BE407348A - - Google Patents
Info
- Publication number
- BE407348A BE407348A BE407348DA BE407348A BE 407348 A BE407348 A BE 407348A BE 407348D A BE407348D A BE 407348DA BE 407348 A BE407348 A BE 407348A
- Authority
- BE
- Belgium
- Prior art keywords
- flaps
- wing
- profiles
- aircraft
- same
- Prior art date
Links
- 238000006073 displacement reaction Methods 0.000 claims description 13
- 239000012530 fluid Substances 0.000 claims description 13
- 230000033001 locomotion Effects 0.000 claims description 12
- 238000012986 modification Methods 0.000 claims description 3
- 230000004048 modification Effects 0.000 claims description 3
- 230000000712 assembly Effects 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
- 210000000941 bile Anatomy 0.000 claims 1
- 230000009471 action Effects 0.000 description 7
- 230000005484 gravity Effects 0.000 description 5
- 239000003381 stabilizer Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 206010010071 Coma Diseases 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000003137 locomotive effect Effects 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000009533 lab test Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE407348A true BE407348A (de) |
Family
ID=72169
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE407348D BE407348A (de) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE407348A (de) |
-
0
- BE BE407348D patent/BE407348A/fr unknown
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP1212238B1 (de) | Verbessertes schwenkrotor-verwandlungsflugzeug | |
| EP0254605B1 (de) | Richtungs- und Stabilisierungsvorrichtung mit einem geneigt eingelassenen Heckrotor und asymmetrischem V-förmigem Leitwerk sowie damit ausgestatteter Hubschrauber | |
| EP2691299B1 (de) | Ferngesteuertes mikro/nanoflugzeug ausgestattet mit einem system tur rollen am boden und senkrechtstarten und landen | |
| EP3615424B1 (de) | Flugzeug mit rhomboedrischer flügelstruktur für senkrechtes starten und/oder landen | |
| EP1375342B1 (de) | Flugzeug mit aktiver Verwindungskontrolle seiner Tragflächen | |
| FR2948628A1 (fr) | Avion a controle en lacet par trainee differentielle | |
| EP3589544B1 (de) | Flugzeug mit rhomboedrischem, variabler geometrie- flügel | |
| FR2929591A1 (fr) | Avion a controle en tangage et en lacet par un ensemble propulsif. | |
| FR2473466A1 (fr) | Avion a voilure fixe comportant des surfaces portantes placees en tandem | |
| EP2233396A1 (de) | Verfahren und Vorrichtung zur Leistungsoptimierung von Luftschrauben, die an beiden Seiten vom Rumpf eines Drehflüglers angeordnet sind | |
| FR2946317A1 (fr) | Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante | |
| WO2012101352A1 (fr) | Avion motorisé à structure mixte hydrodynamique et aérodynamique pour le décollage et l'atterrissage sur l'eau, le sol ou la neige | |
| US10766584B2 (en) | Rotating machines with fluid rotor having adjustable blades | |
| FR2946316A1 (fr) | Procede de controle en lacet d'un helicoptere hybride,et helicoptere hybride muni d'un dispositif de commande en lacet apte a mettre en oeuvre ledit procede | |
| EP0084995A1 (de) | Antriebssystem für Segelboote und -fahrzeuge | |
| FR2719548A1 (fr) | Avion de transport à empennage avant. | |
| WO2018229356A1 (fr) | Navire a plans porteurs a haute stabilite | |
| FR3022217A1 (fr) | Aeronef convertible a aile basculante | |
| WO2023118210A1 (fr) | Hydrofoil rhomboedrique et embarcation le comportant | |
| WO2018229351A1 (fr) | Navire à plans porteurs à haute stabilité | |
| WO2018229355A1 (fr) | Navire a plans porteurs a haute stabilite | |
| FR2937005A1 (fr) | Planeur a propulsion eolienne | |
| FR3121424A1 (fr) | Dispositif aerien pour optimiser les engins a voiles | |
| WO2018229354A1 (fr) | Navire a plans porteurs a haute stabilite | |
| FR2655309A1 (fr) | Systeme de propulsion et de sustentation eoliennes pour engins de vitesse nautiques, terrestres ou amphibies. |