Patent ID: 8733698

Claim:
A method for implementing thrust reversers, upon a landing or a takeoff, of an aircraft provided with at least two turboengines, the speeds of which are individually controlled, between an idling speed and a full speed, by throttle levers respectively associated with said engines, said thrust reversers being controlled by at least one control member ( 1 ) for being able to switch from an inactive folded position to an active deployed position and, reversely, from said active deployed position to said inactive folded position, wherein the successive steps are automatically performed: a) a deployment (E 3 ) of said beforehand armed thrust reversers when: an actual speed of said engines is at the most equal to a low predetermined speed threshold; the actual speed of the aircraft is higher than a first predetermined speed threshold; and said aircraft is considered being in contact with the ground; b) an application (E 5 ) to said engines of a predetermined speed being at least equal to said low speed threshold as long as the speed of the aircraft is higher than said first speed threshold; c) as soon as the speed of said aircraft is at the most equal to said first speed threshold, a reduction (E 6 ) of the speed of said engines so that they reach a speed at the most equal to said low speed threshold; d) then, an folding (E 7 ) of said thrust reversers.