ATE334307T1 - Apparat mit pulsierender verbrennung und verteilter zündung - Google Patents
Apparat mit pulsierender verbrennung und verteilter zündungInfo
- Publication number
- ATE334307T1 ATE334307T1 AT03258153T AT03258153T ATE334307T1 AT E334307 T1 ATE334307 T1 AT E334307T1 AT 03258153 T AT03258153 T AT 03258153T AT 03258153 T AT03258153 T AT 03258153T AT E334307 T1 ATE334307 T1 AT E334307T1
- Authority
- AT
- Austria
- Prior art keywords
- tube
- pulsating combustion
- utilized
- distributed ignition
- distributed
- Prior art date
Links
Classifications
-
- 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
- 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
- F02C5/10—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect
- F02C5/11—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect using valveless combustion chambers
-
- 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
- F02K3/06—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 with front fan
-
- 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
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)
- Air Bags (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/334,019 US7047724B2 (en) | 2002-12-30 | 2002-12-30 | Combustion ignition |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE334307T1 true ATE334307T1 (de) | 2006-08-15 |
Family
ID=32507369
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT03258153T ATE334307T1 (de) | 2002-12-30 | 2003-12-24 | Apparat mit pulsierender verbrennung und verteilter zündung |
Country Status (4)
| Country | Link |
|---|---|
| US (2) | US7047724B2 (de) |
| EP (1) | EP1435449B1 (de) |
| AT (1) | ATE334307T1 (de) |
| DE (1) | DE60307033T2 (de) |
Families Citing this family (61)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2829528B1 (fr) * | 2001-09-07 | 2004-02-27 | Bernard Gilbert Macarez | Pulsomoteur-turbomoteur a impulsion-turbine a gaz a chambre de combustion impulsionnelle et a detente de bouffees |
| US7367194B2 (en) * | 2003-02-12 | 2008-05-06 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Pulse detonation engine system for driving turbine |
| FR2855556B1 (fr) * | 2003-05-28 | 2007-04-13 | Mbda France | Moteur a detonations pulsees |
| US7124573B2 (en) * | 2004-03-18 | 2006-10-24 | General Electric Company | Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine |
| US20050210862A1 (en) * | 2004-03-25 | 2005-09-29 | Paterro Von Friedrich C | Quantum jet turbine propulsion system |
| US7131260B2 (en) * | 2004-06-18 | 2006-11-07 | General Electric Company | Multiple detonation initiator for frequency multiplied pulsed detonation combustion |
| US7228683B2 (en) * | 2004-07-21 | 2007-06-12 | General Electric Company | Methods and apparatus for generating gas turbine engine thrust using a pulse detonator |
| US7080504B2 (en) * | 2004-07-23 | 2006-07-25 | Northrop Grumman Corporation | Laser augmented turbojet propulsion system |
| US7328570B2 (en) * | 2004-09-01 | 2008-02-12 | General Electric Company | Pulse detonation system for a gas turbine engine having multiple spools |
| US20060053801A1 (en) * | 2004-09-15 | 2006-03-16 | Orlando Robert J | Cooling system for gas turbine engine having improved core system |
| US7093446B2 (en) * | 2004-09-15 | 2006-08-22 | General Electric Company | Gas turbine engine having improved core system |
| US7096674B2 (en) * | 2004-09-15 | 2006-08-29 | General Electric Company | High thrust gas turbine engine with improved core system |
| US7278256B2 (en) * | 2004-11-08 | 2007-10-09 | United Technologies Corporation | Pulsed combustion engine |
| US7637096B2 (en) * | 2004-11-25 | 2009-12-29 | Rolls-Royce Plc | Pulse jet engine having pressure sensor means for controlling fuel delivery into a combustion chamber |
| 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 |
| US7685806B2 (en) * | 2005-12-29 | 2010-03-30 | General Electric Company | Method and apparatus for supersonic and shock noise reduction in aircraft engines using pneumatic corrugations |
| US20090320439A1 (en) * | 2006-01-31 | 2009-12-31 | General Electric Company | Pulsed detonation combustor cleaning device and method of operation |
| KR100785611B1 (ko) | 2006-07-14 | 2007-12-12 | 산 지 타이 | 제트 터빈용 회전체 및 그 제조 방법 |
| 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 |
| US20080155959A1 (en) * | 2006-12-22 | 2008-07-03 | General Electric Company | Detonation combustor to turbine transition piece for hybrid engine |
| US8146371B2 (en) * | 2007-12-21 | 2012-04-03 | United Technologies Corporation | Direct induction combustor/generator |
| US20090165438A1 (en) * | 2007-12-26 | 2009-07-02 | Occhipinti Anthony C | Pulse detonation engine |
| DE102008028208B4 (de) * | 2008-06-09 | 2012-03-22 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Brennkammervorrichtung und Verfahren zu deren Betrieb |
| US8205433B2 (en) * | 2008-08-21 | 2012-06-26 | Lockheed Martin Corporation | Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production |
| US8438834B2 (en) * | 2009-03-30 | 2013-05-14 | Alliant Techsystems Inc. | Helical cross flow (HCF) pulse detonation engine |
| US20100251992A1 (en) * | 2009-04-06 | 2010-10-07 | Davis Frank S | Radial pulsed rotary internal combustion engine |
| US8429893B2 (en) | 2009-08-11 | 2013-04-30 | Northrop Grumman Corporation | Airflow modulation for dual mode combined cycle propulsion systems |
| US20120102916A1 (en) * | 2010-10-29 | 2012-05-03 | General Electric Company | Pulse Detonation Combustor Including Combustion Chamber Cooling Assembly |
| WO2012061742A1 (en) | 2010-11-05 | 2012-05-10 | ThermoChem Recovery International | Solids circulation system and method for capture and conversion of reactive solids |
| US8539752B2 (en) * | 2010-11-30 | 2013-09-24 | General Electric Company | Integrated deflagration-to-detonation obstacles and cooling fluid flow |
| US8650856B2 (en) * | 2010-12-10 | 2014-02-18 | General Electric Company | Fluidic deflagration-to-detonation initiation obstacles |
| WO2013049368A1 (en) | 2011-09-27 | 2013-04-04 | Thermochem Recovery International, Inc. | System and method for syngas clean-up |
| US9140456B2 (en) * | 2011-12-01 | 2015-09-22 | General Electric Company | Variable initiation location system for pulse detonation combustor |
| US20130139486A1 (en) * | 2011-12-01 | 2013-06-06 | General Electric Company | Variable initiation location system for pulse detonation combustor |
| US20140338348A1 (en) * | 2011-12-16 | 2014-11-20 | Daniel Guy Pomerleau | Rotary pulse detonation engine |
| KR20150032911A (ko) * | 2012-07-24 | 2015-03-30 | 브렌트 웨이-테 이 | 내부 폭발 엔진, 그것을 포함하는 하이브리드 엔진, 및 그것의 제조 및 사용 방법 |
| US9021783B2 (en) * | 2012-10-12 | 2015-05-05 | United Technologies Corporation | Pulse detonation engine having a scroll ejector attenuator |
| WO2015138033A1 (en) * | 2013-12-31 | 2015-09-17 | Hill James D | Inlet manifold for multi-tube pulse detonation engine |
| FI127525B (en) * | 2014-01-08 | 2018-08-15 | Finno Energy Oy | System and method for generating electrical energy |
| US9869190B2 (en) | 2014-05-30 | 2018-01-16 | General Electric Company | Variable-pitch rotor with remote counterweights |
| US10072510B2 (en) | 2014-11-21 | 2018-09-11 | General Electric Company | Variable pitch fan for gas turbine engine and method of assembling the same |
| US11225913B2 (en) | 2015-02-19 | 2022-01-18 | Raytheon Technologies Corporation | Method of providing turbine engines with different thrust ratings |
| US10100653B2 (en) | 2015-10-08 | 2018-10-16 | General Electric Company | Variable pitch fan blade retention system |
| US20170114752A1 (en) * | 2015-10-27 | 2017-04-27 | Honda Patents & Technologies North America, Llc | Standing wave compressor pulsejet engine |
| US10240794B2 (en) | 2016-02-11 | 2019-03-26 | Rolls-Royce Corporation | Thermal and thrust management in dynamic pressure exchangers |
| CA3014874C (en) | 2016-02-16 | 2019-03-19 | Thermochem Recovery International, Inc. | Two-stage energy-integrated product gas generation system and method |
| ES2923073T3 (es) | 2016-03-25 | 2022-09-22 | Thermochem Recovery Int Inc | Sistema de generación de producto gaseoso integrada en energía de tres fases |
| US10526965B2 (en) * | 2016-04-29 | 2020-01-07 | Rolls-Royce Corporation | Ignition system for constant volume combustor |
| US20180010800A1 (en) * | 2016-06-14 | 2018-01-11 | Adithya Ananth NAGESH | Shock compression based supersonic combustor |
| US10364398B2 (en) | 2016-08-30 | 2019-07-30 | Thermochem Recovery International, Inc. | Method of producing product gas from multiple carbonaceous feedstock streams mixed with a reduced-pressure mixing gas |
| EP3619471B1 (de) * | 2017-04-30 | 2021-02-24 | King Abdullah University Of Science And Technology | Verbrennungsmotor mit automatisch angesteuerter plasmaaktuator für übergang vom deflagrations- zum detonationsverbrennungsraum und verfahren zum betrieb eines solchen motors |
| US9920926B1 (en) | 2017-07-10 | 2018-03-20 | Thermochem Recovery International, Inc. | Pulse combustion heat exchanger system and method |
| US10099200B1 (en) | 2017-10-24 | 2018-10-16 | Thermochem Recovery International, Inc. | Liquid fuel production system having parallel product gas generation |
| US20210140641A1 (en) * | 2019-11-13 | 2021-05-13 | General Electric Company | Method and system for rotating detonation combustion |
| US11555157B2 (en) | 2020-03-10 | 2023-01-17 | Thermochem Recovery International, Inc. | System and method for liquid fuel production from carbonaceous materials using recycled conditioned syngas |
| US11466223B2 (en) | 2020-09-04 | 2022-10-11 | Thermochem Recovery International, Inc. | Two-stage syngas production with separate char and product gas inputs into the second stage |
| CN113153569B (zh) * | 2021-04-27 | 2022-10-28 | 西北工业大学 | 一种平稳排气的多管脉冲爆震发动机 |
| US11674435B2 (en) | 2021-06-29 | 2023-06-13 | General Electric Company | Levered counterweight feathering system |
| US11795964B2 (en) | 2021-07-16 | 2023-10-24 | General Electric Company | Levered counterweight feathering system |
| US12510249B2 (en) * | 2023-06-20 | 2025-12-30 | Pratt & Whitney Canada Corp. | Auxiliary power unit with pulse detonation combustion |
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-
2002
- 2002-12-30 US US10/334,019 patent/US7047724B2/en not_active Expired - Fee Related
-
2003
- 2003-06-27 US US10/608,238 patent/US7100360B2/en not_active Expired - Fee Related
- 2003-12-24 DE DE60307033T patent/DE60307033T2/de not_active Expired - Lifetime
- 2003-12-24 EP EP03258153A patent/EP1435449B1/de not_active Expired - Lifetime
- 2003-12-24 AT AT03258153T patent/ATE334307T1/de not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| US7100360B2 (en) | 2006-09-05 |
| US7047724B2 (en) | 2006-05-23 |
| EP1435449A1 (de) | 2004-07-07 |
| EP1435449B1 (de) | 2006-07-26 |
| US20050000205A1 (en) | 2005-01-06 |
| US20040123583A1 (en) | 2004-07-01 |
| DE60307033T2 (de) | 2006-12-21 |
| DE60307033D1 (de) | 2006-09-07 |
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