PL2525062T3 - Maszyna wirowa z komorą detonacyjną i statek powietrzny wyposażony w taką maszynę wirową - Google Patents

Maszyna wirowa z komorą detonacyjną i statek powietrzny wyposażony w taką maszynę wirową

Info

Publication number
PL2525062T3
PL2525062T3 PL12290159T PL12290159T PL2525062T3 PL 2525062 T3 PL2525062 T3 PL 2525062T3 PL 12290159 T PL12290159 T PL 12290159T PL 12290159 T PL12290159 T PL 12290159T PL 2525062 T3 PL2525062 T3 PL 2525062T3
Authority
PL
Poland
Prior art keywords
turbomachine
detonation chamber
aircraft provided
aircraft
detonation
Prior art date
Application number
PL12290159T
Other languages
English (en)
Inventor
Françoise Falempin
Naour Bruno Le
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 PL2525062T3 publication Critical patent/PL2525062T3/pl

Links

Classifications

    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • 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
    • 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
    • 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
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
PL12290159T 2011-05-16 2012-05-09 Maszyna wirowa z komorą detonacyjną i statek powietrzny wyposażony w taką maszynę wirową PL2525062T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1101483A FR2975434B1 (fr) 2011-05-16 2011-05-16 Turbomachine a chambre de detonation et engin volant pourvu d'une telle turbomachine
EP12290159.8A EP2525062B1 (fr) 2011-05-16 2012-05-09 Turbomachine à chambre de détonation et engin volant pourvu d'une telle turbomachine

Publications (1)

Publication Number Publication Date
PL2525062T3 true PL2525062T3 (pl) 2018-01-31

Family

ID=46062190

Family Applications (1)

Application Number Title Priority Date Filing Date
PL12290159T PL2525062T3 (pl) 2011-05-16 2012-05-09 Maszyna wirowa z komorą detonacyjną i statek powietrzny wyposażony w taką maszynę wirową

Country Status (9)

Country Link
US (1) US9556794B2 (pl)
EP (1) EP2525062B1 (pl)
JP (1) JP5985613B2 (pl)
ES (1) ES2643041T3 (pl)
FR (1) FR2975434B1 (pl)
PL (1) PL2525062T3 (pl)
RU (1) RU2597735C2 (pl)
UA (1) UA115033C2 (pl)
WO (1) WO2012156597A1 (pl)

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RU2595005C9 (ru) * 2014-08-01 2017-03-02 Федеральное государственное бюджетное учреждение науки Институт гидродинамики им. М.А. Лаврентьева Сибирского отделения Российской академии наук Способ сжигания топлива и детонационное устройство для его осуществления
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US11149954B2 (en) 2017-10-27 2021-10-19 General Electric Company Multi-can annular rotating detonation combustor
US11473780B2 (en) 2018-02-26 2022-10-18 General Electric Company Engine with rotating detonation combustion system
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CN108708788B (zh) * 2018-05-29 2021-07-02 中国人民解放军国防科技大学 双燃烧室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
CN109184950B (zh) * 2018-09-25 2020-09-01 西北工业大学 一种低能量点火起始爆震波的装置
US11092024B2 (en) * 2018-10-09 2021-08-17 General Electric Company Heat pipe in turbine engine
RU2750082C2 (ru) * 2019-07-24 2021-06-22 Борис Клавдиевич Никитин Многокамерный газовоздушный импульсно-детонационный турбинный двигатель
US11255544B2 (en) 2019-12-03 2022-02-22 General Electric Company Rotating detonation combustion and heat exchanger system
CN111207007A (zh) * 2019-12-26 2020-05-29 中国空气动力研究与发展中心 一种封闭空间中斜爆震波驻定稳定性增强方法
US11549465B1 (en) * 2020-06-09 2023-01-10 Innoveering, LLC Air breathing solid fuel rotating detonation engine
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Also Published As

Publication number Publication date
RU2013151841A (ru) 2015-06-27
RU2597735C2 (ru) 2016-09-20
ES2643041T3 (es) 2017-11-21
EP2525062A1 (fr) 2012-11-21
FR2975434A1 (fr) 2012-11-23
JP2014517194A (ja) 2014-07-17
JP5985613B2 (ja) 2016-09-06
FR2975434B1 (fr) 2015-08-14
UA115033C2 (uk) 2017-09-11
WO2012156597A1 (fr) 2012-11-22
EP2525062B1 (fr) 2017-07-19
US20140245714A1 (en) 2014-09-04
US9556794B2 (en) 2017-01-31

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