Electronic non-linear aircraft dynamic parameter display

G - Physics – 01 – C

Patent

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G01C 23/00 (2006.01) G01D 7/00 (2006.01)

Patent

CA 2494050

A method and apparatus is disclosed for displaying a dynamic parameter of an aircraft, the apparatus comprises a display unit receiving a display signal and displaying a scale that changes dynamically and non-linearly in accordance with a selected display algorithm, the display unit further displaying a pointer pointing (36) to said scale (32) in accordance with a reading of said dynamic parameter, thereby emphasizing a range of said reading of said dynamic parameter.

L'invention concerne un procédé et un appareil d'affichage d'un paramètre dynamique d'un aéronef. L'appareil comprend un dispositif d'affichage, qui reçoit un signal d'affichage et présente une échelle variant de manière dynamique et non linéaire, conformément à un algorithme d'affichage choisi. Le dispositif d'affichage présente en outre un pointeur pointant vers cette échelle selon une lecture du paramètre dynamique, accentuant ainsi une plage de ladite lecture du paramètre dynamique.

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