FR2952034A1 - 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 Download PDFInfo
- Publication number
- FR2952034A1 FR2952034A1 FR0905292A FR0905292A FR2952034A1 FR 2952034 A1 FR2952034 A1 FR 2952034A1 FR 0905292 A FR0905292 A FR 0905292A FR 0905292 A FR0905292 A FR 0905292A FR 2952034 A1 FR2952034 A1 FR 2952034A1
- Authority
- FR
- France
- Prior art keywords
- nozzle
- flying machine
- propulsion
- control means
- flying
- 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.)
- Granted
Links
- 230000001141 propulsive effect Effects 0.000 title claims description 7
- 230000001133 acceleration Effects 0.000 claims description 12
- 230000000087 stabilizing effect Effects 0.000 claims description 5
- 230000010355 oscillation Effects 0.000 description 5
- 230000003068 static effect Effects 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 230000007935 neutral effect Effects 0.000 description 2
- 238000013016 damping Methods 0.000 description 1
- 230000037430 deletion Effects 0.000 description 1
- 238000012217 deletion Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
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)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Toys (AREA)
- Looms (AREA)
Abstract
Description
Claims (5)
- REVENDICATIONS1. Engin volant muni d'un système propulsif (2) comprenant au moins un moteur pourvu d'une tuyère mobile (1) et des premiers moyens de commande (13, 4, 5) aptes à déplacer ladite tuyère (1), lors d'une propulsion, dans le but d'orienter la force propulsive engendrée par le moteur, caractérisé en ce qu'il comporte, de plus, des seconds moyens de commande (15, 4, 5) qui sont activables en l'absence de propulsion générée par le moteur et qui sont aptes à déplacer ladite tuyère (1), en l'absence de propulsion, pour engendrer des forces inertielles destinées à stabiliser ledit engin volant.
- 2. Engin volant selon la revendication 1, caractérisé en ce que lesdits seconds moyens de commande comportent : - des moyens (15) pour engendrer des consignes d'accélération ; et - au moins un actionneur (4, 5) qui reçoit lesdites consignes d'accélération et qui déplace ladite tuyère (1) en fonction de ces consignes d'accélération reçues.
- 3. Engin volant selon l'une des revendications 1 et 2, caractérisé en ce que lesdits seconds moyens de commande comportent deux actionneurs (4, 5) qui agissent selon deux axes différents.
- 4. Engin volant selon l'une des revendications 1 à 3, caractérisé en ce que lesdits premiers et seconds moyens de commande comprennent les mêmes actionneurs (4,
- 5).
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 true FR2952034A1 (fr) | 2011-05-06 |
FR2952034B1 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) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3004762A1 (fr) * | 2013-04-23 | 2014-10-24 | Astrium Sas | Systeme de moteur-fusee orientable |
FR3071552A1 (fr) * | 2017-09-26 | 2019-03-29 | Arianegroup Sas | Dispositif ameliore d'amortissement d'engins spatiaux |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0780298A1 (fr) * | 1995-12-22 | 1997-06-25 | HE HOLDINGS, INC. dba HUGHES ELECTRONICS | ContrÔle d'attitude d'un véhicule spatial utilisant des propulseurs à poussée connectés par cardan |
US20050178886A1 (en) * | 2004-01-28 | 2005-08-18 | Potter Calvin C. | Thrust vector actuation control system and method |
-
2009
- 2009-11-05 FR FR0905292A patent/FR2952034B1/fr active Active
-
2010
- 2010-10-26 WO PCT/FR2010/052287 patent/WO2011055061A1/fr active Application Filing
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0780298A1 (fr) * | 1995-12-22 | 1997-06-25 | HE HOLDINGS, INC. dba HUGHES ELECTRONICS | ContrÔle d'attitude d'un véhicule spatial utilisant des propulseurs à poussée connectés par cardan |
US20050178886A1 (en) * | 2004-01-28 | 2005-08-18 | Potter Calvin C. | Thrust vector actuation control system and method |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3004762A1 (fr) * | 2013-04-23 | 2014-10-24 | Astrium Sas | Systeme de moteur-fusee orientable |
WO2014174163A1 (fr) * | 2013-04-23 | 2014-10-30 | Astrium Sas | Système de moteur-fusée orientable |
JP2016524065A (ja) * | 2013-04-23 | 2016-08-12 | エアバス ディフェンス アンド スペース エスエイエス | 方向付け可能なロケットエンジン・システム |
RU2612978C1 (ru) * | 2013-04-23 | 2017-03-14 | Эрбюс Дефенс Энд Спейс Сас | Система ориентируемого ракетного двигателя |
CN105308301B (zh) * | 2013-04-23 | 2017-07-28 | 空中客车防务及航天公司 | 可定向火箭发动机系统 |
US10612493B2 (en) | 2013-04-23 | 2020-04-07 | Arianegroup Sas | Orientable rocket-motor system |
FR3071552A1 (fr) * | 2017-09-26 | 2019-03-29 | Arianegroup Sas | Dispositif ameliore d'amortissement d'engins spatiaux |
WO2019063938A1 (fr) * | 2017-09-26 | 2019-04-04 | Arianegroup Sas | Dispositif ameliore d'amortissement d'engins spatiaux |
Also Published As
Publication number | Publication date |
---|---|
FR2952034B1 (fr) | 2011-12-09 |
WO2011055061A1 (fr) | 2011-05-12 |
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