Patent ID: 8683105
Filing Date: 2014-03-25
Classification: G06F,G09G

Abstract:
1. A modular avionics system, comprising: one or more centralized processing line-replaceable units (LRUs), wherein the one or more centralized processing LRUs include at least one multi-core computer processor; one or more multi-function display (MFD) units configured to receive imagery data from the one or more centralized processing LRUs and display the imagery data on at least one display device of the one or more MFD units; one or more control display units (CDUs) configured to receive imagery data from the one or more centralized processing LRUs and display the imagery data on at least one display device of the one or more CDUs, wherein each of the one or more MFD units and the one or more CDUs include one or more user input devices, wherein each of the one or more MFD units and the one or more CDUs include at least one logic module, wherein the one or more CDUs and the one or more MFD units are configured to transmit user input data from the user input devices to the one or more centralized processing LRUs, wherein the one or more centralized processing LRUs are constructed from a plurality of component slices, wherein a first component slice of the plurality of component slices and at least a second component slice of the plurality of component slices are reversibly couplable via a high-speed common interconnection.