LIFTING-TYPE AEROPLANE FUSELAGE

摘要

The invention relates to an aeroplane having a lifting-type fuselage which comprises a wing provided with engines mounted on the hands thereof and whose width is substantially larger than the height thereof and the front section gradually transforms, in the plane view, from the narrow nose part into a large main section, wherein the tail assembly is provided with two stabilisers which are remote along the fuselage width away from the aeroplane vertical symmetry plane, are placed at an angle with respect thereto and are provided with a control surfaces. Each stabiliser is provided with an all-movable arrow-type rudder which forms a T-shaped fin and whose axis of rotation is situated on the stabiliser on the rudder plane. The stabiliser construction planes cross each other on the aeroplane symmetry plane on the main longitudinal axis of the aeroplane or bellow said axis.