EP2573504B8 - System for piloting an aircraft using pairs of lateral nozzles - Google Patents
System for piloting an aircraft using pairs of lateral nozzles Download PDFInfo
- Publication number
- EP2573504B8 EP2573504B8 EP20120290307 EP12290307A EP2573504B8 EP 2573504 B8 EP2573504 B8 EP 2573504B8 EP 20120290307 EP20120290307 EP 20120290307 EP 12290307 A EP12290307 A EP 12290307A EP 2573504 B8 EP2573504 B8 EP 2573504B8
- Authority
- EP
- European Patent Office
- Prior art keywords
- piloting
- aircraft
- pairs
- lateral nozzles
- nozzles
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1102870A FR2980265B1 (en) | 2011-09-21 | 2011-09-21 | SYSTEM FOR STEERING A FLYING VEHICLE USING SIDEWALK PAIRS |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2573504A1 EP2573504A1 (en) | 2013-03-27 |
EP2573504B1 EP2573504B1 (en) | 2015-04-15 |
EP2573504B8 true EP2573504B8 (en) | 2015-05-20 |
Family
ID=46888347
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20120290307 Active EP2573504B8 (en) | 2011-09-21 | 2012-09-20 | System for piloting an aircraft using pairs of lateral nozzles |
Country Status (6)
Country | Link |
---|---|
US (1) | US9212880B2 (en) |
EP (1) | EP2573504B8 (en) |
FR (1) | FR2980265B1 (en) |
IL (1) | IL231575A (en) |
SG (1) | SG11201400720XA (en) |
WO (1) | WO2013041784A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9068808B2 (en) * | 2013-01-17 | 2015-06-30 | Raytheon Company | Air vehicle with bilateral steering thrusters |
AU2014276622A1 (en) * | 2013-06-04 | 2015-12-24 | Bae Systems Plc | Drag reduction system |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2386802A1 (en) * | 1977-04-08 | 1978-11-03 | Thomson Brandt | CONTROL DEVICE FOR PROJECTILE OF THE MISSILE GENUS, AND PROJECTILE EQUIPPED WITH THIS DEVICE |
FR2674621B1 (en) * | 1977-07-29 | 1994-08-26 | Thomson Brandt | PROJECTILE GUIDE. |
EP0060726A3 (en) * | 1981-03-17 | 1983-02-09 | Normalair-Garrett (Holdings) Limited | Gas thruster systems |
US4537371A (en) * | 1982-08-30 | 1985-08-27 | Ltv Aerospace And Defense Company | Small caliber guided projectile |
FR2536720A1 (en) * | 1982-11-29 | 1984-06-01 | Aerospatiale | SYSTEM FOR CONTROLLING A MISSILE USING LATERAL GAS JETS AND MISSILE HAVING SUCH A SYSTEM |
FR2620812B1 (en) * | 1987-09-18 | 1992-04-17 | Thomson Brandt Armements | LATERAL GAS JET SWITCHING DEVICE FOR PILOTAGE OF MACHINERY |
FR2659734B1 (en) * | 1990-03-14 | 1992-07-03 | Aerospatiale | SYSTEM FOR THE PILOTAGE OF A MISSILE USING LATERAL GAS JETS. |
FR2659733B1 (en) * | 1990-03-14 | 1994-07-01 | Aerospatiale | SYSTEM FOR THE PILOTAGE OF A MISSILE USING SIDE NOZZLES. |
IL115749A (en) | 1994-10-27 | 2000-02-29 | Thomson Csf | Missile launching and orientating system |
JP2004306762A (en) * | 2003-04-07 | 2004-11-04 | Mitsubishi Heavy Ind Ltd | Propulsion device for three-axis attitude control and flying object with unit |
-
2011
- 2011-09-21 FR FR1102870A patent/FR2980265B1/en active Active
-
2012
- 2012-09-20 WO PCT/FR2012/000372 patent/WO2013041784A1/en active Application Filing
- 2012-09-20 EP EP20120290307 patent/EP2573504B8/en active Active
- 2012-09-20 US US14/346,010 patent/US9212880B2/en active Active
- 2012-09-20 SG SG11201400720XA patent/SG11201400720XA/en unknown
-
2014
- 2014-03-18 IL IL231575A patent/IL231575A/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
WO2013041784A1 (en) | 2013-03-28 |
US20140224923A1 (en) | 2014-08-14 |
US9212880B2 (en) | 2015-12-15 |
FR2980265B1 (en) | 2017-02-24 |
IL231575A (en) | 2017-06-29 |
EP2573504A1 (en) | 2013-03-27 |
SG11201400720XA (en) | 2014-06-27 |
FR2980265A1 (en) | 2013-03-22 |
EP2573504B1 (en) | 2015-04-15 |
IL231575A0 (en) | 2014-04-30 |
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