Flap/spoiler combination

Details Flap/spoiler combination Flap/spoiler combination

1986-08-26

1988-01-19

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244215, 244 76R, B64C 912

Patent

active

047200669

ABSTRACT:
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.

REFERENCES:
patent: 3987983 (1976-10-01), Cole
patent: 4120470 (1978-10-01), Whitener

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