Reinforced cover for gaps in an aerodynamic contour

Abstract

Reinforced cover for gaps in an aerodynamic contour of a vehicle, with a first attachment section la attachable to a structural element 2, 5 of the vehicle 11, on a first axial plane I; a second elastic section 1c which covers a gap 3 which is located between a fixed part 5 and a moving part 6, 12 of the vehicle 11, and provided with a low-friction coating 8 on its inner surface 1e, an outer surface 1k with a fiberglass layer 7a; a main internal body 9 of an elastic material, a flexible transition section 1g between the first and the second section, 1a, 1c; the outer surface 1k of the second section 1c flushing with the outer surface 5a and extending towards the free end 1d as a continuation of the outer surface 5a of the fixed part 5.

Description

RELATED APPLICATION [0001] The present application claims priority from Spanish Application Serial No. 200403163, filed on December 31, 2004. Applicants claim priority under 35 U.S.C. §119 as to said Spanish application, the entire disclosure of which is incorporated herein by reference in its entirety. TECHNICAL FIELD OF THE INVENTION [0002] The present invention pertains to the field of the covers used for covering gaps which have an effect on the aerodynamic properties of outer surfaces of vehicles such as aircraft and high-speed trains. This invention is particularly encompassed within the sector of the covers used for covering gaps located between the surface of a moving element and the surface of a fixed element of such a vehicle. PRIOR ART TO THE INVENTION [0003] On high-speed vehicles such as aircraft and high-speed trains, there are moving elements, such as may be, for example, on aircraft, the elevators and rudders or flaps, which are articulated to fixed elements, between...

AI Technical Summary

Problems solved by technology

This problem is especially important for aircraft.

As the internal (non-aerodynamic) elements are exposed the air current may become deflected, this giving rise to the aforementioned unanticipated behaviors in the air flow.

In addition thereto, when there are gaps of this type in two parts of the structure separated from each other which are connected to each other, a flow of air is generated in the interior of the structure which, at the outlet opening, may cause flow separations, thus reducing the aerodynamic efficiency, it therefore being necessary for the sealing of such gaps to cover the largest part possible thereof in order to create an effective barrier which will restrain or even block this flow of air.

Although these seals are capable of withstanding major deflections, their lack of reinforcement may lead, under certain conditions, such as, for example, at high cruising speeds, to a flapping of the tongue being caused, thus reducing its efficiency and possibly having a negative effect on the aerodynamics.

In addition thereto, in the movements in which the friction against the moving surface tends to contract the seal, blockages may occur, especially if there are grime build-ups.

A second type of seal is a tongue-shaped seal with internal cloth reinforcement, covered with low-friction polyester fabric, which, although it improves the negative aspects of the non-reinforced tongue-shaped seals, entails the drawback of the reinforcement provided by the cloth not being sufficient to reduce the aforementioned flapping to the desired levels.

A third type of seal is a tongue-shaped seal with integrated plastic or metal reinforcement, covered by low-friction fabric, which, although having a suitable rigidity, needs an auxiliary structure for supporting the seal, as a result of which, although positively solving the aerodynamic problems, it is of an unacceptable structural weight.

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