FR2887015B1 - Assemblage d'une chambre de combustion annulaire de turbomachine - Google Patents
Assemblage d'une chambre de combustion annulaire de turbomachineInfo
- Publication number
- FR2887015B1 FR2887015B1 FR0505999A FR0505999A FR2887015B1 FR 2887015 B1 FR2887015 B1 FR 2887015B1 FR 0505999 A FR0505999 A FR 0505999A FR 0505999 A FR0505999 A FR 0505999A FR 2887015 B1 FR2887015 B1 FR 2887015B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- assembly
- combustion chamber
- annular combustion
- annular
- 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.)
- Active
Links
- 238000002485 combustion reaction Methods 0.000 title 1
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
- 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
- F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Connection Of Plates (AREA)
- Portable Nailing Machines And Staplers (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0505999A FR2887015B1 (fr) | 2005-06-14 | 2005-06-14 | Assemblage d'une chambre de combustion annulaire de turbomachine |
EP06114424.2A EP1734305B1 (fr) | 2005-06-14 | 2006-05-23 | Assemblage d'une chambre de combustion annulaire de turbomachine |
US11/447,109 US7849696B2 (en) | 2005-06-14 | 2006-06-06 | Assembling an annular combustion chamber of a turbomachine |
JP2006160646A JP2006349336A (ja) | 2005-06-14 | 2006-06-09 | ターボ機械の環状の燃焼チャンバの組み立て |
CA2548905A CA2548905C (fr) | 2005-06-14 | 2006-06-12 | Assemblage d'une chambre de combustion annulaire de turbomachine |
RU2006120529/06A RU2400674C2 (ru) | 2005-06-14 | 2006-06-13 | Сборка кольцевой камеры сгорания турбомашины |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0505999A FR2887015B1 (fr) | 2005-06-14 | 2005-06-14 | Assemblage d'une chambre de combustion annulaire de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2887015A1 FR2887015A1 (fr) | 2006-12-15 |
FR2887015B1 true FR2887015B1 (fr) | 2010-09-24 |
Family
ID=34955491
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0505999A Active FR2887015B1 (fr) | 2005-06-14 | 2005-06-14 | Assemblage d'une chambre de combustion annulaire de turbomachine |
Country Status (6)
Country | Link |
---|---|
US (1) | US7849696B2 (fr) |
EP (1) | EP1734305B1 (fr) |
JP (1) | JP2006349336A (fr) |
CA (1) | CA2548905C (fr) |
FR (1) | FR2887015B1 (fr) |
RU (1) | RU2400674C2 (fr) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7874059B2 (en) * | 2006-01-12 | 2011-01-25 | Siemens Energy, Inc. | Attachment for ceramic matrix composite component |
FR2911668B1 (fr) * | 2007-01-18 | 2009-03-20 | Snecma Sa | Chambre de combustion d'une turbomachine |
GB2453946B (en) * | 2007-10-23 | 2010-07-14 | Rolls Royce Plc | A Wall Element for use in Combustion Apparatus |
GB0800294D0 (en) * | 2008-01-09 | 2008-02-20 | Rolls Royce Plc | Gas heater |
GB0801839D0 (en) * | 2008-02-01 | 2008-03-05 | Rolls Royce Plc | combustion apparatus |
GB2457281B (en) * | 2008-02-11 | 2010-09-08 | Rolls Royce Plc | A Combustor Wall Arrangement with Parts Joined by Mechanical Fasteners |
GB2460634B (en) * | 2008-06-02 | 2010-07-07 | Rolls Royce Plc | Combustion apparatus |
FR2935753B1 (fr) * | 2008-09-08 | 2011-07-01 | Snecma Propulsion Solide | Liaisons souples a butee pour fixation de piece en cmc |
GB0920371D0 (en) * | 2009-11-23 | 2010-01-06 | Rolls Royce Plc | Combustor system |
US8607577B2 (en) * | 2009-11-24 | 2013-12-17 | United Technologies Corporation | Attaching ceramic matrix composite to high temperature gas turbine structure |
US9322334B2 (en) * | 2012-10-23 | 2016-04-26 | General Electric Company | Deformable mounting assembly |
FR2998038B1 (fr) | 2012-11-09 | 2017-12-08 | Snecma | Chambre de combustion pour une turbomachine |
US10422532B2 (en) * | 2013-08-01 | 2019-09-24 | United Technologies Corporation | Attachment scheme for a ceramic bulkhead panel |
US10012104B2 (en) | 2014-10-14 | 2018-07-03 | United Technologies Corporation | Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle |
US10480321B2 (en) | 2014-12-05 | 2019-11-19 | Rolls-Royce Corporation | Attachment of piloting feature |
US9976746B2 (en) | 2015-09-02 | 2018-05-22 | General Electric Company | Combustor assembly for a turbine engine |
US11149646B2 (en) | 2015-09-02 | 2021-10-19 | General Electric Company | Piston ring assembly for a turbine engine |
US10168051B2 (en) | 2015-09-02 | 2019-01-01 | General Electric Company | Combustor assembly for a turbine engine |
US10197278B2 (en) | 2015-09-02 | 2019-02-05 | General Electric Company | Combustor assembly for a turbine engine |
US10281153B2 (en) * | 2016-02-25 | 2019-05-07 | General Electric Company | Combustor assembly |
US9951649B2 (en) | 2016-04-26 | 2018-04-24 | Pratt & Whitney Canada Corp. | Fuel flow divider valve mounting arrangement for a gas turbine engine |
US10935242B2 (en) | 2016-07-07 | 2021-03-02 | General Electric Company | Combustor assembly for a turbine engine |
US10280959B2 (en) | 2016-07-13 | 2019-05-07 | Rohr, Inc. | Sliding fastener systems to accommodate differential thermal growth |
GB201613110D0 (en) | 2016-07-29 | 2016-09-14 | Rolls Royce Plc | A combustion chamber |
US20180051880A1 (en) * | 2016-08-18 | 2018-02-22 | General Electric Company | Combustor assembly for a turbine engine |
US10385709B2 (en) * | 2017-02-23 | 2019-08-20 | General Electric Company | Methods and features for positioning a flow path assembly within a gas turbine engine |
US11402097B2 (en) | 2018-01-03 | 2022-08-02 | General Electric Company | Combustor assembly for a turbine engine |
US11054136B2 (en) * | 2018-11-30 | 2021-07-06 | Pratt & Whitney Canada Corp. | Interface for double-skin combustor liner |
US11378012B2 (en) * | 2019-12-12 | 2022-07-05 | Rolls-Royce Plc | Insert-mounted turbine assembly for a gas turbine engine |
US11525577B2 (en) * | 2020-04-27 | 2022-12-13 | Raytheon Technologies Corporation | Extended bulkhead panel |
EP3929487A1 (fr) * | 2020-06-25 | 2021-12-29 | General Electric Company | Ensemble chambre de combustion pour moteur de turbine à gaz |
CN113931872B (zh) * | 2021-12-15 | 2022-03-18 | 成都中科翼能科技有限公司 | 一种燃气轮机压气机的双层鼓筒加强型转子结构 |
CN116697399A (zh) * | 2022-02-28 | 2023-09-05 | 通用电气公司 | 具有柔性连接的燃烧器圆顶-导流板和衬里 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2825786B1 (fr) * | 2001-06-06 | 2003-10-17 | Snecma Moteurs | Fixation de casquettes metalliques sur des parois de chambre de combustion cmc de turbomachine |
FR2825779B1 (fr) * | 2001-06-06 | 2003-08-29 | Snecma Moteurs | Chambre de combustion munie d'un systeme de fixation de fond de chambre |
US6904757B2 (en) * | 2002-12-20 | 2005-06-14 | General Electric Company | Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor |
FR2855249B1 (fr) * | 2003-05-20 | 2005-07-08 | Snecma Moteurs | Chambre de combustion ayant une liaison souple entre un fond de chambre et une paroi de chambre |
-
2005
- 2005-06-14 FR FR0505999A patent/FR2887015B1/fr active Active
-
2006
- 2006-05-23 EP EP06114424.2A patent/EP1734305B1/fr active Active
- 2006-06-06 US US11/447,109 patent/US7849696B2/en active Active
- 2006-06-09 JP JP2006160646A patent/JP2006349336A/ja not_active Withdrawn
- 2006-06-12 CA CA2548905A patent/CA2548905C/fr active Active
- 2006-06-13 RU RU2006120529/06A patent/RU2400674C2/ru active
Also Published As
Publication number | Publication date |
---|---|
EP1734305B1 (fr) | 2014-07-02 |
US7849696B2 (en) | 2010-12-14 |
CA2548905C (fr) | 2013-09-17 |
FR2887015A1 (fr) | 2006-12-15 |
US20070107710A1 (en) | 2007-05-17 |
EP1734305A2 (fr) | 2006-12-20 |
RU2400674C2 (ru) | 2010-09-27 |
JP2006349336A (ja) | 2006-12-28 |
RU2006120529A (ru) | 2007-12-20 |
EP1734305A3 (fr) | 2013-05-01 |
CA2548905A1 (fr) | 2006-12-14 |
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Legal Events
Date | Code | Title | Description |
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CD | Change of name or company name | ||
CL | Concession to grant licences | ||
PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |
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PLFP | Fee payment |
Year of fee payment: 19 |
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PLFP | Fee payment |
Year of fee payment: 20 |