Method and device for controlling the thrust of a...

Details Method and device for controlling the thrust of a... Method and device for controlling the thrust of a...

B - Operations, Transporting

64

D

B64D 31/10 (2006.01) G05D 1/00 (2006.01)

Patent

CA 2640925

The device (1) comprises a means (3) for determining the current weight of the aircraft, a means (4) for calculating a reduced thrust value which is proportional to the said current weight, a means (5) for determining at least one engine command, so that the engines deliver a thrust equal to the said reduced thrust value, and a means (7) for applying this command to those engines of the aircraft which have not failed.

Le dispositif (1) comporte un moyen (3) pour déterminer le poids courant de l'aéronef, un moyen (4) pour calculer une valeur de poussée réduite qui est proportionnelle audit poids courant, un moyen (5) pour déterminer au moins un ordre de commande des moteurs, afin qu'ils délivrent une poussée égale à ladite valeur de poussée réduite, et un moyen (7) pour appliquer cet ordre de commande aux moteurs non en panne de l'aéronef.

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