IN2015DN02789A - - Google Patents
Info
- Publication number
- IN2015DN02789A IN2015DN02789A IN2789DEN2015A IN2015DN02789A IN 2015DN02789 A IN2015DN02789 A IN 2015DN02789A IN 2789DEN2015 A IN2789DEN2015 A IN 2789DEN2015A IN 2015DN02789 A IN2015DN02789 A IN 2015DN02789A
- Authority
- IN
- India
- Prior art keywords
- adjacent
- sealing band
- seal strip
- seal
- annular gap
- 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
- F01D11/005—Sealing means between non relatively rotating elements
-
- 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
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
- F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
-
- 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
- F05D2240/00—Components
- F05D2240/55—Seals
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A sealing band for use in a turbomachine having a plurality of stages, each stage comprising a rotatable disk and blades carried thereby. At least one pair of adjacent rotatable disks define an annular gap therebetween and have respective opposing sealing band receiving slots aligned with the annular gap. The sealing band includes a plurality of seal strips located in series adjacent to one another , and adjacent seal strips include opposing end faces located in facing relationship adjacent to one another. An underlap portion is affixed adjacent to an end of at least one seal strip and extends past the end face of an adjacent seal strip , along a radially facing side of the adjacent seal strip.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/665,952 US9200519B2 (en) | 2012-11-01 | 2012-11-01 | Belly band seal with underlapping ends |
| PCT/US2013/064907 WO2014070438A1 (en) | 2012-11-01 | 2013-10-15 | Belly band seal with underlapping ends |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN2015DN02789A true IN2015DN02789A (en) | 2015-09-04 |
Family
ID=49956343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN2789DEN2015 IN2015DN02789A (en) | 2012-11-01 | 2013-10-15 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US9200519B2 (en) |
| EP (1) | EP2914814B1 (en) |
| JP (1) | JP6072930B2 (en) |
| CN (1) | CN104755701B (en) |
| IN (1) | IN2015DN02789A (en) |
| RU (1) | RU2629103C2 (en) |
| SA (1) | SA515360331B1 (en) |
| WO (1) | WO2014070438A1 (en) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9347322B2 (en) * | 2012-11-01 | 2016-05-24 | Siemens Aktiengesellschaft | Gas turbine including belly band seal anti-rotation device |
| US10208612B2 (en) * | 2013-03-08 | 2019-02-19 | Siemens Energy, Inc. | Gas turbine sealing band arrangement having an underlap seal |
| US9808889B2 (en) * | 2014-01-15 | 2017-11-07 | Siemens Energy, Inc. | Gas turbine including sealing band and anti-rotation device |
| EP2907977A1 (en) * | 2014-02-14 | 2015-08-19 | Siemens Aktiengesellschaft | Component that can be charged with hot gas for a gas turbine and sealing assembly with such a component |
| US9631507B2 (en) * | 2014-07-14 | 2017-04-25 | Siemens Energy, Inc. | Gas turbine sealing band arrangement having a locking pin |
| US9915159B2 (en) | 2014-12-18 | 2018-03-13 | General Electric Company | Ceramic matrix composite nozzle mounted with a strut and concepts thereof |
| US9845698B2 (en) * | 2015-06-24 | 2017-12-19 | Siemens Energy, Inc. | Belly band seal with anti-rotation structure |
| US10161257B2 (en) | 2015-10-20 | 2018-12-25 | General Electric Company | Turbine slotted arcuate leaf seal |
| US10215043B2 (en) | 2016-02-24 | 2019-02-26 | United Technologies Corporation | Method and device for piston seal anti-rotation |
| KR102821442B1 (en) * | 2022-11-23 | 2025-06-16 | 두산에너빌리티 주식회사 | Turbine vane platform sealing assembly, turbine vane and gas turbine comprising it |
| US12152493B2 (en) | 2022-12-09 | 2024-11-26 | Doosan Enerbility Co., Ltd. | Turbine vane having sealing assembly, turbine, and turbomachine including same |
| KR102791366B1 (en) | 2022-12-12 | 2025-04-07 | 두산에너빌리티 주식회사 | Turbine vane platform sealing assembly, turbine vane and gas turbine comprising it |
| GB2635130A (en) * | 2023-10-30 | 2025-05-07 | Siemens Energy Global Gmbh & Co Kg | Seal assembly for gas turbine engine |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5260506U (en) * | 1975-10-31 | 1977-05-02 | ||
| US5320488A (en) | 1993-01-21 | 1994-06-14 | General Electric Company | Turbine disk interstage seal anti-rotation system |
| US5456576A (en) * | 1994-08-31 | 1995-10-10 | United Technologies Corporation | Dynamic control of tip clearance |
| JP2941698B2 (en) | 1995-11-10 | 1999-08-25 | 三菱重工業株式会社 | Gas turbine rotor |
| US5882012A (en) * | 1995-11-30 | 1999-03-16 | Ntn Corporation | Oil seal ring |
| JPH10103013A (en) * | 1996-09-30 | 1998-04-21 | Toshiba Corp | Gas turbine shroud structure |
| DE69820207T2 (en) | 1997-06-11 | 2004-10-21 | Mitsubishi Heavy Ind Ltd | ROTOR FOR GAS TURBINES |
| JP3477347B2 (en) | 1997-07-30 | 2003-12-10 | 三菱重工業株式会社 | Gas turbine interstage seal device |
| JP3643692B2 (en) | 1998-03-02 | 2005-04-27 | 三菱重工業株式会社 | Rotating machine sealing device |
| FR2829796B1 (en) * | 2001-09-20 | 2003-12-12 | Snecma Moteurs | DEVICE FOR HOLDING JOINTS OF PLATFORMS OF DISTRIBUTOR SECTORS OF TURBOMACHINE WITH SEALING BLADES |
| JP4822716B2 (en) | 2005-02-07 | 2011-11-24 | 三菱重工業株式会社 | Gas turbine with seal structure |
| US7470113B2 (en) | 2006-06-22 | 2008-12-30 | United Technologies Corporation | Split knife edge seals |
| JP2008031870A (en) * | 2006-07-26 | 2008-02-14 | Mitsubishi Heavy Ind Ltd | Seal structure of gas turbine |
| US7581931B2 (en) | 2006-10-13 | 2009-09-01 | Siemens Energy, Inc. | Gas turbine belly band seal anti-rotation structure |
| US20090191050A1 (en) | 2008-01-24 | 2009-07-30 | Siemens Power Generation, Inc. | Sealing band having bendable tang with anti-rotation in a turbine and associated methods |
| US8376697B2 (en) | 2008-09-25 | 2013-02-19 | Siemens Energy, Inc. | Gas turbine sealing apparatus |
| US8511982B2 (en) * | 2008-11-24 | 2013-08-20 | Alstom Technology Ltd. | Compressor vane diaphragm |
| KR101105402B1 (en) | 2009-09-30 | 2012-01-17 | 한국전력공사 | Gas turbine disc sealing band using weld bead method |
| US8348280B2 (en) * | 2010-10-22 | 2013-01-08 | General Electric Company | Seal apparatus |
| GB201109143D0 (en) * | 2011-06-01 | 2011-07-13 | Rolls Royce Plc | Flap seal spring and sealing apparatus |
| US9017015B2 (en) * | 2011-10-27 | 2015-04-28 | General Electric Company | Turbomachine including an inner-to-outer turbine casing seal assembly and method |
-
2012
- 2012-11-01 US US13/665,952 patent/US9200519B2/en active Active
-
2013
- 2013-10-15 JP JP2015539654A patent/JP6072930B2/en active Active
- 2013-10-15 WO PCT/US2013/064907 patent/WO2014070438A1/en active Application Filing
- 2013-10-15 EP EP13821224.6A patent/EP2914814B1/en active Active
- 2013-10-15 IN IN2789DEN2015 patent/IN2015DN02789A/en unknown
- 2013-10-15 RU RU2015115973A patent/RU2629103C2/en active
- 2013-10-15 CN CN201380056472.2A patent/CN104755701B/en active Active
-
2015
- 2015-04-23 SA SA515360331A patent/SA515360331B1/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| RU2015115973A (en) | 2016-12-20 |
| JP2015533995A (en) | 2015-11-26 |
| WO2014070438A1 (en) | 2014-05-08 |
| EP2914814A1 (en) | 2015-09-09 |
| RU2629103C2 (en) | 2017-08-24 |
| US9200519B2 (en) | 2015-12-01 |
| CN104755701B (en) | 2016-11-16 |
| SA515360331B1 (en) | 2017-03-20 |
| JP6072930B2 (en) | 2017-02-01 |
| US20140119899A1 (en) | 2014-05-01 |
| CN104755701A (en) | 2015-07-01 |
| EP2914814B1 (en) | 2016-12-28 |
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