Patent ID: 8384563
Filing Date: 2013-02-26
Classification: B64D,G01D

Abstract:
1. A device for confirming a thrust of at least one engine of an aircraft while it is running on a ground surface, upon a take-off phase thereof, such a device comprising: at least one display screen ( an operating logic unit ( a warning indicator connected at an outlet of said logic unit and able to display, at a level of said cockpit, thrust confirmation information when said information received by said logic unit is validated, wherein said logic unit ( 14 ) comprises, for each engine, at least an AND gate ( 24 ) receiving, at respective inlets thereof, said information on the control parameter of said engine, on the take-off mode position of said throttle lever, and on the ground position of said aircraft, and, when said information is gathered and validated, delivers, at the outlet thereof, said thrust confirmation information in a direction of said warning indicator ( 15 ), and wherein said logic unit ( 14 ) further comprises, for each engine: an OR gate ( a toggle (