Flap/spoiler combination

B - Operations – Transporting – 64 – C

Patent

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244/36

B64C 13/26 (2006.01) B64C 13/50 (2006.01)

Patent

CA 1292972

FLAP/SPOILER COMBINATION ABSTRACT OF THE DISCLOSURE A flap arrangement for an aircraft wing having along its trailing edge independently actuated high lift flap and spoiler. During cruising the flap is used for camber line curvature control while the spoiler is controlled in a follow up configuration such that a gap between the spoiler and the high lift flap does not form.

516987

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