AU2002218781A1 - Partitioned multi-channel combustor - Google Patents
Partitioned multi-channel combustorInfo
- Publication number
- AU2002218781A1 AU2002218781A1 AU2002218781A AU1878102A AU2002218781A1 AU 2002218781 A1 AU2002218781 A1 AU 2002218781A1 AU 2002218781 A AU2002218781 A AU 2002218781A AU 1878102 A AU1878102 A AU 1878102A AU 2002218781 A1 AU2002218781 A1 AU 2002218781A1
- Authority
- AU
- Australia
- Prior art keywords
- partitioned multi
- channel combustor
- combustor
- channel
- partitioned
- 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.)
- Abandoned
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
- F23R7/00—Intermittent or explosive combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/02—Gas-turbine plants characterised by the use of combustion products as the working fluid using exhaust-gas pressure in a pressure exchanger to compress combustion-air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
- F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
-
- 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
- F23R3/56—Combustion chambers having rotary flame tubes
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US21609400P | 2000-07-06 | 2000-07-06 | |
US60/216094 | 2000-07-06 | ||
PCT/US2001/021368 WO2002004794A2 (en) | 2000-07-06 | 2001-07-05 | Partitioned multi-channel combustor |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2002218781A1 true AU2002218781A1 (en) | 2002-01-21 |
Family
ID=22805662
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2002218781A Abandoned AU2002218781A1 (en) | 2000-07-06 | 2001-07-05 | Partitioned multi-channel combustor |
Country Status (3)
Country | Link |
---|---|
US (1) | US6526936B2 (en) |
AU (1) | AU2002218781A1 (en) |
WO (1) | WO2002004794A2 (en) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7621118B2 (en) * | 2002-07-03 | 2009-11-24 | Rolls-Royce North American Technologies, Inc. | Constant volume combustor having a rotating wave rotor |
US7137243B2 (en) * | 2002-07-03 | 2006-11-21 | Rolls-Royce North American Technologies, Inc. | Constant volume combustor |
US6846208B1 (en) | 2003-11-03 | 2005-01-25 | Lockheed Martin Corporation | Wave rotor based power and propulsion generation for a marine vessel |
JP3952202B2 (en) * | 2004-02-19 | 2007-08-01 | 独立行政法人 宇宙航空研究開発機構 | Pulse detonation engine |
WO2006083320A2 (en) | 2004-07-09 | 2006-08-10 | Board Of Trustees Of Michigan State University | Ultra micro gas turbine |
US7228683B2 (en) * | 2004-07-21 | 2007-06-12 | General Electric Company | Methods and apparatus for generating gas turbine engine thrust using a pulse detonator |
JP2006138206A (en) * | 2004-11-10 | 2006-06-01 | Ishikawajima Harima Heavy Ind Co Ltd | Pde drive tip turbine fan engine |
EP2302170A1 (en) | 2004-11-12 | 2011-03-30 | Board of Trustees of Michigan State University | Turbomachine system and method of operation |
US7555891B2 (en) | 2004-11-12 | 2009-07-07 | Board Of Trustees Of Michigan State University | Wave rotor apparatus |
US7500348B2 (en) * | 2005-03-24 | 2009-03-10 | United Technologies Corporation | Pulse combustion device |
WO2008070210A2 (en) | 2006-06-15 | 2008-06-12 | Indiana University Research And Technology Corporation | Pilot fuel injection for a wave rotor engine |
US7937945B2 (en) | 2006-10-27 | 2011-05-10 | Kinde Sr Ronald August | Combining a series of more efficient engines into a unit, or modular units |
US8117824B1 (en) * | 2009-02-04 | 2012-02-21 | The United States of America as represented by the Secterary of the Navy | Pollution free engine using hydrogen as a fuel |
WO2012092495A1 (en) | 2010-12-30 | 2012-07-05 | Rolls-Royce North American Technologies, Inc. | Engine and combustion system |
WO2012116285A2 (en) | 2011-02-25 | 2012-08-30 | Board Of Trustees Of Michigan State University | Wave disc engine apparatus |
US9920689B2 (en) * | 2013-03-15 | 2018-03-20 | Indiana University Research And Technology Corporation | Hybrid wave rotor propulsion system |
US20160053680A1 (en) * | 2014-08-25 | 2016-02-25 | Rolls-Royce North American Technologies, Inc. | Combustion system |
FR3032025B1 (en) * | 2015-01-26 | 2018-06-15 | Safran | COMBUSTION MODULE WITH CONSTANT VOLUME FOR A TURBOMACHINE |
EP3056820B1 (en) | 2015-02-11 | 2019-03-13 | Rolls-Royce North American Technologies, Inc. | Wave rotors with temperature control features |
EP3056713B1 (en) | 2015-02-11 | 2017-10-25 | Rolls-Royce North American Technologies, Inc. | Exhaust mixer for wave rotor assembly |
US10393384B2 (en) | 2015-06-09 | 2019-08-27 | Rolls-Royce North American Technologies Inc. | Wave rotor with canceling resonator |
US10240794B2 (en) * | 2016-02-11 | 2019-03-26 | Rolls-Royce Corporation | Thermal and thrust management in dynamic pressure exchangers |
US10526965B2 (en) | 2016-04-29 | 2020-01-07 | Rolls-Royce Corporation | Ignition system for constant volume combustor |
US10519857B2 (en) * | 2016-10-24 | 2019-12-31 | Rolls-Royce Corporation | Disk with lattice features adapted for use in gas turbine engines |
CN106499516B (en) * | 2016-10-26 | 2018-12-07 | 南京航空航天大学 | Internal combustion wave rotor mixes gas and forms device |
US10627111B2 (en) * | 2017-03-27 | 2020-04-21 | United Technologies Coproration | Rotating detonation engine multi-stage mixer |
US10436110B2 (en) | 2017-03-27 | 2019-10-08 | United Technologies Corporation | Rotating detonation engine upstream wave arrestor |
US11674476B2 (en) | 2017-06-09 | 2023-06-13 | General Electric Company | Multiple chamber rotating detonation combustor |
US20180355792A1 (en) * | 2017-06-09 | 2018-12-13 | General Electric Company | Annular throats rotating detonation combustor |
US10641169B2 (en) | 2017-06-09 | 2020-05-05 | General Electric Company | Hybrid combustor assembly and method of operation |
US10520195B2 (en) | 2017-06-09 | 2019-12-31 | General Electric Company | Effervescent atomizing structure and method of operation for rotating detonation propulsion system |
US20180355795A1 (en) * | 2017-06-09 | 2018-12-13 | General Electric Company | Rotating detonation combustor with fluid diode structure |
US10969107B2 (en) | 2017-09-15 | 2021-04-06 | General Electric Company | Turbine engine assembly including a rotating detonation combustor |
US20190264918A1 (en) * | 2018-02-26 | 2019-08-29 | General Electric Company | Engine With Rotating Detonation Combustion System |
US11236908B2 (en) | 2018-10-24 | 2022-02-01 | General Electric Company | Fuel staging for rotating detonation combustor |
US11371711B2 (en) | 2018-11-28 | 2022-06-28 | General Electric Company | Rotating detonation combustor with offset inlet |
US11105511B2 (en) | 2018-12-14 | 2021-08-31 | General Electric Company | Rotating detonation propulsion system |
CN110131048B (en) * | 2019-05-08 | 2020-06-26 | 中国航空发动机研究院 | Self-contained internal combustion wave rotor ignition device and method |
FR3098859B1 (en) * | 2019-07-15 | 2023-04-28 | Safran Aircraft Engines | CONSTANT VOLUME TURBOMACHINE COMBUSTION CHAMBER |
US20210140641A1 (en) * | 2019-11-13 | 2021-05-13 | General Electric Company | Method and system for rotating detonation combustion |
US11572840B2 (en) | 2019-12-03 | 2023-02-07 | General Electric Company | Multi-mode combustion control for a rotating detonation combustion system |
CN114576005A (en) * | 2022-02-28 | 2022-06-03 | 北京航空航天大学宁波创新研究院 | Core machine based on wave rotor |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2399394A (en) | 1940-12-07 | 1946-04-30 | Bbc Brown Boveri & Cie | Pressure exchanger |
US2705867A (en) | 1949-06-30 | 1955-04-12 | Curtiss Wright Corp | Engine having a rotor with a plurality of circumferentially-spaced combustion chambers |
US3401676A (en) * | 1967-09-06 | 1968-09-17 | Fritz W. Wanzenberg | Ballistic internal-combustion turbine engine |
US3809020A (en) * | 1970-01-22 | 1974-05-07 | H Takitani | Sliding vane rotary engines and process for obtaining high torque power |
US3931553A (en) | 1972-08-07 | 1976-01-06 | Allis-Chalmers Corporation | Electronic commutation system having motor stator windings in push-pull |
US4240394A (en) * | 1978-10-06 | 1980-12-23 | Lay Joachim E | Rotary engine |
ATE28232T1 (en) | 1982-03-03 | 1987-07-15 | Bbc Brown Boveri & Cie | PRESSURE WAVE CHARGER WITH ROTOR ROLLER BEARING. |
DE3470904D1 (en) | 1983-11-30 | 1988-06-09 | Bbc Brown Boveri & Cie | Pressure exchanger |
DE3503071C1 (en) | 1985-01-30 | 1986-01-16 | Adam Opel AG, 6090 Rüsselsheim | Pressure wave supercharger for internal combustion engines, especially in motor vehicles |
CH668807A5 (en) | 1985-07-31 | 1989-01-31 | Bbc Brown Boveri & Cie | GAS TURBINE WITH A PRESSURE SHAFT MACHINE AS A HIGH PRESSURE COMPRESSOR PART. |
LU86156A1 (en) | 1985-11-12 | 1987-06-26 | Xrg Systems | METHOD AND DEVICE FOR EXTRACTING LIQUIDS FROM AGGREGATE AND VAPOR GAS MIXTURES |
EP0298097B1 (en) | 1987-01-05 | 1992-08-12 | HAUGE, Leif J. | Pressure exchanger for liquids |
US5339635A (en) * | 1987-09-04 | 1994-08-23 | Hitachi, Ltd. | Gas turbine combustor of the completely premixed combustion type |
US4924637A (en) | 1987-10-21 | 1990-05-15 | Ngk Insulators, Ltd. | Method of machining ceramic rotor for pressure wave type supercharger |
NO168548C (en) | 1989-11-03 | 1992-03-04 | Leif J Hauge | PRESS CHANGER. |
DE59009885D1 (en) | 1990-07-27 | 1995-12-21 | Asea Brown Boveri | Process for the treatment of the working gas in a gas turbine plant. |
EP0472748A1 (en) | 1990-08-25 | 1992-03-04 | Asea Brown Boveri Ag | Rotor of a pressure wave machine |
DE4204678A1 (en) | 1992-02-17 | 1993-08-19 | Asea Brown Boveri | PRINT WAVE MACHINE WITH INTEGRATED COMBUSTION |
US5267432A (en) | 1992-05-26 | 1993-12-07 | The United States Of America As Represented By The Administrator Of The National Aeronautics & Space Administration | System and method for cancelling expansion waves in a wave rotor |
DE4241613A1 (en) | 1992-12-10 | 1994-06-16 | Asea Brown Boveri | Aircraft engine with fan or propeller drive - has two independently rotating coaxial shafts with fuel combustion in compressed air fuel-enriching machine with bucket wheel |
US5345758A (en) | 1993-04-14 | 1994-09-13 | Adroit Systems, Inc. | Rotary valve multiple combustor pulse detonation engine |
DE4330037A1 (en) | 1993-09-06 | 1995-03-09 | Abb Management Ag | Pressure-wave machine with integral combustion and method for cooling the rotor of the said pressure-wave machine |
US5894719A (en) | 1997-04-18 | 1999-04-20 | The United States Of America, As Represented By The Administrator Of The National Aeronautics And Space Administration | Method and apparatus for cold gas reinjection in through-flow and reverse-flow wave rotors |
US5916125A (en) | 1997-05-16 | 1999-06-29 | Allison Engine Company, Inc. | Forced purge wave rotor |
US6460342B1 (en) | 1999-04-26 | 2002-10-08 | Advanced Research & Technology Institute | Wave rotor detonation engine |
-
2001
- 2001-07-05 WO PCT/US2001/021368 patent/WO2002004794A2/en active Application Filing
- 2001-07-05 US US09/899,801 patent/US6526936B2/en not_active Expired - Lifetime
- 2001-07-05 AU AU2002218781A patent/AU2002218781A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
WO2002004794A2 (en) | 2002-01-17 |
US6526936B2 (en) | 2003-03-04 |
WO2002004794A3 (en) | 2002-05-23 |
US20020068250A1 (en) | 2002-06-06 |
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