Aircraft horizontal stabilizer surface
AssigneeAirbus Espana, S.L.
InventorsRaul Carlos LLAMAS SANDIN, Miguel Luque Buzo
Life of this patent
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Abstract
Aircraft horizontal stabilizer surface (8) in which the sweep angle (40) of this surface (8), where this angle (40) is the one formed by the projection of the reference line of points located at 25% of the local chord (19) of the horizontal stabilizer surface (8) on a plane perpendicular to the aircraft plane of symmetry (21), and which also contains this plane to the flight direction of the aircraft with respect to the aircraft plane of symmetry (21), is less than 90 degrees, with this angle (40) being measured in the flight direction of the aircraft. In addition, the structural connection of this horizontal stabilizer surface (8) to the aircraft fuselage (1) is located at a closing frame (13) of this fuselage (1).
Claims13
Horizontal stabilizer surface (8) of an aircraft, characterized in that the sweep angle (40) of this surface (8), being this angle (40) the one formed by the projection of the reference line of points located at 25% of the local chord (19) of the horizontal stabilizer surface (8) on a plane perpendicular to the aircraft plane of symmetry (21), this plane also comprising the flight direction of the aircraft, with respect to the aircraft plane of symmetry (21), is less than 90 degrees, this angle (40) being measured in the flight direction of the aircraft.
Dependencies are inferred from the claim text.