发明名称 Avionics display architecture with independent processing and monitoring channels
摘要 A high integrity, high availability avionics display architecture for an avionics display system. The architecture includes a plurality of display processing computers (DPC) and a plurality of display integrity feedback interfaces. Each DPC includes at least two independent processing channels. Each independent processing channel includes at least two independent lanes. Each independent lane includes an I/O section and a processor section. Furthermore, each independent processing channel comprises an operative graphics section. At least one of the independent lanes provides a critical display function that provides commands to the graphics section to drive a display signal to displays of the avionics system. A number of display integrity feedback interfaces from the displays of the avionics display system provide integrity by allowing the integrity monitor functions to detect faults within the display signals and/or originating from the displays.
申请公布号 US8743020(B1) 申请公布日期 2014.06.03
申请号 US201213559213 申请日期 2012.07.26
申请人 Rockwell Collins, Inc. 发明人 Mazuk Daniel E.;Anderson Eric N.;Sparks Rachel D.;Murphy Sara A.;Klein Clifford R.;Stover Keith A.;Corbett Matthew P.
分类号 G09G5/00;G06T1/00;G06F15/00 主分类号 G09G5/00
代理机构 代理人
主权项 1. A high integrity, high availability avionics display architecture for an avionics display system, comprising: a) a plurality of display processing computers (DPC), each DPC comprising: at least two independent processing channels, each independent processing channel comprising at least two independent lanes, each independent lane comprising: 1. an I/O section; and,2. a processor section;wherein each independent processing channel comprises an operative graphics section, wherein at least one of said independent lanes provides a critical display function that provides commands to said graphics section to drive a display signal to displays of said avionics system; and, at least one other of said independent lanes provides an integrity monitor function; and, b) a plurality of display integrity feedback interfaces from the displays of said avionics display system, said feedback interfaces providing integrity by allowing the integrity monitor functions to detect faults within the display signals and/or originating from the displays.
地址 Cedar Rapids IA US
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