DE60229019D1 - Zerlegbarer Aufsatz für eine Gasturbinenbrennkammer - Google Patents
Zerlegbarer Aufsatz für eine GasturbinenbrennkammerInfo
- Publication number
- DE60229019D1 DE60229019D1 DE60229019T DE60229019T DE60229019D1 DE 60229019 D1 DE60229019 D1 DE 60229019D1 DE 60229019 T DE60229019 T DE 60229019T DE 60229019 T DE60229019 T DE 60229019T DE 60229019 D1 DE60229019 D1 DE 60229019D1
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- gas turbine
- turbine combustion
- demountable attachment
- demountable
- 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
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
-
- 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
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- 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
- F23R2900/00017—Assembling combustion chamber liners or subparts
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Connection Of Plates (AREA)
- Combustion Of Fluid Fuel (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/836,037 US6449952B1 (en) | 2001-04-17 | 2001-04-17 | Removable cowl for gas turbine combustor |
Publications (1)
Publication Number | Publication Date |
---|---|
DE60229019D1 true DE60229019D1 (de) | 2008-11-06 |
Family
ID=25271070
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60229019T Expired - Lifetime DE60229019D1 (de) | 2001-04-17 | 2002-04-16 | Zerlegbarer Aufsatz für eine Gasturbinenbrennkammer |
Country Status (4)
Country | Link |
---|---|
US (1) | US6449952B1 (de) |
EP (1) | EP1251312B1 (de) |
JP (1) | JP4030341B2 (de) |
DE (1) | DE60229019D1 (de) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1312865A1 (de) * | 2001-11-15 | 2003-05-21 | Siemens Aktiengesellschaft | Ringbrennkammer für eine Gasturbine |
US6681577B2 (en) * | 2002-01-16 | 2004-01-27 | General Electric Company | Method and apparatus for relieving stress in a combustion case in a gas turbine engine |
US6779268B1 (en) * | 2003-05-13 | 2004-08-24 | General Electric Company | Outer and inner cowl-wire wrap to one piece cowl conversion |
US7121095B2 (en) * | 2003-08-11 | 2006-10-17 | General Electric Company | Combustor dome assembly of a gas turbine engine having improved deflector plates |
US7093441B2 (en) * | 2003-10-09 | 2006-08-22 | United Technologies Corporation | Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume |
US7509809B2 (en) * | 2005-06-10 | 2009-03-31 | Pratt & Whitney Canada Corp. | Gas turbine engine combustor with improved cooling |
FR2891351B1 (fr) * | 2005-09-23 | 2007-12-07 | Snecma | Chambre de combustion de moteur a turbine a gaz avec carenage |
US8327538B2 (en) * | 2005-10-17 | 2012-12-11 | General Electric Company | Methods to facilitate extending gas turbine engine useful life |
US7637110B2 (en) * | 2005-11-30 | 2009-12-29 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
US7523616B2 (en) * | 2005-11-30 | 2009-04-28 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
US7493771B2 (en) * | 2005-11-30 | 2009-02-24 | General Electric Company | Methods and apparatuses for assembling a gas turbine engine |
FR2897145B1 (fr) * | 2006-02-08 | 2013-01-18 | Snecma | Chambre de combustion annulaire de turbomachine a fixations alternees. |
FR2897144B1 (fr) * | 2006-02-08 | 2008-05-02 | Snecma Sa | Chambre de combustion de turbomachine a fentes tangentielles |
US7845549B2 (en) * | 2006-05-31 | 2010-12-07 | General Electric Company | MIM braze preforms |
FR2906350B1 (fr) * | 2006-09-22 | 2009-03-20 | Snecma Sa | Chambre de combustion annulaire d'une turbomachine |
US7856826B2 (en) * | 2006-11-10 | 2010-12-28 | General Electric Company | Combustor dome mixer retaining means |
US7765809B2 (en) * | 2006-11-10 | 2010-08-03 | General Electric Company | Combustor dome and methods of assembling such |
US8863527B2 (en) * | 2009-04-30 | 2014-10-21 | Rolls-Royce Corporation | Combustor liner |
US8375548B2 (en) * | 2009-10-07 | 2013-02-19 | Pratt & Whitney Canada Corp. | Fuel nozzle and method of repair |
WO2014022344A1 (en) * | 2012-07-31 | 2014-02-06 | General Electric Company | Cmc core cowl and method of fabricating |
CN102777262B (zh) * | 2012-08-07 | 2014-08-20 | 沈阳黎明航空发动机(集团)有限责任公司 | 一种采用竖直与水平装配结合的重型燃机预装配方法 |
US9677767B2 (en) * | 2014-05-29 | 2017-06-13 | Siemens Energy, Inc. | Combustion turbine with Siamesed wall paired combustor housings |
DE102015224988A1 (de) | 2015-12-11 | 2017-06-14 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Montage einer Brennkammer eines Gasturbinentriebwerks |
DE102015224990A1 (de) | 2015-12-11 | 2017-06-14 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Montage einer Brennkammer eines Gasturbinentriebwerks |
US10378771B2 (en) | 2016-02-25 | 2019-08-13 | General Electric Company | Combustor assembly |
US10281153B2 (en) * | 2016-02-25 | 2019-05-07 | General Electric Company | Combustor assembly |
GB201613110D0 (en) * | 2016-07-29 | 2016-09-14 | Rolls Royce Plc | A combustion chamber |
GB201613299D0 (en) | 2016-08-02 | 2016-09-14 | Rolls Royce Plc | A method of assembling an annular combustion chamber assembly |
US10619856B2 (en) | 2017-03-13 | 2020-04-14 | Rolls-Royce Corporation | Notched gas turbine combustor cowl |
US10774685B2 (en) * | 2018-04-30 | 2020-09-15 | Ratheon Technologies Corporation | Gas turbine engine exhaust component |
US10801731B2 (en) * | 2018-09-13 | 2020-10-13 | United Technologies Corporation | Attachment for high temperature CMC combustor panels |
US10982852B2 (en) | 2018-11-05 | 2021-04-20 | Rolls-Royce Corporation | Cowl integration to combustor wall |
CN112302739B (zh) * | 2020-10-30 | 2023-01-17 | 中国航发沈阳发动机研究所 | 一种可在试验台架上更换的整流机匣结构 |
CN113431703B (zh) * | 2021-06-30 | 2022-07-12 | 中国航发动力股份有限公司 | 一种多层装配结构的复合装配方法 |
US11859819B2 (en) | 2021-10-15 | 2024-01-02 | General Electric Company | Ceramic composite combustor dome and liners |
JP2024007089A (ja) * | 2022-07-05 | 2024-01-18 | 三菱重工航空エンジン株式会社 | 組立方法及び組立装置 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4195476A (en) * | 1978-04-27 | 1980-04-01 | General Motors Corporation | Combustor construction |
US5181377A (en) | 1991-04-16 | 1993-01-26 | General Electric Company | Damped combustor cowl structure |
US5239832A (en) * | 1991-12-26 | 1993-08-31 | General Electric Company | Birdstrike resistant swirler support for combustion chamber dome |
US5237820A (en) | 1992-01-02 | 1993-08-24 | General Electric Company | Integral combustor cowl plate/ferrule retainer |
FR2686683B1 (fr) * | 1992-01-28 | 1994-04-01 | Snecma | Turbomachine a chambre de combustion demontable. |
CA2089272C (en) * | 1992-03-23 | 2002-09-03 | James Norman Reinhold, Jr. | Impact resistant combustor |
CA2089302C (en) | 1992-03-30 | 2004-07-06 | Joseph Frank Savelli | Double annular combustor |
US5289687A (en) | 1992-03-30 | 1994-03-01 | General Electric Company | One-piece cowl for a double annular combustor |
US5924288A (en) | 1994-12-22 | 1999-07-20 | General Electric Company | One-piece combustor cowl |
US6205789B1 (en) * | 1998-11-13 | 2001-03-27 | General Electric Company | Multi-hole film cooled combuster liner |
US6148600A (en) | 1999-02-26 | 2000-11-21 | General Electric Company | One-piece sheet metal cowl for combustor of a gas turbine engine and method of configuring same |
-
2001
- 2001-04-17 US US09/836,037 patent/US6449952B1/en not_active Expired - Lifetime
-
2002
- 2002-04-16 EP EP02252673A patent/EP1251312B1/de not_active Expired - Fee Related
- 2002-04-16 DE DE60229019T patent/DE60229019D1/de not_active Expired - Lifetime
- 2002-04-16 JP JP2002112765A patent/JP4030341B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JP4030341B2 (ja) | 2008-01-09 |
EP1251312A2 (de) | 2002-10-23 |
EP1251312B1 (de) | 2008-09-24 |
JP2002349855A (ja) | 2002-12-04 |
EP1251312A3 (de) | 2003-06-11 |
US6449952B1 (en) | 2002-09-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |