SG11201508609RA - Orientable rocket-motor system - Google Patents

Orientable rocket-motor system

Info

Publication number
SG11201508609RA
SG11201508609RA SG11201508609RA SG11201508609RA SG11201508609RA SG 11201508609R A SG11201508609R A SG 11201508609RA SG 11201508609R A SG11201508609R A SG 11201508609RA SG 11201508609R A SG11201508609R A SG 11201508609RA SG 11201508609R A SG11201508609R A SG 11201508609RA
Authority
SG
Singapore
Prior art keywords
motor system
orientable
rocket
orientable rocket
motor
Prior art date
Application number
SG11201508609RA
Inventor
Fabrice RUFFINO
Benjamin Faure
Original Assignee
Airbus Defence & Space Sas
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 Airbus Defence & Space Sas filed Critical Airbus Defence & Space Sas
Publication of SG11201508609RA publication Critical patent/SG11201508609RA/en

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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • 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
    • F02K9/56—Control
    • 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
    • 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
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/90—Mounting on supporting structures or systems
    • F05B2240/91—Mounting on supporting structures or systems on a stationary structure
    • F05B2240/912—Mounting on supporting structures or systems on a stationary structure on a tower
    • F05B2240/9121—Mounting on supporting structures or systems on a stationary structure on a tower on a lattice tower
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/40—Movement of component
    • F05B2250/43—Movement of component with three degrees of freedom
SG11201508609RA 2013-04-23 2014-04-22 Orientable rocket-motor system SG11201508609RA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1353684A FR3004762B1 (en) 2013-04-23 2013-04-23 ENGINE-ROCKET SYSTEM
PCT/FR2014/000089 WO2014174163A1 (en) 2013-04-23 2014-04-22 Orientable rocket-motor system

Publications (1)

Publication Number Publication Date
SG11201508609RA true SG11201508609RA (en) 2015-11-27

Family

ID=49322461

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201508609RA SG11201508609RA (en) 2013-04-23 2014-04-22 Orientable rocket-motor system

Country Status (11)

Country Link
US (1) US10612493B2 (en)
EP (1) EP2989314B1 (en)
JP (1) JP6375366B2 (en)
CN (1) CN105308301B (en)
BR (1) BR112015026634A2 (en)
ES (1) ES2630527T3 (en)
FR (1) FR3004762B1 (en)
PL (1) PL2989314T3 (en)
RU (1) RU2612978C1 (en)
SG (1) SG11201508609RA (en)
WO (1) WO2014174163A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106368852B (en) * 2016-10-14 2018-08-03 南京航空航天大学 A kind of miniature liquid/solid-rocket vector spray servo-control system and method
JP6882667B2 (en) * 2017-03-29 2021-06-02 シンフォニアテクノロジー株式会社 Drive gear lock control device and actuator lock control device
CN107021209A (en) * 2017-04-21 2017-08-08 杨爱迪 total factor vector propulsion system
FR3072947B1 (en) * 2017-10-30 2021-12-17 Airbus Operations Sas AIRCRAFT COMPRISING AT LEAST ONE ENGINE ASSEMBLY CONNECTED TO THE AIRCRAFT FUSELAGE BY TWO PUSH RODS POSITIONED AT LEAST PARTLY IN AN AIR INLET OF THE ENGINE ASSEMBLY
CN108082452A (en) * 2017-12-04 2018-05-29 安徽工程大学 A kind of jet reversing arrangement of aircraft
CN109878702A (en) * 2017-12-06 2019-06-14 林瑤章 Thrust vector control device
EP3829979A4 (en) 2018-05-25 2022-05-18 Radian Aerospace, Inc. Earth to orbit transportation system
EP3891376A4 (en) 2018-07-03 2022-10-26 Radian Aerospace, Inc. Rocket propulsion systems and associated methods
CN111121703B (en) * 2019-12-11 2021-08-13 西安航天发动机有限公司 Swing interference detection system for liquid rocket engine
CN113443119B (en) * 2021-06-15 2022-07-29 中国科学院力学研究所 Novel high-speed aircraft control method based on rocket range extension

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3070329A (en) * 1960-02-16 1962-12-25 United Aircraft Corp Directional control for rockets
US3048011A (en) * 1960-04-22 1962-08-07 United Aircraft Corp Dirigible reaction motor
US3392918A (en) * 1962-07-09 1968-07-16 Thiokol Chemical Corp Rocket motor thrust control system
US3188024A (en) * 1963-05-06 1965-06-08 Schneider Albert Peter Aircraft steering and propulsion unit
US3191316A (en) * 1963-06-26 1965-06-29 Hugh L Dryden Lunar landing flight research vehicle
US3270505A (en) * 1964-10-21 1966-09-06 Norman L Crabill Control system for rocket vehicles
DE1301649B (en) * 1965-02-03 1969-08-21 Martin Marietta Corp Thrust augmentation device for a missile which has at least one rocket motor
US4955559A (en) * 1988-01-26 1990-09-11 Trw Inc. Thrust vector control system for aerospace vehicles
JP2848410B2 (en) * 1989-11-24 1999-01-20 防衛庁技術研究本部長 Flight object attitude control device
JPH0769300A (en) * 1993-09-02 1995-03-14 Masayuki Suzuki Propellant consumption reducing method of space craft
US5505408A (en) * 1993-10-19 1996-04-09 Versatron Corporation Differential yoke-aerofin thrust vector control system
JP3519206B2 (en) * 1996-03-11 2004-04-12 宇宙開発事業団 Rocket control method by adjusting engine thrust
US6758437B1 (en) * 1997-02-07 2004-07-06 Mcdonnell Douglas Corporation Rocket engine nacelle
RU2159862C2 (en) * 1998-06-22 2000-11-27 Московский государственный авиационный институт Aircraft power unit
RU2159352C2 (en) * 1999-01-21 2000-11-20 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Chamber swinging unit of reheat liquid propellant rocket engine
RU2158838C2 (en) * 1999-01-21 2000-11-10 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Liquid-propellant rocket engine
JP3771793B2 (en) * 2000-11-01 2006-04-26 三菱重工業株式会社 Thrust deflector
KR101042456B1 (en) * 2002-07-04 2011-06-16 에스엔에쎄엠아 프로폴지옹 솔리드 Swivelling nozzle for a rocket engine
JP4155081B2 (en) * 2003-04-02 2008-09-24 トヨタ自動車株式会社 Vertical take-off and landing equipment
US7481038B2 (en) * 2004-10-28 2009-01-27 United Technologies Corporation Yaw vectoring for exhaust nozzle
DE102007036883B4 (en) * 2007-08-04 2010-11-04 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh rocket engine
FR2952034B1 (en) * 2009-11-05 2011-12-09 Astrium Sas FLYING, SPACE OR AIR VEHICLE EQUIPPED WITH A PROPULSIVE SYSTEM WITH AN ADJUSTABLE TUYERE
RU2418970C1 (en) * 2009-12-07 2011-05-20 Николай Борисович Болотин Liquid-propellant engine and turbo-pump unit
RU2420669C1 (en) * 2010-05-18 2011-06-10 Сергей Евгеньевич Варламов Liquid propellant engine with controlled thrust vector, and nozzle block of roll

Also Published As

Publication number Publication date
US10612493B2 (en) 2020-04-07
JP2016524065A (en) 2016-08-12
EP2989314A1 (en) 2016-03-02
CN105308301B (en) 2017-07-28
PL2989314T3 (en) 2017-07-31
FR3004762A1 (en) 2014-10-24
CN105308301A (en) 2016-02-03
JP6375366B2 (en) 2018-08-15
BR112015026634A2 (en) 2017-07-25
ES2630527T3 (en) 2017-08-22
US20160069299A1 (en) 2016-03-10
FR3004762B1 (en) 2017-09-01
WO2014174163A1 (en) 2014-10-30
EP2989314B1 (en) 2017-03-08
RU2612978C1 (en) 2017-03-14

Similar Documents

Publication Publication Date Title
GB201301576D0 (en) System
SG11201506246WA (en) Ranging and positioning system
EP2972777A4 (en) Review system
GB2516958B (en) Growing system
ZA201601850B (en) Messaging system
GB201316940D0 (en) Tranaction system
SG11201508609RA (en) Orientable rocket-motor system
GB201304859D0 (en) Flow system
GB201413570D0 (en) Energy system
EP2975254A4 (en) Intake system
GB2522110B (en) System integration
PL2865823T3 (en) Fastening system
GB201513068D0 (en) Distributed system
GB201301654D0 (en) Tracking system
EP2967459A4 (en) Blood-donation system
GB201307628D0 (en) Seeker system
GB2517013B (en) Facing system
GB201420097D0 (en) Attachment system
PL2824265T3 (en) Fitting system
GB201301942D0 (en) Tracking System
GB201320929D0 (en) Dazzler system
GB201319579D0 (en) Denester system
GB201313816D0 (en) System
GB201312704D0 (en) System
GB201309022D0 (en) System