AIRCRAFT CONTROL SYSTEM Russian patent published in 2015 - IPC B64C13/28 B64C13/50

Abstract RU 2544251 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft (AC) control and concerns AC main control system. Flight control system includes control surfaces and connected with them power drives to control flight functions of roll, yaw, pitching and aerodynamic braking of AC. All power drives are electromechanical. In this system, part of control surfaces connected with electromechanical power drives represents split control surfaces each one of which consists of independent surfaces.

EFFECT: reliability, rigidity, simplicity of flight control system.

11 cl, 24 dwg

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RU 2 544 251 C2

Authors

Fervel' Mark

Lekanju Arno

Moss'On Antuan

Andrie Loran

Dates

2015-03-20—Published

2011-01-17—Filed