PL2525070T3 - Odrzutowy silnik strumieniowy z komorą detonacyjną i obiekt latający zawierający taki odrzutowy silnik strumieniowy - Google Patents

Odrzutowy silnik strumieniowy z komorą detonacyjną i obiekt latający zawierający taki odrzutowy silnik strumieniowy

Info

Publication number
PL2525070T3
PL2525070T3 PL12290156T PL12290156T PL2525070T3 PL 2525070 T3 PL2525070 T3 PL 2525070T3 PL 12290156 T PL12290156 T PL 12290156T PL 12290156 T PL12290156 T PL 12290156T PL 2525070 T3 PL2525070 T3 PL 2525070T3
Authority
PL
Poland
Prior art keywords
ramjet engine
aircraft
detonation chamber
ramjet
engine
Prior art date
Application number
PL12290156T
Other languages
English (en)
Inventor
François Falempin
Bruno Le Naour
Original Assignee
Mbda France
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 Mbda France filed Critical Mbda France
Publication of PL2525070T3 publication Critical patent/PL2525070T3/pl

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
    • F02K7/10—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 characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/20—Composite ram-jet/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
    • 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
    • F02K7/10—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 characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Nozzles (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
PL12290156T 2011-05-16 2012-05-09 Odrzutowy silnik strumieniowy z komorą detonacyjną i obiekt latający zawierający taki odrzutowy silnik strumieniowy PL2525070T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1101485A FR2975439B1 (fr) 2011-05-16 2011-05-16 Statoreacteur a chambre de detonation, engin volant comprenant un tel statoreacteur
EP12290156.4A EP2525070B1 (fr) 2011-05-16 2012-05-09 Statoréacteur à chambre de détonation et engin volant comprenant un tel statoréacteur

Publications (1)

Publication Number Publication Date
PL2525070T3 true PL2525070T3 (pl) 2018-06-29

Family

ID=46084962

Family Applications (1)

Application Number Title Priority Date Filing Date
PL12290156T PL2525070T3 (pl) 2011-05-16 2012-05-09 Odrzutowy silnik strumieniowy z komorą detonacyjną i obiekt latający zawierający taki odrzutowy silnik strumieniowy

Country Status (9)

Country Link
US (1) US9816463B2 (pl)
EP (1) EP2525070B1 (pl)
JP (1) JP6165717B2 (pl)
FR (1) FR2975439B1 (pl)
PL (1) PL2525070T3 (pl)
RU (1) RU2605162C2 (pl)
SG (1) SG194622A1 (pl)
UA (1) UA111077C2 (pl)
WO (1) WO2012156595A1 (pl)

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US20180274787A1 (en) * 2017-03-27 2018-09-27 United Technollgies Corporation Rotating detonation engine combustor wave reflector
US11761635B2 (en) * 2017-04-06 2023-09-19 University Of Cincinnati Rotating detonation engines and related devices and methods
US20180355792A1 (en) * 2017-06-09 2018-12-13 General Electric Company Annular throats rotating detonation combustor
US20180356094A1 (en) * 2017-06-09 2018-12-13 General Electric Company Variable geometry rotating detonation combustor
US11674476B2 (en) * 2017-06-09 2023-06-13 General Electric Company Multiple chamber rotating detonation combustor
US10969107B2 (en) 2017-09-15 2021-04-06 General Electric Company Turbine engine assembly including a rotating detonation combustor
US11536456B2 (en) * 2017-10-24 2022-12-27 General Electric Company Fuel and air injection handling system for a combustor of a rotating detonation engine
US11149954B2 (en) 2017-10-27 2021-10-19 General Electric Company Multi-can annular rotating detonation combustor
RU186094U1 (ru) * 2018-01-11 2018-12-29 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Сверхзвуковой прямоточный воздушно-реактивный двигатель (варианты)
US11486579B2 (en) 2018-02-26 2022-11-01 General Electric Company Engine with rotating detonation combustion system
RU2690236C1 (ru) * 2018-04-03 2019-05-31 Сергей Евгеньевич Угловский Сверхзвуковая вращающаяся ракета
CN110541774B (zh) * 2018-05-29 2021-07-16 中国人民解放军国防科技大学 旋转爆震冲压发动机及高超声速飞行器
US11359578B2 (en) * 2018-08-06 2022-06-14 General Electric Company Ramjet engine with rotating detonation combustion system and method for operation
CN109139295B (zh) * 2018-10-22 2019-09-27 中国人民解放军国防科技大学 超燃冲压发动机爆震稳定控制系统及其控制方法
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
US12292198B2 (en) * 2019-02-05 2025-05-06 General Electric Company Rotating detonation combustor with discrete detonation annuli
RU2710037C1 (ru) * 2019-03-25 2019-12-24 федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский государственный авиационный технический университет" Система электроснабжения летательного аппарата
RU2724557C1 (ru) * 2019-06-21 2020-06-23 Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Способ работы прямоточного воздушно-реактивного двигателя и устройство для его реализации
US11255544B2 (en) 2019-12-03 2022-02-22 General Electric Company Rotating detonation combustion and heat exchanger system
US20220325893A1 (en) * 2021-04-02 2022-10-13 Raytheon Technologies Corporation Chamber for rotating detonation engine and wall obstacles for same
US11852077B2 (en) * 2021-04-15 2023-12-26 Rtx Corporation Regenerative cooling and adjustable throat for rotating detonation engine
US20220389884A1 (en) * 2021-06-04 2022-12-08 Raytheon Technologies Corporation Variable cycle jet engine
CN114321980B (zh) * 2022-01-07 2023-05-16 中国人民解放军国防科技大学 超声速气流中爆震自持稳定的喷注混合控制方法及装置
WO2023171681A1 (ja) * 2022-03-07 2023-09-14 Ｐｄエアロスペース株式会社 燃焼モード切替エンジン
US20230280035A1 (en) * 2022-03-07 2023-09-07 General Electric Company Bimodal combustion system
US12253050B2 (en) 2022-04-12 2025-03-18 General Electric Company Combined cycle propulsion system for hypersonic flight
CN114941575B (zh) * 2022-05-12 2025-06-24 中国人民解放军空军工程大学 一种低损失可调旋转爆震燃烧室进口装置
US11970995B2 (en) * 2022-05-31 2024-04-30 Venus Aerospace Corp. Oblique detonation rocket engine
US20260022680A1 (en) * 2023-07-11 2026-01-22 University Of Central Florida Research Foundation, Inc. Supersonic Oblique Rotating Detonation Engine and Method of Creating a Supersonic Oblique Rotating Detonation Wave

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Also Published As

Publication number Publication date
WO2012156595A1 (fr) 2012-11-22
EP2525070A1 (fr) 2012-11-21
FR2975439B1 (fr) 2013-07-05
US20140196460A1 (en) 2014-07-17
US9816463B2 (en) 2017-11-14
EP2525070B1 (fr) 2018-02-21
RU2605162C2 (ru) 2016-12-20
RU2013151842A (ru) 2015-06-27
JP6165717B2 (ja) 2017-07-19
FR2975439A1 (fr) 2012-11-23
UA111077C2 (uk) 2016-03-25
SG194622A1 (en) 2013-12-30
JP2014516130A (ja) 2014-07-07

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