Patent ID: 9573693
Date: 2017-02-21
CPC Classifications: B64C,B64D,Y02T

Claim:
1. An aeroplane comprising: a fuselage elongated in a longitudinal direction of the aeroplane, including a wing attached to the fuselage in a midsection of said fuselage in the longitudinal direction, such that part of the fuselage extends forward of the wing toward a front extremity of the fuselage, and part of the fuselage extends to the rear of the wing toward a rear extremity of the fuselage, and including a rear fuselage section, having at least one engine attached to the fuselage and located to the rear of the wing, wherein the at least one engine is attached to the fuselage in a rear position and the rear fuselage section does not include any aerodynamic surfaces intended to assure at least one of stability and aerodynamic control of the aeroplane; wherein the aerodynamic surfaces for at least one of aerodynamic stabilisation and control of the aeroplane are located outside of a projection space for engine debris associated with the at least one engine.