BE446037A - - Google Patents

Info

Publication number
BE446037A
BE446037A BE446037DA BE446037A BE 446037 A BE446037 A BE 446037A BE 446037D A BE446037D A BE 446037DA BE 446037 A BE446037 A BE 446037A
Authority
BE
Belgium
Prior art keywords
fuselage
jet
control
nozzles
change
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE446037A publication Critical patent/BE446037A/fr

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8245Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft using air jets

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
BE446037D BE446037A (enrdf_load_stackoverflow)

Publications (1)

Publication Number Publication Date
BE446037A true BE446037A (enrdf_load_stackoverflow)

Family

ID=102265

Family Applications (1)

Application Number Title Priority Date Filing Date
BE446037D BE446037A (enrdf_load_stackoverflow)

Country Status (1)

Country Link
BE (1) BE446037A (enrdf_load_stackoverflow)

Similar Documents

Publication Publication Date Title
EP0254605B1 (fr) Dispositif directionnel et stabilisateur à rotor anti-couple caréné et incliné et à empennage en "V" dissymétrique, et hélicoptère équipé d'un tel dispositif
FR2928621A1 (fr) Commande de vol d'un aeronef.
EP3239049A1 (fr) Drone comportant au moins trois rotors de sustentation et de propulsion
EP0706937B1 (fr) Dispositif de commande du pas des pales d'un rotor de giravion
CH387461A (fr) Aérodyne
CA2397626A1 (fr) Aeronef a ailes tournantes
US5058825A (en) Steering aid for rotor aircraft
BE446037A (enrdf_load_stackoverflow)
US2818122A (en) Jet powered adjustable pitch helicopter rotor
FR2761658A1 (fr) Dispositif de commande de gouvernes d'un aeronef et aeronef equipe de ce dispositif
EP0318477B1 (fr) Perfectionnements aux aeronefs a decollage vertical
EP0317554B1 (fr) Dispositif d'assistance au pilotage d'aeronefs a voilure tournante
EP0104163B1 (fr) Aeronef sans moteur
CA1064885A (fr) Helicopteres a rotors coaxiaux, et notamment de type convertible_
FR2668116A1 (fr) Perfectionnement d'aeronefs ultralegers ou hyperlegers quant au cockpit et a la propulsion.
BE415874A (enrdf_load_stackoverflow)
BE537527A (enrdf_load_stackoverflow)
CA2306496A1 (fr) Helicoptere a levier
CH214763A (fr) Machine volante à ailes articulées.
BE434423A (enrdf_load_stackoverflow)
BE462058A (enrdf_load_stackoverflow)
CH95181A (fr) Hélicoptère à une seule hélice sustentatrice.
FR2813060A1 (fr) Dispositif de propulsion velique pour engins nautiques et terrestres
BE332834A (enrdf_load_stackoverflow)
BE410576A (enrdf_load_stackoverflow)