Mobile surfaces for aircraft with sealed slots
View Patent ↗A lifting or stabilising component ( 11 ) for an aircraft comprising in the area of its trailing edge a rotary control element ( 13 ) rotating around an axis ( 61 ) with at least one slot ( 21 ) between the tip ( 15 ) of the component ( 11 ) and the control element ( 13 ), the edges of which are configured such that the distance therebetween, that is, the dimension of the slot ( 21 ), is constant for different angles of deflection of the control element ( 13 ), being located between them a seal ( 23 ) that assure the aerodynamic continuity of the component ( 11 ) when the control element ( 13 ) is at rest. In a preferred embodiment, the component ( 11 ) is a horizontal tail stabilizer and the control element ( 13 ) is a rudder.
1. A lifting or stabilising component for an aircraft comprising:
a tip located at a distal end of said lifting or stabilising component in a spanwise direction;
a rotary control element rotating relative to said lifting or stabilising component about an axis of rotation;
at least one slot formed between said tip and said rotary control element; and
sealing means arranged in said at least one slot for assuring aerodynamic continuity between said lifting or stabilising component and said rotary control element when said rotary control element is at rest;
characterised in that the edges of said tip and said rotary control element around said at least one slot are configured such that the distance therebetween is constant for different angles of deflection of the rotary control element;
wherein said edges comprise a first section that extends perpendicular to said axis of rotation in the direction of the trailing edge of said lifting or stabilizing component, a second section extending from the first section in a direction opposite the flight direction, and a softened transition area therebetween, the length of said first section being between 5 and 15% of the length of said second section.
2. The lifting or stabilising component for an aircraft according to claim 1 , characterised in that said component is a horizontal tail stabiliser and said control element is a rudder.