ES2040336T3 - Montaje de rotor para turbo-maquina. - Google Patents
Montaje de rotor para turbo-maquina.Info
- Publication number
- ES2040336T3 ES2040336T3 ES198888301854T ES88301854T ES2040336T3 ES 2040336 T3 ES2040336 T3 ES 2040336T3 ES 198888301854 T ES198888301854 T ES 198888301854T ES 88301854 T ES88301854 T ES 88301854T ES 2040336 T3 ES2040336 T3 ES 2040336T3
- Authority
- ES
- Spain
- Prior art keywords
- sealing plate
- turbo
- machine
- rotor assembly
- rotor disc
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Braking Arrangements (AREA)
Abstract
UN ROTOR ENSAMBLADO PARA USO EN UNA MAQUINA ROTODINAMICA COMPRENDE UN DISCO ROTOR (10) CON UNA PLURALIDAD DE HOJAS (14) UNIDAS POR SUS BORDES EXTERIORES (12) Y UNA PLACA DE SELLADO (22) PARA PREVENIR SUSTANCIALMENTE EL ESCAPE DE AIRE ENFRIADO. EL DISCO ROTOR (10) ESTA PROVISTO DE UNA PLURALIDAD DE MIEMBROS (30) DE FRENADO CADA UNO INCLUYE UNA PARTE INTERNA RADIAL DIRIGIDA HACIA EL LIMITE EXTERNO (32) EL CUAL FRENA LA PLACA DE SELLADO DEL MOVIMIENTO AXIAL Y DEL MOVIMIENTO RADIAL EXTERNO, BAJO LA FUERZA CENTRIFUGA POR PROXIMIDAD CON LA PLACA DE SELLADO. DE ESTE MODO LAS LAMINAS (14) NO SE SUJETAN POR EL PLATO DE SELLADO. FIG 1
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB878705216A GB8705216D0 (en) | 1987-03-06 | 1987-03-06 | Rotor assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2040336T3 true ES2040336T3 (es) | 1993-10-16 |
Family
ID=10613399
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES198888301854T Expired - Lifetime ES2040336T3 (es) | 1987-03-06 | 1988-03-03 | Montaje de rotor para turbo-maquina. |
Country Status (6)
Country | Link |
---|---|
US (1) | US4854821A (es) |
EP (1) | EP0286227B1 (es) |
JP (1) | JPS63230909A (es) |
DE (1) | DE3880873T2 (es) |
ES (1) | ES2040336T3 (es) |
GB (1) | GB8705216D0 (es) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4872810A (en) * | 1988-12-14 | 1989-10-10 | United Technologies Corporation | Turbine rotor retention system |
FR2666623B1 (fr) * | 1990-09-11 | 1993-05-07 | Turbomeca | Roue de turbomachine a pales rapportees. |
US5201849A (en) * | 1990-12-10 | 1993-04-13 | General Electric Company | Turbine rotor seal body |
US5275534A (en) * | 1991-10-30 | 1994-01-04 | General Electric Company | Turbine disk forward seal assembly |
US5211407A (en) * | 1992-04-30 | 1993-05-18 | General Electric Company | Compressor rotor cross shank leak seal for axial dovetails |
US5257909A (en) * | 1992-08-17 | 1993-11-02 | General Electric Company | Dovetail sealing device for axial dovetail rotor blades |
FR2695433B1 (fr) * | 1992-09-09 | 1994-10-21 | Snecma | Joint annulaire d'étanchéité disposé à une extrémité axiale d'un rotor et recouvrant des brochages d'aubes. |
US5310319A (en) * | 1993-01-12 | 1994-05-10 | United Technologies Corporation | Free standing turbine disk sideplate assembly |
FR2700807B1 (fr) * | 1993-01-27 | 1995-03-03 | Snecma | Système de rétention et d'étanchéité d'aubes engagées dans des brochages axiaux d'un disque de rotor. |
US5318405A (en) * | 1993-03-17 | 1994-06-07 | General Electric Company | Turbine disk interstage seal anti-rotation key through disk dovetail slot |
US5800124A (en) * | 1996-04-12 | 1998-09-01 | United Technologies Corporation | Cooled rotor assembly for a turbine engine |
GB2317652B (en) * | 1996-09-26 | 2000-05-17 | Rolls Royce Plc | Seal arrangement |
US5984636A (en) * | 1997-12-17 | 1999-11-16 | Pratt & Whitney Canada Inc. | Cooling arrangement for turbine rotor |
US6019580A (en) * | 1998-02-23 | 2000-02-01 | Alliedsignal Inc. | Turbine blade attachment stress reduction rings |
DE19960896A1 (de) * | 1999-12-17 | 2001-06-28 | Rolls Royce Deutschland | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
CZ20002685A3 (cs) * | 1999-12-20 | 2001-08-15 | General Electric Company | Zařízení pro uchycení lopatek otáčivého stroje a způsob jejich uchycení |
US6276896B1 (en) | 2000-07-25 | 2001-08-21 | Joseph C. Burge | Apparatus and method for cooling Axi-Centrifugal impeller |
FR2814495B1 (fr) * | 2000-09-28 | 2003-01-17 | Snecma Moteurs | Systeme de retention amont pour aubes et plates-formes de soufflante |
US6575703B2 (en) | 2001-07-20 | 2003-06-10 | General Electric Company | Turbine disk side plate |
US6951448B2 (en) * | 2002-04-16 | 2005-10-04 | United Technologies Corporation | Axial retention system and components thereof for a bladed rotor |
JP2005009382A (ja) * | 2003-06-18 | 2005-01-13 | Ishikawajima Harima Heavy Ind Co Ltd | タービンロータ、タービンディスク、及びタービン |
US7052240B2 (en) * | 2004-04-15 | 2006-05-30 | General Electric Company | Rotating seal arrangement for turbine bucket cooling circuits |
US7238008B2 (en) * | 2004-05-28 | 2007-07-03 | General Electric Company | Turbine blade retainer seal |
FR2900437B1 (fr) * | 2006-04-27 | 2008-07-25 | Snecma Sa | Systeme de retention des aubes dans un rotor |
US7870742B2 (en) * | 2006-11-10 | 2011-01-18 | General Electric Company | Interstage cooled turbine engine |
US8128371B2 (en) * | 2007-02-15 | 2012-03-06 | General Electric Company | Method and apparatus to facilitate increasing turbine rotor efficiency |
JP4991663B2 (ja) * | 2007-09-11 | 2012-08-01 | 株式会社日立製作所 | 蒸気タービン動翼組立体 |
US20090110561A1 (en) * | 2007-10-29 | 2009-04-30 | Honeywell International, Inc. | Turbine engine components, turbine engine assemblies, and methods of manufacturing turbine engine components |
US8152436B2 (en) * | 2008-01-08 | 2012-04-10 | Pratt & Whitney Canada Corp. | Blade under platform pocket cooling |
US20100117473A1 (en) * | 2008-11-12 | 2010-05-13 | Masoudipour Mike M | Robust permanent magnet rotor assembly |
EP2239419A1 (de) * | 2009-03-31 | 2010-10-13 | Siemens Aktiengesellschaft | Axialturbomaschinenrotor mit Dichtscheibe |
US8444387B2 (en) * | 2009-11-20 | 2013-05-21 | Honeywell International Inc. | Seal plates for directing airflow through a turbine section of an engine and turbine sections |
US8007230B2 (en) * | 2010-01-05 | 2011-08-30 | General Electric Company | Turbine seal plate assembly |
US8579538B2 (en) | 2010-07-30 | 2013-11-12 | United Technologies Corporation | Turbine engine coupling stack |
US8662845B2 (en) | 2011-01-11 | 2014-03-04 | United Technologies Corporation | Multi-function heat shield for a gas turbine engine |
US8740554B2 (en) | 2011-01-11 | 2014-06-03 | United Technologies Corporation | Cover plate with interstage seal for a gas turbine engine |
US8840375B2 (en) | 2011-03-21 | 2014-09-23 | United Technologies Corporation | Component lock for a gas turbine engine |
US8740573B2 (en) * | 2011-04-26 | 2014-06-03 | General Electric Company | Adaptor assembly for coupling turbine blades to rotor disks |
US9175570B2 (en) * | 2012-04-24 | 2015-11-03 | United Technologies Corporation | Airfoil including member connected by articulated joint |
WO2015038605A1 (en) | 2013-09-12 | 2015-03-19 | United Technologies Corporation | Disk outer rim seal |
FR3011031B1 (fr) * | 2013-09-25 | 2017-12-29 | Herakles | Ensemble rotatif pour turbomachine |
EP2860350A1 (de) * | 2013-10-10 | 2015-04-15 | Siemens Aktiengesellschaft | Turbinenschaufel sowie Gasturbine |
US10774666B2 (en) | 2014-01-24 | 2020-09-15 | Raytheon Technologies Corporation | Toggle seal for a rim seal |
KR101882109B1 (ko) * | 2016-12-23 | 2018-07-25 | 두산중공업 주식회사 | 가스 터빈 |
US10975714B2 (en) * | 2018-11-22 | 2021-04-13 | Pratt & Whitney Canada Corp. | Rotor assembly with blade sealing tab |
US11168615B1 (en) * | 2020-08-25 | 2021-11-09 | Raytheon Technologies Corporation | Double ring axial sealing design |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA590470A (en) * | 1960-01-12 | Rolls-Royce Limited | Bladed rotor for axial-flow fluid machines | |
GB699582A (en) * | 1950-11-14 | 1953-11-11 | Rolls Royce | Improvements in or relating to gas-turbine engines |
GB779059A (en) * | 1954-07-15 | 1957-07-17 | Rolls Royce | Improvements in or relating to axial-flow fluid machines, for example compressors orturbines of gas-turbine engines |
BE551145A (es) * | 1955-09-26 | |||
GB802476A (en) * | 1955-09-29 | 1958-10-08 | Rolls Royce | Improvements in or relating to rotors of axial-flow fluid machines for example compressors and turbines |
DE1182474B (de) * | 1961-10-25 | 1964-11-26 | Siemens Ag | Gasturbine der Scheibenbauart mit die verspannten Scheiben gegeneinander abstuetzenden Zwischenringen sowie einer Schaufelfusskuehlung durch ein gasfoermiges Medium |
NL295165A (es) * | 1962-07-11 | |||
DE1258662B (de) * | 1964-10-28 | 1968-01-11 | Goerlitzer Maschb Veb | Deckscheibe fuer die Kuehlgasfuehrung von Gasturbinenlaeufern |
US3295825A (en) * | 1965-03-10 | 1967-01-03 | Gen Motors Corp | Multi-stage turbine rotor |
US3490852A (en) * | 1967-12-21 | 1970-01-20 | Gen Electric | Gas turbine rotor bucket cooling and sealing arrangement |
US3572966A (en) * | 1969-01-17 | 1971-03-30 | Westinghouse Electric Corp | Seal plates for root cooled turbine rotor blades |
FR2324873A1 (fr) * | 1975-09-17 | 1977-04-15 | Snecma | Perfectionnements aux flasques de rotors de turbomachines |
US4017209A (en) * | 1975-12-15 | 1977-04-12 | United Technologies Corporation | Turbine rotor construction |
US4111603A (en) * | 1976-05-17 | 1978-09-05 | Westinghouse Electric Corp. | Ceramic rotor blade assembly for a gas turbine engine |
US4094615A (en) * | 1976-12-27 | 1978-06-13 | Electric Power Research Institute, Inc. | Blade attachment structure for gas turbine rotor |
FR2393931A1 (fr) * | 1977-06-08 | 1979-01-05 | Snecma | Dispositif de maintien des aubes d'un rotor |
US4192633A (en) * | 1977-12-28 | 1980-03-11 | General Electric Company | Counterweighted blade damper |
FR2419389A1 (fr) * | 1978-03-08 | 1979-10-05 | Snecma | Perfectionnements aux flasques de rotors de turbomachines |
US4344740A (en) * | 1979-09-28 | 1982-08-17 | United Technologies Corporation | Rotor assembly |
US4304523A (en) * | 1980-06-23 | 1981-12-08 | General Electric Company | Means and method for securing a member to a structure |
GB2095763A (en) * | 1980-12-29 | 1982-10-06 | Rolls Royce | Enhancing turbine blade coolant seal force |
JPS5896105A (ja) * | 1981-12-03 | 1983-06-08 | Hitachi Ltd | スペ−サ先端空気漏洩防止ロ−タ |
FR2523208A1 (fr) * | 1982-03-12 | 1983-09-16 | Snecma | Dispositif d'amortissement des vibrations d'aubes mobiles de turbine |
US4701105A (en) * | 1986-03-10 | 1987-10-20 | United Technologies Corporation | Anti-rotation feature for a turbine rotor faceplate |
-
1987
- 1987-03-06 GB GB878705216A patent/GB8705216D0/en active Pending
-
1988
- 1988-02-25 US US07/160,316 patent/US4854821A/en not_active Expired - Lifetime
- 1988-03-03 ES ES198888301854T patent/ES2040336T3/es not_active Expired - Lifetime
- 1988-03-03 EP EP88301854A patent/EP0286227B1/en not_active Expired - Lifetime
- 1988-03-03 DE DE8888301854T patent/DE3880873T2/de not_active Expired - Lifetime
- 1988-03-04 JP JP63051442A patent/JPS63230909A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
JPS63230909A (ja) | 1988-09-27 |
US4854821A (en) | 1989-08-08 |
DE3880873T2 (de) | 1993-09-02 |
EP0286227B1 (en) | 1993-05-12 |
EP0286227A2 (en) | 1988-10-12 |
DE3880873D1 (de) | 1993-06-17 |
GB8705216D0 (en) | 1987-04-08 |
EP0286227A3 (en) | 1989-09-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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