RU2012122108A - Сопловой аппарат турбины, турбинная лопатка и турбина - Google Patents
Сопловой аппарат турбины, турбинная лопатка и турбина Download PDFInfo
- Publication number
- RU2012122108A RU2012122108A RU2012122108/06A RU2012122108A RU2012122108A RU 2012122108 A RU2012122108 A RU 2012122108A RU 2012122108/06 A RU2012122108/06 A RU 2012122108/06A RU 2012122108 A RU2012122108 A RU 2012122108A RU 2012122108 A RU2012122108 A RU 2012122108A
- Authority
- RU
- Russia
- Prior art keywords
- axial tooth
- nozzle apparatus
- axial
- turbine
- essentially
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/118,686 US20120308360A1 (en) | 2011-05-31 | 2011-05-31 | Overlap seal for turbine nozzle assembly |
US13/118,686 | 2011-05-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
RU2012122108A true RU2012122108A (ru) | 2013-12-10 |
Family
ID=47173518
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2012122108/06A RU2012122108A (ru) | 2011-05-31 | 2012-05-30 | Сопловой аппарат турбины, турбинная лопатка и турбина |
Country Status (4)
Country | Link |
---|---|
US (1) | US20120308360A1 (de) |
DE (1) | DE102012104620A1 (de) |
FR (1) | FR2976019A1 (de) |
RU (1) | RU2012122108A (de) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108431369B (zh) * | 2015-12-24 | 2020-08-14 | 三菱日立电力系统株式会社 | 蒸汽涡轮 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1819864A (en) * | 1930-03-24 | 1931-08-18 | Gen Electric | Elastic fluid turbine |
US2552239A (en) * | 1946-10-29 | 1951-05-08 | Gen Electric | Turbine rotor cooling arrangement |
US4882902A (en) * | 1986-04-30 | 1989-11-28 | General Electric Company | Turbine cooling air transferring apparatus |
US6506016B1 (en) * | 2001-11-15 | 2003-01-14 | General Electric Company | Angel wing seals for blades of a gas turbine and methods for determining angel wing seal profiles |
US7488153B2 (en) * | 2002-07-01 | 2009-02-10 | Alstom Technology Ltd. | Steam turbine |
FR2851010B1 (fr) * | 2003-02-06 | 2005-04-15 | Snecma Moteurs | Dispositif de ventilation d'un rotor de turbine a haute pression d'une turbomachine |
GB0319002D0 (en) * | 2003-05-13 | 2003-09-17 | Alstom Switzerland Ltd | Improvements in or relating to steam turbines |
US7465152B2 (en) * | 2005-09-16 | 2008-12-16 | General Electric Company | Angel wing seals for turbine blades and methods for selecting stator, rotor and wing seal profiles |
US8262342B2 (en) * | 2008-07-10 | 2012-09-11 | Honeywell International Inc. | Gas turbine engine assemblies with recirculated hot gas ingestion |
-
2011
- 2011-05-31 US US13/118,686 patent/US20120308360A1/en not_active Abandoned
-
2012
- 2012-05-24 FR FR1254744A patent/FR2976019A1/fr not_active Withdrawn
- 2012-05-29 DE DE102012104620A patent/DE102012104620A1/de not_active Withdrawn
- 2012-05-30 RU RU2012122108/06A patent/RU2012122108A/ru not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
US20120308360A1 (en) | 2012-12-06 |
DE102012104620A1 (de) | 2012-12-06 |
FR2976019A1 (fr) | 2012-12-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FA93 | Acknowledgement of application withdrawn (no request for examination) |
Effective date: 20150601 |