Aircraft with optimised utility volume and method for...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/00 (2006.01) B64D 37/04 (2006.01) B64G 1/40 (2006.01)

Patent

CA 2661788

The present invention essentially relates to an aircraft comprising a fuselage (2) with a cockpit (4) for receiving passengers and/or a load and a propulsion system, said propulsion system comprising at least a tank (6) and/or a combustion chamber, wherein a portion of the propulsion system is used as an extension of said cockpit (4) for receiving passengers and/or a load, said portion of the propulsion system being adjacent to the cockpit (4) and separated from the cockpit by a partition (10).

La présente invention a principalement pour objet un aéronef comportant un fuselage (2) comprenant un habitacle (4) pour recevoir des personnes et/ou un chargement et système de propulsion, ledit système de propulsion comportant au moins un réservoir (6) et/ou une chambre de combustion, dans lequel une partie du système de propulsion est utilisable comme extension dudit habitacle (4) pour recevoir des personnes et/ou un chargement, ladite partie du système de propulsion étant adjacente à l'habitacle (4) et séparée de l'habitacle par une cloison (10).

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