Patent ID: 8548714
Filing Date: 2013-10-01
Classification: B60K,B64D,F02C,G05G,Y02T

Abstract:
1. A method for facilitating the standardization of a thrust control for a plurality of turbo-engines ( 3 ) of an aircraft (AC) provided with at least two turbo-engines ( 3 ) being symmetrical compared to the fuselage ( 1 ), speeds of said turbo-engines ( 3 ) being individually controlled by throttle control levers ( 4 ), respectively associated with said turbo-engines ( 3 ) and able to occupy several positions, each one of said levers ( 4 ) being associated with artificial force gradient means and with at least one position sensor (S), comprising: A/ a current position of each one of said throttle levers is determined by the at least one position sensor (S); B/ a mean of said current positions is calculated by a calculating means ( C/ for each one of said levers (