BE469744A - - Google Patents

Info

Publication number
BE469744A
BE469744A BE469744DA BE469744A BE 469744 A BE469744 A BE 469744A BE 469744D A BE469744D A BE 469744DA BE 469744 A BE469744 A BE 469744A
Authority
BE
Belgium
Prior art keywords
blades
helicopter
rings
pitch
axis
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE469744A publication Critical patent/BE469744A/fr

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • B64C27/10Helicopters with two or more rotors arranged coaxially
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
BE469744D BE469744A (de)

Publications (1)

Publication Number Publication Date
BE469744A true BE469744A (de)

Family

ID=120108

Family Applications (1)

Application Number Title Priority Date Filing Date
BE469744D BE469744A (de)

Country Status (1)

Country Link
BE (1) BE469744A (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2804403A1 (fr) * 2000-01-28 2001-08-03 Jean Francois Gonzalez Plateau cyclique avec commande de mouvement de lacet pour un helicoptere birotor contra-rotatif coaxial

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2804403A1 (fr) * 2000-01-28 2001-08-03 Jean Francois Gonzalez Plateau cyclique avec commande de mouvement de lacet pour un helicoptere birotor contra-rotatif coaxial

Similar Documents

Publication Publication Date Title
EP0808768B1 (de) Senkrecht startendes und landendes Flugzeug
EP0238588B1 (de) Drehflügelflugzeug
CA2705655A1 (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
WO2001053150A1 (fr) Aeronef a ailes tournantes
FR2623318A1 (fr) Manege a effet ascensionnel equipe d'un avion
WO2001034466A1 (fr) Helicoptere a pilotage pendulaire a haute stabilite et a grande manoeuvrabilite
CA1330788C (fr) Dispositif de transport et de soulevement de charges pour leur deplacement par propulsion aerienne
BE469744A (de)
FR2620106A1 (fr) Helicoptere leger a 2 rotors contrarotatifs
EP0318477B1 (de) Senkrechtstarter
EP0317554B1 (de) Servosteuerungsvorrichtung eines drehflügelflugzeuges
CA1064885A (fr) Helicopteres a rotors coaxiaux, et notamment de type convertible_
FR2555910A1 (fr) Systeme de commandes d'un helicoptere a rotor contre rotatif
EP0225346A1 (de) Ultraleichtflugzeuge mit schwenkbarem propellerantrieb
FR2963776A1 (fr) Aeronef motorise leger a equilibrage ameliore
EP0104163B1 (de) Flugzeug ohne motor
CH120686A (fr) Hélicoptère.
BE344333A (de)
CH334205A (fr) Aérodyne
BE544313A (de)
BE333545A (de)
BE419068A (de)
CA2306496A1 (fr) Helicoptere a levier
BE331615A (de)
BE475200A (de)