FR2615903B1 - AEROBIC HEAT ENGINE, PARTICULARLY FOR THE PROPULSION OF HYPERSONIC AIRCRAFT - Google Patents
AEROBIC HEAT ENGINE, PARTICULARLY FOR THE PROPULSION OF HYPERSONIC AIRCRAFTInfo
- Publication number
- FR2615903B1 FR2615903B1 FR8707396A FR8707396A FR2615903B1 FR 2615903 B1 FR2615903 B1 FR 2615903B1 FR 8707396 A FR8707396 A FR 8707396A FR 8707396 A FR8707396 A FR 8707396A FR 2615903 B1 FR2615903 B1 FR 2615903B1
- Authority
- FR
- France
- Prior art keywords
- propulsion
- heat engine
- hypersonic aircraft
- aerobic heat
- aerobic
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
- F02C6/006—Open cycle gas-turbine in which the working fluid is expanded to a pressure below the atmospheric pressure and then compressed to atmospheric pressure
-
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/02—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being an unheated pressurised gas
-
- 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
- F02C3/36—Open cycles
-
- 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8707396A FR2615903B1 (en) | 1987-05-26 | 1987-05-26 | AEROBIC HEAT ENGINE, PARTICULARLY FOR THE PROPULSION OF HYPERSONIC AIRCRAFT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8707396A FR2615903B1 (en) | 1987-05-26 | 1987-05-26 | AEROBIC HEAT ENGINE, PARTICULARLY FOR THE PROPULSION OF HYPERSONIC AIRCRAFT |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2615903A1 FR2615903A1 (en) | 1988-12-02 |
FR2615903B1 true FR2615903B1 (en) | 1992-11-20 |
Family
ID=9351464
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8707396A Expired - Lifetime FR2615903B1 (en) | 1987-05-26 | 1987-05-26 | AEROBIC HEAT ENGINE, PARTICULARLY FOR THE PROPULSION OF HYPERSONIC AIRCRAFT |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2615903B1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3942022A1 (en) * | 1989-12-20 | 1991-06-27 | Mtu Muenchen Gmbh | METHOD AND DEVICE FOR COOLING AN AIRCRAFT ENGINE |
FR2687433B1 (en) * | 1992-02-14 | 1994-05-06 | Onera | INVERTER COMPONENT PROPELLER, WITH MODULATED FEEDING. |
FR2795456A1 (en) * | 1999-06-22 | 2000-12-29 | Georges Bouchet | Oceanic thermal energy converter for exploiting sea-water temperature differentials, comprises several turbo-compressor generating units with common humidifying reheater, on quasi-closed cycle |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE852015C (en) * | 1944-05-12 | 1952-10-09 | Rudolf Dipl-Ing Hingst | Process for generating energy from gases and gas vapor mixtures of low pressure, e.g. B. exhaust gases from internal combustion engines |
CH292538A (en) * | 1950-01-10 | 1953-08-15 | Adolf Mueller Max | Gas turbine plant. |
FR1058197A (en) * | 1951-06-15 | 1954-03-15 | Power Jets Res & Dev Ltd | Improvements to installations with gas turbines |
FR1111257A (en) * | 1953-09-11 | 1956-02-24 | Power Jets Res & Dev Ltd | Improvements to energy-producing installations with gas turbines |
GB2074249A (en) * | 1980-01-30 | 1981-10-28 | Iweka M G O | Power Plant |
DE3232318A1 (en) * | 1982-08-31 | 1984-04-19 | Karl Dipl.-Phys. 4600 Dortmund Winter | Method and device for generating usable mechanical energy by combustion |
GB2126658B (en) * | 1982-09-07 | 1986-07-02 | Secr Defence | Generation of power from liquid hydrogen |
-
1987
- 1987-05-26 FR FR8707396A patent/FR2615903B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2615903A1 (en) | 1988-12-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT8922684A0 (en) | AIRCRAFT PROPELLER SPEED CONTROL | |
FR2517368B1 (en) | CONVERTIBLE AIRPLANE ENGINE | |
GB8511610D0 (en) | Cooling i c engines | |
FR2619076B1 (en) | AIRPLANE PYLON | |
GB2212218B (en) | Ducted fan turbine engines | |
FR2553596B1 (en) | ENGINE PROPELLER OPERATION SYSTEM | |
FR2481748B1 (en) | THRUST DEFLECTOR FOR AVIATION ENGINE | |
FR2521639B1 (en) | HIGH PERFORMANCE PROPELLER PROPULSION ENGINE | |
IT8349374A0 (en) | IMPROVEMENT IN THE FUSELAGES OF MISSILE AND SIMILAR | |
IT1176388B (en) | CIRCUITUAL ARRANGEMENT FOR THE IGNITION OF HEAT ENGINES | |
FR2653742B1 (en) | AIRPLANE PROPELLER. | |
GB8630178D0 (en) | Fluid propulsion engine | |
GB8619881D0 (en) | Increasing speed of turbo-charger on i c engine | |
GB8722750D0 (en) | Adjusting torque of i c engine | |
FR2636377B1 (en) | ENGINE FOR AIRCRAFT, ESPECIALLY AIRCRAFT OR ROCKET | |
GB2189292B (en) | Engine cooling system | |
FR2698911B1 (en) | Aircraft engine layout. | |
GB8525030D0 (en) | Regulation of idling speed of i c engine | |
IT8103606A0 (en) | SYSTEM FOR THE COOLING OF AIR SUPPLY IN SUPERCHARGED ENDothermic Engines | |
EP0270102A3 (en) | System for controlling idle speed of an engine | |
FR2615903B1 (en) | AEROBIC HEAT ENGINE, PARTICULARLY FOR THE PROPULSION OF HYPERSONIC AIRCRAFT | |
IT1176384B (en) | CIRCUITUAL ARRANGEMENT FOR THE IGNITION OF HEAT ENGINES | |
EP0184082A3 (en) | Ship's propulsion for multiple engine drive | |
FR2543225B3 (en) | HYDRAULIC MOTOR SAID "SPHERICAL PROPELLER" | |
GB8704951D0 (en) | Engine cooling systems |