Aircraft wing and flap arrangement
AssigneeBritish Aerospace Public Limited Company
InventorsBarry Sharrock, David P. Halliday
Life of this patent
Estimating the term…
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AssigneeBritish Aerospace Public Limited Company
InventorsBarry Sharrock, David P. Halliday
Estimating the term…
An aircraft wing and flap arrangement comprises a fixed wing (1) a flap (2) pivoted at (3) to the fixed wing and a variable camber upper surface member (6) anchored to the fixed wing and resiliently biased toward the flap at all times; a cam track (9) secured to upper surface member (6) and associated cam track engaging member (10) on an arm (11) secured to the flap to control movement of the upper surface member so that on relatively small deflections of the flap (2) the upper surface of the wing is substantially continuous, while on relatively large downward deflections the upper surface is urged, by cam track engaging member (10), away from the flap (2) to open a slot (12); the arrangement may include a lower surface member (14) which is urged towards the upper surface membr (6) on relatively large downward deflections of the flap (2).
A wing and flap arrangement including a fixed wing portion, a flap member extending rearwardly of the fixed wing portion, a variable camber upper surface member in the form of a cantilevered leaf spring, said upper surface member being anchored to said fixed wing portion such that it trails therefrom and is biassed toward said flap member at all times, a pivot pivoting said flap member to said fixed wing portion about a generally spanwise axis, actuation means adapted to effect deflection of said flap member about its pivot, and upper surface urging means for urging said upper surface member from said flap member against the bias of the leaf spring when a slot is required, said upper surface urging means including a cam track and cam track engaging member, one of which is carried by said upper surface member and the other is carried by said flap member and arranged so that on relatively small upward and downward deflection from a neutral position, said upper surface member and the upper surfaces of said fixed wing portion and said flap member together define a substantially continuous surface, whilst on relatively large downward deflection from the neutral position said cam track and cam track engaging member co-operate to urge said upper surface member from said flap member.
Dependencies are inferred from the claim text.