SET OF FLAPS ON WING OF FIXED-WING AIRCRAFT Russian patent published in 2009 - IPC B64C3/00 

Abstract RU 2346851 C2

FIELD: transportation.

SUBSTANCE: proposed set of flaps consists of apparatus for aiding ascentional force in form of leading-edge flaps and/or trailing-edge flaps, movably fitted on the leading edge and/or trailing edge of a wing. The system of flaps has a unit for controlling the flaps so as to regulate change in position of the flaps on the wing, several groups of flaps, each of which has apparatus for aiding ascentional force, and several power-drive stations, each of which is related to one group of flaps. A power-drive station comprises two actuators, linked to the unit of controlling flaps, and two more devices for mechanical linkage of actuators with apparatus for aiding ascentional force. The group of flaps are individually controlled through power-drive stations corresponding to these groups of flaps.

EFFECT: increased functionality of flaps with increase in flexibility of operation of the system of flaps at the same time.

18 cl, 7 dwg

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RU 2 346 851 C2

Authors

Rekzik Martin

Rekhter Kharal'D

Bezing Vol'Fgang

Dates

2009-02-20Published

2004-03-26Filed