DE602004003283D1 - Gerät mit pulsierender Verbrennung - Google Patents

Gerät mit pulsierender Verbrennung

Info

Publication number
DE602004003283D1
DE602004003283D1 DE602004003283T DE602004003283T DE602004003283D1 DE 602004003283 D1 DE602004003283 D1 DE 602004003283D1 DE 602004003283 T DE602004003283 T DE 602004003283T DE 602004003283 T DE602004003283 T DE 602004003283T DE 602004003283 D1 DE602004003283 D1 DE 602004003283D1
Authority
DE
Germany
Prior art keywords
nozzle
communication
upstream
location
combustor
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.)
Expired - Lifetime
Application number
DE602004003283T
Other languages
English (en)
Other versions
DE602004003283T2 (de
Inventor
Kirk R Lupkes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RTX Corp
Original Assignee
United Technologies Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of DE602004003283D1 publication Critical patent/DE602004003283D1/de
Application granted granted Critical
Publication of DE602004003283T2 publication Critical patent/DE602004003283T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • 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
    • 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
    • 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
    • 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

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)
DE602004003283T 2003-04-30 2004-04-22 Gerät mit pulsierender Verbrennung Expired - Lifetime DE602004003283T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/426,741 US6931833B2 (en) 2003-04-30 2003-04-30 Pulse combustion device
US426741 2003-04-30

Publications (2)

Publication Number Publication Date
DE602004003283D1 true DE602004003283D1 (de) 2007-01-04
DE602004003283T2 DE602004003283T2 (de) 2007-05-31

Family

ID=32990423

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004003283T Expired - Lifetime DE602004003283T2 (de) 2003-04-30 2004-04-22 Gerät mit pulsierender Verbrennung

Country Status (5)

Country Link
US (1) US6931833B2 (de)
EP (1) EP1473457B1 (de)
JP (1) JP3943094B2 (de)
AT (1) ATE346230T1 (de)
DE (1) DE602004003283T2 (de)

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* Cited by examiner, † Cited by third party
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US7137243B2 (en) * 2002-07-03 2006-11-21 Rolls-Royce North American Technologies, Inc. Constant volume combustor
US7621118B2 (en) 2002-07-03 2009-11-24 Rolls-Royce North American Technologies, Inc. Constant volume combustor having a rotating wave rotor
US7360508B2 (en) * 2004-06-14 2008-04-22 Diamond Power International, Inc. Detonation / deflagration sootblower
US7278256B2 (en) * 2004-11-08 2007-10-09 United Technologies Corporation Pulsed combustion engine
US7448200B2 (en) * 2005-03-24 2008-11-11 United Technologies Corporation Pulse combustion device
US7500348B2 (en) * 2005-03-24 2009-03-10 United Technologies Corporation Pulse combustion device
CN100365256C (zh) * 2005-12-26 2008-01-30 王菲 脉动式燃气轮机
US7634904B2 (en) * 2006-01-09 2009-12-22 General Electric Company Methods and apparatus to facilitate generating power from a turbine engine
US20080310981A1 (en) * 2007-06-12 2008-12-18 General Electric Company Positive displacement flow separator
US20080310984A1 (en) * 2007-06-12 2008-12-18 General Electric Company Positive displacement capture device
US8205433B2 (en) * 2008-08-21 2012-06-26 Lockheed Martin Corporation Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production
US20100192874A1 (en) * 2009-01-30 2010-08-05 Hughes Dennis R Pulse combustion system for a water heater
US8341932B2 (en) * 2009-03-19 2013-01-01 General Electric Company Rotary air valve firing patterns for resonance detuning
US10900443B2 (en) * 2009-10-06 2021-01-26 De Zhen Corporation Pty Ltd. Optimal feedback heat energy internal combustion engine and applications
US20110126510A1 (en) * 2009-11-30 2011-06-02 General Electric Company Pulse detonation combustor
CN101718236A (zh) * 2010-02-10 2010-06-02 周林 有爆震转射器连通的多管脉冲爆震燃烧室
EP2383515B1 (de) * 2010-04-28 2013-06-19 Siemens Aktiengesellschaft Brennersystem zur Dämpfung eines solchen Brennersystems
US9359973B2 (en) 2010-06-15 2016-06-07 Exponential Technologies, Inc. Multitube valveless pulse detonation engine
AU2011323198B2 (en) 2010-11-05 2015-06-18 Thermochem Recovery International, Inc. Solids circulation system and method for capture and conversion of reactive solids
US20120131901A1 (en) * 2010-11-30 2012-05-31 General Electric Company System and method for controlling a pulse detonation engine
WO2013049368A1 (en) 2011-09-27 2013-04-04 Thermochem Recovery International, Inc. System and method for syngas clean-up
CN104100411B (zh) * 2014-07-08 2016-01-20 北京理工大学 一种并联式燃烧室结构的双脉冲燃气发生装置
FR3032024B1 (fr) * 2015-01-26 2018-05-18 Safran Module de combustion a volume constant pour une turbomachine comportant un allumage par communication
ES2940894T3 (es) 2016-02-16 2023-05-12 Thermochem Recovery Int Inc Sistema y método de generación de gas producto de energía integrada de dos etapas
US10286431B1 (en) 2016-03-25 2019-05-14 Thermochem Recovery International, Inc. Three-stage energy-integrated product gas generation method
US11428413B2 (en) * 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
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
US11761635B2 (en) * 2017-04-06 2023-09-19 University Of Cincinnati Rotating detonation engines and related devices and methods
US10641169B2 (en) * 2017-06-09 2020-05-05 General Electric Company Hybrid combustor assembly and method of operation
US11674476B2 (en) * 2017-06-09 2023-06-13 General Electric Company Multiple chamber rotating detonation combustor
US9920926B1 (en) 2017-07-10 2018-03-20 Thermochem Recovery International, Inc. Pulse combustion heat exchanger system and method
FR3071545B1 (fr) * 2017-09-27 2019-10-11 Safran Chambre de combustion a volume constant et systeme de combustion pour turbomachine associe
US10099200B1 (en) 2017-10-24 2018-10-16 Thermochem Recovery International, Inc. Liquid fuel production system having parallel product gas generation
US11105511B2 (en) 2018-12-14 2021-08-31 General Electric Company Rotating detonation propulsion system
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
US11572840B2 (en) * 2019-12-03 2023-02-07 General Electric Company Multi-mode combustion control for a rotating detonation combustion system
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

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB743498A (en) * 1952-04-24 1956-01-18 Snecma Jet propulsion engines with pulse-jet units
US3332236A (en) * 1965-09-23 1967-07-25 Foster Wheeler Corp Synchronization of pulse jets
GB1354701A (en) * 1970-02-10 1974-06-05 Senhenn L A Jet propulsion engines
US5873240A (en) * 1993-04-14 1999-02-23 Adroit Systems, Inc. Pulsed detonation rocket engine
US5345758A (en) * 1993-04-14 1994-09-13 Adroit Systems, Inc. Rotary valve multiple combustor pulse detonation engine
US6003301A (en) * 1993-04-14 1999-12-21 Adroit Systems, Inc. Exhaust nozzle for multi-tube detonative engines
US5901550A (en) * 1993-04-14 1999-05-11 Adroit Systems, Inc. Liquid fueled pulse detonation engine with controller and inlet and exit valves
US6584765B1 (en) * 2001-12-21 2003-07-01 United Technologies Corporation Pulse detonation engine having an aerodynamic valve

Also Published As

Publication number Publication date
US6931833B2 (en) 2005-08-23
JP2004332721A (ja) 2004-11-25
EP1473457A3 (de) 2005-01-05
JP3943094B2 (ja) 2007-07-11
EP1473457A2 (de) 2004-11-03
US20040216464A1 (en) 2004-11-04
DE602004003283T2 (de) 2007-05-31
ATE346230T1 (de) 2006-12-15
EP1473457B1 (de) 2006-11-22

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