CA2838168C - Chambre de combustion annulaire de turbomachine - Google Patents
Chambre de combustion annulaire de turbomachine Download PDFInfo
- Publication number
- CA2838168C CA2838168C CA2838168A CA2838168A CA2838168C CA 2838168 C CA2838168 C CA 2838168C CA 2838168 A CA2838168 A CA 2838168A CA 2838168 A CA2838168 A CA 2838168A CA 2838168 C CA2838168 C CA 2838168C
- Authority
- CA
- Canada
- Prior art keywords
- combustion chamber
- turbomachine
- annular wall
- 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
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
-
- 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
- F23R2900/00017—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/70—Interfitted members
- Y10T403/7005—Lugged member, rotary engagement
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
Abstract
Chambre de combustion annulaire (10) de turbomachine présentant une direction axiale (X), une direction radiale (R) et une direction azimutale (Y), comprenant une première paroi annulaire (12) et une deuxième paroi annulaire (14), chaque paroi annulaire délimitant au moins une partie de l'enceinte de la chambre de combustion (10). La première paroi annulaire (12) et la deuxième paroi annulaire ( 14) présentent des moyens complémentaires d'assemblage (12b, 14b) qui coopèrent par emboîtement azimutal.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1154984A FR2976346B1 (fr) | 2011-06-08 | 2011-06-08 | Chambre de combustion annulaire de turbomachine |
FR1154984 | 2011-06-08 | ||
PCT/FR2012/051240 WO2012168636A2 (fr) | 2011-06-08 | 2012-06-04 | Chambre de combustion annulaire de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2838168A1 CA2838168A1 (fr) | 2012-12-13 |
CA2838168C true CA2838168C (fr) | 2018-10-23 |
Family
ID=46420420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2838168A Active CA2838168C (fr) | 2011-06-08 | 2012-06-04 | Chambre de combustion annulaire de turbomachine |
Country Status (11)
Country | Link |
---|---|
US (1) | US8925331B2 (fr) |
EP (1) | EP2718627B1 (fr) |
JP (1) | JP6073299B2 (fr) |
KR (1) | KR102001690B1 (fr) |
CN (1) | CN103597285B (fr) |
CA (1) | CA2838168C (fr) |
ES (1) | ES2548697T3 (fr) |
FR (1) | FR2976346B1 (fr) |
PL (1) | PL2718627T3 (fr) |
RU (1) | RU2600829C2 (fr) |
WO (1) | WO2012168636A2 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2484064B (en) * | 2010-08-26 | 2016-01-06 | Rotite Ltd | Connector and method of connecting two items together |
FR3017693B1 (fr) * | 2014-02-19 | 2019-07-26 | Safran Helicopter Engines | Chambre de combustion de turbomachine |
US9513011B2 (en) * | 2014-06-03 | 2016-12-06 | Siemens Energy, Inc. | Gas turbine engine combustor top hat cover attachment system with lugged interlocking backing plate |
WO2016032515A1 (fr) * | 2014-08-29 | 2016-03-03 | Siemens Energy, Inc. | Agencement à baïonnette d'un élément carcasse utilisant des crochets inclinés et procédé pour fixer et retirer cet élément |
UA119005C2 (uk) * | 2015-04-02 | 2019-04-10 | Бті Гумковскі Сп. З О.О. Сп. К. | Пальник твердопаливного котла |
RU186048U1 (ru) * | 2018-10-08 | 2018-12-27 | Публичное Акционерное Общество "Одк-Сатурн" | Узел упругого соединения жаровой трубы и газосборника камеры сгорания газотурбинного двигателя |
US10895170B2 (en) * | 2018-10-22 | 2021-01-19 | Raytheon Technologies Corporation | Shear wave resistant flange assembly |
FR3095499B1 (fr) | 2019-04-23 | 2021-06-11 | Safran Helicopter Engines | Injecteur d’un melange d’air et de carburant pour une chambre de combustion d’une turbomachine |
FR3119881B1 (fr) * | 2021-02-18 | 2023-12-22 | Safran Ceram | Sous ensemble comportant des moyens de compensation d'une difference de dilatation |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4411134A (en) * | 1981-10-26 | 1983-10-25 | Moir David L | Apparatus for the repair and replacement of transition ducts on jet engines and bracket therefor |
JPH087246Y2 (ja) * | 1989-08-03 | 1996-03-04 | トヨタ自動車株式会社 | セラミック製燃焼器の組立構造 |
FR2656391B1 (fr) * | 1989-12-27 | 1992-04-03 | Aerospatiale | Systeme pour l'assemblage coaxial de deux pieces de revolution. |
FR2679010B1 (fr) * | 1991-07-10 | 1993-09-24 | Snecma | Chambre de combustion de turbomachine a bols de prevaporisation demontables. |
US5737913A (en) * | 1996-10-18 | 1998-04-14 | The United States Of America As Represented By The Secretary Of The Air Force | Self-aligning quick release engine case assembly |
US7152411B2 (en) * | 2003-06-27 | 2006-12-26 | General Electric Company | Rabbet mounted combuster |
US7093448B2 (en) * | 2003-10-08 | 2006-08-22 | Honeywell International, Inc. | Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engine |
RU2287115C1 (ru) * | 2005-04-15 | 2006-11-10 | Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") | Кольцевая камера сгорания газотурбинного двигателя |
FR2885201B1 (fr) * | 2005-04-28 | 2010-09-17 | Snecma Moteurs | Chambre de combustion aisement demontable a performance aerodynamique amelioree |
US7334960B2 (en) * | 2005-06-23 | 2008-02-26 | Siemens Power Generation, Inc. | Attachment device for removable components in hot gas paths in a turbine engine |
FR2897145B1 (fr) * | 2006-02-08 | 2013-01-18 | Snecma | Chambre de combustion annulaire de turbomachine a fixations alternees. |
FR2897922B1 (fr) * | 2006-02-27 | 2008-10-10 | Snecma Sa | Agencement pour une chambre de combustion de turboreacteur |
US7623940B2 (en) * | 2006-06-02 | 2009-11-24 | The Boeing Company | Direct-manufactured duct interconnects |
US7984615B2 (en) * | 2007-06-27 | 2011-07-26 | Honeywell International Inc. | Combustors for use in turbine engine assemblies |
US8579538B2 (en) * | 2010-07-30 | 2013-11-12 | United Technologies Corporation | Turbine engine coupling stack |
-
2011
- 2011-06-08 FR FR1154984A patent/FR2976346B1/fr active Active
-
2012
- 2012-06-04 WO PCT/FR2012/051240 patent/WO2012168636A2/fr active Application Filing
- 2012-06-04 CN CN201280028205.XA patent/CN103597285B/zh active Active
- 2012-06-04 US US14/124,511 patent/US8925331B2/en active Active
- 2012-06-04 KR KR1020137034350A patent/KR102001690B1/ko active IP Right Grant
- 2012-06-04 EP EP12731106.6A patent/EP2718627B1/fr active Active
- 2012-06-04 PL PL12731106T patent/PL2718627T3/pl unknown
- 2012-06-04 ES ES12731106.6T patent/ES2548697T3/es active Active
- 2012-06-04 JP JP2014514132A patent/JP6073299B2/ja not_active Expired - Fee Related
- 2012-06-04 CA CA2838168A patent/CA2838168C/fr active Active
- 2012-06-04 RU RU2013158179/06A patent/RU2600829C2/ru active
Also Published As
Publication number | Publication date |
---|---|
RU2013158179A (ru) | 2015-07-20 |
JP6073299B2 (ja) | 2017-02-01 |
EP2718627A2 (fr) | 2014-04-16 |
JP2014516152A (ja) | 2014-07-07 |
US8925331B2 (en) | 2015-01-06 |
FR2976346B1 (fr) | 2013-07-05 |
ES2548697T3 (es) | 2015-10-20 |
KR102001690B1 (ko) | 2019-07-18 |
US20140109595A1 (en) | 2014-04-24 |
PL2718627T3 (pl) | 2015-12-31 |
CA2838168A1 (fr) | 2012-12-13 |
EP2718627B1 (fr) | 2015-08-26 |
CN103597285B (zh) | 2015-09-30 |
RU2600829C2 (ru) | 2016-10-27 |
WO2012168636A3 (fr) | 2013-03-28 |
CN103597285A (zh) | 2014-02-19 |
WO2012168636A2 (fr) | 2012-12-13 |
KR20140037885A (ko) | 2014-03-27 |
FR2976346A1 (fr) | 2012-12-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request |
Effective date: 20170510 |