G - Physics – 01 – C
Patent
G - Physics
01
C
G01C 23/00 (2006.01)
Patent
CA 2567609
The invention concerns a device comprising a set of data sources, a data processing unit, and a display which presents on a display unit (8) attitude control indicators (9, 10, 11) representing at least speed, altitude and attitude data of the aircraft and a heading scale (12) including a characteristic symbol (13) indicating at least one next route point of the aircraft flight plan, said heading scale (12) being independent of said attitude control indicators (9, 10, 11), as well as a quantitative value (14) which indicates the remaining distance of flight of the aircraft to reach said next route point and which is associated with said characteristic symbol (13).
Le dispositif comporte un ensemble de sources d'informations, une unité de traitement d'informations, et un moyen d'affichage qui présente sur un écran de visualisation (8) des indicateurs de pilotage (9, 10, 11 ) illustrant au moins des informations de vitesse, d'altitude et d'attitude de l'aéronef et une échelle de cap (12) comprenant un signe caractéristique (13) illustrant le cap d'au moins un prochain point de route d'un plan de vol de l'aéronef, ladite échelle de cap (12) étant indépendante desdits indicateurs de pilotage (9, 10, 11 ), ainsi qu'une valeur quantitative (14) qui illustre la distance restant à parcourir à l'aéronef pour atteindre ledit prochain point de route et qui est associée audit signe caractéristique (13).
Brehin Didier
Dattler Stephane
Airbus France
Airbus Operations Sas
Robic
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