EP1881179A3 - Wandbelüftungssystem für die Brennkammer einer Strömungsmaschine - Google Patents
Wandbelüftungssystem für die Brennkammer einer Strömungsmaschine Download PDFInfo
- Publication number
- EP1881179A3 EP1881179A3 EP07290753A EP07290753A EP1881179A3 EP 1881179 A3 EP1881179 A3 EP 1881179A3 EP 07290753 A EP07290753 A EP 07290753A EP 07290753 A EP07290753 A EP 07290753A EP 1881179 A3 EP1881179 A3 EP 1881179A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- combustion chamber
- turbomachine
- wall
- ventilating
- chamber
- 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
- 238000002485 combustion reaction Methods 0.000 title abstract 4
- 238000002347 injection Methods 0.000 abstract 2
- 239000007924 injection Substances 0.000 abstract 2
- 238000009423 ventilation Methods 0.000 abstract 2
- 210000003462 vein Anatomy 0.000 abstract 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/26—Controlling the air flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0606547A FR2904048B1 (fr) | 2006-07-19 | 2006-07-19 | Systeme de ventilation de paroi de chambre de combustion dans une turbomachine |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1881179A2 EP1881179A2 (de) | 2008-01-23 |
EP1881179A3 true EP1881179A3 (de) | 2008-09-17 |
EP1881179B1 EP1881179B1 (de) | 2018-08-15 |
Family
ID=37771119
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07290753.8A Active EP1881179B1 (de) | 2006-07-19 | 2007-06-18 | Wandbelüftungssystem für die Brennkammer einer Strömungsmaschine |
Country Status (4)
Country | Link |
---|---|
US (1) | US7827798B2 (de) |
EP (1) | EP1881179B1 (de) |
FR (1) | FR2904048B1 (de) |
RU (1) | RU2446296C2 (de) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2920032B1 (fr) * | 2007-08-13 | 2014-08-22 | Snecma | Diffuseur d'une turbomachine |
FR2927951B1 (fr) * | 2008-02-27 | 2011-08-19 | Snecma | Ensemble diffuseur-redresseur pour une turbomachine |
US8087249B2 (en) * | 2008-12-23 | 2012-01-03 | General Electric Company | Turbine cooling air from a centrifugal compressor |
US7712314B1 (en) | 2009-01-21 | 2010-05-11 | Gas Turbine Efficiency Sweden Ab | Venturi cooling system |
FR2941742B1 (fr) * | 2009-02-05 | 2011-08-19 | Snecma | Ensemble diffuseur-redresseur pour une turbomachine |
FR2952126B1 (fr) * | 2009-11-04 | 2011-12-23 | Snecma | Turbomachine a double flux pour aeronef, comprenant des moyens structuraux de rigidification du carter central |
FR2970512B1 (fr) * | 2011-01-14 | 2013-01-04 | Snecma | Piece annulaire de guidage d'air autour d'une chambre de combustion dans une turbomachine |
US9134029B2 (en) | 2013-09-12 | 2015-09-15 | Siemens Energy, Inc. | Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans |
US9528706B2 (en) | 2013-12-13 | 2016-12-27 | Siemens Energy, Inc. | Swirling midframe flow for gas turbine engine having advanced transitions |
CN104879324B (zh) * | 2015-05-21 | 2017-11-14 | 中国南方航空工业(集团)有限公司 | 发动机空气冷却系统 |
CN105114983B (zh) * | 2015-09-24 | 2017-12-12 | 北京动力机械研究所 | 一种ω型火焰筒 |
DE102015219556A1 (de) | 2015-10-08 | 2017-04-13 | Rolls-Royce Deutschland Ltd & Co Kg | Diffusor für Radialverdichter, Radialverdichter und Turbomaschine mit Radialverdichter |
US10830144B2 (en) | 2016-09-08 | 2020-11-10 | Rolls-Royce North American Technologies Inc. | Gas turbine engine compressor impeller cooling air sinks |
DE102016122735A1 (de) | 2016-11-24 | 2018-05-24 | Kt Projektentwicklungs-Gmbh | Kraftfahrzeug mit einer Verdichteranordnung |
US11098730B2 (en) | 2019-04-12 | 2021-08-24 | Rolls-Royce Corporation | Deswirler assembly for a centrifugal compressor |
US11525393B2 (en) | 2020-03-19 | 2022-12-13 | Rolls-Royce Corporation | Turbine engine with centrifugal compressor having impeller backplate offtake |
US11286952B2 (en) | 2020-07-14 | 2022-03-29 | Rolls-Royce Corporation | Diffusion system configured for use with centrifugal compressor |
US11441516B2 (en) | 2020-07-14 | 2022-09-13 | Rolls-Royce North American Technologies Inc. | Centrifugal compressor assembly for a gas turbine engine with deswirler having sealing features |
US11578654B2 (en) | 2020-07-29 | 2023-02-14 | Rolls-Royce North American Technologies Inc. | Centrifical compressor assembly for a gas turbine engine |
DE102021125045A1 (de) | 2021-09-28 | 2023-03-30 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerk mit Zentrifugalverdichter, Ringbrennkammer und einer unterschiedliche Leitkanalelemente aufweisenden Leitkanalanordnung |
US11773773B1 (en) | 2022-07-26 | 2023-10-03 | Rolls-Royce North American Technologies Inc. | Gas turbine engine centrifugal compressor with impeller load and cooling control |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2030993A5 (de) * | 1969-08-18 | 1970-11-13 | Motoren Turbinen Union | |
US4429527A (en) * | 1981-06-19 | 1984-02-07 | Teets J Michael | Turbine engine with combustor premix system |
US5555721A (en) * | 1994-09-28 | 1996-09-17 | General Electric Company | Gas turbine engine cooling supply circuit |
US6148617A (en) * | 1998-07-06 | 2000-11-21 | Williams International, Co. L.L.C. | Natural gas fired combustion system for gas turbine engines |
US20050247065A1 (en) * | 2004-05-04 | 2005-11-10 | Honeywell International Inc. | Rich quick mix combustion system |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1152331A (en) * | 1966-05-18 | 1969-05-14 | Rolls Royce | Improvements in Gas Turbine Blade Cooling |
SU556221A1 (ru) * | 1975-11-20 | 1977-04-30 | Уфимский авиационный институт им. Орджоникидзе | Устройство дл охлаждени диска турбомашины |
US4277222A (en) * | 1979-01-11 | 1981-07-07 | Teledyne Industries, Inc. | Turbine engine compressor |
US4462204A (en) * | 1982-07-23 | 1984-07-31 | General Electric Company | Gas turbine engine cooling airflow modulator |
US4845941A (en) * | 1986-11-07 | 1989-07-11 | Paul Marius A | Gas turbine engine operating process |
RU2130124C1 (ru) * | 1996-05-28 | 1999-05-10 | Акционерное общество "Авиадвигатель" | Ротор многоступенчатой турбины |
DE19845375A1 (de) * | 1998-10-02 | 2000-04-06 | Asea Brown Boveri | Verfahren und Vorrichtung zur indirekten Kühlung der Strömung in zwischen Rotoren und Statoren von Turbomaschinen ausgebildeten Radialspalten |
WO2001011215A1 (en) * | 1999-08-09 | 2001-02-15 | Technion Research And Development Foundation Ltd. | Novel design of adiabatic combustors |
US7568343B2 (en) * | 2005-09-12 | 2009-08-04 | Florida Turbine Technologies, Inc. | Small gas turbine engine with multiple burn zones |
-
2006
- 2006-07-19 FR FR0606547A patent/FR2904048B1/fr active Active
-
2007
- 2007-06-18 EP EP07290753.8A patent/EP1881179B1/de active Active
- 2007-07-18 RU RU2007127554/06A patent/RU2446296C2/ru active
- 2007-07-19 US US11/780,246 patent/US7827798B2/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2030993A5 (de) * | 1969-08-18 | 1970-11-13 | Motoren Turbinen Union | |
US4429527A (en) * | 1981-06-19 | 1984-02-07 | Teets J Michael | Turbine engine with combustor premix system |
US5555721A (en) * | 1994-09-28 | 1996-09-17 | General Electric Company | Gas turbine engine cooling supply circuit |
US6148617A (en) * | 1998-07-06 | 2000-11-21 | Williams International, Co. L.L.C. | Natural gas fired combustion system for gas turbine engines |
US20050247065A1 (en) * | 2004-05-04 | 2005-11-10 | Honeywell International Inc. | Rich quick mix combustion system |
Also Published As
Publication number | Publication date |
---|---|
EP1881179A2 (de) | 2008-01-23 |
US20080019828A1 (en) | 2008-01-24 |
RU2007127554A (ru) | 2009-01-27 |
US7827798B2 (en) | 2010-11-09 |
RU2446296C2 (ru) | 2012-03-27 |
FR2904048A1 (fr) | 2008-01-25 |
FR2904048B1 (fr) | 2012-12-14 |
EP1881179B1 (de) | 2018-08-15 |
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