Air-jet propeller

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 15/00 (2006.01) F02K 1/00 (2006.01) F02K 5/02 (2006.01)

Patent

CA 2570542

The invention relates to an air-jet propeller comprising three bodies. The first body or head takes the form of a half-ellipse, the upper part of which is provided with a grille, while the lower part thereof is closed at one section, said first body being equipped with a closure ring. The second body or central part takes the form of a tubular cylinder comprising a helical round honeycomb rotor which is coupled to a spark ignition engine. The third body or rear part takes the form of a truncated cone and is equipped with a series of openings, gates and butterfly valves which balance, stabilise and direct the aircraft, such as to reduce fuel consumption and, consequently, pollution since the aircraft can fly at low speeds (km/h), thereby facilitating landing and take-off with minimum runway lengths and eliminating the risks associated with the high speed required for take-off and landing.

L'invention concerne un propulseur de souffle d'air, formé de trois corps de base. Le premier corps est constitué d'une tête de rotation en demi-ellipse pourvue d'un maillage sur sa partie supérieure tandis que sa partie inférieure est fermée par un côté présentant un arc de fermeture. Le deuxième corps, ou partie centrale, de forme cylindrique tubulaire, incorpore un rotor hélicoïdal à panneau rond couplé à un moteur à explosion, tandis que le troisième corps, ou partie arrière, de forme tronconique, présente une série de fenêtres, de vannes et de papillons équilibrant, stabilisant et orientant les aéronefs, avec une diminution de la consommation de combustible et, par conséquent, une contamination réduite en vol à vitesse réduite en kms/h, facilitant l'atterrissage et le décollage sur une longueur de piste minimale, et éliminant, de plus, les risques à l'atterrissage et au décollage dus à la vitesse élevée nécessaire.

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