Gyropter having increased safety

Details Gyropter having increased safety Gyropter having increased safety

B - Operations, Transporting

64

C

B64C 27/20 (2006.01) A63H 29/22 (2006.01) B64C 39/02 (2006.01)

Patent

CA 2531820

The invention relates to a gyropter having coaxial contrarotating rotating aerofoils, in particular, one having two crown rotors (2,1) that rotate in opposite directions about a pod (6) either provided in the form of a drone or of a manned pod with a machine piloting process involving the control of the angle of attack of the blades by control rings. The safety is advantageously increased by adapted structures, by a multifunctional protective envelop (27), and by a lift system between the crowns (2,1) and the pod (6) with regard to both the radial forces as well as the axial forces, assisting in the optimized control of stresses. The gyropter also comprises electronic controls that are adapted to both model making and drones as well as to manned and/or piloted aircraft.

Gyroptère à voilures tournantes contrarotatives coaxiales, avec en particulier celui de deux rotors couronnes tournantes (2,1) en sens inverse autour d'une nacelle (6) soit en version drone, soit en version nacelle habitée, avec procédé du pilotage de la machine par la commande de l'incidence des pales par des anneaux de commande, la sécurité est avantageusement renforcée par des structures adaptée, une enveloppe protectrice multifonction (27) par un système de sustentation entre les couronnes (2,1) et la nacelle (6) tant pour les forces radiales qu'axiales participe à la maîtrise optimisée des tensions, et avec commandes électriques adaptée tant pour modélisme, drone, qu'aéronef habité et ou piloté.

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