MIXED CONTROL SYSTEM FOR AERODYNAMIC SURFACE OF AN AIRCRAFT.

摘要

SYSTEM FOR THE CONTROL OF AN AERODYNAMIC SURFACE (1) (FIN, ALERON, TIMON, ...) OF AN AIRCRAFT. ACCORDING TO THE INVENTION, THIS SYSTEM INCLUDES: - AN ELECTRICAL MACHINE (8) THAT CAN OPERATE WELL WITH MOTOR, WELL WITH GENERATOR, WHOSE OUTPUT IS MECHANICALLY CONNECTED TO SUCH AERODYNAMIC SURFACE (1) AND - A LOGICAL DEVICE (17) THAT RECEIVES INFORMATION OF THE OPERATING STATES OF THE ELECTRIC POWER SUPPLY (11) OF THE MACHINE (8) AND OF THE HYDRAULIC SERVOCONTROL (2,5) AND THAT CONTROLLES THE OPERATION OF THE SUCH SURFACE (1) WELL BY THE MACHINE (8), WELL BY THE SERVOCONTROL (2, 5).