Variable camber wings
AssigneeBritish Aerospace Public Limited Company
InventorBarry Sharrock
Life of this patent
Estimating the term…
Loading patent…
AssigneeBritish Aerospace Public Limited Company
InventorBarry Sharrock
Estimating the term…
A variable camber wing which may act as an aileron and as a slotted flap comprises a leading wing portion 1, a chordwise arm 4 tiltably mounted thereon and carrying a flap element 5, and an intermediate wing portion 6 slidably mounted on the chordwise arm by means of trackways 8 and associated rollers 9. An upper flexible but inextensible skin 11 is anchored to both the leading wing portion 1 and the intermediate wing portion 6. Downward tilting of the arm 4 from a median position causes the upper skin 11 to draw the intermediate wing portion 6 away from the flap element 5. On tilting through small angles, the intermediate wing portion 6 moves chordwise and the skin 11 slides over flap element 5 and defines a smooth and continuous surface between the leading wing portion 1 and the flap element, while on tilting through large angles, the intermediate wing portion moves upwardly relative to the flap element and lifts the skin 11 therefrom.
A variable camber wing which comprises a leading wing portion, movable flap means carried by and tiltable with respect to the leading wing portion, an intermediate wing portion lying between the leading wing portion and the flap means, and a flexible but substantially inextensible upper skin attached both to the leading portion and the intermediate wing portion, which skin includes a trailing portion extending generally rearwardly of the intermediate wing portion, one of the intermediate wing portion and the flap means including a trackway and the other including an associated engaging member received in the trackway for sliding movement, said trackway including spaced upper and lower leading and trailing generally chordwise track portions which are bridged by an intermediate track portion, the arrangement being such that when the flap means is tilted through relatively small angles, the upper skin defines a substantially continuous and smooth surface between the leading wing portion and the flap means, whilst when the flap means is tilted downwardly through relatively large angles, the resultant effective foreshortening of the upper skin causes the intermediate wing portion to be displaced from the flap means in a generally chordwise direction as the engaging member passes along the trackway until the engaging member enters the intermediate portion, whereupon the intermediate wing portion is displaced generally upwardly relative to the flap means and lifts the trailing portion of the skin therefrom.
Dependencies are inferred from the claim text.