Patent ID: 9567098
Date: 2017-02-14
CPC Classifications: B64D,G01C

Claim:
1. A display system for an aircraft, comprising main display means including: at least one basic screen, and means for handling the graphic interface of said or each basic screen, the handling means being configured to separately display on the main display means at least one first display window and at least one second display window, each display window displaying at least one pictogram representative of a parameter and/or a control of the aircraft, wherein the system includes additional display means including: at least one additional screen, and additional means for handling the graphic interface of the additional screen configured to display on the additional screen, a summary window depending on one of a transitional state between two air control centers, a preparation state for a descent phase towards a landing runway, a preparation state for entering an air control area with specific requirements, a detection of a deviation between two redundant sensors on the aircraft, a change in the navigation configuration, and a malfunction on the aircraft, the summary window comprising at least one first pictogram configured to be displayed on the first display window of the main display means without being displayed on the second display window of the main display means, and at least one second pictogram intended to be displayed on the second display window of the main display means without being displayed on the first display window of the main display means, said first and second pictograms displaying available data configured to and required for the one of the transitional state between two air control centers, the preparation state for a descent phase towards a landing runway, the preparation state for entering an air control area with specific requirements, the detection of a deviation between two redundant sensors on the aircraft, the change in the navigation configuration, and the malfunction on the aircraft.