ES2032178A6 - Alabe de montaje libre para utilizacion en turbinas de vapor de baja presion. - Google Patents
Alabe de montaje libre para utilizacion en turbinas de vapor de baja presion.Info
- Publication number
- ES2032178A6 ES2032178A6 ES9100456A ES9100456A ES2032178A6 ES 2032178 A6 ES2032178 A6 ES 2032178A6 ES 9100456 A ES9100456 A ES 9100456A ES 9100456 A ES9100456 A ES 9100456A ES 2032178 A6 ES2032178 A6 ES 2032178A6
- Authority
- ES
- Spain
- Prior art keywords
- low pressure
- pressure steam
- steam turbines
- free assembly
- alabe
- 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 - Fee Related
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
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
ALABE DE MONTAJE LIBRE PARA UTILIZACION EN UNA TURBINA DE BAJA PRESION. SE HA DISEÑADO UN ALABE DE TURBINA PARA EVITAR TENER QUE MECANIZAR UNA PARTE DEL ULTIMO ALABE ENSAMBLADO EN UNA FILA PARA LOGRAR SU AJUSTE. LA SITUACION DEL CENTRO DE GIRO DE LA RAIZ FUE ELEGIDA CUIDADOSAMENTE PARA QUE ESTUVIERA EN LA PROXIMIDAD VERTICAL AL BORDE DE ATAQUE DE LA PLATAFORMA.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/484,760 US5017091A (en) | 1990-02-26 | 1990-02-26 | Free standing blade for use in low pressure steam turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2032178A6 true ES2032178A6 (es) | 1993-01-01 |
Family
ID=23925495
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES9100456A Expired - Fee Related ES2032178A6 (es) | 1990-02-26 | 1991-02-22 | Alabe de montaje libre para utilizacion en turbinas de vapor de baja presion. |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5017091A (es) |
| JP (1) | JPH04219403A (es) |
| KR (1) | KR0152444B1 (es) |
| CN (1) | CN1026019C (es) |
| CA (1) | CA2037001A1 (es) |
| ES (1) | ES2032178A6 (es) |
| IT (1) | IT1245142B (es) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5160242A (en) * | 1991-05-31 | 1992-11-03 | Westinghouse Electric Corp. | Freestanding mixed tuned steam turbine blade |
| US5474419A (en) * | 1992-12-30 | 1995-12-12 | Reluzco; George | Flowpath assembly for a turbine diaphragm and methods of manufacture |
| US5586864A (en) * | 1994-07-27 | 1996-12-24 | General Electric Company | Turbine nozzle diaphragm and method of assembly |
| US6419464B1 (en) * | 2001-01-16 | 2002-07-16 | Honeywell International Inc. | Vane for variable nozzle turbocharger |
| FR2856728B1 (fr) * | 2003-06-27 | 2005-10-28 | Snecma Moteurs | Aube de compresseur de turboreacteur |
| US7300253B2 (en) * | 2005-07-25 | 2007-11-27 | Siemens Aktiengesellschaft | Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring |
| US8459956B2 (en) * | 2008-12-24 | 2013-06-11 | General Electric Company | Curved platform turbine blade |
| US20100166562A1 (en) * | 2008-12-30 | 2010-07-01 | General Electric Company | Turbine blade root configurations |
| US20100166561A1 (en) * | 2008-12-30 | 2010-07-01 | General Electric Company | Turbine blade root configurations |
| US8439643B2 (en) * | 2009-08-20 | 2013-05-14 | General Electric Company | Biformal platform turbine blade |
| US8967973B2 (en) * | 2011-10-26 | 2015-03-03 | General Electric Company | Turbine bucket platform shaping for gas temperature control and related method |
| US9033669B2 (en) * | 2012-06-15 | 2015-05-19 | General Electric Company | Rotating airfoil component with platform having a recessed surface region therein |
| US20140023517A1 (en) * | 2012-07-23 | 2014-01-23 | General Electric Company | Nozzle for turbine system |
| 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 |
| US9670781B2 (en) * | 2013-09-17 | 2017-06-06 | Honeywell International Inc. | Gas turbine engines with turbine rotor blades having improved platform edges |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1793468A (en) * | 1929-05-28 | 1931-02-24 | Westinghouse Electric & Mfg Co | Turbine blade |
| US1719415A (en) * | 1927-09-14 | 1929-07-02 | Westinghouse Electric & Mfg Co | Turbine-blade attachment |
| DE1049872B (es) * | 1953-06-04 | 1954-02-05 | ||
| US3986793A (en) * | 1974-10-29 | 1976-10-19 | Westinghouse Electric Corporation | Turbine rotating blade |
| US4621979A (en) * | 1979-11-30 | 1986-11-11 | United Technologies Corporation | Fan rotor blades of turbofan engines |
| US4585395A (en) * | 1983-12-12 | 1986-04-29 | General Electric Company | Gas turbine engine blade |
| US4767275A (en) * | 1986-07-11 | 1988-08-30 | Westinghouse Electric Corp. | Locking pin system for turbine curved root side entry closing blades |
-
1990
- 1990-02-26 US US07/484,760 patent/US5017091A/en not_active Expired - Fee Related
-
1991
- 1991-02-07 IT ITMI910317A patent/IT1245142B/it active IP Right Grant
- 1991-02-22 ES ES9100456A patent/ES2032178A6/es not_active Expired - Fee Related
- 1991-02-25 KR KR1019910003034A patent/KR0152444B1/ko not_active Expired - Fee Related
- 1991-02-25 CA CA002037001A patent/CA2037001A1/en not_active Abandoned
- 1991-02-26 JP JP3054060A patent/JPH04219403A/ja active Pending
- 1991-02-26 CN CN91101186A patent/CN1026019C/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US5017091A (en) | 1991-05-21 |
| ITMI910317A1 (it) | 1992-08-07 |
| CA2037001A1 (en) | 1991-08-27 |
| KR0152444B1 (ko) | 1998-11-02 |
| JPH04219403A (ja) | 1992-08-10 |
| KR910021518A (ko) | 1991-12-20 |
| IT1245142B (it) | 1994-09-13 |
| ITMI910317A0 (it) | 1991-02-07 |
| CN1026019C (zh) | 1994-09-28 |
| CN1054289A (zh) | 1991-09-04 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FD1A | Patent lapsed |
Effective date: 20040916 |