BE508930A - - Google Patents
Info
- Publication number
- BE508930A BE508930A BE508930DA BE508930A BE 508930 A BE508930 A BE 508930A BE 508930D A BE508930D A BE 508930DA BE 508930 A BE508930 A BE 508930A
- Authority
- BE
- Belgium
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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
-
- 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
- F02C7/224—Heating fuel before feeding to the burner
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US210347A US2704438A (en) | 1951-02-10 | 1951-02-10 | Starting fuel system for jet and rocket motors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE508930A true BE508930A (US08088918-20120103-C00476.png) |
Family
ID=22782546
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE508930D BE508930A (US08088918-20120103-C00476.png) | 1951-02-10 |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US2704438A (US08088918-20120103-C00476.png) |
| BE (1) | BE508930A (US08088918-20120103-C00476.png) |
| GB (1) | GB704622A (US08088918-20120103-C00476.png) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2323884A1 (fr) * | 1975-09-12 | 1977-04-08 | Rolls Royce | Circuit de carburant pour turbomachines |
| FR2728627A1 (fr) * | 1994-12-27 | 1996-06-28 | Europ Propulsion | Autopressurisation de reservoir |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2958189A (en) * | 1955-05-31 | 1960-11-01 | Phillips Petroleum Co | Method and apparatus for providing improved combustion in jet engines |
| US2953898A (en) * | 1956-10-22 | 1960-09-27 | Holley Carburetor Co | Afterburner apparatus |
| US3077073A (en) * | 1957-10-29 | 1963-02-12 | United Aircraft Corp | Rocket engine having fuel driven propellant pumps |
| US3073119A (en) * | 1958-12-08 | 1963-01-15 | United Aircraft Corp | Rocket propellant system |
| US3094838A (en) * | 1959-06-17 | 1963-06-25 | United Aircraft Corp | Thrust control system |
| US3162009A (en) * | 1959-06-30 | 1964-12-22 | United Aircraft Corp | Rocket motor control system |
| US3078659A (en) * | 1959-06-30 | 1963-02-26 | United Aircraft Corp | Liquid rocket engine system |
| US3049870A (en) * | 1960-04-14 | 1962-08-21 | United Aircraft Corp | Rocket propellant cycle |
| US3135088A (en) * | 1961-03-02 | 1964-06-02 | United Aircraft Corp | Sequencing system |
| US3410092A (en) * | 1961-07-17 | 1968-11-12 | Marquardt Corp | Reliquefaction cycle for liquid air cycle engine |
| US3200583A (en) * | 1962-10-15 | 1965-08-17 | Gen Motors Corp | Rocket propulsion apparatus |
| DE1751962C2 (de) * | 1968-08-24 | 1974-07-04 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Raketenbrennkammer für flüssige, mittels Strahlpumpen geförderte Treibstoffe, insbesondere für hypergole Treibstoffe |
| DE1776010A1 (de) * | 1968-09-03 | 1971-09-16 | Messerschmitt Boelkow Blohm | Verfahren zum Foerdern von fluessigen Treibstoffen fuer Gaserzeuger bzw.Raketenbrennkammern,und Foerdersystem zur Durchfuehrung des Verfahrens |
| US3707074A (en) * | 1970-09-30 | 1972-12-26 | Westinghouse Electric Corp | Spontaneous ignition of fuel in a combustion chamber |
| US3861141A (en) * | 1971-08-17 | 1975-01-21 | Brown Engineering Company Inc | Fuel pressurization for momentum compression ramjet engine |
| GB2191821B (en) * | 1978-12-07 | 1988-05-25 | Rolls Royce | Fuel preheater for an integrated rocket/ramjet engine |
| GB2119447A (en) * | 1982-05-01 | 1983-11-16 | Kershaw H A | Vapourising systems in jet propulsion or gas turbine engines |
| US5551230A (en) * | 1994-03-14 | 1996-09-03 | Rockwell International Corporation | Heat induced high pressure lox pump rocket engine cycle |
| FR2921979B1 (fr) * | 2007-10-08 | 2014-06-13 | Astrium Sas | Dispositif et procede de motorisation de pompe pour moteur fusee par moteur a combustion interne |
| US8844293B2 (en) * | 2011-03-22 | 2014-09-30 | Pratt & Whitney Canada Corp. | Fuel system for gas turbine engine |
| US20170356304A1 (en) * | 2016-06-13 | 2017-12-14 | General Electric Company | Systems and methods for reducing fluid viscosity in a gas turbine engine |
| US10718294B1 (en) | 2017-10-27 | 2020-07-21 | United Launch Alliance, L.L.C. | Integrated vehicle fluids |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB191003407A (en) * | 1910-02-11 | 1910-10-27 | James Alexander Main | Improvements in the Generation of Gases and Products of Combustion under Pressure for Operating Motive Power Engines. |
| US2395403A (en) * | 1939-03-06 | 1946-02-26 | Daniel And Florence Guggenheim | Rotatable combustion apparatus for aircraft |
| US2612752A (en) * | 1944-05-20 | 1952-10-07 | Daniel And Florence Guggenheim | Feeding apparatus, including injectors adapted to supply combustion liquids under pressure to a combustion chamber |
| US2558483A (en) * | 1944-05-20 | 1951-06-26 | Daniel And Florence Guggenheim | Feeding apparatus, including injectors adapted to supply combustion liquids under pressure to a combustion chamber |
| US2505798A (en) * | 1946-06-20 | 1950-05-02 | Leslie A Skinner | Liquid fuel jet propulsion system |
-
0
- BE BE508930D patent/BE508930A/xx unknown
-
1951
- 1951-02-10 US US210347A patent/US2704438A/en not_active Expired - Lifetime
- 1951-05-24 GB GB12155/51A patent/GB704622A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2323884A1 (fr) * | 1975-09-12 | 1977-04-08 | Rolls Royce | Circuit de carburant pour turbomachines |
| FR2728627A1 (fr) * | 1994-12-27 | 1996-06-28 | Europ Propulsion | Autopressurisation de reservoir |
| EP0719935A1 (fr) * | 1994-12-27 | 1996-07-03 | Societe Europeenne De Propulsion | Autopressurisation de réservoir |
| US5697212A (en) * | 1994-12-27 | 1997-12-16 | Societe Europeenne De Propulsion | Rocket propellant tank self-pressurization |
Also Published As
| Publication number | Publication date |
|---|---|
| US2704438A (en) | 1955-03-22 |
| GB704622A (en) | 1954-02-24 |
