FR2863314B1 - Systeme de detonation pulsee a deux etages - Google Patents

Systeme de detonation pulsee a deux etages

Info

Publication number
FR2863314B1
FR2863314B1 FR0410664A FR0410664A FR2863314B1 FR 2863314 B1 FR2863314 B1 FR 2863314B1 FR 0410664 A FR0410664 A FR 0410664A FR 0410664 A FR0410664 A FR 0410664A FR 2863314 B1 FR2863314 B1 FR 2863314B1
Authority
FR
France
Prior art keywords
floors
detonation system
pulsed detonation
pulsed
detonation
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 - Fee Related
Application number
FR0410664A
Other languages
English (en)
Other versions
FR2863314A1 (fr
Inventor
Venkat Eswarlu Tangirala
Anthony John Dean
Ivett Alejandra Leyva
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2863314A1 publication Critical patent/FR2863314A1/fr
Application granted granted Critical
Publication of FR2863314B1 publication Critical patent/FR2863314B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • 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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F02K7/075—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
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
    • 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)
FR0410664A 2003-12-08 2004-10-08 Systeme de detonation pulsee a deux etages Expired - Fee Related FR2863314B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/730,219 US6983586B2 (en) 2003-12-08 2003-12-08 Two-stage pulse detonation system

Publications (2)

Publication Number Publication Date
FR2863314A1 FR2863314A1 (fr) 2005-06-10
FR2863314B1 true FR2863314B1 (fr) 2012-10-19

Family

ID=33452856

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0410664A Expired - Fee Related FR2863314B1 (fr) 2003-12-08 2004-10-08 Systeme de detonation pulsee a deux etages

Country Status (5)

Country Link
US (1) US6983586B2 (fr)
JP (1) JP4555654B2 (fr)
FR (1) FR2863314B1 (fr)
GB (1) GB2409025B (fr)
RU (1) RU2357093C2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2672240C1 (ru) * 2016-07-20 2018-11-12 Виталий Валериевич Кожевин Пульсирующий реактивный двигатель

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US7828546B2 (en) * 2005-06-30 2010-11-09 General Electric Company Naturally aspirated fluidic control for diverting strong pressure waves
EP1907685A1 (fr) * 2005-07-05 2008-04-09 Stéphane Véronneau Configurations de foyers
JP4912659B2 (ja) * 2005-10-14 2012-04-11 国立大学法人 筑波大学 衝撃波連続発生装置
US20070180814A1 (en) * 2006-02-03 2007-08-09 General Electric Company Direct liquid fuel injection and ignition for a pulse detonation combustor
US7784265B2 (en) * 2006-02-07 2010-08-31 General Electric Company Multiple tube pulse detonation engine turbine apparatus and system
US7950219B2 (en) * 2006-10-31 2011-05-31 General Electric Company Dual mode combustion operation of a pulse detonation combustor in a hybrid 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
FR2918415B1 (fr) * 2007-07-02 2013-07-12 Mbda France Moteur a detonations pulsees fonctionnant avec un melange carburant-air
US20090139203A1 (en) * 2007-11-15 2009-06-04 General Electric Company Method and apparatus for tailoring the equivalence ratio in a valved pulse detonation combustor
US8205433B2 (en) * 2008-08-21 2012-06-26 Lockheed Martin Corporation Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production
US8302377B2 (en) * 2009-01-30 2012-11-06 General Electric Company Ground-based simple cycle pulse detonation combustor based hybrid engine for power generation
US8429893B2 (en) 2009-08-11 2013-04-30 Northrop Grumman Corporation Airflow modulation for dual mode combined cycle propulsion systems
US20110047961A1 (en) * 2009-08-28 2011-03-03 General Electric Company Pulse detonation inlet management system
CN101718226B (zh) * 2009-11-03 2012-07-04 上海大学 发动机无间歇爆轰转子
US10125674B2 (en) 2010-06-10 2018-11-13 Waseda University Engine
JP5892622B2 (ja) * 2010-06-15 2016-03-23 エクスポネンシャル テクノロジーズ, インコーポレイテッドExponential Technologies, Inc. 多管式バルブレス・パルスデトネーションエンジン
DE202010008228U1 (de) 2010-08-05 2011-11-30 Gustav Klauke Gmbh Hydraulisches Arbeitsgerät
US8707674B2 (en) * 2010-09-30 2014-04-29 General Electric Company Pulse detonation tube with local flexural wave modifying feature
GB201016481D0 (en) 2010-10-01 2010-11-17 Rolls Royce Plc An igniter
RU2493399C2 (ru) * 2011-09-16 2013-09-20 Константин Валентинович Мигалин Способ реализации циклического детонационного сгорания в пульсирующем воздушно-реактивном двигателе
WO2014178746A1 (fr) * 2013-04-30 2014-11-06 Некоммерческое Партнерство По Научной, Образовательной И Инновационной Деятельности "Центр Импульсного Детонационного Горения" Procédé et dispositif de détonation dans une chambre de combustion d'un moteur à turbine à gaz
EP3186558B1 (fr) * 2014-08-26 2020-06-24 Siemens Energy, Inc. Agencement de trous de refroidissement de film pour résonateurs acoustiques dans des moteurs à turbine à gaz
FR3037384B1 (fr) * 2015-06-11 2017-06-23 Turbomeca Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion
RU2613755C1 (ru) * 2015-09-23 2017-03-21 Федеральное Государственное Унитарное Предприятие Тушинское Машиностроительное Конструкторское Бюро "Союз" Турбопрямоточный воздушно-реактивный двигатель
US11226242B2 (en) 2016-01-25 2022-01-18 Rosemount Inc. Process transmitter isolation compensation
US11226255B2 (en) 2016-09-29 2022-01-18 Rosemount Inc. Process transmitter isolation unit compensation
US10221763B2 (en) 2016-12-23 2019-03-05 General Electric Company Combustor for rotating detonation engine and method of operating same
US20180231256A1 (en) * 2017-02-10 2018-08-16 General Electric Company Rotating Detonation Combustor
RU186578U1 (ru) * 2017-05-11 2019-01-24 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Выходное устройство двигателя прямой реакции
US10641169B2 (en) 2017-06-09 2020-05-05 General Electric Company Hybrid combustor assembly and method of operation
RU192799U1 (ru) * 2019-05-15 2019-10-01 Общество с ограниченной ответственностью "ВНХ-Энерго" Устройство для создания тяги
US11879415B2 (en) * 2020-07-13 2024-01-23 Rafael Mártinez-Vilanova Piñó Jet engine for aircraft
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CN115653759B (zh) * 2022-10-13 2024-06-18 中国航发四川燃气涡轮研究院 基于流量分配的加力燃烧室供油***及控制流程设计方法

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2672240C1 (ru) * 2016-07-20 2018-11-12 Виталий Валериевич Кожевин Пульсирующий реактивный двигатель

Also Published As

Publication number Publication date
JP2005171984A (ja) 2005-06-30
RU2357093C2 (ru) 2009-05-27
JP4555654B2 (ja) 2010-10-06
GB0422410D0 (en) 2004-11-10
FR2863314A1 (fr) 2005-06-10
US6983586B2 (en) 2006-01-10
US20050120700A1 (en) 2005-06-09
RU2004129606A (ru) 2006-03-20
GB2409025A (en) 2005-06-15
GB2409025B (en) 2008-06-04

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Legal Events

Date Code Title Description
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Year of fee payment: 12

ST Notification of lapse

Effective date: 20170630