FR2952034B1 - Engin volant, spatial ou aerien, pourvu d'un systeme propulsif a tuyere orientable - Google Patents

Engin volant, spatial ou aerien, pourvu d'un systeme propulsif a tuyere orientable

Info

Publication number
FR2952034B1
FR2952034B1 FR0905292A FR0905292A FR2952034B1 FR 2952034 B1 FR2952034 B1 FR 2952034B1 FR 0905292 A FR0905292 A FR 0905292A FR 0905292 A FR0905292 A FR 0905292A FR 2952034 B1 FR2952034 B1 FR 2952034B1
Authority
FR
France
Prior art keywords
flying
space
vehicle equipped
air vehicle
propulsive system
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
FR0905292A
Other languages
English (en)
Other versions
FR2952034A1 (fr
Inventor
Paul Caye
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.)
ArianeGroup SAS
Original Assignee
Astrium 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 Astrium SAS filed Critical Astrium SAS
Priority to FR0905292A priority Critical patent/FR2952034B1/fr
Priority to PCT/FR2010/052287 priority patent/WO2011055061A1/fr
Publication of FR2952034A1 publication Critical patent/FR2952034A1/fr
Application granted granted Critical
Publication of FR2952034B1 publication Critical patent/FR2952034B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/008—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector in any rearward direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/1005—Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/1028—Vibration-dampers; Shock-absorbers using inertia effect the inertia-producing means being a constituent part of the system which is to be damped

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Toys (AREA)
  • Looms (AREA)

Abstract

- Engin volant, spatial ou aérien, pourvu d'un système propulsif à tuyère orientable. - L'engin volant comporte des moyens (4) qui sont aptes à déplacer la tuyère (1), en l'absence de propulsion, pour engendrer des forces inertielles destinées à le stabiliser.
FR0905292A 2009-11-05 2009-11-05 Engin volant, spatial ou aerien, pourvu d'un systeme propulsif a tuyere orientable Active FR2952034B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0905292A FR2952034B1 (fr) 2009-11-05 2009-11-05 Engin volant, spatial ou aerien, pourvu d'un systeme propulsif a tuyere orientable
PCT/FR2010/052287 WO2011055061A1 (fr) 2009-11-05 2010-10-26 Engin volant, spatial ou aérien, pourvu d'un système propulsif à tuyère orientable

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0905292A FR2952034B1 (fr) 2009-11-05 2009-11-05 Engin volant, spatial ou aerien, pourvu d'un systeme propulsif a tuyere orientable

Publications (2)

Publication Number Publication Date
FR2952034A1 FR2952034A1 (fr) 2011-05-06
FR2952034B1 true FR2952034B1 (fr) 2011-12-09

Family

ID=42097118

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0905292A Active FR2952034B1 (fr) 2009-11-05 2009-11-05 Engin volant, spatial ou aerien, pourvu d'un systeme propulsif a tuyere orientable

Country Status (2)

Country Link
FR (1) FR2952034B1 (fr)
WO (1) WO2011055061A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3004762B1 (fr) * 2013-04-23 2017-09-01 Astrium Sas Systeme de moteur-fusee orientable
FR3071552B1 (fr) * 2017-09-26 2019-10-11 Arianegroup Sas Dispositif ameliore d'amortissement d'engins spatiaux

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6102337A (en) * 1995-12-22 2000-08-15 Hughes Electronics Corporation Spacecraft attitude control with gimbaled thrusters
US7185857B2 (en) * 2004-01-28 2007-03-06 Honeywell International, Inc. Thrust vector actuation control system and method

Also Published As

Publication number Publication date
FR2952034A1 (fr) 2011-05-06
WO2011055061A1 (fr) 2011-05-12

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