EP2527743A3 - Composant segmenté à base de matériau réfractaire pour une chambre de combustion annulaire, chambre de combustion annulaire pour un moteur d'aéronef, moteur d'aéronef et procédé de fabrication d'une chambre de combustion annulaire - Google Patents
Composant segmenté à base de matériau réfractaire pour une chambre de combustion annulaire, chambre de combustion annulaire pour un moteur d'aéronef, moteur d'aéronef et procédé de fabrication d'une chambre de combustion annulaire Download PDFInfo
- Publication number
- EP2527743A3 EP2527743A3 EP12169511.8A EP12169511A EP2527743A3 EP 2527743 A3 EP2527743 A3 EP 2527743A3 EP 12169511 A EP12169511 A EP 12169511A EP 2527743 A3 EP2527743 A3 EP 2527743A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- combustion chamber
- annular combustion
- aircraft engine
- producing
- segment component
- 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.)
- Granted
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
- F23R3/50—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
- F23R2900/00018—Manufacturing 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
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/4927—Cylinder, cylinder head or engine valve sleeve making
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Laser Beam Processing (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011076473A DE102011076473A1 (de) | 2011-05-25 | 2011-05-25 | Segmentbauteil aus Hochtemperaturgussmaterial für eine Ringbrennkammer, Ringbrennkammer für ein Flugzeugtriebwerk, Flugzeugtriebwerk und Verfahren zur Herstellung einer Ringbrennkammer |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2527743A2 EP2527743A2 (fr) | 2012-11-28 |
EP2527743A3 true EP2527743A3 (fr) | 2015-01-21 |
EP2527743B1 EP2527743B1 (fr) | 2016-09-28 |
Family
ID=46148713
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12169511.8A Not-in-force EP2527743B1 (fr) | 2011-05-25 | 2012-05-25 | Composant segmenté à base de matériau réfractaire pour une chambre de combustion annulaire, chambre de combustion annulaire pour un moteur d'aéronef, moteur d'aéronef et procédé de fabrication d'une chambre de combustion annulaire |
Country Status (3)
Country | Link |
---|---|
US (1) | US8646279B2 (fr) |
EP (1) | EP2527743B1 (fr) |
DE (1) | DE102011076473A1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102013222863A1 (de) | 2013-11-11 | 2015-05-13 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer sowie Verfahren zu deren Herstellung |
DE102014204468A1 (de) * | 2014-03-11 | 2015-10-01 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer sowie Verfahren zu deren Herstellung |
DE102016201452A1 (de) * | 2016-02-01 | 2017-08-03 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit Wandkonturierung |
CN111059575B (zh) * | 2018-10-16 | 2022-05-10 | 中发天信(北京)航空发动机科技股份有限公司 | 涡喷发动机火焰筒外壳 |
US20200318549A1 (en) * | 2019-04-04 | 2020-10-08 | United Technologies Corporation | Non-axisymmetric combustor for improved durability |
GB202019222D0 (en) | 2020-12-07 | 2021-01-20 | Rolls Royce Plc | Lean burn combustor |
GB202019219D0 (en) * | 2020-12-07 | 2021-01-20 | Rolls Royce Plc | Lean burn combustor |
US11940151B2 (en) | 2022-01-12 | 2024-03-26 | General Electric Company | Combustor with baffle |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1106927A1 (fr) * | 1999-12-09 | 2001-06-13 | Rolls-Royce Deutschland Ltd & Co KG | Procédé de fabrication d'une chambre de combustion de turbo-réacteur |
EP1584871A2 (fr) * | 2004-04-08 | 2005-10-12 | United Technologies Corporation | Articles monocrystalines avec orientation cristallographique contrôlée |
EP1760402A2 (fr) * | 2005-08-30 | 2007-03-07 | United Technologies Corporation | Méthode de moulage de trous de refroidissement |
US20070062198A1 (en) * | 2003-05-30 | 2007-03-22 | Siemens Aktiengesellschaft | Combustion chamber |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB741836A (en) * | 1953-03-05 | 1955-12-14 | Lucas Industries Ltd | Combustion chambers for jet-propulsion engines, gas turbines or other prime movers |
CA2056592A1 (fr) * | 1990-12-21 | 1992-06-22 | Phillip D. Napoli | Chemise de chambre de combustion a refroidissement par gaine d'air a trous multiples avec demarreur a gaine d'air rainuree |
US5964091A (en) * | 1995-07-11 | 1999-10-12 | Hitachi, Ltd. | Gas turbine combustor and gas turbine |
EP1312865A1 (fr) * | 2001-11-15 | 2003-05-21 | Siemens Aktiengesellschaft | Chambre de combustion annulaire de turbine à gaz |
DE50212643D1 (de) | 2002-11-22 | 2008-09-25 | Siemens Ag | Brennkammer zur Verbrennung eines brennbaren Fluidgemisches |
GB2420614B (en) * | 2004-11-30 | 2009-06-03 | Alstom Technology Ltd | Tile and exo-skeleton tile structure |
US7540156B2 (en) * | 2005-11-21 | 2009-06-02 | General Electric Company | Combustion liner for gas turbine formed of cast nickel-based superalloy |
EP2100687A1 (fr) * | 2008-02-29 | 2009-09-16 | Siemens Aktiengesellschaft | Chauffage de fil en acier sans potentiel lors de la soudure et son dispositif |
-
2011
- 2011-05-25 DE DE102011076473A patent/DE102011076473A1/de not_active Withdrawn
-
2012
- 2012-05-25 US US13/480,696 patent/US8646279B2/en active Active
- 2012-05-25 EP EP12169511.8A patent/EP2527743B1/fr not_active Not-in-force
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1106927A1 (fr) * | 1999-12-09 | 2001-06-13 | Rolls-Royce Deutschland Ltd & Co KG | Procédé de fabrication d'une chambre de combustion de turbo-réacteur |
US20070062198A1 (en) * | 2003-05-30 | 2007-03-22 | Siemens Aktiengesellschaft | Combustion chamber |
EP1584871A2 (fr) * | 2004-04-08 | 2005-10-12 | United Technologies Corporation | Articles monocrystalines avec orientation cristallographique contrôlée |
EP1760402A2 (fr) * | 2005-08-30 | 2007-03-07 | United Technologies Corporation | Méthode de moulage de trous de refroidissement |
Also Published As
Publication number | Publication date |
---|---|
EP2527743B1 (fr) | 2016-09-28 |
US20120304658A1 (en) | 2012-12-06 |
US8646279B2 (en) | 2014-02-11 |
EP2527743A2 (fr) | 2012-11-28 |
DE102011076473A1 (de) | 2012-11-29 |
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