WO2014191637A3 - Aerobic and / or anaerobic propulsion device with combined and simultaneous steady-state operation and propelled systems and assemblies including such a device - Google Patents

Aerobic and / or anaerobic propulsion device with combined and simultaneous steady-state operation and propelled systems and assemblies including such a device Download PDF

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Publication number
WO2014191637A3
WO2014191637A3 PCT/FR2014/000117 FR2014000117W WO2014191637A3 WO 2014191637 A3 WO2014191637 A3 WO 2014191637A3 FR 2014000117 W FR2014000117 W FR 2014000117W WO 2014191637 A3 WO2014191637 A3 WO 2014191637A3
Authority
WO
WIPO (PCT)
Prior art keywords
aerobic
combined
state operation
propulsion device
assemblies including
Prior art date
Application number
PCT/FR2014/000117
Other languages
French (fr)
Other versions
WO2014191637A2 (en
WO2014191637A4 (en
Inventor
Pierre François Yannick AGOSTINI
Original Assignee
Agostini Pierre François Yannick
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 Agostini Pierre François Yannick filed Critical Agostini Pierre François Yannick
Publication of WO2014191637A2 publication Critical patent/WO2014191637A2/en
Publication of WO2014191637A3 publication Critical patent/WO2014191637A3/en
Publication of WO2014191637A4 publication Critical patent/WO2014191637A4/en

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention relates to an aerobic and / or anaerobic propulsion device with combined and simultaneous steady-state operation and propelled systems and assemblies including such a device. The invention relates to a propulsion device making it possible to obtain a significant increase in the mass flow and thrust. It is made up of an aerobic and / or anaerobic propulsion device (101) equipped with at least one turbopump (1), a system for converting heat energy into kinetic energy made up of a bypass device and a dense rare gas fluid injection system. The device according to the invention is in particular intended for the propulsion of systems and assemblies.
PCT/FR2014/000117 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 WO2014191637A2 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR1301259 2013-05-31
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
FR1301662 2013-07-09

Publications (3)

Publication Number Publication Date
WO2014191637A2 WO2014191637A2 (en) 2014-12-04
WO2014191637A3 true WO2014191637A3 (en) 2015-01-29
WO2014191637A4 WO2014191637A4 (en) 2015-04-02

Family

ID=50489117

Family Applications (1)

Application Number Title Priority Date Filing Date
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

Country Status (2)

Country Link
FR (2) FR3006380B1 (en)
WO (1) WO2014191637A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108005734A (en) * 2017-11-27 2018-05-08 安徽寅时压缩机制造有限公司 A kind of compressor gas kinetic energy recovery device

Citations (10)

* 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
FR2475634A1 (en) * 1980-02-12 1981-08-14 Nissan Motor STATOREACTOR ROCKER
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
EP1811163A2 (en) * 2006-01-19 2007-07-25 United Technologies Corporation Gas augmented rocket engine
WO2008004744A1 (en) * 2006-07-07 2008-01-10 C & Space Inc. Methane engine for rocket propulsion
US20080053064A1 (en) * 2002-03-15 2008-03-06 Erickson Christopher M Rocket engine power cycle
WO2010004232A1 (en) * 2008-07-11 2010-01-14 Snecma Thruster comprising a plurality of rocket motors

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4998410A (en) * 1989-09-05 1991-03-12 Rockwell International Corporation Hybrid staged combustion-expander topping cycle engine

Patent Citations (10)

* 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
FR2475634A1 (en) * 1980-02-12 1981-08-14 Nissan Motor STATOREACTOR ROCKER
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
US20080053064A1 (en) * 2002-03-15 2008-03-06 Erickson Christopher M Rocket engine power cycle
EP1811163A2 (en) * 2006-01-19 2007-07-25 United Technologies Corporation Gas augmented rocket engine
WO2008004744A1 (en) * 2006-07-07 2008-01-10 C & Space Inc. Methane engine for rocket propulsion
WO2010004232A1 (en) * 2008-07-11 2010-01-14 Snecma Thruster comprising a plurality of rocket motors

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
JUNICHI KUROKAWA ET AL: "ACIAL THRUST BEHAVIOR IN LOX-PUMP OF ROCKET ENGINE", JOURNAL OF PROPULSION AND POWER, AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. NEW YORK, US, vol. 10, no. 2, 1 March 1994 (1994-03-01), pages 244 - 250, XP000438156, ISSN: 0748-4658 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108005734A (en) * 2017-11-27 2018-05-08 安徽寅时压缩机制造有限公司 A kind of compressor gas kinetic energy recovery device
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

Also Published As

Publication number Publication date
WO2014191637A2 (en) 2014-12-04
FR3006380A1 (en) 2014-12-05
FR3006381A1 (en) 2014-12-05
WO2014191637A4 (en) 2015-04-02
FR3006380B1 (en) 2017-05-19
FR3006381B1 (en) 2017-04-14

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