IN2014DN03773A - - Google Patents
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- Publication number
- IN2014DN03773A IN2014DN03773A IN3773DEN2014A IN2014DN03773A IN 2014DN03773 A IN2014DN03773 A IN 2014DN03773A IN 3773DEN2014 A IN3773DEN2014 A IN 3773DEN2014A IN 2014DN03773 A IN2014DN03773 A IN 2014DN03773A
- Authority
- IN
- India
- Prior art keywords
- combustion chamber
- turbine
- contour
- conical contour
- thermal expansion
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00012—Details of sealing devices
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP11186387 | 2011-10-24 | ||
| PCT/EP2012/070930 WO2013060663A2 (fr) | 2011-10-24 | 2012-10-23 | Turbine à gaz |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN2014DN03773A true IN2014DN03773A (fr) | 2015-07-10 |
Family
ID=47045047
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN3773DEN2014 IN2014DN03773A (fr) | 2011-10-24 | 2012-10-23 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US9708920B2 (fr) |
| EP (1) | EP2852735B1 (fr) |
| KR (1) | KR101613096B1 (fr) |
| CN (1) | CN104246373B (fr) |
| IN (1) | IN2014DN03773A (fr) |
| RU (1) | RU2597350C2 (fr) |
| WO (1) | WO2013060663A2 (fr) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2637944T3 (es) * | 2014-06-06 | 2017-10-18 | MTU Aero Engines AG | Disposición de los componentes de una turbina de gas |
| EP2998517B1 (fr) * | 2014-09-16 | 2019-03-27 | Ansaldo Energia Switzerland AG | Agencement d'étanchéité au niveau de l'interface entre une chambre de combustion et une turbine d'une turbine à gaz et turbine à gaz avec un tel agencement d'étanchéité |
| EP3287610B1 (fr) * | 2016-08-22 | 2019-07-10 | Ansaldo Energia Switzerland AG | Conduit de transition de turbine à gaz |
| US10697634B2 (en) | 2018-03-07 | 2020-06-30 | General Electric Company | Inner cooling shroud for transition zone of annular combustor liner |
| US12094625B2 (en) * | 2019-09-24 | 2024-09-17 | Ls Electric Co., Ltd. | Cooling apparatus for superconductor cooling container |
| EP3835657A1 (fr) * | 2019-12-10 | 2021-06-16 | Siemens Aktiengesellschaft | Chambre de combustion avec refroidissement de parois |
| CN112377946B (zh) * | 2020-11-16 | 2022-02-11 | 四川航天中天动力装备有限责任公司 | 一种轴向浮动式回流环形燃烧室大弯管结构 |
| CN114542292B (zh) * | 2022-02-22 | 2024-07-02 | 中国联合重型燃气轮机技术有限公司 | 一种缸体支撑装置 |
Family Cites Families (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2592060A (en) * | 1946-03-25 | 1952-04-08 | Rolls Royce | Mounting of combustion chambers in jet-propulsion and gas-turbine power-units |
| GB638807A (en) * | 1948-07-12 | 1950-06-14 | Havilland Engine Co Ltd | Improvements in or relating to gas turbines |
| GB1010338A (en) * | 1962-09-11 | 1965-11-17 | Lucas Industries Ltd | Means for supporting the downstream end of a combustion chamber in a gas turbine engine |
| DE1186275B (de) * | 1963-07-04 | 1965-01-28 | Daimler Benz Ag | Anordnung der Flammkammer von Ringbrennkammern fuer Gasturbinentriebwerke |
| US3481146A (en) * | 1967-12-28 | 1969-12-02 | Lucas Industries Ltd | Combustion apparatus for gas turbine engines |
| US3670467A (en) | 1970-04-27 | 1972-06-20 | Robert H Walker | Method and apparatus for manufacturing tumbling media |
| US3670497A (en) * | 1970-09-02 | 1972-06-20 | United Aircraft Corp | Combustion chamber support |
| US3928963A (en) * | 1974-11-04 | 1975-12-30 | Gen Motors Corp | Cast in place gas turbine containment ring and method of manufacture |
| GB2102897B (en) * | 1981-07-27 | 1985-06-19 | Gen Electric | Annular seals |
| US4821522A (en) * | 1987-07-02 | 1989-04-18 | United Technologies Corporation | Sealing and cooling arrangement for combustor vane interface |
| FR2624953B1 (fr) * | 1987-12-16 | 1990-04-20 | Snecma | Chambre de combustion, pour turbomachines, possedant un convergent a doubles parois |
| US5271714A (en) * | 1992-07-09 | 1993-12-21 | General Electric Company | Turbine nozzle support arrangement |
| US5265412A (en) * | 1992-07-28 | 1993-11-30 | General Electric Company | Self-accommodating brush seal for gas turbine combustor |
| GB2328011A (en) * | 1997-08-05 | 1999-02-10 | Europ Gas Turbines Ltd | Combustor for gas or liquid fuelled turbine |
| US6098397A (en) * | 1998-06-08 | 2000-08-08 | Caterpillar Inc. | Combustor for a low-emissions gas turbine engine |
| JP2003527973A (ja) * | 2000-03-22 | 2003-09-24 | シーメンス アクチエンゲゼルシヤフト | シール手段の除去方法 |
| US6334310B1 (en) * | 2000-06-02 | 2002-01-01 | General Electric Company | Fracture resistant support structure for a hula seal in a turbine combustor and related method |
| IT1317978B1 (it) | 2000-06-16 | 2003-07-21 | Nuovo Pignone Spa | Transition piece per camere di combustione di turbine a gas nonanulari. |
| SE520594C2 (sv) * | 2000-09-29 | 2003-07-29 | Turbec Ab | Brännkammare för en värmemotorenhet |
| US6442946B1 (en) * | 2000-11-14 | 2002-09-03 | Power Systems Mfg., Llc | Three degrees of freedom aft mounting system for gas turbine transition duct |
| US6450762B1 (en) * | 2001-01-31 | 2002-09-17 | General Electric Company | Integral aft seal for turbine applications |
| US6860108B2 (en) * | 2003-01-22 | 2005-03-01 | Mitsubishi Heavy Industries, Ltd. | Gas turbine tail tube seal and gas turbine using the same |
| US7152411B2 (en) * | 2003-06-27 | 2006-12-26 | General Electric Company | Rabbet mounted combuster |
| US7178340B2 (en) * | 2003-09-24 | 2007-02-20 | Power Systems Mfg., Llc | Transition duct honeycomb seal |
| US6997673B2 (en) * | 2003-12-11 | 2006-02-14 | Honeywell International, Inc. | Gas turbine high temperature turbine blade outer air seal assembly |
| FR2871847B1 (fr) * | 2004-06-17 | 2006-09-29 | Snecma Moteurs Sa | Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz |
| WO2006059979A1 (fr) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Carter intégral, aube fixe, bâti et mélangeur d'un moteur à turbine en bout |
| US7082766B1 (en) * | 2005-03-02 | 2006-08-01 | General Electric Company | One-piece can combustor |
| US7726114B2 (en) * | 2005-12-07 | 2010-06-01 | General Electric Company | Integrated combustor-heat exchanger and systems for power generation using the same |
| US7604456B2 (en) * | 2006-04-11 | 2009-10-20 | Siemens Energy, Inc. | Vane shroud through-flow platform cover |
| US7762766B2 (en) * | 2006-07-06 | 2010-07-27 | Siemens Energy, Inc. | Cantilevered framework support for turbine vane |
| EP2242955B1 (fr) * | 2008-02-20 | 2018-10-17 | General Electric Technology GmbH | Turbine à gaz à chambre de combustion annulaire et procédé d'assemblage |
| WO2009103632A1 (fr) * | 2008-02-20 | 2009-08-27 | Alstom Technology Ltd | Turbine à gaz |
| US9080464B2 (en) * | 2008-02-27 | 2015-07-14 | Mitsubishi Hitachi Power Systems, Ltd. | Gas turbine and method of opening chamber of gas turbine |
| US8534076B2 (en) * | 2009-06-09 | 2013-09-17 | Honeywell Internationl Inc. | Combustor-turbine seal interface for gas turbine engine |
| US8347636B2 (en) * | 2010-09-24 | 2013-01-08 | General Electric Company | Turbomachine including a ceramic matrix composite (CMC) bridge |
| US20150167979A1 (en) * | 2013-12-17 | 2015-06-18 | General Electric Company | First stage nozzle or transition nozzle configured to promote mixing of respective combustion streams downstream thereof before entry into a first stage bucket of a turbine |
| US10309652B2 (en) * | 2014-04-14 | 2019-06-04 | Siemens Energy, Inc. | Gas turbine engine combustor basket with inverted platefins |
-
2012
- 2012-10-23 IN IN3773DEN2014 patent/IN2014DN03773A/en unknown
- 2012-10-23 RU RU2014120759/06A patent/RU2597350C2/ru active
- 2012-10-23 CN CN201280052419.0A patent/CN104246373B/zh active Active
- 2012-10-23 KR KR1020147013476A patent/KR101613096B1/ko active IP Right Grant
- 2012-10-23 EP EP12775033.9A patent/EP2852735B1/fr active Active
- 2012-10-23 WO PCT/EP2012/070930 patent/WO2013060663A2/fr active Application Filing
-
2014
- 2014-04-17 US US14/254,985 patent/US9708920B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2597350C2 (ru) | 2016-09-10 |
| WO2013060663A3 (fr) | 2015-02-26 |
| RU2014120759A (ru) | 2015-12-10 |
| US20140223921A1 (en) | 2014-08-14 |
| KR20140077978A (ko) | 2014-06-24 |
| CN104246373A (zh) | 2014-12-24 |
| CN104246373B (zh) | 2016-06-08 |
| US9708920B2 (en) | 2017-07-18 |
| EP2852735B1 (fr) | 2016-04-27 |
| KR101613096B1 (ko) | 2016-04-20 |
| WO2013060663A2 (fr) | 2013-05-02 |
| EP2852735A2 (fr) | 2015-04-01 |
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