BE393390A - - Google Patents
Info
- Publication number
- BE393390A BE393390A BE393390DA BE393390A BE 393390 A BE393390 A BE 393390A BE 393390D A BE393390D A BE 393390DA BE 393390 A BE393390 A BE 393390A
- Authority
- BE
- Belgium
- Prior art keywords
- aircraft
- propeller
- wing
- flight
- angle
- Prior art date
Links
- 239000003638 chemical reducing agent Substances 0.000 claims description 4
- 230000007246 mechanism Effects 0.000 description 15
- 230000033001 locomotion Effects 0.000 description 8
- 230000004048 modification Effects 0.000 description 7
- 238000012986 modification Methods 0.000 description 7
- 239000003381 stabilizer Substances 0.000 description 6
- 230000003068 static effect Effects 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000001143 conditioned effect Effects 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000002730 additional effect Effects 0.000 description 1
- BNPSSFBOAGDEEL-UHFFFAOYSA-N albuterol sulfate Chemical compound OS(O)(=O)=O.CC(C)(C)NCC(O)C1=CC=C(O)C(CO)=C1.CC(C)(C)NCC(O)C1=CC=C(O)C(CO)=C1 BNPSSFBOAGDEEL-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000003287 bathing Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000003071 parasitic effect Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
BE393390A true BE393390A (enrdf_load_stackoverflow) |
Family
ID=60832
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE393390D BE393390A (enrdf_load_stackoverflow) |
Country Status (1)
Country | Link |
---|---|
BE (1) | BE393390A (enrdf_load_stackoverflow) |
-
0
- BE BE393390D patent/BE393390A/fr unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1212238B1 (fr) | Perfectionnements aux aeronefs convertibles a rotors basculants | |
CA2774259C (fr) | Pale de voilure tournante, rotor comprenant au moins deux telles pales et procede de mise en oeuvre d'un tel rotor | |
FR2547272A1 (fr) | Systeme aerien de soulevement de charges | |
WO2001053150A1 (fr) | Aeronef a ailes tournantes | |
EP0706937B1 (fr) | Dispositif de commande du pas des pales d'un rotor de giravion | |
WO2014111654A1 (fr) | Structure de suspension a géométrie variable d'un turbopropulseur sur un élément structurel d'un aéronef | |
EP0084995A1 (fr) | Système de propulsion pour engins et navires à voile | |
FR2620106A1 (fr) | Helicoptere leger a 2 rotors contrarotatifs | |
FR2523546A1 (fr) | Equipement pour vehicules ayant au moins un dispositif a pales tournantes et un corps helicoptere et aeronef | |
BE393390A (enrdf_load_stackoverflow) | ||
FR2546474A1 (fr) | Appareil pourvu de moyens de propulsion aeriens et susceptible de se deplacer a la surface d'un plan d'eau | |
EP0318477B1 (fr) | Perfectionnements aux aeronefs a decollage vertical | |
CA1064885A (fr) | Helicopteres a rotors coaxiaux, et notamment de type convertible_ | |
FR2581614A1 (fr) | Aeronef de la categorie des ulm ou des atl de securite optimale | |
CH120686A (fr) | Hélicoptère. | |
WO2024074543A1 (fr) | Aéronef à décollage et atterrissage vertical | |
BE431812A (enrdf_load_stackoverflow) | ||
FR2552395A1 (fr) | Perfectionnements apportes aux helices sustentatrices pour aeronefs | |
BE410576A (enrdf_load_stackoverflow) | ||
BE428191A (enrdf_load_stackoverflow) | ||
BE367557A (enrdf_load_stackoverflow) | ||
BE333545A (enrdf_load_stackoverflow) | ||
BE537527A (enrdf_load_stackoverflow) | ||
BE369132A (enrdf_load_stackoverflow) | ||
BE383850A (enrdf_load_stackoverflow) |