FR3006380B1 - AEROBIC AND ANAEROBIC TYPE HYBRID PROPULSION DEVICE HAVING PERMANENT COMBINED TYPE AND SIMULTANEOUS TYPE OPERATION AND SYSTEM AND PROPULSED ASSEMBLIES INCLUDING SUCH A DEVICE - Google Patents
AEROBIC AND ANAEROBIC TYPE HYBRID PROPULSION DEVICE HAVING PERMANENT COMBINED TYPE AND SIMULTANEOUS TYPE OPERATION AND SYSTEM AND PROPULSED ASSEMBLIES INCLUDING SUCH A DEVICEInfo
- Publication number
- FR3006380B1 FR3006380B1 FR1301259A FR1301259A FR3006380B1 FR 3006380 B1 FR3006380 B1 FR 3006380B1 FR 1301259 A FR1301259 A FR 1301259A FR 1301259 A FR1301259 A FR 1301259A FR 3006380 B1 FR3006380 B1 FR 3006380B1
- Authority
- FR
- France
- Prior art keywords
- type
- propulsed
- aerobic
- assemblies including
- simultaneous
- 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.)
- Active
Links
Classifications
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- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
-
- 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
- F02K9/46—Feeding propellants using pumps
- F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
-
- 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
- F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
- F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
-
- 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
- F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
- F04D13/04—Units comprising pumps and their driving means the pump being fluid driven
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/12—Combinations of two or more pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/04—Shafts or bearings, or assemblies thereof
- F04D29/041—Axial thrust balancing
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1301259A FR3006380B1 (en) | 2013-05-31 | 2013-05-31 | AEROBIC AND ANAEROBIC TYPE HYBRID PROPULSION DEVICE HAVING PERMANENT COMBINED TYPE AND SIMULTANEOUS TYPE OPERATION AND SYSTEM AND PROPULSED ASSEMBLIES INCLUDING SUCH A DEVICE |
FR1301662A FR3006381B1 (en) | 2013-05-31 | 2013-07-09 | TURBOPOMPE FOR SUPPLYING AT LEAST ONE PROPERGOL OF AT LEAST ONE PROPULSION CHAMBER OF "AEROBIC AND / OR ANAEROBIC" ENGINES AND SYSTEMS AND PROPELLED ASSEMBLIES COMPRISING SUCH A TURBOPOMPE |
PCT/FR2014/000117 WO2014191637A2 (en) | 2013-05-31 | 2014-05-26 | Aerobic and / or anaerobic propulsion device with combined and simultaneous steady-state operation and propelled systems and assemblies including such a device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1301259A FR3006380B1 (en) | 2013-05-31 | 2013-05-31 | AEROBIC AND ANAEROBIC TYPE HYBRID PROPULSION DEVICE HAVING PERMANENT COMBINED TYPE AND SIMULTANEOUS TYPE OPERATION AND SYSTEM AND PROPULSED ASSEMBLIES INCLUDING SUCH A DEVICE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3006380A1 FR3006380A1 (en) | 2014-12-05 |
FR3006380B1 true FR3006380B1 (en) | 2017-05-19 |
Family
ID=50489117
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1301259A Active FR3006380B1 (en) | 2013-05-31 | 2013-05-31 | AEROBIC AND ANAEROBIC TYPE HYBRID PROPULSION DEVICE HAVING PERMANENT COMBINED TYPE AND SIMULTANEOUS TYPE OPERATION AND SYSTEM AND PROPULSED ASSEMBLIES INCLUDING SUCH A DEVICE |
FR1301662A Active FR3006381B1 (en) | 2013-05-31 | 2013-07-09 | TURBOPOMPE FOR SUPPLYING AT LEAST ONE PROPERGOL OF AT LEAST ONE PROPULSION CHAMBER OF "AEROBIC AND / OR ANAEROBIC" ENGINES AND SYSTEMS AND PROPELLED ASSEMBLIES COMPRISING SUCH A TURBOPOMPE |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1301662A Active FR3006381B1 (en) | 2013-05-31 | 2013-07-09 | TURBOPOMPE FOR SUPPLYING AT LEAST ONE PROPERGOL OF AT LEAST ONE PROPULSION CHAMBER OF "AEROBIC AND / OR ANAEROBIC" ENGINES AND SYSTEMS AND PROPELLED ASSEMBLIES COMPRISING SUCH A TURBOPOMPE |
Country Status (2)
Country | Link |
---|---|
FR (2) | FR3006380B1 (en) |
WO (1) | WO2014191637A2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108005734B (en) * | 2017-11-27 | 2019-12-27 | 安徽寅时压缩机制造有限公司 | Compressor gas kinetic energy recovery device |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2547936A (en) * | 1944-11-17 | 1951-04-10 | Harlow B Grow | Ducted rocket propulsion means for aircraft |
US3173249A (en) * | 1959-08-10 | 1965-03-16 | Thiokol Chemical Corp | Air-breathing solid propellant ducted rocket |
FR2257789A1 (en) * | 1973-07-27 | 1975-08-08 | Onera (Off Nat Aerospatiale) | Propulsive unit for missile - has jet and rocket with coaxial discharges axially displaced from each other |
JPS56113029A (en) * | 1980-02-12 | 1981-09-05 | Nissan Motor Co Ltd | Injector of ram rocket |
US4998410A (en) * | 1989-09-05 | 1991-03-12 | Rockwell International Corporation | Hybrid staged combustion-expander topping cycle engine |
US5209652A (en) * | 1991-12-06 | 1993-05-11 | Allied-Signal, Inc. | Compact cryogenic turbopump |
FR2779771A1 (en) * | 1999-08-18 | 1999-12-17 | G Predpr K Bjurokhimicheskoi A | Turbo pump with multistage pump and turbine assemblies |
US7997060B2 (en) * | 2002-03-15 | 2011-08-16 | Pratt & Whitney Rocketdyne, Inc. | Rocket engine power cycle |
US20070163228A1 (en) * | 2006-01-19 | 2007-07-19 | United Technologies Corporation | Gas augmented rocket engine |
KR100674118B1 (en) * | 2006-07-07 | 2007-01-24 | (주)씨앤스페이스 | A methane engines for rocket propulsion |
FR2933744B1 (en) * | 2008-07-11 | 2011-06-03 | Snecma | ROCKER ENGINE AND REACTOR COMPRISING A PLURALITY OF SUCH ROTOR MOTORS |
-
2013
- 2013-05-31 FR FR1301259A patent/FR3006380B1/en active Active
- 2013-07-09 FR FR1301662A patent/FR3006381B1/en active Active
-
2014
- 2014-05-26 WO PCT/FR2014/000117 patent/WO2014191637A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2014191637A4 (en) | 2015-04-02 |
WO2014191637A2 (en) | 2014-12-04 |
FR3006381A1 (en) | 2014-12-05 |
WO2014191637A3 (en) | 2015-01-29 |
FR3006381B1 (en) | 2017-04-14 |
FR3006380A1 (en) | 2014-12-05 |
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