DE602006000228D1 - Vorrichtung mit pulsierender Verbrennung - Google Patents
Vorrichtung mit pulsierender VerbrennungInfo
- Publication number
- DE602006000228D1 DE602006000228D1 DE602006000228T DE602006000228T DE602006000228D1 DE 602006000228 D1 DE602006000228 D1 DE 602006000228D1 DE 602006000228 T DE602006000228 T DE 602006000228T DE 602006000228 T DE602006000228 T DE 602006000228T DE 602006000228 D1 DE602006000228 D1 DE 602006000228D1
- Authority
- DE
- Germany
- Prior art keywords
- conduits
- combustion
- inlet
- pulsating combustion
- outlet
- 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
- 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
- F02C3/14—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
- 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
- F02C3/165—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 the combustion chamber contributes to the driving force by creating reactive thrust
-
- 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
- F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in 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
- F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
- F02C5/04—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
- F02K7/04—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with resonant combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
- F02K7/06—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with combustion chambers having valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
- F02K7/075—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with multiple pulse-jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/08—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being continuous
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C15/00—Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Gasification And Melting Of Waste (AREA)
- Processes For Solid Components From Exhaust (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/090,754 US7448200B2 (en) | 2005-03-24 | 2005-03-24 | Pulse combustion device |
US90754 | 2005-03-24 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE602006000228D1 true DE602006000228D1 (de) | 2007-12-27 |
DE602006000228T2 DE602006000228T2 (de) | 2008-09-11 |
Family
ID=36658651
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602006000228T Active DE602006000228T2 (de) | 2005-03-24 | 2006-03-23 | Vorrichtung mit pulsierender Verbrennung |
Country Status (5)
Country | Link |
---|---|
US (1) | US7448200B2 (de) |
EP (1) | EP1710425B1 (de) |
JP (1) | JP2006266674A (de) |
AT (1) | ATE378509T1 (de) |
DE (1) | DE602006000228T2 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010016832A1 (de) * | 2010-05-06 | 2011-11-10 | Bundesanstalt für Materialforschung und -Prüfung (BAM) | Brennstoffgemisch zur Geräuschminimierung in Triebwerken |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7500348B2 (en) * | 2005-03-24 | 2009-03-10 | United Technologies Corporation | Pulse combustion device |
US7448200B2 (en) * | 2005-03-24 | 2008-11-11 | United Technologies Corporation | Pulse combustion device |
US8443583B2 (en) * | 2006-06-15 | 2013-05-21 | Indiana University Research And Technology Corp. | Pilot fuel injection for a wave rotor engine |
US20080310981A1 (en) * | 2007-06-12 | 2008-12-18 | General Electric Company | Positive displacement flow separator |
US20100071458A1 (en) * | 2007-06-12 | 2010-03-25 | General Electric Company | Positive displacement flow measurement device |
US20080310984A1 (en) * | 2007-06-12 | 2008-12-18 | General Electric Company | Positive displacement capture device |
US8146371B2 (en) * | 2007-12-21 | 2012-04-03 | United Technologies Corporation | Direct induction combustor/generator |
US10900443B2 (en) * | 2009-10-06 | 2021-01-26 | De Zhen Corporation Pty Ltd. | Optimal feedback heat energy internal combustion engine and applications |
JP6005061B2 (ja) * | 2010-12-30 | 2016-10-12 | ロールス−ロイス・ノース・アメリカン・テクノロジーズ,インコーポレーテッド | エンジンおよび燃焼システム |
US9506654B2 (en) * | 2011-08-19 | 2016-11-29 | General Electric Company | System and method for reducing combustion dynamics in a combustor |
US10060419B2 (en) | 2014-11-21 | 2018-08-28 | Northrop Grumman Systems Corporation | Battery powered vehicle propulsion system |
DE102015200964A1 (de) * | 2015-01-21 | 2016-07-21 | Freie Universität Berlin | Brennkammersystem für eine Gasturbine und Verfahren zur Verbrennung eines brennbaren Gemisches in einer Brennkammer |
FR3032024B1 (fr) * | 2015-01-26 | 2018-05-18 | Safran | Module de combustion a volume constant pour une turbomachine comportant un allumage par communication |
FR3037384B1 (fr) * | 2015-06-11 | 2017-06-23 | Turbomeca | Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion |
FR3092615B1 (fr) * | 2019-02-13 | 2021-01-22 | Safran Aircraft Engines | module de combustion CVC pour turbomachine d’aéronef comprenant des sous-ensembles de chambres indépendants |
CN110905688B (zh) * | 2019-10-16 | 2021-06-11 | 西北工业大学 | 一种利用不可燃液体提高脉冲爆震发动机工作频率的装置 |
US20210140641A1 (en) * | 2019-11-13 | 2021-05-13 | General Electric Company | Method and system for rotating detonation combustion |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2942412A (en) * | 1952-09-30 | 1960-06-28 | Curtiss Wright Corp | Pulse detonation jet propulsion |
US3417564A (en) | 1967-04-19 | 1968-12-24 | John G. Call | Jet engine with relatively rotatable combustion means, intake manifold and exhaust manifold |
DE2232025A1 (de) * | 1972-06-30 | 1974-01-17 | Motoren Turbinen Union | Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung |
US3848408A (en) | 1973-02-08 | 1974-11-19 | L Tompkins | Counter-wave pulse jet engine |
US4241576A (en) * | 1979-01-15 | 1980-12-30 | Gertz David C | Gas turbine engine |
DE4113680A1 (de) | 1991-03-12 | 1992-09-17 | Asea Brown Boveri | Gasturbogruppe |
US5901550A (en) | 1993-04-14 | 1999-05-11 | Adroit Systems, Inc. | Liquid fueled pulse detonation engine with controller and inlet and exit valves |
US5873240A (en) | 1993-04-14 | 1999-02-23 | Adroit Systems, Inc. | Pulsed detonation rocket engine |
US6003301A (en) | 1993-04-14 | 1999-12-21 | Adroit Systems, Inc. | Exhaust nozzle for multi-tube detonative engines |
US5345758A (en) | 1993-04-14 | 1994-09-13 | Adroit Systems, Inc. | Rotary valve multiple combustor pulse detonation engine |
GB2377257B (en) * | 2001-07-06 | 2004-09-01 | Hubert Michael Benians | Compound gas turbine engines and methods of operation thereof |
US6584765B1 (en) * | 2001-12-21 | 2003-07-01 | United Technologies Corporation | Pulse detonation engine having an aerodynamic valve |
US6981365B1 (en) * | 2001-12-28 | 2006-01-03 | Sierra Engineering Incorporated | Supersonic revolving nozzle |
US7621118B2 (en) * | 2002-07-03 | 2009-11-24 | Rolls-Royce North American Technologies, Inc. | Constant volume combustor having a rotating wave rotor |
US6901738B2 (en) * | 2003-06-26 | 2005-06-07 | United Technologies Corporation | Pulsed combustion turbine engine |
US7047724B2 (en) * | 2002-12-30 | 2006-05-23 | United Technologies Corporation | Combustion ignition |
US6889505B2 (en) | 2003-04-02 | 2005-05-10 | General Electric Company | Pulse detonation system for a gas turbine engine |
US6931833B2 (en) * | 2003-04-30 | 2005-08-23 | United Technologies Corporation | Pulse combustion device |
JP3952202B2 (ja) * | 2004-02-19 | 2007-08-01 | 独立行政法人 宇宙航空研究開発機構 | パルスデトネーションエンジン |
US7500348B2 (en) * | 2005-03-24 | 2009-03-10 | United Technologies Corporation | Pulse combustion device |
US7448200B2 (en) * | 2005-03-24 | 2008-11-11 | United Technologies Corporation | Pulse combustion device |
-
2005
- 2005-03-24 US US11/090,754 patent/US7448200B2/en not_active Expired - Fee Related
-
2006
- 2006-03-15 JP JP2006070154A patent/JP2006266674A/ja not_active Ceased
- 2006-03-23 EP EP06251552A patent/EP1710425B1/de not_active Not-in-force
- 2006-03-23 DE DE602006000228T patent/DE602006000228T2/de active Active
- 2006-03-23 AT AT06251552T patent/ATE378509T1/de not_active IP Right Cessation
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010016832A1 (de) * | 2010-05-06 | 2011-11-10 | Bundesanstalt für Materialforschung und -Prüfung (BAM) | Brennstoffgemisch zur Geräuschminimierung in Triebwerken |
Also Published As
Publication number | Publication date |
---|---|
EP1710425B1 (de) | 2007-11-14 |
DE602006000228T2 (de) | 2008-09-11 |
ATE378509T1 (de) | 2007-11-15 |
JP2006266674A (ja) | 2006-10-05 |
EP1710425A1 (de) | 2006-10-11 |
US20060213201A1 (en) | 2006-09-28 |
US7448200B2 (en) | 2008-11-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |