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 DEVICE

Info

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
Application number
FR1301259A
Other languages
French (fr)
Other versions
FR3006380A1 (en
Inventor
Pierre Francois Yannick Agostini
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to FR1301259A priority Critical patent/FR3006380B1/en
Priority to FR1301662A priority patent/FR3006381B1/en
Priority to PCT/FR2014/000117 priority patent/WO2014191637A2/en
Publication of FR3006380A1 publication Critical patent/FR3006380A1/en
Application granted granted Critical
Publication of FR3006380B1 publication Critical patent/FR3006380B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/18Composite ram-jet/rocket engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D3/00Machines or engines with axial-thrust balancing effected by working-fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/46Feeding propellants using pumps
    • F02K9/48Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/74Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78Rocket-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82Rocket-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D13/00Pumping installations or systems
    • F04D13/02Units comprising pumps and their driving means
    • F04D13/04Units comprising pumps and their driving means the pump being fluid driven
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D13/00Pumping installations or systems
    • F04D13/12Combinations of two or more pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/04Shafts or bearings, or assemblies thereof
    • F04D29/041Axial thrust balancing
FR1301259A 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 Active FR3006380B1 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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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