首页>
外国专利>
METHOD FOR INCREASING THE LIFTING POWER OF THE AERODYNAMIC CARRIER SURFACE, PREFERREDLY THE WINGS OF THE AIRCRAFT, AND THE AERODYNAMIC CARRIER SURFACE, PREFERREDLY THE WING OF THE AIRCRAFT
METHOD FOR INCREASING THE LIFTING POWER OF THE AERODYNAMIC CARRIER SURFACE, PREFERREDLY THE WINGS OF THE AIRCRAFT, AND THE AERODYNAMIC CARRIER SURFACE, PREFERREDLY THE WING OF THE AIRCRAFT
1. A method for increasing the lifting force of an aerodynamic bearing surface, mainly of an aircraft wing, providing for the formation of a converger from the leading edge of the bearing surface using the existing aerodynamic bearing surface, and at least one additional airfoil. The method according to claim 1, characterized in that the additional airfoil is located above and / or below the existing airfoil. The method according to claim 1, characterized in that the additional aerodynamic profile is selected from the list including: a fixed profile, an all-turning profile, a pivoting profile with different axes of rotation, a split profile, a one-piece telescopic profile. an aircraft wing, and at least one additional aerodynamic profile, located relative to each other, with the formation of a confuser on the side of the leading edge of the bearing surface. The aerofoil according to claim 4, characterized in that the additional aerofoil is located above and / or below the existing aerofoil. The aerodynamic surface according to claim 4, characterized in that the aerodynamic profile is selected from the list including: a fixed profile, an all-turning profile, a rotary profile with different axes of rotation, a split profile, an all-retractable profile.
展开▼
