Airfoil flap actuation

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244215, 244216, 74521, B64C 338, B64C 920

Patent

active

044051050

ABSTRACT:
A rear-edge flap is held on an aircraft wing by means of two pantograph-like guide systems carrying swivel heads on which the flap is pivoted. Control arms extend from the guide systems to cause the flap to be pivoted and the guide systems extend the flap. Details concerning bearings and kinematics are disclosed. Application of the invention to all rear flaps of two aircraft wings is described.

REFERENCES:
patent: 1845644 (1932-02-01), Bardwell
patent: 2246116 (1941-06-01), Wagner et al.
patent: 2348150 (1944-05-01), Richter
patent: 2492245 (1949-12-01), Sutton et al.
patent: 2779555 (1957-01-01), Danielson
patent: 2973925 (1961-03-01), Wiele
patent: 3985319 (1976-10-01), Dean et al.
patent: 3986689 (1976-10-01), Maltby
patent: 4305177 (1981-12-01), Feifel

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