FR2661454B1 - Perfectionnements apportes aux propulseurs de type statoreacteur. - Google Patents
Perfectionnements apportes aux propulseurs de type statoreacteur.Info
- Publication number
- FR2661454B1 FR2661454B1 FR8510744A FR8510744A FR2661454B1 FR 2661454 B1 FR2661454 B1 FR 2661454B1 FR 8510744 A FR8510744 A FR 8510744A FR 8510744 A FR8510744 A FR 8510744A FR 2661454 B1 FR2661454 B1 FR 2661454B1
- Authority
- FR
- France
- Prior art keywords
- statoreactor
- improvements relating
- type propellers
- propellers
- type
- 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
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
-
- 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)
- Toys (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8510744A FR2661454B1 (fr) | 1985-07-12 | 1985-07-12 | Perfectionnements apportes aux propulseurs de type statoreacteur. |
US06/840,952 US5537815A (en) | 1985-07-12 | 1986-02-27 | Power units of the ram-jet engine type |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8510744A FR2661454B1 (fr) | 1985-07-12 | 1985-07-12 | Perfectionnements apportes aux propulseurs de type statoreacteur. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2661454A1 FR2661454A1 (fr) | 1991-10-31 |
FR2661454B1 true FR2661454B1 (fr) | 1994-02-11 |
Family
ID=9321267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8510744A Expired - Lifetime FR2661454B1 (fr) | 1985-07-12 | 1985-07-12 | Perfectionnements apportes aux propulseurs de type statoreacteur. |
Country Status (2)
Country | Link |
---|---|
US (1) | US5537815A (fr) |
FR (1) | FR2661454B1 (fr) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2755182B1 (fr) * | 1996-10-30 | 1998-12-31 | Aerospatiale | Systeme d'obturation pour un orifice d'entree d'air dans la chambre de combustion d'un statoreacteur |
US6430919B1 (en) | 2000-03-02 | 2002-08-13 | Direct Propulsion Devices, Inc. | Shaped charged engine |
US6568171B2 (en) * | 2001-07-05 | 2003-05-27 | Aerojet-General Corporation | Rocket vehicle thrust augmentation within divergent section of nozzle |
US9759162B1 (en) | 2002-07-23 | 2017-09-12 | Aerojet-General Corporation | Controlled autoignition propellant systems |
DE10245741B4 (de) * | 2002-10-01 | 2005-10-06 | Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh | Schubdüse für eine Feststoffrakete |
US9784545B1 (en) | 2003-03-03 | 2017-10-10 | Aerojet-General Corporation | Rocket motors having controlled autoignition propellant systems |
US7823376B2 (en) * | 2005-09-13 | 2010-11-02 | Aerojet-General Corporation | Thrust augmentation in plug nozzles and expansion-deflection nozzles |
US8056319B2 (en) * | 2006-11-10 | 2011-11-15 | Aerojet—General Corporation | Combined cycle missile engine system |
US8117847B2 (en) * | 2008-03-07 | 2012-02-21 | Raytheon Company | Hybrid missile propulsion system with reconfigurable multinozzle grid |
US20140109551A1 (en) * | 2012-10-23 | 2014-04-24 | Los Alamos National Security, Llc | Solid chemical rocket propulsion system |
JP6268529B2 (ja) * | 2014-03-28 | 2018-01-31 | 三菱重工業株式会社 | 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 |
RU2565131C1 (ru) * | 2014-07-14 | 2015-10-20 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Прямоточный воздушно-реактивный двигатель на твердом горючем и способ функционирования двигателя |
RU2623134C1 (ru) * | 2016-02-02 | 2017-06-22 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Интегральный прямоточный воздушно-реактивный двигатель на твердом горючем |
RU2688054C1 (ru) * | 2018-08-23 | 2019-05-17 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | Устройство газификации твердых углеводородов для прямоточного воздушно-реактивного двигателя |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB505747A (en) * | 1937-08-10 | 1939-05-10 | Rudolf Zwerina | Improvements connected with rockets |
DE1153942B (de) * | 1959-04-08 | 1963-09-05 | Dynamit Nobel Ag | Festtreibstoffrakete |
US3137126A (en) * | 1961-01-11 | 1964-06-16 | North American Aviation Inc | Method and means for forming a gaseous passage |
US3521452A (en) * | 1961-02-01 | 1970-07-21 | Exxon Research Engineering Co | Rocket nozzle cooling |
US3158061A (en) * | 1962-10-29 | 1964-11-24 | Samuel E Lager | Low toxicity rocket motor |
US3848408A (en) * | 1973-02-08 | 1974-11-19 | L Tompkins | Counter-wave pulse jet engine |
US4124976A (en) * | 1976-07-06 | 1978-11-14 | The United States Of America As Represented By The Secretary Of The Navy | Method for reducing the critical injection parameter in a solid fuel ramjet |
US4441312A (en) * | 1979-06-22 | 1984-04-10 | The United States Of America As Represented By The Secretary Of The Air Force | Combined cycle ramjet engine |
DE3115187C2 (de) * | 1981-04-15 | 1983-04-21 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | "Ventil mit drehbar angeordnetem Ventilkörper, insbesondere zum Dosieren der brennstoffreichen Gase von Staustrahl-Raketentriebwerken" |
FR2505404A1 (fr) * | 1981-05-07 | 1982-11-12 | Messerschmitt Boelkow Blohm | Vanne a tiroir rotatif destinee a assurer la commande et la regulation de fluides en ecoulement, notamment le dosage des debits de gaz riches en combustible dans les moteurs-fusees a statoreacteur |
DE3428469A1 (de) * | 1984-08-02 | 1986-02-13 | Bayern-Chemie Gesellschaft für flugchemische Antriebe mbH, 8261 Aschau | Schubduese fuer feststoff-raketentriebwerke |
-
1985
- 1985-07-12 FR FR8510744A patent/FR2661454B1/fr not_active Expired - Lifetime
-
1986
- 1986-02-27 US US06/840,952 patent/US5537815A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5537815A (en) | 1996-07-23 |
FR2661454A1 (fr) | 1991-10-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licences |