06-25 |
KR20020071770A (ko) | 2002-09-13 |
KR100785543B1 (ko) | 2007-12-12 |
US20020127108A1 (en) | 2002-09-12 |
JP2002276301A (ja) | 2002-09-25 |
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