Abstract: A data viewing system for an aircraft includes a concentration unit including a first element for acquiring all of the compound images generated by a plurality of image sources, a second element for processing the acquired compound images, and a third element for managing the display of the processed compound images implemented on a plurality of viewing screens.

Abstract: This invention relates to an aircraft viewing system comprising: a plurality of generation devices (3301, . . . , 330k; 7301, . . . , 730k; 8301, . . . , 830k) adapted to generate video flows from aircraft data; a plurality of display units (3101, . . . , 310n; 7101, . . . , 710n; 8101, . . . , 810n), wherein each display unit is adapted to display an intrinsic display function as well as a video image representing at least one video input; at least one video distribution unit (3201, . . . , 320p; 7201, . . . , 720p; 8201, . . . , 820p) adapted to switch the video flows generated by said generation devices to the video inputs of said display units.

Abstract: The viewing system (1) comprises a concentration means (7) comprising an element for acquiring all the compound images generated by a plurality of sources (S1, S2, S3, Sn), an element for processing these compound images, and an element for managing the display implemented on a plurality of viewing screens (E1, E2, E3, Ei).