Aircraft with rear annular tail
A technology of empennage and aircraft, applied in the field of aircraft
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[0035] [35] figure 1 An example of a structure of an aircraft including a rear empennage assembly 1 according to the invention is shown.
[0036] [36] With respect to the rear empennage assembly, it is understood that it comprises a set of aerodynamic surfaces forming the empennage and situated aft of the wing 2 with respect to the longitudinal axis X of the aircraft in a direction substantially corresponding to The forward orientation of the moving direction of the aircraft in flight is positive.
[0037] [37] Here, the expression "aerodynamic surface" means a structure whose configuration is suitable for generating lifting aerodynamic forces, such as an aircraft wing, a horizontal stabilizer or an aircraft vertical stabilizer.
[0038] [38] The wing 2 and the empennage assembly 1 are generally fixed on the elongated aircraft fuselage 3 .
[0039] [39] Aircraft generally include a reference coordinate system consisting of a longitudinal axis X, a vertical axis Z, and an axi...
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