Aerodynamic float type fuselage for aircraft, has flow-conducting upper surface and flow-conducting lower side that are configured such that upper and lower surfaces comprise flow-favoring convex geometry with respect to each other

摘要

The fuselage (2) has a flow-conducting fuselage upper surface (3) and a flow-conducting fuselage lower side (6) that are configured in segmental geometric cross-sections such that the upper and lower surfaces comprise a flow-favoring convex geometry with respect to each other. The fuselage comprises the form of an aerodynamic float (4). The cross-section of the float has a form of a wing of an airplane (1) in a longitudinal section.