FR2481369B1 - - Google Patents
Info
- Publication number
- FR2481369B1 FR2481369B1 FR8101644A FR8101644A FR2481369B1 FR 2481369 B1 FR2481369 B1 FR 2481369B1 FR 8101644 A FR8101644 A FR 8101644A FR 8101644 A FR8101644 A FR 8101644A FR 2481369 B1 FR2481369 B1 FR 2481369B1
- Authority
- FR
- France
- 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
Links
Classifications
-
- 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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
-
- 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
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/86493—Multi-way valve unit
- Y10T137/86718—Dividing into parallel flow paths with recombining
- Y10T137/86743—Rotary
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Electrically Driven Valve-Operating Means (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19803005864 DE3005864A1 (de) | 1980-02-16 | 1980-02-16 | Einrichtung zum steuern der stroemungsquerschnitte von kanaelen, insbesondere von gasleitrohren eines raketen-staustrahltriebwerks |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2481369A1 FR2481369A1 (fr) | 1981-10-30 |
| FR2481369B1 true FR2481369B1 (US20030204162A1-20031030-M00002.png) | 1984-02-17 |
Family
ID=6094810
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8101644A Granted FR2481369A1 (fr) | 1980-02-16 | 1981-01-28 | Dispositif de commande des sections d'ecoulement de canaux, notamment de tubes d'acheminement de gaz d'un statoreacteur de fusee |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4450679A (US20030204162A1-20031030-M00002.png) |
| DE (1) | DE3005864A1 (US20030204162A1-20031030-M00002.png) |
| FR (1) | FR2481369A1 (US20030204162A1-20031030-M00002.png) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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" |
| DE3144936C1 (de) * | 1981-11-12 | 1983-03-10 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Ventileinrichtung zum Steuern stroemender Medien hoher Temperatur,insbesondere zum Dosieren der Mengen brennstoffreicher Gase bei Staustrahl-Raketentriebwerken |
| DE3633387C1 (en) * | 1986-10-01 | 1987-08-13 | Messerschmitt Boelkow Blohm | Gas generator of a rocket/ram jet motor |
| DE3714425A1 (de) * | 1987-04-30 | 1988-11-17 | Messerschmitt Boelkow Blohm | Ventileinrichtung fuer partikelbeladene heissgase |
| US5817968A (en) * | 1987-08-03 | 1998-10-06 | The United States Of America As Represented By The Secretary Of The Air Force | Gas generation with high pressure sensitivity exponent propellant |
| DE3909050C1 (US20030204162A1-20031030-M00002.png) * | 1989-03-18 | 1990-08-16 | Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De | |
| US5784877A (en) * | 1996-11-08 | 1998-07-28 | Atlantic Research Corporation | Rocket-ramjet engine casing port closure |
| DE102007010349B4 (de) * | 2007-03-03 | 2009-07-09 | Lfk-Lenkflugkörpersysteme Gmbh | Ventilsteuereinheit für Staustrahlantrieb sowie Lenkflugkörper mit einer solchen Ventilsteuereinheit |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1140206A (en) * | 1914-08-11 | 1915-05-18 | Charles A Swackhammer | Rotary valve. |
| US1907191A (en) * | 1930-12-27 | 1933-05-02 | Emmett T Bruce | Balanced valve |
| US2590290A (en) * | 1945-11-30 | 1952-03-25 | Chase Leon Allen | Valve for flexible hose |
| US2912820A (en) * | 1953-07-31 | 1959-11-17 | Quentin R Whitmore | Combined ram jet and rocket engine |
| GB756288A (en) * | 1953-10-15 | 1956-09-05 | Snecma | Improvements relating to thrust augmenters for rocket motors |
| US2948112A (en) * | 1953-12-14 | 1960-08-09 | Kenneth W Smith | Combined rocket and ram-jet engine |
| GB886639A (en) * | 1958-08-08 | 1962-01-10 | Ludwig Haenisch | Improvements in rotary slide valves |
| US3712058A (en) * | 1961-08-14 | 1973-01-23 | Northrop Carolina Inc | Solid propellant controlled rocket motors |
| US3367112A (en) * | 1965-10-18 | 1968-02-06 | Mb Assoc | Multiple plate rocket nozzle |
| DE2458180A1 (de) * | 1974-12-09 | 1976-06-10 | Dynamit Nobel Ag | Trennwand fuer raketentriebwerke |
-
1980
- 1980-02-16 DE DE19803005864 patent/DE3005864A1/de not_active Ceased
-
1981
- 1981-01-16 US US06/225,608 patent/US4450679A/en not_active Expired - Fee Related
- 1981-01-28 FR FR8101644A patent/FR2481369A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| US4450679A (en) | 1984-05-29 |
| FR2481369A1 (fr) | 1981-10-30 |
| DE3005864A1 (de) | 1981-09-03 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |