FR2701293B1 - Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur. - Google Patents

Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur.

Info

Publication number
FR2701293B1
FR2701293B1 FR9301319A FR9301319A FR2701293B1 FR 2701293 B1 FR2701293 B1 FR 2701293B1 FR 9301319 A FR9301319 A FR 9301319A FR 9301319 A FR9301319 A FR 9301319A FR 2701293 B1 FR2701293 B1 FR 2701293B1
Authority
FR
France
Prior art keywords
ramjet
ejector
liquefied
super
modes
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
FR9301319A
Other languages
English (en)
Other versions
FR2701293A1 (fr
Inventor
Clotilde Pauron
David Tonon
Eric Hermant
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR9301319A priority Critical patent/FR2701293B1/fr
Priority to GB9401592A priority patent/GB2274881B/en
Priority to DE19944402941 priority patent/DE4402941B4/de
Priority to JP1251094A priority patent/JPH06241119A/ja
Priority to RU94003399/06A priority patent/RU94003399A/ru
Publication of FR2701293A1 publication Critical patent/FR2701293A1/fr
Application granted granted Critical
Publication of FR2701293B1 publication Critical patent/FR2701293B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K7/10—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
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • F02K7/16—Composite ram-jet/turbo-jet engines
FR9301319A 1993-02-05 1993-02-05 Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur. Expired - Fee Related FR2701293B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR9301319A FR2701293B1 (fr) 1993-02-05 1993-02-05 Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur.
GB9401592A GB2274881B (en) 1993-02-05 1994-01-27 A multi-mode engine integrating the following modes:ejector using liquefied or cooled turbocompressed air;ramjet,and super ramjet
DE19944402941 DE4402941B4 (de) 1993-02-05 1994-02-01 Kombinierter Motor mit integrierten Arbeitsweisen als Ejektor für turbokomprimierte, gekühlte oder verflüssigte Luft, als Staustrahltriebwerk und als Überschall-Staustrahltriebwerk
JP1251094A JPH06241119A (ja) 1993-02-05 1994-02-04 冷却又は液化されタービンで圧縮された空気を使用するエジェクタモードと、ラムジェットモードと、超ラムジェットモードとを統合しているマルチモードエンジン
RU94003399/06A RU94003399A (ru) 1993-02-05 1994-02-04 Комбинированный двигатель для летательного аппарата

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9301319A FR2701293B1 (fr) 1993-02-05 1993-02-05 Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur.

Publications (2)

Publication Number Publication Date
FR2701293A1 FR2701293A1 (fr) 1994-08-12
FR2701293B1 true FR2701293B1 (fr) 1995-04-28

Family

ID=9443798

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9301319A Expired - Fee Related FR2701293B1 (fr) 1993-02-05 1993-02-05 Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur.

Country Status (5)

Country Link
JP (1) JPH06241119A (fr)
DE (1) DE4402941B4 (fr)
FR (1) FR2701293B1 (fr)
GB (1) GB2274881B (fr)
RU (1) RU94003399A (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2775499B1 (fr) * 1998-02-27 2000-05-05 Aerospatiale Moteur mixte susceptible de mettre en oeuvre au moins un mode statoreacteur et un mode superstatoreacteur
DE10033653A1 (de) * 2000-06-16 2002-03-07 Sandor Nagy Kombinationsantrieb
EP1172544A1 (fr) * 2000-07-14 2002-01-16 Techspace Aero S.A. Moteur d'un lanceur spatial avec dispositif de collecte et séparation d'air
DE10126632A1 (de) * 2000-08-08 2002-09-12 Sandor Nagy Kombinationsantrieb
US8572946B2 (en) 2006-12-04 2013-11-05 Firestar Engineering, Llc Microfluidic flame barrier
US7886516B2 (en) * 2006-12-18 2011-02-15 Aerojet-General Corporation Combined cycle integrated combustor and nozzle system
CN102648025A (zh) 2009-07-07 2012-08-22 火星工程有限公司 爆震波防止器
WO2011152912A2 (fr) * 2010-03-12 2011-12-08 Firestar Engineering, Llc Tuyère de fusée à chambre de combustion supersonique
GB201400497D0 (en) * 2014-01-11 2014-02-26 Lewis Stephen D Low weight aircraft engine intake pre-cooler
CN103806968B (zh) * 2014-03-10 2016-06-22 苟仲武 一种液态空气发电装置及工作方法
CN103835766A (zh) * 2014-03-19 2014-06-04 苟仲武 一种高效储能发电方法和系统
JP6310292B2 (ja) 2014-03-26 2018-04-11 三菱重工業株式会社 燃焼器、ジェットエンジン、飛しょう体及びジェットエンジンの動作方法
JP6310293B2 (ja) * 2014-03-26 2018-04-11 三菱重工業株式会社 燃焼器、ジェットエンジン、飛しょう体及びジェットエンジンの動作方法
CN105298682B (zh) * 2015-11-11 2017-03-22 沈阳黎明航空发动机(集团)有限责任公司 一种航空发动机冷加力尾喷管
CN106150566B (zh) * 2016-08-26 2018-08-21 朱小波 一种基于压缩空气驱动技术的发电设备
CN106968835B (zh) * 2017-04-14 2018-07-06 西北工业大学 一种宽范围工作的火箭冲压组合全流道
GB201808352D0 (en) 2018-05-22 2018-07-11 Rolls Royce Plc Air intake system
CN114396341A (zh) * 2022-01-05 2022-04-26 北京航空航天大学 一种组合发动机用中间循环热量排散系统
WO2023238148A1 (fr) * 2022-06-06 2023-12-14 Supnekar Subhash Moteur à réaction à combustion interne

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB805418A (en) * 1955-10-05 1958-12-03 Power Jets Res & Dev Ltd Jet propulsion plant
GB971223A (en) * 1962-12-17 1964-09-30 Rolls Royce Gas turbine power plant
DE1288859B (de) * 1965-04-14 1969-02-06 Daimler Benz Ag Steuereinrichtung fuer druckmittelbetaetigte Vorrichtungen, insbesondere fuer die hydraulische Betaetigung von Fenstern, Tuerverschluessen od. dgl. bei Kraftfahrzeugen
US3981144A (en) * 1975-10-28 1976-09-21 The United States Of America As Represented By The Secretary Of The Air Force Dual stage supersonic diffuser
DE3617757C1 (fr) * 1986-05-30 1987-07-02 Erno Raumfahrttechnik Gmbh, 2800 Bremen, De
GB2222635B (en) * 1987-10-24 1992-05-27 British Aerospace Propulsion units for aerospace vehicles
US5052176A (en) * 1988-09-28 1991-10-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Combination turbojet-ramjet-rocket propulsion system
DE3912331A1 (de) * 1989-01-19 1990-10-18 Mtu Muenchen Gmbh Schubduese
DE3909050C1 (fr) * 1989-03-18 1990-08-16 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
US5094070A (en) * 1989-04-14 1992-03-10 Mtu Motoren- Und Turbinen Union Munchin Gmbh Propelling nozzle for a hypersonic jet plane
DE3942022A1 (de) * 1989-12-20 1991-06-27 Mtu Muenchen Gmbh Verfahren und vorrichtung zur kuehlung eines flugtriebwerkes
DE4016897C1 (en) * 1990-05-25 1991-06-06 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Method of obtaining liq. oxygen in hypersonic flight - uses turbine which reduces pressure of entering air and cools it before liquefying and sepg. into oxygen and nitrogen

Also Published As

Publication number Publication date
GB2274881A (en) 1994-08-10
DE4402941A1 (de) 1994-08-11
GB2274881B (en) 1996-10-02
DE4402941B4 (de) 2005-01-20
GB9401592D0 (en) 1994-03-23
FR2701293A1 (fr) 1994-08-12
RU94003399A (ru) 1997-04-10
JPH06241119A (ja) 1994-08-30

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CD Change of name or company name
TP Transmission of property
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Effective date: 20081031