Deceleration control assistance system for taxying aircraft

Details Deceleration control assistance system for taxying aircraft Deceleration control assistance system for taxying aircraft

B - Operations, Transporting

64

D

B64D 43/00 (2006.01) B60T 8/58 (2006.01) B64C 19/00 (2006.01) B64C 25/42 (2006.01) G05D 1/00 (2006.01) G06F 17/00 (2006.01)

Patent

CA 2472290

-The system (1) includes braking means (2) for braking the aircraft, a braking unit (3) controlling the braking means (2) on the basis of deceleration orders, a computing unit (5) for computing deceleration orders, which determines a plurality of distance/speed pairs relating to the movement of the aircraft over a landing runway, each of said pairs indicating the speed of movement at the associated distance defined relative to the runway threshold of the landing runway, and an interface element (7) that includes means (14) displaying on a screen (15) a representation (16) of the landing runway, showing the exits, and indications illustrating the distance/speed pairs, aiding an operator in choosing one of the exits, and means (17) enabling an operator to select the chosen exit.

- Le système (1) comporte des moyens de freinage (2) permettant de freiner l'aéronef, une unité de freinage (3) commandant les moyens de freinage (2) en fonction d'ordres de décélération, une unité de calcul (5) pour calculer des ordres de décélération, qui détermine une pluralité de couples distance/vitesse relatifs au roulage de l'aéronef sur une piste d'atterrissage, chacun desdits couples indiquant la vitesse de roulage à la distance associée définie par rapport au seuil de piste de la piste d'atterrissage, et un élément d'interface (7) qui comporte des moyens (14) affichant sur un écran (15) une représentation (16) de la piste d'atterrissage montrant les sorties, ainsi que des indications illustrant les couples distance/vitesse permettant d'aider un opérateur à choisir l'une des sorties, et des moyens (17) permettant à un opérateur de sélectionner la sortie choisie.

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