Patent ID: 9296478
Filing Date: 2016-03-29
CPC Classification: B64C

Claim Text:
1. An aircraft, comprising: at least two separate aircraft fuselages; a first wing arrangement with at least two non-connected wing sections that extend outwardly from an exterior of one of the at least two aircraft fuselages; and a second wing arranged between the at least two aircraft fuselages, wherein connecting regions of the first wing arrangement and of the second wing are arranged so as to be offset relative to each other at least on an X-Z-plane of an aircraft-fixed coordinate system, and wherein at least one engine is coupled to the second wing, and wherein the first wing arrangement is arranged in a tail region of the at least two aircraft fuselages, and the second wing is arranged in a forward-directed region of the aircraft, and the center of gravity of the aircraft is situated between the first wing arrangement and the second wing.