▎ 摘　　要

NOVELTY - The fuselage (10) has a fuselage formed as a dual wedge shaped structure with a wedge at the fore end of the fuselage, and another slope at the aft end of the fuselage. The slopes of the fuselage are positioned such that the slopes increase in height towards the center of the fuselage. The slopes of the fuselage are configured to direct airflow over the surface of the fuselage in a manner that allows the airflow to provide lift force to the aircraft. The surface of the fuselage is smooth to produce minimal drag. Sides of the fuselage extend beyond the aft end of the fuselage to form a pair of extended side panels (20). The aft ends of the extended side panels are connected by a connecting structure to form a tail (30) of the aircraft. The fuselage is made of transparent material. The solid layers and mesh layers are made of an ultra-polymer. An airframe of the aircraft is made of a sandwich structure. USE - Wedge-shaped light aircraft with a tail plane and morphing capabilities for providing additional lift and steering, used for short journeys for public transport, such as intercity travel in the form of airbuses. Can also be used for business travel and recreation. ADVANTAGE - The aircraft can reduce the overall drag over the aircraft surface, so as to make the propulsion of the aircraft more efficient, while also allowing the aircraft to reach and maintain a higher overall speed. The aircraft can reduce the overall drag on the aircraft, such as by changing the shape of the aircraft, removing windows, or the need for windows, and by looking at using steering mechanisms that produces less parasite drag, while still providing effective steering. The material needs a relatively high strength, and stiffness in order to withstand not only the force of the aircraft from landing, but also to withstand the forces caused by takeoff and from the pressure changes at high altitudes. The use of an electrical aircraft can vastly decrease the amount of noise pollution created by the aircraft, not only when taxiing across the ground, but also when performing takeoff and landing maneuvers, and thus assists the aircraft to achieve takeoff velocity, rotation velocity on a shorter takeoff distance, and hence enables the aircraft making use of shorter runways. DETAILED DESCRIPTION - The fuselage has a deicing layer comprising a layer of graphene, an electrically conductive material, such as copper wire, carbon nanotube or graphene such that the deicing layer acts as a lightening deflector. DESCRIPTION OF DRAWING(S) - The drawing shows a schematic view of a fuselage. 10Fuselage 20Side panels 30Tail of aircraft 40Wings